MK V MK VI MK VII MK VIII MK XXII
Enhanced Ground Proximity Warning Systems
Line Maintenance Manual
Document No: 060-4199-180, Rev F
Release date: 23 Jun 2009
Honeywell International, Inc. Redmond, Washington 98073-9701
P R O D U C T I O N - R e l e a s e - 25 J u n 2009 15:05:03 M S T - P r i n t e d o n 18 A u g 2009
This document is an unpublished work.
Copyright 2005, 2009 Honeywell International, Inc.
All rights reserved.
This document and all information and expression contained herein are the
property of Honeywell and is provided to the recipient in confidence on a
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Your use of this document constitutes acceptance of these terms.
Typed signatures constitute approval. Actual Signatures are on file at Honeywell in Redmond, WA.
DRAWN R. Halbert 23 FEB 00
CHECK
五羟基己醛ENGR R. Halbert 23 FEB 00
MFG
QA
APVD G. Gilliland 23 FEB 00
APVD
REVISIONS
SHT REV DESCRIPTION DATE
APPROVED
All Initial
release.
Reason 01 Severity 10 23 FEB 00
23 FEB 00
转炉除尘
R. Halbert
G. Gilliland
All A Direct
update:
Incorporate –008 changes
Reason 01 Severity 10 07 AUG 01
07 AUG 01
R. Henderson
L. Matter
All B Direct update to incorporate EGPWC/GNSSU part numbers and troubleshooting information. Revised Level 2
descriptions.
Reason 01 Severity 10 13 FEB 02
13 FEB 02
B. Breen
G. Gilliland
All C Direct update to incorporate Airbus and Boeing part number changes, Revised Flight History Download Card P/Ns,
reformatted TOC and added the following RAAS-related
sections:
(1) Section 2.2.15
(2) “Application Software Version Invalid” and “RCD Failed”
(MK V/VII) aural annunciations to Table 3-2.
(3) Sections 3.8.42 and 3.8.43
(4) Appendix C
Reason 01 Severity 10 08 JAN 04
09 JAN 04
J. Castro
L. Matter
All D 1) Deleted “Revisions Status of Sheets Index” table on
Sheet 3.
2) Section 3.2 (Troubleshooting Guide): Added the
statement “(this sentence does not apply to internal
GPS engines)” after the existing sentence “If no faults
are present, verify that position data from the GPS, IRS,
or FMC is correct”.
3) Section 6.1.2 (Installation): Added step 6 to account for
RAAS equipped EGPWC units.
4) Appendix C:
- Revised Table B1-1 to C1-1.
- Revised Table B1-2 to C1-2.
- Table C1-2: Added note that “Operators/Installers must
refer to their Instructions for Continued Airworthiness
(ICA) documentation to identify the approved RCD
configurations specific to their aircraft type/model having
RAAS installed”.
Reason 01 Severity 10 27 SEP 04
30 SEP 04
K. Christofferson
S. Wright
REVISIONS
SHT REV DESCRIPTION DATE
APPROVED
All E Section 3.3.2 – added RAAS maintenance message to short Level 1 Self-Test sequence and two notes, one to ensure
RAAS messages only occur if RAAS is activated and one to
explain the GPS NOT NAVIGATING enunciation.
Section 3.5 - added note to ensure RAAS message only
occurs if RAAS is activated.
Section 6.1.2 – modified step 6 to add Level 3 Self-Test.
Reason 01 Severity 10 01 FEB 05扩管机
03 FEB 05
S. Wright
K. Christofferson
All F Updated per ECO-65820
Updated document to include MK XXII helicopter EGPWS
and to include software -230-230 changes for RAAS and
展示柜制作newly introduced optional functions for Stabilized Approach Monitor, Long Landing Monitor, Altimeter Monitor, and
Takeoff Flap Configuration Monitor.
EFF PT: 10 23 JUN 09 J. Mulkins
See AeroPDM
for additional
approvals
TABLE OF CONTENTS
1INTRODUCTION (8)
1.1S COPE (8)
毛细管电谱
1.2A PPLICABILITY (8)
1.3R EFERENCE D OCUMENTS (9)
2DESCRIPTION AND OPERATION (10)
2.1G ENERAL S YSTEM D ESCRIPTION (10)
2.1.1Enhanced Ground Proximity Warning Computer (EGPWC) (11)
2.2O PERATION (11)
2.2.1Mode 1 – Excessive Descent Rate (11)
2.2.2Mode 2A/2B - Terrain Closure Rate (11)
2.2.3Mode 3 - Descent After Takeoff (11)
2.2.4Mode 4A/4B/4C - Unsafe Terrain Clearance (11)
2.2.5Mode 5 - Descent Below Glideslope (12)
2.2.6Mode 6 - Advisory Callouts (optional) (12)
2.2.7Mode 7 - Windshear Detection (Optional for MK V/VII only) (14)
2.2.8Envelope Modulation (not available in MK VI/VIII -001) (14)
2.2.9Terrain Clearance Floor and Runway Field Clearance Floor (14)
2.2.10Terrain Alerting and Display (optional) (15)
2.2.11Peaks Display Mode (optional) (16)
2.2.12Geometric Altitude (GPS Required) (16)
2.2.13Weather Radar AutoTilt (MK V and MK VII only) (16)
2.2.14System Display and Annunciation (17)
2.2.15Runway Awareness and Advisory System (option for MK V and MK VII only) (17)
2.2.16Stabilized Approach Monitor (option for MK V and MK VII only) (17)
2.2.17Altimeter Monitor (option for MK V and MK VII only) (17)
2.2.18Takeoff Flap Configuration Monitor (option for MK V and MK VII only) (18)
2.2.19Long Landing Monitor (option for MK V and MK VII only) (18)
2.2.20Lamp Format (19)
2.3S YSTEM M AINTENANCE (20)
2.3.1Maintenance Philosophy (20)
2.3.2System Operation During an Inop Condition (20)
挤压比2.3.3BIT Description (20)
2.3.4EGPWC Front Panel (21)
2.3.5Self-Test Functions (22)
3FAULT ISOLATION (TROUBLESHOOTING) (23)
3.1G ENERAL (23)
3.2T ROUBLESHOOTING G UIDE (23)
3.3L EVEL 1S ELF-T EST -G O/N O G O T EST (24)
3.3.1Self-Test Preamble (24)
3.3.2Short Level 1 Self-Test (25)
3.3.3Long Level 1 Self-Test (26)
3.4L EVEL 2S ELF-T EST -C URRENT F AULTS (26)
3.4.1Current Faults - Internal (27)
3.4.2Current Faults - External (27)
3.5L EVEL 3S ELF-T EST -S YSTEM C ONFIGURATION (33)
3.6L EVEL 4S ELF-T EST -F AULT H ISTORY (36)
3.7L EVEL 5S ELF-T EST -A LERT H ISTORY (37)
3.8L EVEL 6S ELF-T EST -D ISCRETE I NPUT T EST (37)
3.8.1ARINC 552 / ALT 55 Radio Altitude Validity Flag Discretes (38)
3.8.2GND Landing Gear Discrete (38)
3.8.3+28V Landing Gear Discrete (38)
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