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时间:2011-04-16 09:58来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
OIL SCAVENGE OIL SCAVENGE
TUBE (LR22) TUBE (LR21)
CLAMP
INTERNAL FWD BOLT TUBE NUT
L-B2787 (0000)
H
G L-B2784 (0000)
CLAMP CLAMP
SPRAYSPRAY NUT SHIELDSHIELD LR21 TUBE
CLAMP LR05 TUBE
CLAMP
FWD
OIL SCAVENGE FWD
TUBE (LR05)
OIL SCAVENGE BOLT
TUBE (LR21) BOLT
ENGINES WITHOUT PW SB 79-75 ENGINES WITH PW SB 79-75 II
L-B2786 (0000)
Test 12 - Engines with PW SB 79-76
Figure 510B (Sheet 3)

G86324
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
BOLT  CLAMP 
NUT 
FWD 
OIL SCAVENGE 
TUBE (LR21) 

L-B2787 (0000) 
CLAMP 
OIL TUBE  OIL SCAVENGE 
(LP48)  TUBE (LR21) 
FWD  BOLT 

NUT 
FWD 

OIL TUBE (LP48)
CLAMP
OIL SCAVENGE
TUBE (LR21)

BOLT
L
L-B2788 (0000)
Test 12 - Engines with PW SB 79-76
Figure 510B (Sheet 4)

G86385
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
TEST NO. 12 - ENGINE VACUUM TEST________________________________
 (b)  Remove the clamps on the oil scavenge tube (LR22) (Fig. 510B,
 Views C, D, E and F).
 (c)  Remove the oil scavenge tube (LR22) from the oil scavenge tube
 (LR21) and the port for the internal tube on the exhaust case
 (Fig. 510B, Views B and G).
 (d)  Remove the clamps, nuts and bolts that attach the oil scavenge
 tube (LR21) (Fig. 510B, Views H, J, K and L).
 (e)  Remove the oil scavenge tube (LR21) from the oil scavenge tube
 (LR05) (Fig. 510B, View I).

 S 495-215-N00
 (10)
 Install the PWA 85843 adapter to the internal tube nut on the exhaust case at the 10 o'clock position.

 S 435-217-N00

 (11)
 Install caps on all oil supply tubes, breather tubes, and scavenge tubes.


 NOTE: During the vacuum test, all of the oil supply tubes,
____ breather tubes, and scavenge tubes must be installed unless specified.
 S 435-227-N00
 (12)
 If the integrated drive generator (IDG) or the hydraulic pump are removed, install the protection cover(s) on the gearbox pad(s).

 S 495-216-N00

 (13)
 Attach the vacuum hose and the pressure line hose from the CTE 6075 Vaccum Cart to the PWA 85843 (Tee) Adapter.

 S 795-228-N00

 (14)
 For this test, set the vacuum cart pressure at the ambient pressure (PAMB) minus 10 psi (69 kPa) or PAMB minus 20 inches (508 mm) Hg.


 NOTE: At sea level, this is 5.0 psia (34.5 kPa ABSOLUTE).
____
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TEST NO. 12 - ENGINE VACUUM TEST
________________________________
 S 795-249-N00
 (15) Find the airflow leakage rate in the No. 4 bearing compartment.
 (a)  Make sure the airflow leakage rate in the No. 4 bearing compartment is not more than a maximum of 10 pounds/hour (4.5 kg/hour).
 S 095-218-N00
 (16)
 Disconnect the vacuum cart hoses and remove the PWA 85843 Adapter from the internal tube nut.
 
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