(2)
Installation of the P5-17 temperature control module
TASK 21-61-01-004-004
2. Temperature Control Module Removal (Fig. 401)
__________________________________
A. Access
(1) Location Zone
102 Control Cabin - Right
B. Procedure
S 864-006
(1)
Make sure that the L and R PACK switches on the P5-10 air conditioning panel are set to OFF.
S 864-007
(2)
Open all the circuit breakers on the P6-4 panel for the air conditioning system and the temperature control system and install DO-NOT-CLOSE tags.
S 864-008
(3)
Open these circuit breakers on the P6-3 panel and install DO-NOT-CLOSE tags:
(a)
MASTER CAUTION (all except FUEL, if installed)
(b)
INDICATOR LIGHTS, MASTER DIM BUS (9 locations)
(c)
DIM & TEST (1 location)
(d)
NOSE GEAR AIR/GND
(e)
LANDING GEAR AIR/GND RELAY & LTS
S 014-009
(4)
Lower the P5 panel to get access to the P5-17 temperature control module on the forward overhead panel in the flight deck.
S 034-010
(5)
Disconnect all electrical connectors at the back of the P5-17 temperature control module.
S 034-011
(6)
Loosen the 1/4 turn fasteners at the four corners of the P5-17 temperature control module that attach the module to the P5 forward overhead panel.
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21-61-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
P5-17 CABIN TEMPERATURE MODULE
1/4 TURN FASTENER (4 LOCATIONS)
CABIN TEMPERATURE MODULE
Cabin Temperature Module Installation
Figure 401
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ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G16395
A 737-300/400/500MAINTENANCE MANUAL
S 024-012
(7) Remove the P5-17 temperature control module.
TASK 21-61-01-404-005
3. Temperature Control Module Installation (Fig. 401)
_______________________________________
A. References
(1) AMM 36-05-00/201, Pressurize/Depressurize Pneumatic System
B. Access
(1) Location Zone
101 Control Cabin - Left
102 Control Cabin - Right
C. Procedure
S 424-013
(1)
Put the P5-17 temperature control module in its position in the P5 forward overhead panel.
S 434-014
(2)
Tighten the 1/4 turn fasteners that secure the temperature control module to the P5 forward overhead panel.
S 434-015
(3)
Install the electrical connectors at the back of the panel.
S 414-016
(4)
Raise the P5 forward overhead panel to its installed position and secure the fasteners at the lower corners of the panel.
S 864-017
(5)
Remove the DO-NOT-CLOSE tags on the P6-4 circuit breaker panel and close the circuit breakers for the air conditioning system and the tempeature control system.
S 864-018
(6)
Remove the DO-NOT-CLOSE tags on the P6-3 circuit breaker panel and close these circuit breakers:
(a)
MASTER CAUTION (all except FUEL, if installed)
(b)
INDICATOR LIGHTS, MASTER DIM BUS (9 locations)
(c)
DIM & TEST (1 location)
(d)
NOSE GEAR AIR/GND
(e)
LANDING GEAR AIR/GND RELAY & LTS
D. Temperature Control Module (P5-17) Test
S 864-001
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 空調 AIR CONDITIONING 2(141)
