(a)  
Tighten the bolts (10) to 85-95 pound-inches (9.6-10.7 newton-meters).

 S 644-067-N00
 (28)
 Lubricate the threads of the bolts (5) with engine oil.

 S 434-044-N00

 (29)
 Attach the tube clamps (6) on the oil inlet tube (9) to the bracket with the bolts (5).

 (a)  
Tighten the bolts (5).

 S 644-068-N00
 (30)
 Lubricate the tube nuts for the servo fuel supply (20), return (24), and drain (23) tubes with the antigalling compound.

 S 434-045-N00

 (31)
 Connect the tube nuts for the servo fuel supply (20), return (24), and drain (23) tubes.

 (a)  
Tighten the tube nuts to 140-160 pound-inches (15.8-18.0 newton-meters).

 S 434-046-N00
 (32) Connect the cable connector for the valve (18) and the harness support bracket (26) to the bracket on the HPC case.
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S 644-069-N00
 (33)
 Lubricate the threads of the bolts (27) with the antigalling compound.

 S 434-070-N00

 (34)
 Attach the collar of the cable connector with the bolts (27).

 (a)  Tighten the bolts (27) to 36-40 pound-inches (4.1-4.5
 newton-meters).

 S 434-078-N00
 CAUTION: USE THE CORRECT ASSEMBLY PROCEDURE, AND TOOLS, FOR THE HARNESS
_______ CONNECTOR INSTALLATION (AMM 70-24-05/201). IF YOU USE THE INCORRECT ASSEMBLY PROCEDURE, OR TOOLS, A DAMAGED OR LOOSE CONNECTOR CAN OCCUR. A LOOSE CONNECTOR PERMITS VIBRATION, WHICH CAUSES THE CONTACTS TO WEAR AND DECREASES THE LIGHTNING PROTECTION.
 (35)
 Connect the EEC electrical connector (25) to the cable connector (AMM 70-24-05/201).

 S 414-048-N00

 (36)
 Install the fan exit liner at the No. 6 position (AMM 72-34-03/401).

 S 614-049-N00

 (37)
 Do the servicing procedure for the engine oil system (AMM 12-13-03/301).

 S 414-083-N00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (38) Close the left thrust reverser (AMM 78-31-00/201).
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////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 414-084-N00
 (39)
 Close the left core cowl panel (AMM 71-11-06/201).

 S 414-085-N00

 (40)
 Close the left fan cowl panel (AMM 71-11-04/201).

 S 444-086-N00

 (41)
 Do the activation procedure for the thrust reversers (AMM 78-31-00/201).

 S 864-051-N00

 (42)
 For the applicable engine, remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6 Main Power Distribution Panel
 1) 6G1 FUEL SHUTOFF VALVE ENG 1
 2) 6G2 FUEL SHUTOFF VALVE ENG 2
 3) 6G3 FUEL SHUTOFF VALVE ENG 3
 4) 6G4 FUEL SHUTOFF VALVE ENG 4

 5) 6G15 SCU ALT PWR ENG 1
 6) 6G23 ENG SCU 1
 7) 6G16 SCU ALT PWR ENG 2
 8) 6G24 ENG SCU 2
 9) 6G17 SCU ALT PWR ENG 3
 10) 6G25 ENG SCU 3
 11) 6G18 SCU ALT PWR ENG 4
 12) 6G26 ENG SCU 4

 S 864-052-N00
 (43)
 Remove the DO-NOT-OPERATE tag from the FUEL CONTROL switch.

 S 794-053-N00

 (44)
 Do the Test No. 3 - Ground Test - Idle Power and the Test No. 6 -Electonic Engine Control (EEC) Idle Test (AMM 71-00-00/501).

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