Honeywell FMZ Series Pilot's Manual

Flight management system fms for the agusta aw139/ab139 helicopter software version nz 7.1
Table of Contents

Quick Links

Honeywell International Inc.
21111 N. 19th Ave.
Phoenix, Arizona 85027-2708
U.S.A.
CAGE: 55939
Telephone: 1- -800- -601- -3099 (U.S.A./Canada)
Telephone: 1- -602- -365- -3099 (International)
Web site:
http://portal.honeywell.com/wps/portal/aero
TO:
HOLDERS OF THE FLIGHT MANAGEMENT SYSTEM
(FMS) FOR THE AGUSTA AW139/AB139 HELICOPTER
PILOT'S GUIDE, HONEYWELL PUB. NO. A28--1146--181
REVISION NO. 4 DATED AUGUST 2010
Pages that have been revised are outlined below. Remove and insert
the affected pages listed. The revision number has been added to the
bottom of the revised pages and revision bars have been used to
indicate the revised or added text. Insert this highlights letter in the
manual in your possession ahead of page RR-1, Record of Revisions.
The List of Effective Pages shows the order in which to insert the
attached new pages into your guide.
The Record of Revisions page shows Honeywell has already put
Revision No. 4 dated August 2010 in the guide.
The revised pages are described in the following outline.
Page No.
T--1, T--4
LEP--1,
LEP--5, and
LEP--7
RR--1
1--1
7--26
Honeywell International Inc. Do not copy without express permission of Honeywell.
HIGHLIGHTS
Description of Change
Updated the title page and the proprietary notice
to reflect the new revision number and date.
Updated to reflect Revision 4.
Updated to reflect Revision 4.
Added note with SIL information.
Changed reference to APPR button to APP in
two places. Changed FAF reference to MAP.
Added new bullet to Engagement of VGP Mode.
Highlights
Page 1 of 2
August 2010
Table of Contents
loading

Summary of Contents for Honeywell FMZ Series

  • Page 1 Changed reference to APPR button to APP in two places. Changed FAF reference to MAP. Added new bullet to Engagement of VGP Mode. Highlights Page 1 of 2 August 2010 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 2 RHT, TD/H, MOT, and WTR. Deleted VNAV and FLCH buttons. Changed APPR button reference to APP and LNAV button reference to NAV. Abbrev--2, Added acronyms. Abbrev--17, and Abbrev 19 Highlights Page 2 of 2 August 2010 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 4 United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 7E994, NLR Eligible Revised August 2010 Printed in U.S.A. Pub. No. A28--1146--181--004 August 2004 Page T--1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 5 Honeywell aerospace products only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell’s Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair of...
  • Page 6 Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell. 2. Rights In Materials - - Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets.
  • Page 7 State of New York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties.
  • Page 8 Write the revision number and date, and the date put in the guide. Put your initials in the applicable columns on the Record of Revisions. The initial H shows that Honeywell put the changed pages in the guide.
  • Page 9 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Record of Revisions RR- - 2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 10 1--1 Aug 2010 indicates a changed or added page. indicates a foldout page. A28- - 1146- - 181 List of Effective Pages REV 4 Aug 2010 LEP- - 1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 11 Mar 2009 4--43 Mar 2009 5--36 Mar 2009 4--44 Mar 2009 5--37 Mar 2009 A28- - 1146- - 181 List of Effective Pages LEP- - 2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 12 Mar 2009 6--86 Mar 2009 6--41 Mar 2009 6--87 Mar 2009 6--42 Mar 2009 A28- - 1146- - 181 List of Effective Pages REV 3 Mar 2009 LEP- - 3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 13 Mar 2009 6--175 Mar 2009 6--130 Mar 2009 6--176 Mar 2009 6--131 Mar 2009 A28- - 1146- - 181 List of Effective Pages LEP- - 4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 14 Mar 2009 7--55 Mar 2009 7--10 Mar 2009 7--56 Mar 2009 7--11 Mar 2009 A28- - 1146- - 181 List of Effective Pages REV 4 Aug 2010 LEP- - 5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 15 F A--11/A--12 Mar 2009 10--9 Mar 2009 F A--13/A--14 Mar 2009 10--10 Mar 2009 A28- - 1146- - 181 List of Effective Pages LEP- - 6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 16 Mar 2009 Index--9 Mar 2009 Abbrev--8 Mar 2009 Index--10 Mar 2009 Abbrev--9 Mar 2009 A28- - 1146- - 181 List of Effective Pages REV 4 Aug 2010 LEP- - 7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 17 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 List of Effective Pages LEP- - 8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 18: Table Of Contents

    ..... . 4-15 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 19 ......A28- - 1146- - 181 Table of Contents TC- - 2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 20 ......6-133 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 21 7-13 Build a Flight Plan by Entering Waypoints ..7-14 A28- - 1146- - 181 Table of Contents TC- - 4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 22 ....10-1 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 23 ....4-11 A28- - 1146- - 181 Table of Contents TC- - 6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 24 ....... . 4-48 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 25 ......6-17 A28- - 1146- - 181 Table of Contents TC- - 8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 26 ......6-70 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 9 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 27 ......6-120 A28- - 1146- - 181 Table of Contents TC- - 10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 28 ....6-184 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 29 ..... . 7-41 A28- - 1146- - 181 Table of Contents TC- - 12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 30 ....9-20 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 31 ....A--1 A28- - 1146- - 181 Table of Contents TC- - 14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 32 ..... 6-186 A28- - 1146- - 181 Table of Contents REV 3 Mar 2009 TC- - 15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 33 9--5 Intercept an Arc Using Radial/Course ... 9-15 A28- - 1146- - 181 Table of Contents TC- - 16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 34: Introduction

    Service Information Letter D200904000018. Refer to page 1-3 for information on ordering additional copies of this guide or other Honeywell FMS publications. A28- - 1146- - 181 Introduction REV 4 Aug 2010 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 35: Honeywell Product Support

    For more information regarding the SPEX program, including maintenance, pricing, warranty, support, and access to an electronic copy of the Exchange/Rental Program for Corporate Operators, Pub. No. A65--8200--001, you can go to the Honeywell web site at: http://www.honeywell.com/sites/aero/Avionics_Services1.htm.. FMS PRODUCT SUPPORT...
  • Page 36: Customer Support

    Identify a change of address, telephone number, or e--mail address Register for revisions of this guide. Honeywell Aerospace Technical Publications If you have access to the Internet, go to the Honeywell Online Technical Publications web site at http://portal.honeywell.com/wps/portal/aero to: Download or see publications online...
  • Page 37 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Introduction REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 38: System Description

    The FMS interfaces primarily with the following components: Multifunction control display unit (MCDU) Modular avionics unit (MAU). A28- - 1146- - 181 System Description REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 39 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter The FMS has the following major functions: Figure 2- -1 FMS System Block Diagram A28- - 1146- - 181 System Description REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 40: Functional Description

    LNAV automatically flies pilot--defined or database holding patterns, including entry and exit procedures. A28- - 1146- - 181 System Description REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 41: Vertical Navigation (Vnav)

    Electronic displays integrate map data with weather radar displays and terrain maps. A28- - 1146- - 181 System Description REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 42: System Components

    FMS interfaces. Pilots enter data using the alphanumeric keyboard and the line select keys. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 43 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 3- -1 MCDU Display A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 44: Mcdu Display

    The MCDU is adjusted for parallax, as well as view angle, based on the installed location in the cockpit. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 45: Alphanumeric Keys

    Data is retained in the scratchpad throughout all mode and page changes. Follow Procedure 3--1 to edit any scratchpad entry of the MCDU. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 46: Line Select Keys (Lsk)

    The pilot also accesses functions through the main navigation and performance indices. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 47: Clear (Clr) Key

    With a dash (--) at the end of the scratchpad entry, pushing the DEL key deletes the entire scratchpad entry. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 48: Function Keys

    — Performance initialization — Fuel management — Takeoff and landing data — Performance planning — Approach speeds — Performance data. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 49 LSK. 00606.13 Figure 3- -3 NAV INDEX Page 1 00607.09 Figure 3- -4 NAV INDEX Page 2 A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 50 The PROGRESS pages summarize important flight parameters including the aircraft relationship to the flight plan. A28- - 1146- - 181 System Components REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 51 Menu -- The MCDU menu page permits accesses to maintenance and status information, is displayed by pushing the MENU function key. A28- - 1146- - 181 System Components 3-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 52: Accessing Any Fms Function

    AHRS (attitude and heading reference system) and GPS (global positioning system). A28- - 1146- - 181 System Components REV 3 Mar 2009 3-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 53 — The sensors being used for navigation are not approved for the current phase of flight. — The FMS is the selected aircraft navigation source on EDS. A28- - 1146- - 181 System Components 3-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 54 — ACTIVE MODE IS MAG HDG -- This is an alerting system message indicating that magnetic (mag) heading has been automatically selected. A28- - 1146- - 181 System Components REV 3 Mar 2009 3-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 55 The FMS computes a baro set based on the baro and pressure altitude inputs from the air data computer. A28- - 1146- - 181 System Components 3-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 56 14 -- Bad initial cruise altitude 15 -- Bad cruise speed 16 -- Bad cruise winds 17 -- Bad cruise fuel flow A28- - 1146- - 181 System Components REV 3 Mar 2009 3-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 57 2D -- Disk error during write 30 -- No response to WRITE command 31 -- No response to CLOSE command A28- - 1146- - 181 System Components 3-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 58 A28- - 1146- - 181 System Components REV 3 Mar 2009 3-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 59 — DATALOADER IN USE -- This is an advisory system message indicating some storage device is already being used. A28- - 1146- - 181 System Components 3-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 60 ACDB or when the gross weight value minus the HOOK weight exceeds the ACDB value for maximum takeoff weight. A28- - 1146- - 181 System Components REV 3 Mar 2009 3-19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 61 GPS current RAIM (receiver autonomous integrity monitor) exceeds the alarm limit for the present phase of flight. A28- - 1146- - 181 System Components 3-20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 62 — INVALID ENTRY -- This is an advisory operator message indicating the entry is not in the correct format and/or range. A28- - 1146- - 181 System Components REV 3 Mar 2009 3-21 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 63 This message is displayed when exiting the approach transition page with no approach transition selected and dashes are displayed as the course. A28- - 1146- - 181 System Components 3-22 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 64 — PERF VNAV UNAVAILABLE -- This is an alerting system message indicating the pilot requested a performance/VNAV function before sufficient data was entered. A28- - 1146- - 181 System Components REV 3 Mar 2009 3-23 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 65 — TEMP COMP CANCELED -- This is an alerting system message indicating the temperature compensation mode has been canceled. A28- - 1146- - 181 System Components 3-24 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 66 *PD waypoint fell within an area that can not have *PD waypoints. For example, procedure turns and arc turns. A28- - 1146- - 181 System Components REV 3 Mar 2009 3-25 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 67 PROGRESS 3 page. The annunciator is removed or turned off when the offset is removed. A28- - 1146- - 181 System Components 3-26 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 68 NOTE: A VOR without DME is only flown by the FMS when GPS or DME/DME is available. A28- - 1146- - 181 System Components REV 3 Mar 2009 3-27 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 69: Brightness Control

    Note that the brightness is adjusted during evening hours such that, during daylight hours, the display cannot be seen. A28- - 1146- - 181 System Components 3-28 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 70: Operational Example

    KDAL ARDIA ELLVR BLUBL COWZZ SNBAY TABBS PARKS KHOU fms00290.01 Figure 4- -1 KDAL to KHOU Flight Route A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 71 116.2 TORNN 6000 (JPOOL9.TORNN) COLLEGE STATION (JPOOL9.CLL) 7000 7000 ARDIA (JPOOL9.ARDIA) Figure 4- -2 Dallas, TX JPOOL9 Departure A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 72 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 4- -3 Houston, TX BLUBL Arrival A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 73 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 4- -4 Houston, TX ILS Approach A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 74: Predeparture

    Figure 4--5 is a flow chart showing the preflight procedure for a normal flight. Figure 4- -5 FMS Preflight Procedure Flow Chart A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 75: Power--Up

    The next initialization step (POS INIT in reverse video) is displayed and selected at 6R. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 76: Position Initialization

    KDAL ARP is shown. At 3L, the coordinates of the highest priority valid GPS is displayed. 00799.06 Figure 4- -7 POSITION INIT 1/1 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 77 Selecting the LOAD prompt continues the preflight process. Figure 4- -8 POSITION INIT 1/1 Page A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 78: Active Flight Plan

    /1435) and put the entry into 1L. Entering an ETD supports predictive receiver autonomous integrity monitor (RAIM) calculations. 00817.09 Figure 4- -9 ACTIVE FLT PLAN 1/1 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 79 The FLT PLAN LIST page is displayed when a stored flight plan has the same origin and destination. A28- - 1146- - 181 Operational Example 4-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 80: Waypoint Entry

    (3R) adjacent to KHOU. KHOU is moved to the scratchpad, as shown in Figure 4--12. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 81 (ETE) to the destination on the PROGRESS page. The destination is also required to calculate performance data. Figure 4- -13 Destination on ACTIVE FLT PLAN 1/2 Page A28- - 1146- - 181 Operational Example 4-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 82 The alternate destination is entered in 1R. San Antonio (KSAT) is used for this example, as shown in Figure 4--15. 01784.05 Figure 4- -15 ALTERNATE FPL 5/5 Page A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 83 Pushing the lower right line select key (6R) begins performance initialization (PERF INIT). When performance has already been initialized, 6R shows ARRIVAL or PERF DATA. A28- - 1146- - 181 Operational Example 4-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 84: Performance Initialization

    FMS. Many values PERFORMANCE INIT page aircraft--dependent. Actual values vary from those shown in these examples. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 85 — Aircraft type (1L) — Selected performance mode (2L) — Tail Number (1R). Figure 4- -17 PERFORMANCE INIT 1/3 Page A28- - 1146- - 181 Operational Example 4-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 86 The approach/go--around speed prompt (6L), as shown in Figure 4--18, is used to access approach and go--around speed schedules. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 87 Figure 4--19. Data associated with the weight of the aircraft is displayed on the PERFORMANCE INIT 3/3 page. Figure 4- -19 PERFORMANCE INIT 3/3 A28- - 1146- - 181 Operational Example 4-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 88: Performance Data

    4 and best endurance speed and distance are displayed on line 5. Figure 4- -20 PERF DATA 1/4 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 89 4 and current endurance speed and distance are displayed on line 5. Figure 4- -21 PERF DATA 2/4 A28- - 1146- - 181 Operational Example 4-20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 90 PERF DATA 3/4 page, shown in Figure 4--22. Figure 4- -22 PERF DATA 3/4 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-21 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 91 PERF DATA 4/4 page, shown in Figure 4--23. Figure 4- -23 PERF DATA 4/4 A28- - 1146- - 181 Operational Example 4-22 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 92: Departure Selection

    PLAN page 1. - - Selecting the DEPARTURE prompt (6L) on the ACTIVE FLT PLAN page 1. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-23 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 93 ACTIVATE prompt (6R) selects the runway and the ACTIVE FLT PLAN page is displayed. 00660.08 Figure 4- -25 SIDs 1/1 A28- - 1146- - 181 Operational Example 4-24 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 94 For this flight, the College Station (CLL) transition (5L) is selected. 00661.07 Figure 4- -26 DEPARTURE TRANS 1/1 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-25 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 95 1. Pushing the DEL key and the adjacent line select key to delete the discontinuity. 2. Moving any waypoint into the line where the discontinuity is located. A28- - 1146- - 181 Operational Example 4-26 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 96 The ACTIVE FLT PLAN page, shown in Figure 4--28, is displayed when activating the departure. Figure 4- -28 ACTIVE FLT PLAN 1/5 Page A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-27 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 97: Takeoff Data

    (large font). Surface wind is a required entry and is normally the only entry made on the TAKEOFF 1/2 page. A28- - 1146- - 181 Operational Example 4-28 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 98 — Surface stopway (2L) — Headwind/tailwind and crosswind (2R) — Density altitude (3L). Figure 4- -30 TAKEOFF 2/2 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-29 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 99: Runway Position (Rw Pos)

    Figure 4--31. The POSITION INIT page is displayed when pushing the RW POS prompt. Figure 4- -31 ACTIVE FLIGHT PLAN 1/5 Page A28- - 1146- - 181 Operational Example 4-30 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 100 Figure 4--32, and makes the coordinates available for loading. Figure 4- -32 Runway Coordinates on POSITION INIT 1/1 Page A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-31 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 101 FMS, as shown in Figure 4--33. Figure 4- -33 LOAD Prompt on POSITION INIT 1/1 Page A28- - 1146- - 181 Operational Example 4-32 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 102: Takeoff

    50 NM from the origin airport. The DEPARTURE prompt is displayed only when the origin is an airport. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-33 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 103 Figure 4--35. This process is called waypoint sequencing. Figure 4- -35 Waypoint Sequencing on ACTIVE FLT PLAN 1/5 A28- - 1146- - 181 Operational Example 4-34 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 104 ACTIVE FLT PLAN page 1 and PROGRESS page 1 are considered the primary pages of the FMS during flight. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-35 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 105 Changes to the flight plan also effect the TOC and TOD positions. A28- - 1146- - 181 Operational Example 4-36 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 106 — FMS computed wind, headwind, and crosswind(3L) — FMS computed ground speed (3R). 01574.02 Figure 4- -38 PROGRESS 3/3 Page A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-37 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 107: Climb

    When the aircraft is within 200 NM, the PERF DATA prompt changes to ARRIVAL. The ARRIVAL prompt permits access to the ARRIVAL page described in Section 6, Navigation. A28- - 1146- - 181 Operational Example 4-38 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 108: En Route

    The entered IDENT becomes the TO waypoint. Either of these actions results in the FMS to immediately alter course. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-39 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 109: Descent

    ARRIVAL page is always accessed from the NAV INDEX. Figure 4- -41 ARRIVAL Prompt on ACTIVE FLT PLAN 1/2 A28- - 1146- - 181 Operational Example 4-40 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 110 2L to choose an approach. Selecting an approach automatically selects a surface. 02131.05 Figure 4- -42 ARRIVAL 1/1 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-41 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 111 KHOU APPROACH page, the ILS 04 approach (5R) is selected. 01867.02 Figure 4- -43 KHOU APPROACH 1/2 A28- - 1146- - 181 Operational Example 4-42 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 112 Entry of a course in 1L is permitted. 01868.02 Figure 4- -44 KHOU APPROACH TRANS 1/1 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-43 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 113 STAR page. From the STAR page, the BLUBL2 arrival is selected (1L). 0 1869.03 Figure 4- -45 KHOU STAR 1/1 A28- - 1146- - 181 Operational Example 4-44 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 114 ACTIVATE prompt at 6R inserts the selected procedures in the active flight plan. 0 1870.03 Figure 4- -46 KHOU STAR TRANS 1/1 A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-45 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 115: Approach

    When a nonprecision approach is selected, the FMS is used for guidance on final approach. A28- - 1146- - 181 Operational Example 4-46 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 116: Landing

    (ADC) value, or default of 29.92 and is used to calculate the pressure altitude for the surface elevation. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-47 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 117 — Surface threshold (1R) — Headwind/tailwind and crosswind (2R) — Density altitude (3L). Figure 4- -49 LANDING 2/2 A28- - 1146- - 181 Operational Example 4-48 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 118: Missed Approach

    When MISSED APPR is selected, any portion of the flight plan past the MAP is replaced with the missed approach procedure. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-49 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 119: Alternate Flight Plan

    DIR key. 01791.02 Figure 4- -51 ALTERNATE FPL 1/2 A28- - 1146- - 181 Operational Example 4-50 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 120: Clearing Of Flight Plans

    Another action conducted on the ground for clearing the active flight plan is to activate the previously inactive database on the NAV IDENT page of the MCDU. A28- - 1146- - 181 Operational Example REV 3 Mar 2009 4-51 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 121 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Operational Example 4-52 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 122: Performance

    FMS fuel management data must not be used in lieu of the primary fuel flow indicator display of the aircraft. A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 123: Performance Index

    2R -- LANDING is shown in Figure 5--18, page 5-32. 3R -- APPRCH SPD is shown in Figure 5--7, page 5-13. A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 124: Performance Initialization

    NOTE: The pilot must verify and review all the entered and computed data. A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 125 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 126 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 5- -3 Performance Initialization Block Diagram A28- - 1146- - 181 Performance REV 3 Mar 2009 5-5/5- - 6 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 127: Spd/Ff And Current Ground Speed/Ff Method

    The pilot verifies the ACFT TYPE data field has the correct aircraft type. The system generates incorrect performance predictions when the FMS contains the wrong ACDB. A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 128 CURRENT SPD/FF and PILOT SPD/FF — 2R -- The PERF MODE page is displayed when the OR prompt at 2R is pushed. A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 129 Entered winds and sensed winds (once airborne) are included in the ground speed predictions used for time en route estimates. A28- - 1146- - 181 Performance REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 130 Entering *DELETE* returns to the cruise speed schedule as defined in the ACDB. A28- - 1146- - 181 Performance 5-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 131 INIT CRZ ALT stays the same. Performance data, however, is recalculated to reflect the higher cruise altitude. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 132 Figure 5--7, is used to enter approach speed and restriction limits. Approach speed and restriction limits are used to compute FMS speed targets during approach. A28- - 1146- - 181 Performance 5-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 133 NEXT key when the APPROACH SPEED page is displayed. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 134 PERFORMANCE INIT - - LB 3/3 -- The data associated with the weight of the aircraft is displayed on the PERFORMANCE INIT 3/3 page, shown in Figure 5--9. A28- - 1146- - 181 Performance 5-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 135 Pilot weight from the previous flight remains when the aircraft is not powered down. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 136 Agusta), the value of GROSS CG is displayed in reverse video and an EXCEEDS CG LIMIT scratchpad error message is displayed. A28- - 1146- - 181 Performance 5-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 137: Performance Data

    The following line select keys correspond to the associated definitions on the PERF DATA pages 1 and 2. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 138 HOV CEIL OGE altitude at 2R is displayed in reverse video and pilot entry is not permitted. A28- - 1146- - 181 Performance 5-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 139 OAT. The best endurance speed is obtained from Agusta performance tables using average gross weight, pressure altitude, and OAT. No pilot entry is permitted. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 140: Performance Data Page 3 Definition

    PERF DATA 3/4 page, shown in Figure 5--11. Figure 5- -11 PERF DATA 3/4 Page A28- - 1146- - 181 Performance 5-20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 141 When the CATEGORY A CEILING BACKUP altitude is less than the DENS ALT (1R), the CATEGORY A CEILING BACKUP altitude is displayed in reverse video. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-21 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 142: Performance Data Page 4 Definition

    3L -- The operational status of the EAPS when installed is displayed at 3L. 4L -- The operational status of the HEATER is displayed at 4L. A28- - 1146- - 181 Performance 5-22 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 143: Performance Plan

    (W/T) prompt (right line--selects) for each waypoint. 00558.05 Figure 5- -13 PERF PLAN 1/X A28- - 1146- - 181 Performance REV 3 Mar 2009 5-23 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 144: Wind And Temperature Pages

    3R -- The predicted static air temperature is a blend of sensed and entered values. Temperature is entered in degrees Celsius (_C). A28- - 1146- - 181 Performance 5-24 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 145 100%. At 350 NM, sensed is blended 50% and entered at 50%. For other distances, wind and temperatures are blended proportionately. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-25 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 146 For shorter flight plans, entered wind matters for preflight. Once in cruise, the sensed wind takes precedence. A28- - 1146- - 181 Performance 5-26 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 147: Takeoff Pages

    A28- - 1146- - 181 Performance REV 3 Mar 2009 5-27 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 148 2R -- The surface wind is entered here. Surface wind is entered as magnetic wind. The default is entry prompts. Entering *DELETE* returns to the default. A28- - 1146- - 181 Performance 5-28 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 149 Entering *DELETE* removes any pilot--entry of both pressure altitude and baro set and the highest priority value is displayed. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-29 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 150 Figure 5--17. The TAKEOFF 2/2 page is displayed by pushing the NEXT function key when the TAKEOFF 1/2 page is displayed. A28- - 1146- - 181 Performance 5-30 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 151 3L -- Density altitude computed from the pressure altitude and the surface temperature is displayed. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-31 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 152: Landing Pages

    When the surface is a helipad: The selected surface identifier is displayed. The helipad identifier is displayed for helipads in the navigation database. A28- - 1146- - 181 Performance 5-32 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 153 The pressure altitude is displayed in the following priority order: Pilot--entered value (large characters) A28- - 1146- - 181 Performance REV 3 Mar 2009 5-33 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 154 Entry of *DELETE* removes any pilot entry and the highest priority value is displayed. A28- - 1146- - 181 Performance 5-34 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 155 The width of the surface is displayed when a surface has been selected. No entry is permitted. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-35 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 156: Fuel Management

    FMS. Pilot entries are permitted and displayed in large characters. The sensed fuel flow, when available, is displayed when entering DELETE*. A28- - 1146- - 181 Performance 5-36 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 157 The specific ranges are based on the ground speed, airspeed, and fuel flow shown on the page. No entries are permitted. A28- - 1146- - 181 Performance REV 3 Mar 2009 5-37 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 158: Aircraft Database

    (i.e., when replacing the FMS). Uploading the saved file preserves the learned information so the system does not have to start over again. A28- - 1146- - 181 Performance 5-38 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 159: Navigation

    The following figures correspond to the line select keys shown in Figure 6--1 and the associated functions are described further in this section. A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 160 5R -- PATTERNS is shown in Figure 6--88, page 6-110. 6R -- ARRIVAL is shown in Figure 6--39, page 6-47. A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 161 1R -- CONVERSION is shown in Figure 6--75, page 6-96. 2R -- MAINTENANCE is shown in Figure 6--131, page 6-177. A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 162: Flight Plan List

    When no flight plans are stored in the FMS, the flight plan list page is blank, as shown in Figure 6--3. 01592.01 Figure 6- -3 FLIGHT PLAN LIST 1/1 A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 163 When flight plans have been defined, the page lists the flight plans by name, as shown in Figure 6--4. 01593.01 Figure 6- -4 Flight Plan Defined A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 164: Defining Stored Flight Plans

    Selecting SHOW FPL (1L), as shown in Figure 6--5. 01594.01 Figure 6- -5 SHOW FPL A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 165 (GS) at 1R. Distance and time are updated as waypoints are added to the flight plan. The defaulted ground speed is 120 knots (kts). A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 166: Deleting Stored Flight Plans

    Pushing the line select key adjacent to the flight plan name erases the stored flight plan from the FMS memory. A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 167: Flight Plan Select

    Select desired flight plan from the list by pushing the adjacent line select key. The name is displayed in the scratchpad. Select FPL SEL at 6R. A28- - 1146- - 181 Navigation REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 168 Select ACTIVATE by pushing 1R and INVERT/ACTIVATE by pushing 2R, as shown in Figure 6--8. 01597.02 Figure 6- -8 INVERT/ACTIVATE FPL A28- - 1146- - 181 Navigation 6-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 169 The FMS requires a confirmation step, as shown in Figure 6--9. 01598.01 Figure 6- -9 CONFIRM REPLACING ACTIVE FLIGHT PLAN A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 170: Pilot Waypoint List

    Enter an identifier of one to five characters and line select to the SHOW WAYPOINT line (1L). DAISY is used for this example. A28- - 1146- - 181 Navigation 6-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 171 LAT/LON coordinates of the pilot--defined waypoint. Enter latitude/longitude and select to 2L. N3320.77W11152.58 is used in this example. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 172 (NM). Bearing inputs are assumed magnetic. True bearings are designated by placing the letter T after the bearing. A28- - 1146- - 181 Navigation 6-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 173 TFD in degrees. Bearing inputs are assumed to be magnetic. True bearings are designated by placing the letter T after the bearing. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 174 Figure 6--14. When a waypoint is defined by P/B/P/B, only the coordinates are stored and displayed. Figure 6- -14 Waypoint Defined by P/B/P/B A28- - 1146- - 181 Navigation 6-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 175 Procedure 6- -5 Stored Waypoints Option Two Enter latitude/longitude and select to 1L. N3320.77W11152.58 is used in Figure 6--15. Figure 6- -15 Show Waypoint A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 176 (NDB) or custom database (CDB), the ALREADY EXISTS scratchpad message is displayed. This prevents the duplication of waypoint names. A28- - 1146- - 181 Navigation 6-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 177: Database

    (6R) pages are accessed using the prompts at the bottom of the DATA BASE WPT page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 178: Airports/Heliports

    — Waypoint type (1R) — Airport/heliport name (2L) — Country (3L). 00621.04 Figure 6- -18 DATA BASE WPT 1/3 A28- - 1146- - 181 Navigation 6-20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 179 — Coordinate position (2L) — Field elevation (3L) — Magnetic variation (3R). 00622.05 Figure 6- -19 DATA BASE WPT 2/3 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-21 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 180 — Access to airport runways (2L), when available — Access to heliport helipads (3L), when available. 01601.02 Figure 6- -20 DATA BASE WPT 3/3 A28- - 1146- - 181 Navigation 6-22 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 181 Figure 6--21, is displayed in this example by pushing 2L. 01091.04 Figure 6- -21 KPHX RUNWAYS 1/1 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-23 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 182 Figure 6--21, is displayed when the RETURN prompt in 6R is selected. 00623.04 Figure 6- -22 DATA BASE WPT 1/3 Return Prompt A28- - 1146- - 181 Navigation 6-24 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 183: Surfaces/Helipads

    — Airport or heliport name (2L) and country (3L). 01603.02 Figure 6- -23 DATA BASE WPT 1/3 for Runway/Helipad A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-25 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 184 — Coordinate position (2L) — Elevation (3L) — Magnetic variation (3R). 01604.02 Figure 6- -24 DATA BASE WPT 2/3 for Runway/Helipad A28- - 1146- - 181 Navigation 6-26 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 185 — ILS glideslope when applicable (3L) — Displaced threshold (3R). 01605.03 Figure 6- -25 DATA BASE WPT 3/3 for Runway/Helipad A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-27 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 186: Navaids

    — UR (unrestricted). Coordinate position (2L) Elevation (3L) Magnetic declination (3R). 00626.03 Figure 6- -26 DATA BASE WPT 1/1 Navaids A28- - 1146- - 181 Navigation 6-28 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 187 The letters NB are entered after the identifier. 01607.02 Figure 6- -27 DATA BASE WPT 1/1 NB A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-29 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 188: Instrument Landing Systems

    — III. Localizer antenna coordinates (2L) Magnetic declination (3R). 00627.03 Figure 6- -28 DATA BASE WPT 1/1 ILS A28- - 1146- - 181 Navigation 6-30 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 189: Intersections

    Intersection identifier (1L) Country (1L) Intersection coordinates (2L) Magnetic variation (3R). 00628.03 Figure 6- -29 DATA BASE WPT 1/1 Intersections A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-31 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 190: Multiple Waypoints

    FMS switches to the PILOT WAYPOINT page and shows the waypoint, as well as the data about the waypoint. A28- - 1146- - 181 Navigation 6-32 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 191: Undefined Waypoints

    The navigation database contains the following: Navaids Airports Heliports Runways Helipads Airways (high and low) SIDs and STARs Approaches Named intersections Outer markers. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-33 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 192: Custom Database

    The pilot defines temporary waypoints. Temporary waypoints are not given a permanent name and are not permanently stored in the custom database. A28- - 1146- - 181 Navigation 6-34 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 193: Departures

    Delete the procedure by activating a flight plan from the custom database. Delete the FROM waypoint in the active flight plan. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-35 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 194 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 6- -31 Denver, CO PIKES4 Departure A28- - 1146- - 181 Navigation 6-36 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 195 SURFACES page, shown in Figure 6--32. Runway 25 (4L) is selected in this example. Figure 6- -32 DEPARTURE SURFACES 2/3 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-37 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 196 Select the SID from the SIDs page, shown in Figure 6--33. PIKES4 (3L) is selected in this example. Figure 6- -33 SIDs 1/1 Page A28- - 1146- - 181 Navigation 6-38 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 197 TRANS page, shown in Figure 6--34. ALS (2L) is selected in this example. Figure 6- -34 DEPARTURE TRANS 1/1 Page A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-39 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 198 The selected portion of the procedure is reviewed and/or inserted into the flight plan. A28- - 1146- - 181 Navigation 6-40 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 199 DELETE button, is a climb on the heading of 194_ from the waypoint DEN to the waypoint SOLAR. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-41 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 200 However, when the airport is not part of the active flight plan, the SID cannot be activated. A28- - 1146- - 181 Navigation 6-42 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 201: Arrival

    — Replace a procedure segment already in the active flight plan — Delete a procedure segment from the active flight plan. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-43 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 202 Delete the hold attribute from the course reversal hold waypoint. Figure 6--38 shows the STAR plate. Refer to Procedure 6--7 for arrival selection. A28- - 1146- - 181 Navigation 6-44 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 203 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 6- -38 Minneapolis, MN KASPR2 Arrival A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-45 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 204 Select ARRIVAL from the active flight plan or NAV INDEX. Select RUNWAY, APPROACH, or STAR from the ARRIVAL page, shown in Figure 6--39. A28- - 1146- - 181 Navigation 6-46 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 205 When an approach is to be selected, a step is saved by selecting APPROACH from this page. The surface is automatically selected when an approach is selected. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-47 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 206 Any previously selected surface is labeled as (ACT) or (SEL). When necessary, more than one page of runways is displayed. A28- - 1146- - 181 Navigation 6-48 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 207 When only the straight-in portion of an approach is desired, select the approach without selecting an approach transition. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-49 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 208 TRANSITION shown on the page is able to be selected. In this example, (1L) is selected. Figure 6- -42 KMSP APPROACH TRANS 1/1 A28- - 1146- - 181 Navigation 6-50 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 209 Select the STAR from the STAR page, shown in Figure 6--43. In this example, KASPR2 (4L) is selected. 00699.05 Figure 6- -43 KMSP STAR 1/1 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-51 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 210 Figure 6--44. In this example, MCW (3L) is selected. 00700.05 Figure 6- -44 KMSP STAR TRANS 1/1 A28- - 1146- - 181 Navigation 6-52 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 211 REVIEW (6L). In this example, REVIEW (6L) is selected. 02126.01 Figure 6- -45 ARRIVAL 1/1 REVIEW A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-53 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 212 NEXT (paging keys) from page 1/4, shown in Figure 6--46 . 00701.07 Figure 6- -46 ARRIVAL REVIEW 1/4 A28- - 1146- - 181 Navigation 6-54 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 213 00702.05 Figure 6- -47 ARRIVAL REVIEW 2/4 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-55 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 214: Approach

    These differences are the result of changes in magnetic variation and are normally less than 2 degrees. Verify possible changes before starting an approach. A28- - 1146- - 181 Navigation 6-56 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 215 MDA until the runway is visible and the approach is able to be made. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-57 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 216: Missed Approach

    When MISSED APRCH is selected, the APRCH annunciator goes out and the FMS transfers from the approach mode to the terminal mode. A28- - 1146- - 181 Navigation 6-58 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 217 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Table 6- -1 Typical FMS Pattern Displays Approach Chart Depiction FMS Groundtrack Transition DME Arc Procedure Turn A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-59 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 218 45_ intercept to the final approach course. Typically, the aircraft banks until the final approach course is captured. A28- - 1146- - 181 Navigation 6-60 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 219: Position Sensors

    However, the FMS annunciates the navigation mode as the radio is updating. Some mode changes require several minutes to complete. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-61 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 220 From the POS SENSORS page, the pilot can remove sensors from being used for position updating (refer to Procedure 6--8). A28- - 1146- - 181 Navigation 6-62 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 221: Fms Position Update

    In this example, the FMS position is checked when the aircraft passes over the ZUN VORTAC. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-63 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 222 Before reaching ZUN, select the UPDATE prompt (1R), as shown in Figure 6--50. Figure 6- -50 POS SENSORS UPDATE A28- - 1146- - 181 Navigation 6-64 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 223 POSITION is not the current FMS position, but is the FMS position when the manual prompt was pushed. The FMS continues to update current aircraft position. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-65 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 224 Enter either an identifier or coordinates for the REF WPT. For this example, enter ZUN as the REF WPT. Figure 6- -52 REF WPT A28- - 1146- - 181 Navigation 6-66 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 225 GPS or radios. When the CLEAR prompt is selected, no correction is applied to the FMS position. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-67 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 226 FMS POSITION DETAILS -- Any position sensor set to receive an update is also updated to the new position. A28- - 1146- - 181 Navigation 6-68 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 227 Select POS SENSORS from the NAV INDEX. Select the UPDATE prompt (1R), as shown in Figure 6--55. Figure 6- -55 UPDATE Prompt A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-69 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 228 Procedure 6- -9 FMS Position Update to Long- -Range Sensor Select the SENSOR prompt, as shown in Figure 6--56. 00711.03 Figure 6- -56 SENSOR Prompt A28- - 1146- - 181 Navigation 6-70 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 229 Figure 6--57, for the sensor to be used for updating the FMS. In this example, GPS 1 (2R) is selected. Figure 6- -57 GPS UPDATE Prompt A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-71 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 230 Reset Update Function DETAILS -- Any position sensors set to receive an update are also updated to the new position. A28- - 1146- - 181 Navigation 6-72 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 231: Sensor Status Pages

    POS SENSORS prompt at the bottom of any STATUS page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-73 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 232 Ground speed Altitude (altitude above the earth) Miles from FMS position. 00718.03 Figure 6- -60 GPS 1 STATUS 1/2 A28- - 1146- - 181 Navigation 6-74 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 233 HEIGHT ABOVE MSL HEIGHT ABOVE ELLIPSOID EARTH’S SURFACE WGS- -84 ELLIPSOID fms055995.01 Figure 6- -61 GPS Altitude vs. Pressure Altitude A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-75 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 234 Satellites tracked. Figure 6- -62 GPS 1 STATUS 2/2 RAIM and FOM indicate current uncertainty of position expressed in A28- - 1146- - 181 Navigation 6-76 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 235 YES indicates RAIM is predicted to be within approach criteria. NO indicates RAIM is predicted to be unacceptable or unavailable. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-77 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 236 Access to the position sensors (POS SENSORS) prompt (6L) Return access to the GPS status page (RETURN) (6R). A28- - 1146- - 181 Navigation 6-78 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 237 The DESTINATION RAIM 1/2 page, shown in Figure 6--64, is displayed by pushing the DEST prompt on the PREDICTIVE RAIM page. 00721.04 Figure 6- -64 DESTINATION RAIM 1/2 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-79 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 238 Destination RAIM predicted for ETA+15 minutes (3R) Access to the POS SENSORS prompt (6L) Return access to the PRED RAIM page (6R). A28- - 1146- - 181 Navigation 6-80 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 239 2L, 2R, 3L and 3R -- The satellite PRN is entered on these lines. Dashes are displayed when *DELETE* is entered. All PRN numbers are cleared after the aircraft has landed. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-81 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 240 RAIM predicted for ETA+15 minutes (3R) Access to the POS SENSORS prompt (6L) Return access to the PRED RAIM page (6R). A28- - 1146- - 181 Navigation 6-82 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 241 There are only 32 PRN codes available for use by the GPS satellites in the current GPS constellation. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-83 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 242 FMS has its own page. Access to the NOTAM page is given at 6R. 00709.04 Figure 6- -68 VOR/DME 1 1/2 Page A28- - 1146- - 181 Navigation 6-84 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 243: Notice To Airmen

    An entry is permitted to be replaced with another navaid without first being deleted. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-85 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 244: Sensors Being Used By The Fms

    ≤ Lesser of 130 NM or Line of Sight > 12,000 ft MSL ≤ Lesser of 200 NM or Line of Sight A28- - 1146- - 181 Navigation 6-86 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 245: Position Sensor Deselection

    Push the left line select key next to the sensor that is to be used. The DESEL adjacent to the sensor identifier is deleted and the FMS can use the sensor. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-87 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 246 Push the left line select key next to a station identifier. DESEL is removed from all the selected station identifiers and the FMS can use the radio. A28- - 1146- - 181 Navigation 6-88 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 247: Tuning Nav Radios

    Select the NAV 1 (6L) or NAV 2 (6R) prompt at the bottom of the PROGRESS page, shown in Figure 6--70. In the example, NAV 1 is selected. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-89 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 248 Select the desired station from the ten closest stations, as shown in Figure 6--71. TFD is selected in this example. 00730.04 Figure 6- -71 Desired Station A28- - 1146- - 181 Navigation 6-90 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 249 PROGRESS page. The identifier is marked with an R to indicate the radio has been remotely tuned. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-91 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 250 Regardless of the tuning mode, the FMS constantly tunes the scanning channels of the DME (when available) for position update. A28- - 1146- - 181 Navigation 6-92 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 251: Autotune

    ILS mode or preview mode. Confirm the VOR radio is not in the manual tune mode. Select PROG from the MCDU panel. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-93 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 252 PROGRESS page. The FMS switches to autotuning and the letter A is displayed, as shown in Figure 6--74. Figure 6- -74 FMS Switches to Autotune A28- - 1146- - 181 Navigation 6-94 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 253: Vor Tuning

    DME channel. Tuning is done only by the pilot through the radio tune source. The FMS still tunes the blind channels of the scanning DME during this mode. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-95 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 254: Conversion

    The pilot must verify the FL displayed by the FMS agrees with the metric altitude conversions displayed on en route navigation charts. A28- - 1146- - 181 Navigation 6-96 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 255 3L and 3R -- The equivalent weight in the opposite unit is displayed when entry of gallons or liters is made. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-97 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 256 3L and 3R -- The equivalent distance in the opposite unit is displayed when entry of NM or kilometers (KM) is made. A28- - 1146- - 181 Navigation 6-98 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 257 The remaining parameters are displayed when entry of pounds, kilograms, gallons, or liters is made. Figure 6--79 is an example with an entry of 10,000 pounds. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-99 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 258 FMS. Figure 6--80 shows the variation of the specific weight of fuel as temperature varies. A28- - 1146- - 181 Navigation 6-100 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 259 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure 6- -80 Average Specific Weight Variation of Aviation Fuels and Lubricants A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-101 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 260 FMS is unable to covert to the QFE/QNH altimeter seetting, the equivalent unit(s) for the entered altimeter setting are computed and displayed. A28- - 1146- - 181 Navigation 6-102 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 261 QFE in inches of mercury (2L), millibars/hectopascals (3L), and millimeters (4L) is displayed. Entering *DELETE* returns the default of dashes. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-103 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 262 QNH in inches of mercury (2R), millibars/hectopascals (3R), and millimeters (4R) is displayed. Entering *DELETE* returns the default of dashes. A28- - 1146- - 181 Navigation 6-104 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 263: Patterns

    The ORBIT and RADIAL pattern prompts are displayed when SPECIAL MISSION is turned ON. See setting special mission under Flight Configuration for details. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-105 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 264 TO NEXT WAYPOINT PILOT ENTERED OR PROCEDURE FIX SYSTEM GENERATED FIX FLYOVER PATTERN fms049175.01 Figure 6- -83 Pattern Formats A28- - 1146- - 181 Navigation 6-106 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 265: Pattern Review

    REVIEW (6L). The pilot can review all patterns of all types in the applicable flight plan. 01674.02 Figure 6- -84 Pattern Review A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-107 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 266: Holding Pattern

    DIRECT ENTRY - - TURN 1 TURN ONE PARALLEL ENTRY OUTBOUND LEG fms049173.01 Figure 6- -86 Entry Geometry A28- - 1146- - 181 Navigation 6-108 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 267 DETAILS -- As an alternative, the PATTERNS prompt can also be selected from the NAV INDEX (Page 1). A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-109 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 268 Select the HOLD prompt at 1L, as shown in Figure 6--88. *HOLD* is placed in the scratchpad. Figure 6- -88 HOLD Prompt A28- - 1146- - 181 Navigation 6-110 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 269 Figure 6--89. In this example, MCW (2L) is selected. 00738.06 Figure 6- -89 Desired Holding Fix A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-111 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 270 To adjust only the turn direction, enter a slash (/) followed by an L or R. A28- - 1146- - 181 Navigation 6-112 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 271 Possible entries for the quadrant are as follows: Quadrant Inbound Course (180_) (225_) (270_) (315_) (000_) (045_) (090_) (135_) A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-113 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 272 90 kts. Leg time defaults to 1.0 minutes. A28- - 1146- - 181 Navigation 6-114 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 273 FMS does not insert the holding pattern into the active flight plan. The HOLDING PATTERN page shows the holding fix as undefined. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-115 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 274 Push the line select key (1L) of the FROM waypoint (first waypoint on the first page of the ACTIVE FLT PLAN). A28- - 1146- - 181 Navigation 6-116 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 275 H. This deletes the HOLD but not the waypoint. A second *DELETE* deletes the waypoint. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-117 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 276 Select the DELETE prompt at 6R, as shown in Figure 6--94. 01639.03 Figure 6- -94 Selecting the DELETE Prompt Return to the active flight plan page. A28- - 1146- - 181 Navigation 6-118 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 277 Figure 6--96, on the ACTIVE FLT PLAN page. When RESUME HOLD is selected, the FMS continues to the holding fix and then resumes the holding pattern. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-119 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 278 When holding is resumed, exiting the holding pattern requires pilot action. A28- - 1146- - 181 Navigation 6-120 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 279: Procedure Turn

    HOT VOR. The procedure turn begins with an outbound leg starting at the initial approach fix (IAF) HOSSY. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-121 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 280 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter & Figure 6- -98 Hot Springs, AR ILS Rwy 5 A28- - 1146- - 181 Navigation 6-122 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 281 When the high ground speed is maintained, the aircraft can overshoot the turn inbound and possibly exceed protected airspace. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-123 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 282 FAF. In this example, the *INTXX waypoint (XX represents a number to distinguish from other *INTXX waypoints) is assigned the number 01 by the FMS. A28- - 1146- - 181 Navigation 6-124 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 283 The procedure turn is still defined with these values. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-125 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 284 The process does not ensure compliance with procedure turn rules, but does give a manual procedure for turning inbound, when requested by ATC. A28- - 1146- - 181 Navigation 6-126 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 285: Flyover Pattern

    There are no exit procedures. Either deleting the flyover or changing the flight plan eliminates the flyover waypoint. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-127 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 286: Orbit Pattern

    ORBIT and compute VDEV. Figure 6- -102 Orbit Definition A28- - 1146- - 181 Navigation 6-128 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 287 ORBIT 1/1 Enter the required radius at 1R. Enter the required speed at 2R (when different from the default). A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-129 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 288 6L on the active flight plan page. When EXIT is selected, the aircraft immediately leaves the orbit and proceeds to the next waypoint in the flight plan. A28- - 1146- - 181 Navigation 6-130 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 289: Radial Pattern

    Select the RADIAL prompt at 3L. This action places *RADIAL* into the scratchpad. Push the left line select key corresponding to the radial pattern fix waypoint. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-131 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 290 Since a radial pattern is flown as normal legs between waypoints, there is no exit procedure. The normal direct--to and waypoint delete procedures exit the radial pattern. A28- - 1146- - 181 Navigation 6-132 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 291: Multiple Patterns

    FLYOVER, HOLD, RADIAL. When a HOLD or ORBIT is defined on a waypoint with a FLYOVER, the FLYOVER is automatically deleted. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-133 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 292: Navigation

    PATTERNS are selected from the NAV INDEX (page 1). Select the SUSPEND prompt at 4L. This action places *SUSPEND* into the scratchpad. A28- - 1146- - 181 Navigation 6-134 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 293 Figure 6--107. In this example, MCW (2L) is selected. Figure 6- -107 ACTIVE FLT PLAN 6/9 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-135 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 294 Select the PATTERN prompt at 6L. As an alternative, PATTERNS are selected from the NAV INDEX page, shown in Figure 6--109. Select the PATTERN prompt (5R). A28- - 1146- - 181 Navigation 6-136 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 295 Step Procedure 6- -25 Flight Plan Suspend Definition at Present Position (cont) 01674.02 Figure 6- -109 PATTERNS Prompt A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-137 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 296 Select the SUSPEND prompt (4L), as shown in Figure 6--110. This action places *SUSPEND* into the scratchpad. Figure 6- -110 PATTERNS 1/1 SUSPEND Prompt A28- - 1146- - 181 Navigation 6-138 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 297 The flight plan is also resumed by initiation of direct--to to any waypoint on the active flight plan. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-139 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 298 Resume Flight Plan Select the RESUME prompt (6L). Confirm the initiation of DIR TO operation to SUS01 waypoint. A28- - 1146- - 181 Navigation 6-140 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 299 S. This deletes the SUSPEND, but not the waypoint. A second DELETE deletes the waypoint. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-141 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 300: Search Patterns

    Select the PATTERNS prompt (5R) from the NAV INDEX, shown in Figure 6--114. 01674.02 Figure 6- -114 PATTERNS Prompt on NAV INDEX Page A28- - 1146- - 181 Navigation 6-142 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 301 Select the SEARCH prompt (3R), as shown in Figure 6--115. *SEARCH* is placed into the scratchpad. Figure 6- -115 PATTERNS 1/1 SEARCH Prompt A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-143 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 302 When *SEARCH* is placed on an invalid waypoint, an INVALID ENTRY scratchpad message displayed. PBPB (place/bearing/place/bearing) or PD (place/distance) temporary waypoint are invalid search waypoint. A28- - 1146- - 181 Navigation 6-144 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 303: Expanding Square Search

    *SEARCH* into the scratchpad. After *SEARCH* from the scratchpad is up--selected onto a waypoint, the active flight plan waypoint transitions to the SEARCH PATTERNS page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-145 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 304 2L. The active turn direction is displayed in large green font and the inactive turn direction is displayed in small white font. A28- - 1146- - 181 Navigation 6-146 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 305 Entry of a leg length value greater than the radius results in an INVALID ENTRY scratchpad message. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-147 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 306 The ACTIVATE prompt is displayed at 6R when one of the search pattern definition parameters are changed. Selecting the ACTIVATE prompt activates the search pattern. A28- - 1146- - 181 Navigation 6-148 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 307: Sector Search Pattern

    *SEARCH* into the scratchpad. After *SEARCH* from the scratchpad is up--selected onto a waypoint, the active flight plan waypoint transitions to the SEARCH PATTERNS page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-149 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 308 A28- - 1146- - 181 Navigation 6-150 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 309 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-151 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 310 The ACTIVATE prompt is displayed at 6R when one of the search pattern definition parameters is changed. Selecting the ACTIVATE prompt activates the search pattern. A28- - 1146- - 181 Navigation 6-152 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 311: Creeping Ladder Search Pattern

    (SP) waypoint, the active flight plan waypoint transitions to the SEARCH PATTERNS page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-153 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 312 A28- - 1146- - 181 Navigation 6-154 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 313 The pattern width is modifiable on the LADDER SEARCH page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-155 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 314 The ACTIVATE prompt is displayed at 6R when one of the search pattern definition parameters are changed. Selecting the ACTIVATE prompt activates the search pattern. A28- - 1146- - 181 Navigation 6-156 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 315: Parallel Search Pattern

    (SP) waypoint, the active flight plan waypoint transitions to the SEARCH PATTERNS page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-157 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 316 A28- - 1146- - 181 Navigation 6-158 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 317 No turn anticipation distance is added to the pattern length. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-159 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 318 The ACTIVATE prompt is displayed at 6R when one of the search pattern definition parameters is changed. Selecting the ACTIVATE prompt activates the search pattern. A28- - 1146- - 181 Navigation 6-160 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 319: Search Pattern Construction

    The SAR speed target is the predicted speed for SAR approach waypoints and SAR waypoints. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-161 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 320 Suspension of the search pattern is permitted at any point in the search pattern. A28- - 1146- - 181 Navigation 6-162 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 321: Mark On Target (Mot)

    At all times during the MOT maneuver, the FMS gives speed, lateral deviation, and vertical deviation information as displayed on the PFD. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-163 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 322: Phases To The Mot Flight Plan

    3. Final Target Approach -- During this phase, the pilot flies the helicopter manually from the HOV waypoint to the target location at or near the MOT waypoint. A28- - 1146- - 181 Navigation 6-164 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 323 Collective beep sets RHT height Collective FTR does nothing Cyclic beep does nothing Cyclic FTR does nothing. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-165 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 324 HOV waypoint, the flight director automatically engages the HOV mode with a zero longitudinal velocity as the reference. A28- - 1146- - 181 Navigation 6-166 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 325 After the last MOTxx waypoint is created, any subsequent MOTxx waypoint overwrites any previously existing MOTxx waypoint. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-167 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 326 DISCONTINUITY in the MOT flight plan. The SUSPEND waypoint is located on the currently active leg in the active flight plan. A28- - 1146- - 181 Navigation 6-168 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 327 FMS. Subsequently, pushing NAV on the guidance controller disconnects LNAV while the MOT flight plan continues to be displayed. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-169 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 328: Mot Flight Plan

    Valid indicated airspeed (IAS) is greater than or equal to 60 kts Valid pressure altitude MOT mode is enabled and enhanced AHRS is installed by way of the APM A28- - 1146- - 181 Navigation 6-170 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 329 Modifications to the active MOT flight plan are not permitted (for example, no changing constraints, no changing angles, no vertical direct--to, no deleting waypoints). A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-171 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 330: Mot Page Operation

    Inserting a new waypoint at or deleting any of the following waypoints is not permitted: — FHAF — HOV — DISCONTINUITY before the MOT waypoint A28- - 1146- - 181 Navigation 6-172 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 331 MCDU are displayed on 2R through 5R. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-173 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 332 ARRIVAL prompt is displayed at 6R. Pushing the ARRIVAL prompt shows the ARRIVAL page, permitting selection of the arrival procedure and surface. A28- - 1146- - 181 Navigation 6-174 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 333: Navigation Identification

    Figure 6--130, and pushing the line select key adjacent to the item being changed. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-175 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 334 0900Z. Depending on the location, the database cycle date does not agree with the current local date. A28- - 1146- - 181 Navigation 6-176 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 335: Maintenance

    DUAL, the selected operating group is DUAL. 00753.07 Figure 6- -131 FMS 1 MAINTENANCE 1/3 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-177 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 336 Figure 6--132. After selecting an operating mode or the RETURN prompt (1R), MAINTENANCE 1/3 page is displayed. 00756.07 Figure 6- -132 OPERATING MODE 1/1 A28- - 1146- - 181 Navigation 6-178 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 337: Failed Sensors

    SENSOR HISTORY prompt (6R). The SENSOR HISTORY page is displayed in Figure 6--134. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-179 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 338 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter 00760.05 Figure 6- -134 SENSOR HISTORY 1/1 A28- - 1146- - 181 Navigation 6-180 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 339: True/Magnetic Selection

    2R. The RETURN TO SERVICE page is directly accessed by pushing the line select key at 6L. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-181 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 340: High Latitude Flying

    When leaving the region (below 88_ N or above 88_ S), the message EXITING POLAR REGION is displayed. A28- - 1146- - 181 Navigation 6-182 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 341: Return To Service

    FMS being returned to aircraft service. Figure 6- -136 RETURN TO SERVICE 1/1 A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-183 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 342: Fms Setup Pages

    Select SETUP prompt at 6L, as shown in Figure 6--137. 00759.05 Figure 6- -137 FMS 1 MAINTENANCE 2/3 Page A28- - 1146- - 181 Navigation 6-184 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 343 Selectable options are as follows: 1R -- FLIGHT CONFIG 2R -- ENGR DATA 00761.08 Figure 6- -138 FMS SETUP 1/1 Page A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-185 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 344: Flight Configuration

    Review the current configuration, as shown in Figure 6--139. Make changes, as necessary, using the required steps. Figure 6- -139 Review Current Configuration A28- - 1146- - 181 Navigation 6-186 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 345 FPL AUTO PAGE OFF -- All flight plan page changes are done using the NEXT and PREV keys. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-187 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 346 SPECIAL MISSIONS OFF -- Only standard patterns (HOLDING, PROCEDURE TURN, FLYOVER) are available for use. Push NEXT to select page 2. A28- - 1146- - 181 Navigation 6-188 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 347 ACTIVE FLT PLAN page 3 of 10 is displayed. When the FPL key is pushed again, page 4 of 10 is displayed. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-189 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 348 PCMCIA 2. When no DMU is installed, LAN is the storage device. A28- - 1146- - 181 Navigation 6-190 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 349: Engineering Data

    1R -- NT (NAVAID TUNING) DATA shows pages of information about each navaid that permits tuning. These are display--only pages and no input is permitted. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-191 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 350 4R -- ZERO BITE clears the previous recordings of built--in test equipment (BITE) results. 5L -- RM index. 5R -- Query information. A28- - 1146- - 181 Navigation 6-192 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 351: Position Initialization

    Using this feature, the runway position is updated when the aircraft is at the end of the runway ready for takeoff. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-193 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 352 Figure 6--144. The position is loaded to the FMS and transmitted to any long--range sensors connected to the FMS. A28- - 1146- - 181 Navigation 6-194 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 353 POSITION INIT page, shown in Figure 6--145, is displayed. The update feature of the FMS is used only in flight. Figure 6- -145 POSITION INIT UPDATE Prompt A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-195 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 354: Crossing Points

    1 page. The CROSSING POINTS 1/1 page is an index of the available crossing point options. 00802.05 Figure 6- -146 CROSSING POINTS 1/1 Page A28- - 1146- - 181 Navigation 6-196 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 355: Present Position (Ppos) Direct

    The CROSS PTS prompt at 6L returns to the CROSSING POINTS index. 00803.03 Figure 6- -147 PPOS DIRECT 1/1 Page A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-197 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 356: Point Abeam

    When no POINT ABEAM exists for the current flight plan, the message NO CROSSING POINT FOUND is displayed in the scratchpad. A28- - 1146- - 181 Navigation 6-198 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 357: Crossing Radial

    When the entered radial does not cross the flight plan, the message NO CROSSING POINT FOUND is displayed in the scratchpad. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-199 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 358: Latitude/Longitude Crossing

    When the flight plan does not cross the entered latitude/longitude, the message NO CROSSING POINT FOUND is displayed in the scratchpad. A28- - 1146- - 181 Navigation 6-200 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 359: Data Load

    The DATA LOAD page, shown in Figure 6--151, is used to access the database crossloading function of the FMS. 00810.03 Figure 6- -151 Accessing Database Crossloading A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-201 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 360: Crossloading Custom Or Aircraft Database

    In this example, the CUSTOM DB prompt at 1L is selected. 00810.05 Figure 6- -152 CUSTOM DB Prompt A28- - 1146- - 181 Navigation 6-202 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 361 TO FMS 2 prompt at 2L is selected. 02120.02 Figure 6- -153 TO FMS 2 Prompt A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-203 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 362 Confirm selection and select YES (6R) or NO (6L) on the DATA LOAD page, shown in Figure 6--154. 0 1723.06 Figure 6- -154 CONFIRM YES or NO A28- - 1146- - 181 Navigation 6-204 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 363 Repeat steps 1 thru 4 for each FMS. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-205 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 364: Flight Summary

    3L and 3R -- The air and ground distance for the flight is displayed on these lines. No entry is permitted. A28- - 1146- - 181 Navigation 6-206 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 365 PRINTER output configuration. 6R -- The PROGRESS 3 prompt gives access to the PROGRESS 3/3 page. A28- - 1146- - 181 Navigation REV 3 Mar 2009 6-207 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 366 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Navigation 6-208 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 367: Flight Plan

    A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 368 For example, the ABC NDB is stored in the database as ABCNB. This reduces the list of duplicate waypoint names. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 369 CROSSING POINTS pages are also sources for definition. As the name indicates, temporary waypoints are not retained in the FMS past the current flight. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 370 The origin or destination must be an airport defined in the navigation database to activate the respective runway, SID, STAR, or approach. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 371 ACTIVE FLT PLAN. Leg definitions contained in the flight plan are preserved using the described method. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 372 Linked flight plans or procedures are deleted under the same operation for deleting waypoints. This operation does not result in discontinuity. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 373 FMS for the departure, climb, cruise, descent, approach and go--around phase of flight. Speed schedules are defined during performance initialization. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 374 — The altitude preselector is set to a lower altitude — The FMS is selected as the navigation source — LNAV and VNAV are engaged. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 375 However, a specific angle constraint is permitted to be entered at a waypoint in the flight plan. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 376 Recall a previously stored flight plan (3R) Create a stored flight plan (3R) Build a flight plan by entering waypoints (2R). A28- - 1146- - 181 Flight Plan 7-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 377 3R. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 378 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter 01677.01 Figure 7- -3 FLIGHT PLAN LIST 1/1 Page 01678.01 Figure 7- -4 Required Flight Plan A28- - 1146- - 181 Flight Plan 7-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 379 When a flight plan name entered in 3R is already defined, the flight plan becomes active. 01597.02 Figure 7- -5 Flight Plan Identifier A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 380 RETURN prompt is used without a definition being entered. Temporary Waypoint -- Any temporary waypoint is permitted to be entered. A28- - 1146- - 181 Flight Plan 7-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 381 VIA.TO entry. Any waypoints in the stored flight plan after the specified waypoint are eliminated. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 382 (1R through 5R), as shown in Figure 7--8. 0 1721.02 Figure 7- -8 Vertical Entries A28- - 1146- - 181 Flight Plan 7-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 383 0 1722.02 Figure 7- -9 Speed Displayed A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 384 When this occurs, a CHANGE ACT LEG prompt is displayed, as shown in Figure 7--10. A28- - 1146- - 181 Flight Plan 7-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 385 When found, the waypoints earlier in the active flight plan are deleted. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 386 (DRK). The FMS automatically places the waypoint on the flight plan at the specified distance. Enter the altitude constraint. A28- - 1146- - 181 Flight Plan 7-20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 387 DUPLICATE FLT PLAN NAME is displayed. When this occurs, the active flight plan is not stored. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-21 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 388: Lateral Navigation

    LNAV uses up to the limits of bank angle to stay within protected airspace. A28- - 1146- - 181 Flight Plan 7-22 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 389: Lnav Submodes

    A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-23 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 390: Vertical Navigation

    Moving the throttle during VFLCH changes the aircraft pitch and vertical speed. However, the aircraft speed remains the same. A28- - 1146- - 181 Flight Plan 7-24 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 391 (MAP) regardless of the setting of the altitude preselector. This is similar in concept to glideslope capture for ILS approaches. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-25 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 392 VGP mode. The message RESET ALT SEL? is suppressed in VGP mode. A28- - 1146- - 181 Flight Plan 7-26 REV 4 Aug 2010 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 393: Vnav Operation In Flight

    (initial cruise altitude or higher when set on the selector), the FMS enters the cruise phase of flight. The speed command is adjusted to the cruise values. A28- - 1146- - 181 Flight Plan REV 4 Aug 2010 7-27 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 394 The path angle associated with the constraint is either a default angle computed by the FMS, procedure specified, or pilot--entered. A28- - 1146- - 181 Flight Plan 7-28 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 395: Vnav Special Operations

    PERFORMANCE INIT missed approach speed until the destination waypoint is changed or a flight plan is changed. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-29 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 396: Vnav Approach Temperature Compensation

    Go to Page 2 of FLIGHT CONFIG pages. The FLIGHT CONFIG page is displayed, shown in Figure 7--12. A28- - 1146- - 181 Flight Plan 7-30 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 397 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Step Procedure 7- -2 FMS Temperature Compensation Configuration (cont) Figure 7- -12 FLIGHT CONFIG 2/2 Page A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-31 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 398 Selecting 3R changes the temperature compensation mode by displaying the TEMP COMP CONFIG page, shown in Figure 7--13. A28- - 1146- - 181 Flight Plan 7-32 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 399 LANDING page and an arrival has been strung into the active flight plan. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-33 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 400 LANDING From the PERF INDEX Page On the LANDING page, enter/verify the correct OAT (outside air temperature) for the destination airport. A28- - 1146- - 181 Flight Plan 7-34 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 401 No changes are applied to performance computed values or the pilot--entered constraints. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-35 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 402 Figure 7--15, until the last page is displayed. The default page of the MDA TEMP COMP page is shown in Figure 7--17. A28- - 1146- - 181 Flight Plan 7-36 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 403 INVALID ENTRY scratchpad message. A entry is consider invalid when a number outside the range 0 to 9999 is entered. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-37 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 404 Procedure 7--4 is an example of the steps necessary for removing existing values of temperature compensated arrival altitude constraints from the active flight plan. A28- - 1146- - 181 Flight Plan 7-38 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 405 LANDING 1/2 page, shown in Figure 7--19. 01874.01 Figure 7- -19 LANDING 1/2 Page Select TEMP COMP on the LANDING page. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-39 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 406 Select ACTIVATE to apply the changes in the ACTIVE FLT PLAN page, shown in Figure 7--21. A28- - 1146- - 181 Flight Plan 7-40 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 407 The aircraft is within 30 NM of the destination An approach has been activated Valid OAT (on the LANDING page) is entered. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-41 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 408: Vnav Operational Scenarios

    (6) switching from VFLCH to ASEL to ALT with the normal 1000 ft selector alert. A28- - 1146- - 181 Flight Plan 7-42 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 409 An ATC clearance (5) is received to a lower altitude and the altitude preselector is lowered (6). IAS is pushed (5) and the aircraft begins a descent. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-43 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 410 VNAV tries to satisfy both the altitude preselector and the waypoint constraint altitude. However, VNAV never flies through the altitude preselector. A28- - 1146- - 181 Flight Plan 7-44 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 411 The flight guidance computer does a normal level off switching from VPATH to VASEL to VALT (1). A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-45 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 412 The IAS button (4) is pushed to begin the descent. As the path is approached, the vertical deviation is displayed on the EFIS. A28- - 1146- - 181 Flight Plan 7-46 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 413 A vertical direct--to is conducted (5) to the constrained waypoint (1). The FMS calculates the new angle and FMS transitions to VPATH. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-47 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 414 A vertical direct--to is conducted (6) to the constrained waypoint (1). The FMS calculates the angle and FMS transitions to VPATH. A28- - 1146- - 181 Flight Plan 7-48 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 415: Speed Command

    The active speed command is also displayed on EFIS and the guidance panel. 01683.02 Figure 7- -29 Speed Command Rules A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-49 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 416: Automatic

    Manually entering the lower cruise altitude on the PERF INIT 3 page is necessary to enable the FMS to transition to the cruise speed command. A28- - 1146- - 181 Flight Plan 7-50 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 417: Waypoint Speed Constraint

    FMS attempts to return to the automatic speed schedules when no other waypoint speed constraint exists. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-51 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 418 (e.g., 120/) and then line select 2R was pushed. 01682.01 Figure 7- -30 Lateral Waypoint A28- - 1146- - 181 Flight Plan 7-52 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 419: Manual

    1R, as shown in Figure 7--31. Manual speed command mode is not available on all aircraft types. 01683.02 Figure 7- -31 Manually Entered Speed A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-53 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 420: Speed Protection

    LATCHED at 1R is displayed, as shown in Figure 7--32, on the ACTIVE FLT PLAN page. A28- - 1146- - 181 Flight Plan 7-54 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 421 The LATCHED SPEED mode is removed by entering *DELETE* from the scratchpad to line select key 1R on page 1 of the ACTIVE FLT PLAN. A28- - 1146- - 181 Flight Plan REV 3 Mar 2009 7-55 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 422 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Flight Plan 7-56 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 423: Progress

    DTG, ETE and estimated fuel remaining is displayed for the entered waypoint. No entry is permitted on 1R, 2R and 3R. A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 424: Progress 2/3 Page

    The PROGRESS 2/3 page, shown in Figure 8--2, displays the current VNAV commands being transmitted to the flight guidance computer (FGC). Figure 8- -2 PROGRESS 2/3 Page A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 425: Progress 3/3 Page

    Current wind, ground speed, and tracking information is provided on the PROGRESS 3/3 page, as shown in Figure 8--3. A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 426 6L -- This prompt gives access to the AIR DATA page. 6R -- This prompt gives access to the FLIGHT SUMMARY page. A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 427: Vnav Data

    3R -- Shows TOD and/or BOD altitude. 6L -- Gives access to PERFORMANCE INIT page 1. 6R -- Gives access to PROGRESS page 2. A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 428: Lateral Offset

    Enter the offset by pushing line select 1R. The PROGRESS page is shown in Figure 8--5. 01574.02 Figure 8- -5 Progress 3/3 Page A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 429 To manually cancel the lateral offset waypoint, push the DEL key and line select *DELETE* to 1R. A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 430: Air Data

    This page shows direct and derived data from the digital air data computer (DADC). Figure 8- -6 AIR DATA 1 1/1 Page A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 431: Required Navigation Performance (Rnp)

    6L -- When the pilot enters a manual override RNP value, selection of the NO prompt returns the manual override RNP to the original value. A28- - 1146- - 181 Progress REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 432 RNP while in DUAL mode permits the entered RNP to transfer to the coupled FMS. A28- - 1146- - 181 Progress 8-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 433: Direct/Intercept

    (FMS). They remain displayed while paging through the active flight plan. Figure 9- -1 DIRECT Prompt on ACTIVE FLT PLAN 1/4 Page A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 434 1_ and 6_. When the actual angle is less than 1_ or greater than 6_, the FMS begins a descent to intercept the limiting angle of 1_ or 6_. A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 435 Figure 9--2. The FMS recalls the flight plan from the selected waypoint and proceeds directly to the selected waypoint. 00833.05 Figure 9- -2 Direct- -To Waypoint A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 436: Pattern

    Procedure 9- -3 Intercept Using Radial/Course Push the DIR key. Push the line select key adjacent to the INTERCEPT prompt (6R). A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 437 110_ radial inbound to PGS. Insert *INTERCEPT* at 3L, to define an intercept waypoint between DRK and PGS. A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 438 The INTERCEPT 1/1 page, shown in Figure 9--4, is displayed to define the *INTERCEPT* waypoint. 00836.03 Figure 9- -4 INTERCEPT 1/1 Page A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 439 DRK. Figure 9--5 shows the INTERCEPT page following entry of the 30_ radial. 01577.01 Figure 9- -5 30 Degree Radial From Drake A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 440 Inbound Radial to PGS Select ACTIVATE (6R) or CLEAR (6L). ACTIVATE is displayed at 6R after the intercept is defined. A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 441 The defined temporary *INTERCEPT* waypoint (now labeled *RRxx) is inserted into the flight plan, as shown in Figure 9--7. Figure 9- -7 Temporary *INTERCEPT* A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 442: Intercept Using Heading Select

    040_ radial inbound to PGS. Insert *INTERCEPT* at 3L to define an intercept between DRK and PGS. A28- - 1146- - 181 Direct/Intercept 9-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 443 The INTERCEPT 1/1 page, shown in Figure 9--9, is displayed to define the *INTERCEPT* waypoint. 00836.03 Figure 9- -9 *INTERCEPT* Defined A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 9-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 444 HDG SEL at 1R, as shown in Figure 9--9. FLY HDG SEL is displayed at 1L, as shown in Figure 9--10. 01583.01 Figure 9- -10 Intercept Inbound Radial A28- - 1146- - 181 Direct/Intercept 9-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 445 3L, as shown in Figure 9--11. The course (220) is automatically displayed. 00837.03 Figure 9- -11 Fly Inbound Radial to PGS A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 9-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 446 A28- - 1146- - 181 Direct/Intercept 9-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 447: Intercepting An Arc

    *INTERCEPT* is displayed in the scratchpad, as shown in Figure 9--13. Figure 9- -13 *INTERCEPT* on ACTIVE FLT PLAN 1/6 Page A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 9-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 448 For this example, this would be waypoint D207G at 4L on page 1 of the ACTIVE FLT PLAN, as shown in Figures 9--14 and 9--15. A28- - 1146- - 181 Direct/Intercept 9-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 449 ( cont ) Figure 9- -14 End of Arc Leg 01580.02 Figure 9- -15 ACTIVE FLT PLAN 2/6 Page A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 9-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 450 The FROM waypoint at 1L (SSI) is the waypoint in the active flight plan preceding the arc. 01584.01 Figure 9- -16 Waypoint Preceding the Arc A28- - 1146- - 181 Direct/Intercept 9-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 451 SSI intercepts the 7 NM DME arc. This waypoint has replaced D302G, the published starting point for the arc. A28- - 1146- - 181 Direct/Intercept REV 3 Mar 2009 9-19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 452 Radial/Course ( cont ) Figure 9- -18 Defined Intercept Waypoint 01582.02 Figure 9- -19 Defined Intercept Waypoint Entered A28- - 1146- - 181 Direct/Intercept 9-20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 453: Multifunction Control Display Unit

    (STARs) and approaches are available only with an airport from the Jeppesen database. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 454 Range from FL000 to FL600, from --1300 to 60,000 feet. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 455 Entry in feet up to four digits Range is from 0 to 9999. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 456 Entry range is from 0 to 999,999.9 Ft page format) in 0.1 increments (decimal required for tenths). A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 457 Range is 2000.0 to 29,999.9 MHz in increments of .1. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 458 0.1 increments (decimal required for tenths) A decimal is not required when tenths position is zero. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 459 A decimal is not required when tenths position is zero. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 460 A decimal is not required when tenths position is zero. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 461 A decimal is not required when tenths position is zero. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-9 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 462 The letter in the third position indicates longitude is 100 or greater. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 463 Range is from --80_ to 54_ Celsius Range is from --112_ to 129_ Fahrenheit. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 464 Bearing is True by placing after the number (e.g., PXR/090 /30). A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 465 Entry is one or two digits Noise (PRN) Range is from 1 to 32. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 466 Entry is one to six digits Range is from 0 to 999,999. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 467 A decimal is not required when all numbers following are zero. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 468 Entry is in feet up to four digits Range is from 0 to 9999. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 469 The range of direction is 0 to 360 degrees The range of speed is 0 to 250 kts. A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format REV 3 Mar 2009 10-17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 470 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Multifunction Control Display Unit (MCDU) Entry Format 10-18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 471 AIRCRAFT DB ADVISORY The pilot must load an REQD aircraft database before selecting the FULL PERF mode. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 472 (CLB or DES) and current flight mode (climbing or descending). A28- - 1146- - 181 Messages 11-2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 473 10 nautical miles POSITION (NM) from the FMS position. CHECK GPS 2 POSITION CHECK GPS 3 POSITION A28- - 1146- - 181 Messages REV 3 Mar 2009 11-3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 474 The positions of the FMSs POSITIONS have a difference greater than 5 NM. The systems continue to operate normally. A28- - 1146- - 181 Messages 11-4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 475 DME 1 FAILED ALERTING Indicates the FMS senses a DME failure for the identified DME 2 FAILED unit. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 476 The pressure altitude limit is ALTITUDE LIMIT exceeded. EXCEEDS WIND ALERTING The wind limits for takeoff or LIMITS landing are exceeded. A28- - 1146- - 181 Messages 11-6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 477 FPL CONTAINS ADVISORY The stored flight plan has INVALID WPT undefined or invalid waypoints. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 478 INVALID AIRCRAFT ALERTING The aircraft database has been corrupted and has been cleared and initialized. A28- - 1146- - 181 Messages 11-8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 479 LANDING OUT OF ALERTING The landing calculation is LIMITS out of limits after the initial calculation. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-9 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 480 FMS operating in SINGLE and Auto load in a triple FMS installation. A28- - 1146- - 181 Messages 11-10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 481 PERF--VNAV ALERTING The pilot requested a UNAVAILABLE performance/VNAV function before sufficient data had been entered. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 482 OVERRIDDEN side could not be accepted because of a conflict. The change was overridden by the master FMS. A28- - 1146- - 181 Messages 11-12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 483 UNABLE OFFSET ADVISORY An attempt was made to insert an offset during holding, a STAR, or a SID. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 484 In this case, the angle is set to the maximum limit (6_). A28- - 1146- - 181 Messages 11-14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 485 WPT STORAGE ADVISORY The storage area for FULL pilot--defined waypoints is full. A28- - 1146- - 181 Messages REV 3 Mar 2009 11-15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 486 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Messages 11-16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 487 SIZE the database being downloaded.* DB SIZE IN HDR See 09* NE FILE SIZE A28- - 1146- - 181 Maintenance REV 3 Mar 2009 12-1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 488 NUM WPTS OUT The flight plan file contains a OF RANGE waypoint count less than 2 or greater than 50.{ A28- - 1146- - 181 Maintenance 12-2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 489 A read file command was sent to the ATTEMPTED AT data loader but the current open file does not contain any more data. A28- - 1146- - 181 Maintenance REV 3 Mar 2009 12-3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 490 Unused IN READ BUFFER PREV READ Internal software error (buffer BUFFER overflowed) -- probably a software OVERFLOW error. A28- - 1146- - 181 Maintenance 12-4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 491 01 when the FMS has been updated with the new asynchronous download mode). ASYNC CMD NO Unused RESPONSE A28- - 1146- - 181 Maintenance REV 3 Mar 2009 12-5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 492 Honeywell support for assistance. These codes are associated with errors in flight plan format requirements. Contact flight plan for assistance. A28- - 1146- - 181 Maintenance 12-6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 493 PARALLAX ADJUST page is accessed by pushing and holding the FN key for 5 seconds. 01686.01 Figure 12- -1 PARALLAX ADJUST 1/1 Page A28- - 1146- - 181 Maintenance REV 3 Mar 2009 12-7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 494 (or performance computer, when installed) is operating. Pushing RETURN also saves the system status for recall on subsequent flights. A28- - 1146- - 181 Maintenance 12-8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 495 Takeoff Data Page Tree A--14 Arrival/Missed Approach Page Tree A--15 Landing Page Tree A--16 A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 496 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 MCDU Page Access Trees A- - 2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 497 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -1 Function Keys Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 3/A- - 4 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 498 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -2 Perf Index Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 5/A- - 6 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 499 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -3 NAV Index Page 1/2 Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 7/A- - 8 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 500 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -4 NAV Index Page 2/2 Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 9/A- - 10 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 501 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -5 Progress Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 11/A- - 12 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 502 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -6 Direct Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 13/A- - 14 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 503 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -7 Patterns Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 15/A- - 16 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 504 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -8 Pos Sensors Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 17/A- - 18 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 505 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -9 Maintenance Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 19/A- - 20 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 506 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -10 NAV Ident/Position Init Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 21/A- - 22 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 507 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -11 Active Flight Plan/Alternate Flight Plan Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 23/A- - 24 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 508 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -12 Performance Init Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 25/A- - 26 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 509 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -13 Departure Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 27/A- - 28 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 510 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -14 Takeoff Data Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 29/A- - 30 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 511 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -15 Arrival/Missed Approach Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 31/A- - 32 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 512 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Figure A- -16 Landing Page Tree A28- - 1146- - 181 MCDU Page Access Trees REV 3 Mar 2009 A- - 33/A- - 34 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 513 AFIS airborne flight information system Aircraft Flight Manual AFMS advanced flight management system A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 514 ASEL altitude preselect altitude select above sea level ASYNC asynchronous A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 2 REV 4 Aug 2010 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 515 Celsius combiner assembly CABN cabin capture calibrated airspeed (FMS) Category A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 516 CTRL control A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 517 DISC disconnect DISENG disengage DIST distance data loader distance measuring equipment debug maintenance terminal A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 518 A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 519 FREQ frequency flight summary FSBY forced standby feet/foot orce trim release A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 520 HFOM horizontal figure of merit high power gain antenna Honeywell generated information A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 521 INIT initial initialization INMARSAT International Maritime Satellite Organization INOP inoperative internal INTERSCTN intersections inverter A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 9 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 522 LEN, LN length leading edge up limit lat/long LNAV lateral navigation landing localizer A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 523 MICSTK microphone stuck minute minimum marker microwave landing system mm/hr millimeter/hour maximum operating Mach A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 11 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 524 NORM normal NOTAM notice to airmen navaid tuning nonuniformity correction A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 12 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 525 Pacific Ocean Region position POST power on system test A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 13 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 526 RCT, REACT rain echo attenuation compensation technique RCVD received reference remaining A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 14 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 527 SELCAL selective call SERV service setting symbol generator A28- - 1146- - 181 Acronyms and Abbreviations REV 3 Mar 2009 Abbrev- - 15 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 528 TACAN tactical air navigation terrain alerting and display A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 16 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 529 TTFF time--to--first--fix transition up TWIP terminal weather information for pilots transmitting A28- - 1146- - 181 Acronyms and Abbreviations REV 4 Aug 2010 Abbrev- - 17 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 530 VORAP VOR approach VORTAC combined VOR and TACAN station A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 18 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 531 WX/T weather/turbulence XFER transfer XMIT transmission XPDR transponder cross track yaw damper A28- - 1146- - 181 Acronyms and Abbreviations REV 4 Aug 2010 Abbrev- - 19 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 532 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Acronyms and Abbreviations Abbrev- - 20 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 533 (GCC), 1-3 additions/deletions to the flight plan, 7-18 Honeywell online technical airway, 7-15 publications, 1-3 A28- - 1146- - 181 Index REV 3 Mar 2009 Index- - 1 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 534 Deleting stored flight plans, 6-8 waypoints, 7-14 Departure selection, 4-23 recall a previously stored departure surfaces, 4-23 flight plan, 7-11 A28- - 1146- - 181 Index Index- - 2 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 535 Honeywell online technical FMS position updata, 6-63 publications, 1-3 FMS product support, 1-2 Honeywell product support, 1-2 A28- - 1146- - 181 Index REV 3 Mar 2009 Index- - 3 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 536 3-7 LNAV ARM, 7-23 line select keys (LSK), 3-5 LNAV CAPTURE, 7-23 MCDU display, 3-3 A28- - 1146- - 181 Index Index- - 4 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 537 6-131 flight plan list, 6-4 defining stored flight plans, suspend, 6-134 Pilot waypoint list, 6-12 A28- - 1146- - 181 Index REV 3 Mar 2009 Index- - 5 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 538 4-47 performance data pages 1 arrival, 4-41 clearing of flight plans, 4-52 and 2 definition, 5-17 A28- - 1146- - 181 Index Index- - 6 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 539 Phases to the MOT flight plan, 6-164 PROGRESS 1/3 page, 8-1 Pilot defined waypoints, 6-32 PROGRESS 2/3 page, 8-2 A28- - 1146- - 181 Index REV 3 Mar 2009 Index- - 7 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 540 2-3 parallel search pattern, 6-157 search pattern construction, flight planning, 2-3 6-161 lateral navigation (LNAV), 2-3 A28- - 1146- - 181 Index Index- - 8 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 541 5-26 VNAV approach temperature Wind and temperature pages, 5-24 compensation, 7-30 WIND/TEMP 2/X , 5-24 A28- - 1146- - 181 Index REV 3 Mar 2009 Index- - 9 Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 542 Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter Blank Page A28- - 1146- - 181 Index Index- - 10 REV 3 Mar 2009 Honeywell International Inc. Do not copy without express permission of Honeywell.

Table of Contents