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77-21-01
ALL ú ú C01 Page 604 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 416-008-C00 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(5)
Close the thrust reverser (AMM 78-31-00/201). S 416-012-C00
(6)
Close the fan cowl panels (AMM 71-11-02/201). S 866-014-C00
(7)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
EXHAUST GAS TEMPERATURE (EGT) INDICATOR - REMOVAL/INSTALLATION
______________________________________________________________
1. General_______
A. This procedure has two tasks. The first task removes the EGT indicator.
The second task installs the EGT indicator.
TASK 77-21-02-014-001-C00
2. Remove the EGT Indicator________________________
A. Access
(1) Location Zone
(a) 101, 102 Control Cabin
B. Procedure
S 864-002-C00
(1) For the applicable engine, open these circuit breakers and attach the DO-NOT-CLOSE identifiers:
(a) P6 Load Control Center
1) EGT IND ENG 1
2) EGT IND ENG 2
S 024-003-C00
(2) Remove the EGT indicator (Fig. 401).
(a) Loosen the adjustment screw of the clamp that attaches the indicator to the instrument panel.
NOTE: The adjustment screw has a round head.
____
(b) Carefully pull the indicator from the instrument panel.
CAUTION: CLEARLY IDENTIFY CONNECTIONS BEFORE YOU DISCONNECT THEM.
_______ CROSS-CONNECTION OF THE EGT INDICATOR (ON THE P2 INSTRUMENT PANEL) IS A POSSIBILITY WHEN YOU WORK WITH THIS COMPONENT.
(c) Disconnect the electrical connector from the indicator.
TASK 77-21-02-404-009-C00
3. Install the EGT Indicator_________________________
A. References
(1) AMM 77-21-00/501, Exhaust Gas Temperature (EGT) Indication System
B. Access
(1) Location Zone
(a) 101, 102 Control Cabin
C. Procedure
S 424-006-C00
(1) Install the EGT indicator (Fig. 401).
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77-21-02
ú ú C02 Page 401 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
12
CLAMP PANEL CLAMP ADJUSTMENT
RETAINING SCREW
SCREW
N1 TACHOMETER INDICATOR
EXHAUST GAS TEMPERATURE (EGT) INDICATOR
SEE B
900`C ON HORIZONTAL CENTERLINE
N2 TACHOMETER INDICATOR
CLAMP
EGT INDICATOR
REVERSER REVERSER
UNLOCKED UNLOCKED
% RPM X 10 % RPM X 10
8
8 12
88 7 0
887 0 N1 12
6 6N1
10 2 10 2
8 84 4
86.4
86.4
C X 100 C X 100
66 745 745 10EGT40 10EGT40
82 82
64 64
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發動機指示 ENGINE INDICATIN(54)
