(28)
AMM 20-10-91/401, Control Cables
(29)
AMM 20-10-37/401, Bonding Jumpers and Ground Leads
(30)
AMM 20-30-00/201, Specifications and Materials
(31)
AMM 20-40-11/201, Static Grounding
(32)
AMM 24-31-11/201, Main Battery
(33)
AMM 27-11-00/501, Aileron and Aileron Trim Control Unit
(34)
AMM 27-18-00/001, Aileron Position Indicating System
(35)
AMM 27-21-00/501, Rudder and Rudder Trim Control System
(36)
AMM 27-28-00/001, Rudder Position Indicating System
(37)
AMM 27-31-00/501, Elevator Control System
(38)
AMM 27-38-00/001, Elevator Position Indicating System
(39)
AMM 27-41-00/501, Horizontal Stabilizer Trim Control System
(40)
AMM 27-51-00/501, Trailing Edge Flap System
(41)
AMM 27-58-01/501, TE Flap Position Indicating System
(42)
AMM 27-61-00/501, Spoiler Control System
(43)
AMM 27-62-00/501, Speedbrake Control System
(44)
AMM 27-81-00/501, Leading Edge Slat Control System
(45)
AMM 27-88-00/501, Leading Edge Slat Position Indicating System
(46)
AMM 28-23-00/201, Defuel
(47)
AMM 29-15-00/501, Hydraulic System A, B, and Standby
(48)
AMM 29-22-00/501, Power Transfer Unit System
(49)
AMM 29-22-21/201, PTU Pressure Filter
(50)
AMM 29-32-12/401, Hydraulic Fluid Overheat Warning System
(51)
AMM 29-33-12/401, Hydraulic Fluid Quantity Transmitter/Indicator
(52)
AMM 30-31-00/501, Pitot Static Probe Anti-Icing
(53)
AMM 30-43-11/401, Nozzle - Rain Repellant Spray
(54)
AMM 30-43-00/201, Windshield Rain Repellent System
(55)
AMM 32-00-01/201, Landing Gear Downlocks
(56)
AMM 33-51-02/501, Emergency Light Batteries
(57)
AMM 34-11-01/501, Pitot-Static System
(58)
AMM 35-22-00/501, Passenger Oxygen System
(59)
AMM 38-32-00/501, Toilet System
(60)
AMM 49-11-00/201, Auxiliary Power Unit
(61)
AMM 71-00-03/201, Power Plant
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
Air Conditioning System S 212-004
(1) Examine the water separator bags to make sure they are clean.
S 422-005
(2) Install new water separator bags if it is necessary.
Electrical/Electronic and Flight Systems
S 862-006
(1)
Put all the circuit breakers in the ON position.
S 422-007
(2)
Connect the main battery.
S 862-008
(3)
Move the DC meter select switch to the BAT position.
S 212-009
(4)
Make sure the DC voltmeter shows 24 to 28 volts.
S 962-010
(5)
Replace all the gyros if they are not installed.
S 422-011
(6)
Install the batteries for the emergency exit lights and the escape slide lights.
S 862-012
(7)
Operate the Emergency Exit Lights switch in the control cabin and the aft attendant's panel.
S 212-013
(8)
Make sure the emergency exit and the escape slide lights come on.
S 422-014
(9)
Install the batteries (if removed) in the bullhorn and make sure it operates correctly.
S 422-015
(10)
AIRPLANES WITH CRASH POSITION INDICATORS; Install the beacon and the control dispenser batteries, and install the shutoff battery package.
Control Cabin Equipment
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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本文链接地址：737-300 400 500 AMM 飞机维护手册 PARKING AND MOORING(31)
