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时间:2011-04-11 09:17来源:蓝天飞行翻译 作者:航空
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Flow No. 5  _________________  Flow No. 12 
Flow No. 6  _________________  Flow No. 13 
Flow No. 7  _________________  Flow No. 14 

Maximum 
_____________________________________________Determine Individual Component Leakage Values:  Actual  Recommended 
Flow___________  Flow_____________ 
Flow No. 3, Elevator Feel Computer Null Leakage  0.13 GPM 
Flow No. 3A, Stabilizer Pitch Trim Null Leakage 
(No. 2 ) -(No. 3 )____________  = 3A ______  0.53 GPM 
Flow No. 4A, Right INBD Elevator and Upper Rudder 
Control Package Null Leakage 
(No. 1 ) -(No. 4 )____________  = 4A ______ 
Flow No. 5A, Right INBD Elevator Control 
Package Null Leakage 
(No. 1 ) -(No. 5 )____________  = 5A ______  1.06 GPM 
Flow No. 5B, Upper Rudder Control Package 
Null Leakage 
(No. 4A ) -(No. 5A )____________  = 5B ______  1.06 GPM 
Flow No. 6A, Null Leakage of Right Central 
Lateral Control Package, Left INBD Aileron 
Power Package, Right OUTBD Aileron Power 
Package, and Internal Leakage Other Than 
Valve Null Leakage in Spoilers 1,4,9,12 
(No. 6 )(No. 1 ) -____________  = 6A ______ 

Airplane No.________
Hours ________

Hydraulic System No. 3 Leakage Test Data and Analysis Sheet
Figure 605 (Sheet 1)

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 29-11-00
 ALL  ú ú 01 Page 659 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

Airplane No.________
Hours ________

Maximum 
Determine Individual Component Leakage Values:_____________________________________________  Actual  Recommended 
___________Flow  _____________Flow 
Flow No. 8A, Left INBD Aileron Power Package 
Null Leakage 
(No. 7 ) -(No. 8 )______ ______  = 8A ______  0.66 GPM 
Flow No. 9A, Left INBD and Right OUTBD Aileron 
Power Package Null Leakage 
(No. 9 )(No. 7 ) -______ ______  = 9A ______ 
Flow No. 9B, Right OUTBD Aileron Power Package 
Null Leakage 
(No. 9A ) -(No. 8A ____________  = 9B ______  0.66 GPM 
Flow No. 11A, Spoiler Package 1 and 4 Internal 
Leakage 
(No. 10 ) -(No. 11 )____________  = 11A______  0.8 each GPM 
Flow No. 12A, Spoiler Package 9 and 12 
Internal Leakage 
(No. 12 )(No. 7 ) -______ ______  = 12A______  0.8 each GPM 
Flow No. 14A, Left Central Lateral Control 
Package Null Leakage 
(No. 13 ) -(No. 14 )____________  = 14A______  0.53 GPM 

Hydraulic System No. 3 Leakage Test Data and Analysis Sheet
Figure 605 (Sheet 2)

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 ALL  ú ú 01 Page 660 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

GROUND
SERVICE
DISCONNECT


PRV - PRESSURE RELIEF VALVE
Hydraulic System 3 Schematic
Figure 606

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 10 Page 661 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 TASK 29-11-00-706-217
 9.  Hydraulic System No. 4 - Full Internal Leakage Check____________________________________________________
 A. Special Tools and Equipment
 (1)  
4MIT65B80307-1 - Protractor

 (2)  
3MIT65B80307-1 - Control Wheel Adapter

 B.
Standard Tools and Equipment

 (1)  
410DME-10AR Flowmeter (commercially available)
 
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