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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
INTERMEDIATE
1. 2.5 BLEED CASE
VALVE ACTUATOR
SEE A
FAN EXIT SEE B LINER SEGMENT
INTERMEDIATE
CASE ROD END

FWD
CLEVIS
A
1
NUT (3 LOCATIONS) FLANGE E BRACKET
BRACKET
1.  2.5 BLEED VALVE
ACTUATOR

PISTON SHAFT
BOLT
(3 LOCATIONS)
NUT
BOLT

2. SHOULDER BOLT (LEFT-HAND THREAD)
14.  WASHER (4 LOCATIONS)
13.  BOLT (4 LOCATIONS)
5.  PACKING 3. COTTER PIN
6.  PACKING
12.  UNION
7. ADAPTER
4.  EEC ELECTRICAL CONNECTOR
8.  ADAPTER
11.  
DRAIN TUBE

9.  SERVO FUEL
10.  
SERVO FUEL SUPPLY TUBE
RETURN TUBE

B
1
ENGINES WITHOUT PW SB 75-126
2.5 Bleed Valve Actuator Installation Figure 401
A76387
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(b)  Make sure the applicable FUEL SPAR VLV 1, 2, 3, or 4 status message does not show.
___
 S 864-005-N00
 (4)  For the applicable engine, open these circuit breakers and install the DO-NOT-CLOSE tags:
 (a)  P6 Main Power Distribution Panel
 1) 6G1 FUEL SHUTOFF VALVE ENG 1
 2) 6G15 SCU ALT PWR ENG 1
 3) 6G23 ENG SCU 1
 4) 6G2 FUEL SHUTOFF VALVE ENG 2
 5) 6G16 SCU ALT PWR ENG 2
 6) 6G24 ENG SCU 2
 7) 6G3 FUEL SHUTOFF VALVE ENG 3
 8) 6G17 SCU ALT PWR ENG 3
 9) 6G25 ENG SCU 3
 10) 6G4 FUEL SHUTOFF VALVE ENG 4
 11) 6G18 SCU ALT PWR ENG 4
 12) 6G26 ENG SCU 4

 S 014-029-N00
 (5)  Open the left fan cowl panel (AMM 71-11-04/201).
 S 044-038-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.
 (6)  
Do this procedure: Thrust Reverser Deactivation for Ground Maintenance (AMM 78-31-00/201).

 S 014-030-N00

 (7)  
Open the left core cowl panel (AMM 71-11-06/201).

 S 014-039-N00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (8)  Open the left thrust reverser (AMM 78-31-00/201).
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 ALL  ú ú N03 Page 403 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
E.  Procedure
 S 024-047-N00
 (1)  
Remove the actuator for the 2.5 bleed valve:

 (a)  
Remove the No. 5 segment of the fan exit liner (AMM 72-34-03/401).

 (b)  
Disconnect the EEC electrical connector (4) from the receptacle on the actuator (1). 1) Install protection caps to the EEC electrical connector (4)

 and the receptacle on the actuator (1).

 (c)  
Put a container below the actuator (1) to catch the remaining fuel.

 NOTE: Approximately 1/2 pint (1/4 liter) of fuel will drain
____
 from the actuator.

 (d)  
Disconnect the coupling nut of the drain tube (11) from the union (12).

 (e)  
Disconnect the coupling nuts of the servo fuel supply tube (9) and the servo fuel return tube (10) from the adapters (7, 8) on the actuator (1).

 (f)  
Remove the support bracket for the actuator with the steps that follow: 1) ENGINES PRE-PW-SB 75-126;

 Remove the three bolts and nuts which attach the support bracket to the bracket on the flange E.
　
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