APU CURRENT TRANSFORMER, T1503
APU CURRENT SEE D
TRANSFORMER, T1504 FWD
FWD SEE D
11. NUT
(3 LOCATIONS) LEFT STATION 2160 BULKHEAD RIGHT STATION 2160 BULKHEAD
C
B
10. SCREW BRACKET(3 LOCATIONS)
9.  NUT
1.  ELECTRICAL(2 LOCATIONS)
CONNECTOR,
DT1503 (LEFT SIDE),

8.  CLAMP DT1504 (RIGHT SIDE)
(2 LOCATIONS)
2.  APU CURRENT TRANSFORMER,
T1503 (LEFT SIDE), (2 LOCATIONS)
7.  WASHER T1504 (RIGHT SIDE)
6.  SCREW (2 LOCATIONS)
3. COVER GENERATOR CABLELANYARD FWD
5.  WASHER (2 LOCATIONS)
D
4.  SCREW (2 LOCATIONS)
APU Current Transformer Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 49-61-11
 ALL  ú ú 01 Page 403 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 C. Access
 (1)  
Location Zones
 151 Area Aft of Bulk Cargo Compartment - Left
 152 Area Aft of Bulk Cargo Compartment - Right
 221 Control Cabin - Left
 222 Control Cabin - Right

 (2)  
Access Panels
 146AZ Access Station 2160 Bulkhead Door
 823R Bulk Cargo Compartment Door

 D.
Procedure

 S 424-039
 CAUTION: REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY.
_______ IF YOU DO NOT REMOVE THE PROTECTION COVERS, DAMAGE TO THE APU CAN OCCUR.
 (1)  
Do these steps to install the APU current transformer (2):

 (a)  
Install the APU current transformer (2) on the bracket with the three screws (10) and three nuts (11).

 (b)  
Put the generator cable in the APU current transformer (2).

 (c)  
Install the two clamps (8) on the generator cable with the two screws (6), two washers (7) and two nuts (9).

 (d)  
Install the cover (3) and lanyard with the two washers (5) and two screws (4).

 (e)  
Do the electrical bonding test between the APU current transformer (2) and the airplane structure (AMM 20-22-01/601). 1) The maximum bonding resistance between the APU current

 transformer (2) and airplane structure is 0.0025 ohm.

 (f)  
Connect the electrical connector (1) to the APU current transformer (2).

 E.
Put the Airplane Back to Its Usual Condition

 (1)  
Close the access station 2160 bulkhead door, 146AZ.

 (2)  
Close the bulk cargo compartment door, 823R.

 S 864-018

 (3)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6-2 Main Power Distribution Panel
 1) 6K18, APU ALTN CONT

 S 414-017
 S 414-038
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 49-61-11
 ALL  ú ú 02 Page 404 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  P83 Aft APU Equipment Control and Circuit Breaker Panel 1) APU PRIME CONT
 S 864-019
 (4)  Remove the DO-NOT-OPERATE tag from the APU control switch on the P5 overhead panel.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 49-61-11
 ALL  ú ú 02 Page 405 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 APU EICAS INDICATING SYSTEM - DESCRIPTION AND OPERATION
_______________________________________________________
 1.  General_______
 A.  The EICAS memo message APU RUNNING (white) will show on the main EICAS display when the APU N1 speed is 95% or more than 95%. Other APU indications can be displayed by selecting either the EICAS status page or maintenance page.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 機載輔助動力 2(132)