B. Procedure
S 014-002
(1)
Gain access to the forward overhead panel (P5).
S 034-003
(2)
Loosen the panhead screw that holds the indicator tightly in the clamp.
NOTE: It is not necessary to loosen the flathead screw that
____
holds the clamp to the panel.
S 024-004
(3)
Remove the cabin rate of climb indicator from the panel.
S 034-005
(4)
Disconnect the electrical connector from the cabin rate of climb indicator.
TASK 21-33-05-404-006Cabin Rate of Climb Indicator Installation
__________________________________________
A. Access
(1) Location Zone
102 Right Control Cabin
B. Procedure
S 434-007
(1)
Connect the electrical connector to the cabin rate of climb indicator.
S 424-008
(2)
Put the cabin rate of climb indicator in position in the P5-16 module.
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A 737-300/400/500MAINTENANCE MANUAL
CABIN RATE OF CLIMB INDICATOR
FORWARD OVERHEAD PANEL (P5)
(LOWER RIGHT PART)
Cabin Rate of Climb Indicator Installation
Figure 401
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E64825
A
737-300/400/500MAINTENANCE MANUAL
S 434-009
(3) Tighten the panhead screw to 7 +1/-2 in-lbs.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1.
2.
3.
A
737-300/400/500MAINTENANCE MANUAL
CABIN ALTITUDE/DIFFERENTIAL PRESSURE INDICATOR - REMOVAL/INSTALLATION
_____________________________________________________________________General
_______
A. The cabin altitude/differential pressure indicator is located in the P5-16 module on the lower right part of the forward overhead panel.
TASK 21-33-07-004-001
Cabin Altitude/Differential Pressure Indicator Removal (Fig. 401)
______________________________________________________
A. Access
(1) Location Zone
102 Right Control Cabin
B. Procedure
S 014-002
(1)
Gain access to the cabin altitude/differential pressure indicator on the P5-16 module on the forward overhead panel.
S 034-003
(2)
Loosen the two screws that hold the indicator tightly in the clamp.
NOTE: You do not have to loosen the two screws that hold the
____
clamp to the panel.
S 024-004
(3)
Remove the cabin altimeter/differential pressure indicator from the panel.
S 034-005
(4)
Remove the electrical connector from the indicator.
TASK 21-33-07-404-009Cabin Altitude/Differential Pressure Indicator Installation
___________________________________________________________
A. Access
(1) Location Zone
102 Right Control Cabin
B. Procedure
S 434-006
(1)
Connect the electrical connector to the cabin altitude/differential pressure indicator.
(2)
Put the indicator in its installed position in the P5-16 module.
S 434-008 中國航空網 m.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 空調 AIR CONDITIONING 1(117)
