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时间:2011-04-17 09:17来源:蓝天飞行翻译 作者:航空
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 445 Left Thrust Reverser Half - Engine 4


 C.
Preconditions


 S 865-073-N00
 (1)  
These conditions are necessary for this task:

 (a)  
Electric power on (AMM 24-22-00/201).

 (b)  
Oil tank must be full (AMM 12-13-03/301).

 (c)  
Engine Indicating and Crew Alert System (EICAS), serviceable (AMM 31-61-00/201).

 D.
Do a Test of the Indicating System for the Oil Quantity


 S 615-002-N00
 (1)  
Do the servicing procedure for the engine oil tank
 (Ref 12-13-03/301).


 S 865-003-N00

 (2)  
Supply electrical power (Ref 24-22-00/201).

 S 865-004-N00

 (3)  
Make sure these circuit breakers that follow are closed:

 (a)  
P7 Overhead Circuit Breaker Panel
 1) 7F9 EIU L
 2) 7F10 EIU C
 3) 7F15 EIU R


 (4)  
Look at the oil quantity indication on the auxiliary EICAS display.


 S 215-063-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-31-00
 ALL  ú ú N01 Page 502 ú Jun 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 215-082-N00
 (5)
Make sure the oil quantity indication shows 22 |3 liters.

 S 865-006-N00

 (6)  
Remove electrical power if it is not necessary (Ref 24-22-00/201).


 TASK 79-31-00-705-007-N00
 3. System Test - Oil Quantity Indicating System (Fig. 501)
____________________________________________
 A. References
 (1)  
12-13-03/301, Engine - Servicing

 (2)  
12-22-03/301, Engine - Servicing

 (3)  
24-22-00/201, Manual Control

 (4)  
AMM 31-61-00/501, Integrated Display System

 (5)  
71-11-04/201, Fan Cowl Panels

 (6)  
71-11-06/201, Core Cowl Panels

 (7)  
78-31-00/201, Thrust Reverser System

 B.
Standard Tools and Equipment

 (1)  
Beaker - Calibrated, 1 U.S. quart (1 liter)
 size minimum, used to catch the oil


 C.
Consumable Materials

 (1)  
D00390 Oil - Engine

 D.
Access

 (1)  
Location Zone 221 Control Cabin, LH 222 Control Cabin, RH 412 Engine 1 - Main Gearbox Aft Face 8 o'clock 422 Engine 2 - Main Gearbox Aft Face 8 o'clock 432 Engine 3 - Main Gearbox Aft Face 8 o'clock 442 Engine 4 - Main Gearbox Aft Face 8 o'clock

 (2)  
Access Panel
 415 Left Thrust Reverser Half - Engine 1
 425 Left Thrust Reverser Half - Engine 2
 435 Left Thrust Reverser Half - Engine 3
 445 Left Thrust Reverser Half - Engine 4

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-31-00
 ALL  ú ú N03 Page 503 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
E. Preconditions
 S 865-074-N00
 (1)  
These conditions are necessary for this task:

 (a)  
Electric power on (AMM 24-22-00/201).

 (b)  
Oil tank must be empty (AMM 12-22-03/301).

 (c)  
Engine Indicating and Crew Alert System (EICAS), serviceable (AMM 31-61-00/201).

 F.
Prepare for the Test


 S 015-022-N00
 (1)  Open the left fan cowl panel (Ref 71-11-04/201).
 S 045-037-N00
 WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______
 OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF
 THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO
 EQUIPMENT.

 (2)  
Do this procedure: Thrust Reverser Deactivation for Ground
 Maintenance (Ref 78-31-00/201).


 S 015-023-N00

 (3)  
Open the left core cowl panel (Ref 71-11-06/201).


 
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