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时间:2011-03-28 18:28来源:蓝天飞行翻译 作者:航空
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 4. Fault Isolation
_______________
 A. Procedure
 CAUTION Do not close the tripped C/B until a check for a short circuit in the aircraft wiring has been done. Damage to the aircraft systems can occur.
 (1) Do a check and repair as neccessary the aircraft wiring (Ref. ASM 30-11/01) between:
 - the circuit breaker (2DL) and the P/BSW (3DL)

 - the P/BSW (3DL) and the relay (5DL)

 - the relay (9DL) and the valves (9DL) and (10DL)

 - the valve (9DL) and the valve (10DL)

 - the relay (5DL) and the relay (6DL)

 - the relay (6DL) and the relay (7DL).


 NOTE : More information about the relays can be found in the Task
____ Supporting Data (Ref. TSM 30-11-00 P.Block 301).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-11-00∞∞∞∞∞∞∞∞∞∞Page 215
 Aug 01/05R CES


 (a) Make sure that the circuit breaker (2DL) is closed (Ref. ASM 30-11/01).

 (b) Do the test in Para. 3.A.


 - if the fault continues, do the next step.
 (2) Do a check of the C/B ANTI ICE/WING/CTL (2DL).

 (a) If the check is unsatisfactory, replace the circuit breaker (2DL).

 (b) Do the fault confirmation in Para. 3.A.


 - if the fault continues, do the next step.

 (3) Do a check of the Diode 1160VD.

 (a) If the check is unsatisfactory, replace the diode.

 (b) Do the fault confirmation in Para. 3.A.

 

 


 WING ICE PROTECTION - TASK SUPPORTING DATA
__________________________________________
R 1. Table of Relay Sets.
____________________
 A. The relay configurations that follow are valid for their aplicable
 diagram. R FIGURE 301 - Wing Anti-ice Not Selected In Air R (A/C Power On, P/BSW 3DL Not Operated, No Faults)
R If a fault occurs: any discrepency of 5DL,6DL,9DL,10DL. or if a wiring fault removes the 28VDC from the coil of TDL. TDL de-energizes, to cause 4LP/11LP to energize. FAULT lamp comes on.
R FIGURE 302 - Wing Anti-ice Selected In Air R (A/C Power On, P/BSW 3DL Operated, No Faults) R
If a fault occurs:
Any discrepency of 6DL,9DL,10DL, or a
 wiring fault ,will remove the 28VDC
from the coil of 7DL.
TDL de-energizes to cause 4LP/11LP
to energize. FAULT lamp comes on.

FIN STATE
1DL Closed
2DL Closed
3DL Open
4DL De-energized
5DL De-energized
6DL De-energized
 7DL Energized
 9DL De-energized

 valve closed 10DL De-energized valve closed 4LP De-energized
 FAULT lamp off 11LP De-energized FAULT lamp off
FIN STATE
1DL Closed

3DL Closed
4DL Energized

after 30 secs5DL Energized 6DL Energized 7DL Energized 9DL Energized
 valve open 10DL Energized valve open 4LP De-energized FAULT lamp Off 11LP De-energized FAULT lamp off


R  FIGURE 303 - Wing Anti-ice Test Selected On Ground 
R  (30 Seconds Delay Not Expired, P/BSW 3DL Operated) 
R  FIN  STATE
 If a fault occurs: 1DL  Closed
 Any discrepency of 6DL, 9DL,10DL,or a 2DL  Closed
 wiring fault removes 28VDC from the coil 3DL  Closed
 of 7DL. 7DL de-energizes,to cause 4LP/ 4DL  De-energized
 11LP to energize. FAULT lamp comes on. 5DL  Energized
 6DL  Energized
 7DL  Energized
 9DL  Energized
 valve open
 10DL  Energized
 valve open
 4LP  De-energized
 FAULT lamp on
 11LP  De-energized
 FAULT lamp on 
R  FIGURE 304 - Wing Anti-ice Test Selected On Ground 
R  (30 Seconds Delay Expired, P/BSW 3DL Not Released) 
R  FIN  STATE
 If a fault occurs: 1DL  Closed
 Any discrepency of 5DL,6DL,9DL,10DL, 2DL  Closed
 or a wiring fault, removes 28VDC from 3DL  Closed
 the coil of 7DL. 7DL de-energizes to 4DL  Energized
 cause 4LP/11LP to energize. 5DL  De-energized
 FAULT lamp comes on. 6DL  De-energized
 7DL  Energized
 9DL  De-energized
 valves closed
 10DL  De-energized
 valves closed
 4LP  De-energized
 FAULT lamp off
 11LP  De-energized
 FAULT lamp off

 

 Wing Anti-ice Not Selected In Air (A/C Power On, P/BSW 3DL Not Operated, No
 Faults)
 
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