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时间:2011-04-10 09:48来源:蓝天飞行翻译 作者:航空
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 TASK 26-19-01-004-001
 2.  Remove the Thermal Switch (Fig. 401)____________________________________
 A.  References
 (1)
AMM 51-31-01/201, Seals and Sealing

 (2)
AIPC 26-14-10, Fig. 1

 (3)
AIPC 26-19-00, Fig. 1

 (4)
WDM 49-52-21

 (5)
SSM 49-52-02


 B.  Access
 (1)  
Location Zone
 137 Body Landing Gear Well L.H.
 142 Aft Cargo Container Compartment, LH
 145 Bulk Cargo Compartment, LH
 311 Area Aft of Pressure Bulkhead, LH
 313 Stabilizer Torsion Box Compartment, LH


 (2)  
Access Panel 193J Keel Beam Access Panel 312AR Horizontal Stabilizer Jackscrew Access Door 731 Door - Wing Landing Gear - Center Section Inboard Left 751 Door - Body Landing Gear - Aft Inboard Left 752 Door - Body Landing Gear - Aft Outboard Left


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-19-01
 ALL  ú ú 04 Page 401 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

ASEE AFT LOWER CARGO COMPARTMENT 
BSEE COMPARTMENT BULK CARGO 
APU BLEED AIR DUCT  SEE  C 
FWD  THERMAL SWITCH 
SIDEWALL (TYP) LINING PANEL VERTICAL LINING PANEL (TYP) SLOPING SIDEWALL  DOORWAY CARGO (REF) 

BULKHEAD LINING PANEL  2160 STA  PANEL (TYP) ENCLOSURE LINING VACUUM WASTE TANK 
1920 STA 
FWD DOORWAY (REF) BULK CARGO  B  OPENING 312A ACCESS VERTICAL SIDEWALL LINING PANEL (TYP) SLOPING SIDEWALL LINING PANEL FLOOR (REF) BULK COMPARTMENT (TYP)  C  FWD 
Figure 401 (Sheet 1) Thermal Switch Installation 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-19-01
 ALL  ú ú 01 Page 402 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 

STA 1248
STA 1480
-APU DUCT APUTHERMAL SWITCH


Thermal Switch Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-19-01
 ALL  ú ú 05 Page 403 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 C. Procedure
 S 864-002
 (1)  
Open the circuit breaker, APU DUCT OVERHEAT, on the P83 panel and attach a DO-NOT-CLOSE tag.

 S 014-003

 (2)  
For thermal switches S969 thru S983 installed in the aft cargo compartment, remove the left vertical side wall panel in the aft and bulk cargo compartment. Thermal switches S978 and S983 are more easily accessible from the main deck. Remove the main deck floor panels directly above them for accesss.


 NOTE: The thermal switches are installed on the airplane frame
____
 along the APU air duct.

 S 014-004
 (3)  For thermal switches S1173, S1924, S984, S985, and S986 installed in the aft of the bulk cargo compartment, get access to the thermal switches through the access door, 312A, installed in the area aft of the pressure bulkhead.
 NOTE: The thermal switches are installed on the airplane frame
____
 along the APU air duct.

 S 014-035
 (4)  ALL AIRPLANES; Remove the applicable access panels in the main wheel well for the seven thermal switches.
 ~....................................
 | THERMAL SWITCH | ACCESS PANEL |
 ......................................
 | S2207 | None |
 ......................................
 | S2208 | 193J |
 ......................................
 | S2209 | 731 |
 ......................................
 | S2210 | 751 |
 ......................................
 | S2211 | 751 |
 
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