曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(4) Continue to turn the screw until the unit is
fully installed in the mounting rack.
(5) Close the GPS COMM circuit-breaker.
(6) Do a functional test. Refer to paragraph C.
Navigation
DA20-C1 AMM
Page 216
30 Apr 2009 34-50-00 Doc # DA 201-C1
Rev. 15
C. Garmin GNS530W Adjustment/Test
If possible, do an operational flight check after the radio has been replaced. Alternatively, use a
GPS COMM test set to make sure that the system operates correctly. Refer to the GNS530W
installation manual for performance specifications.
WARNING: DO NOT OPERATE THE GPS USING AN OUT-OF-DATE DATABASE.
OUT-OF-DATE DATABASE CAN CAUSE A FLIGHT SAFETY
HAZARD.
Detail Steps/Work Items Key Items
(1) Do a test of each control function. Refer to 500W Series Pilot’s Guide and
Reference to test each control function.
(2) Make sure that the database date is valid. Once the database has been
acknowledged, the instrument panel selftest
page will appear.
Refer to 500W Series Pilot’s Guide and
Reference for Instrument Panel Self-Test.
D. Data Base Loading
The GNS430W has two data card slots on the face of the unit. The NaVData card is inserted in
the left-most slot and the second slot is provided for the terrain card. Refer to 500W Series
Pilot’s Guide and Reference for NavData card use.
DA20-C1 AMM
Navigation
Doc # DA 201-C1
Rev. 15 34-50-00 Page 217
30 Apr 2009
10. Remove Install the GNS430W/GNS530W VOR, LOC, G/S Indicator
A. Remove the GNS430W/GNS530W VOR, LOC, G/S Indicator
Detail Steps/Work Items Key Items
(1) Open the related NAV COMM 1 or 2 circuitbreaker.
(2) Remove the instrument panel cover. Refer to Chapter 25-10
(3) Disconnect the electrical connector.
(4) Remove the mounting screws. Hold the indicator!
(5) Remove the indicator from the instrument
panel.
B. Install the GNS430W/GNS530W VOR, LOC, G/S Indicator
Detail Steps/Work Items Key Items
(1) Put the indicator in position in the instrument
panel.
(2) Install the mounting screws.
(3) Connect the electrical connector.
(4) Install the instrument panel cover. Refer to Chapter 25-10
(5) Do an operational test of the system.
Navigation
DA20-C1 AMM
Page 218
30 Apr 2009 34-50-00 Doc # DA 201-C1
Rev. 15
11. Antennas
Use a thin coat of ‘Penatrox’ (Manufacturer: Burndy) or ‘Noalox’ (Manufacturer: Ideal) corrosion
inhibitor between the aluminum antenna backing plate and the copper foil ground plane. Apply a
bead of Dow Corning 732 RTV around the base of the antenna where it touches the outer skin to
give a waterproof seal.
12. Connectors
Remove contacts from connectors in the radio rack with Hand Ejector Tool Molex part number HT-
1884. Crimp solderless contact terminals with Molex part number 6115.
Remove contacts from KI 208/209 connectors with Burndy part number RXK20-25 Extraction Tool
Tip and part number RXT20-4P3 Extraction Tool Handle. Crimp Burndy Socket part number
SC20M-6TK6 with Burndy Hytool M8ND.
DA20-C1 AMM
Vacuum
Doc # DA201-C1
Rev. 9 37-TITLE Page 1
29 Apr 2004
CHAPTER 37
VACUUM SYSTEM (IF FITTED)
Vacuum
DA20-C1 AMM
Page 2
19 Dec 1997 37-TITLE Doc # DA201-C1
Rev. 0
Intentionally left blank
DA20-C1 AMM
Vacuum
Doc # DA201-C1
Rev. 0 37-CONTENTS Page 1
19 Dec 1997
TABLE OF CONTENTS
CHAPTER 37-00 VACUUM - GENERAL.................................................................................................1
1. General .............................................................................................................................1
2. Description ........................................................................................................................1
3. Operation ..........................................................................................................................3
CHAPTER 37-10 VACUUM DISTRIBUTION............................................................................................1
1. General .............................................................................................................................1
TROUBLE-SHOOTING...............................................................................................................101
1. General .........................................................................................................................101
MAINTENANCE PRACTICES ....................................................................................................201
1. General .........................................................................................................................201
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
钻石20系列AMM 2(39)
