S 015-034-002
(2)
Open the CSD access door.
S 985-035-002
(3)
Push and hold the switch on the VSCF to LAMP TEST.
(a) Make sure that the VSCF FAULT and the AIRCRAFT OPEN PHASE lights come on.
S 985-037-002
(4)
AIRPLANES WITH -15, -16, -19 AND -20 VSCF;
Release the LAMP TEST button on the VSCF.
S 985-038-002
(5)
Push and hold the switch on the VSCF to INDICATE.
(a) Make sure that the VSCF FAULT and the AIRCRAFT OPEN PHASE lights go off. 1) If the VSCF FAULT light is on, do the following step:
a) Do trouble-shooting the AC Generation System (AMM 24-21-00/101). 2) If the AIRCRAFT OPEN PHASE light is on, do as follows: a) Do trouble-shooting to the power feeder cables and the main power circuit breakers (AMM 24-21-00/101). b) Supply electrical power from the engine generator (AMM 24-22-00/201).
NOTE: This will operate the VSCF and remove the
____ AIRCRAFT OPEN PHASE failure indication.
S 985-040-002
(6)
Release the switch on the VSCF.
S 415-042-002
(7)
Close the CSD access door.
H. Make Sure that the VSCF Connected Correctly.
S 985-043-002
(1)
Push and release the applicable GEN 1 or GEN 2 switch on the P5-4 panel to ON.
(2)
Start the engine (AMM 71-00-00/201).
S 865-044-002
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
VARIABLE SPEED CONSTANT FREQUENCY ú 24-11-11
GENERATOR/CONVERTERS ú CONFIG 2 ú 02 Page 508 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 215-046-002
(3)
Make sure that the applicable DRIVE or LOW OIL PRESSURE light on the P5-5 panel goes off.
S 865-047-002
(4)
Make sure that the ac meters switch is set to the applicable GEN 1 or GEN 2 position.
(a)
Make sure that the frequency meter shows 400 | 5 Hz.
(b)
Make sure that the ac voltmeter shows 115 | 5 volts.
(c)
Push and release the applicable GEN 1 or GEN 2 switch to ON.
1) Make sure that the applicable GEN OFF BUS No. 1 or No. 2 light goes off.
(d)
Momentarily push the GRD PWR or the APU GEN No. 1 and No. 2 switches to ON.
S 865-048-002
(5)
Do a shutdown of the engine (AMM 71-00-00/201).
S 865-049-002
(6)
Remove electrical power if it is not necessary (AMM 24-22-00/201).
TASK 24-11-11-715-050-002
3. System Load Test - Variable Speed Constant Frequency Generator/Converter________________________________________________________________________
A. General
(1)
This test will make sure that the variable speed constant frequency generator/converter (VSCF) will supply power to loads correctly. During this test, it is necessary to operate the engine and connect the VSCF to loads. The loads that you will use are the lights, air conditioning, fuel boost pumps, hydraulic pumps and galleys.
(2)
The VSCF is on the accessory gearbox at the 8 o'clock position.
B.
References
(1)
AMM 24-11-11/401, Variable Speed Constant Frequency
Generator/Converter
(2)
AMM 24-21-00/101, AC Generation System
(3)
AMM 24-22-00/201, Manual Control
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
VARIABLE SPEED CONSTANT FREQUENCY ú 24-11-11
GENERATOR/CONVERTERS ú CONFIG 2 ú 03 Page 509 ú Nov 12/00
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 電源 ELECTRICAL POWER(47)
