587 587 EGT 97 623
535
65
66 78 78 2 21 XB 81 UPGEARUP
65 12
N
17.6 17.6 FF 0.0 15 18.3
DN DN 65 65 OIL P 12 66 105 105 OIL T 103 107
F
105 OIL T 103105
L A
107
15 15 OIL Q 19 15
NN N
5
S
15 15 OIL Q 19 15
N2
P
21.2 2 1.2 VIBN20.5 21.2
N2 N N22
12 DUCT PRESS 12
1.2
1.2 VIB 0.5
1.2 CAB ALT 7500 RATE +250
TOTAL FUEL 345.0 LBS X LDG ALT 200AUTO ~P 5.6
TEMP +10c 1000
AUXILIARY EICAS DISPLAY COMPACTED EICAS DISPLAY
A AORB
Oil Quantity Indication
Figure 2
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////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
DM7351
M7351 EIU-1
T675 ENGINE OIL QUANTITY E2-6 EIU RACK
TRANSMITTER
Oil Quantity Indicating System Simplified Schematic
Figure 3
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
OIL QUANTITY INDICATING SYSTEM - ADJUSTMENT/TEST
________________________________________________
1. General
_______
A. This procedure gives the instructions to do an operational or system test of the indicating system for the engine oil quantity.
B. You can do the operational test when there is an electrical power on the airplane. The operational test is used to make sure the indicating system operates and that quantity indications with the oil tank full are correct. The operational test is used to make sure the system operates correctly after the replacement of the oil quantity transmitter.
C. When you make an analysis of the system performance at the minimum oil level, if you are not sure at this time that the precision is correct, you must drain the oil tank. It is easier to drain the oil tank when you do the system test procedure.
TASK 79-31-00-705-001-N00
2. Operational Test - Oil Quantity Indicating System (Fig. 501)
_________________________________________________
A. References
(1)
AMM 12-13-03/301, Engine - Servicing
(2)
AMM 24-22-00/201, Manual Control
78 21 81
N2
X-BLD
17.6 17.6 FF 0.0 18.3
OIL P
65 65 12 66
OIL T
105 105 103 107
15 15 OIL Q 19 15
N2
N2
N2 N2
SEE A
1.2
1.2 VIB 0.5
1.2
AUXILIARY EICAS DISPLAY A
Oil Quantity Indication Figure 501
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////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(3)
AMM 31-61-00/501, Integrated Display System
(4)
WDM 79-31-11
(5)
SSM 79-31-01
B.
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
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本文链接地址：747-400 AMM 飞机维护手册 滑油 OIL(105)
