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时间:2011-03-28 13:42来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
 1. Possible Causes_______________
RR R  - SFCC-1 (21CV) - SFCC-2 (22CV) - VALVE BLOCK-FLAP 1 (23CV) - VALVE BLOCK-FLAP 2 (24CV) - SOLENOID VALVE - valveblock filters - aircraft wiring
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R  No specific No specific  Multimeter 45Vdc Isolation Tester

 


 B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM AMM AMM AMM AMM  27-50-00-866-008 27-50-00-866-009 27-51-34-000-001 27-51-34-400-001 27-54-53-000-001 
AMM  27-54-53-000-002 
AMM AMM  27-54-53-000-003 27-54-53-400-001 
AMM  27-54-53-400-002 
AMM ASM ASM  27-54-53-400-003 27-51/0227-51/03
 3. Fault Confirmation__________________ 

R R  A. Test 

Extension of the Flaps on the GroundRetraction of the Flaps on the GroundRemoval of the SFCC (21CV,22CV)Installation of the SFCC (21CV,22CV)Removal of the Valve Blocks 23CV, 24CV of the Power Control Unit (Flap)Removal of the Solenoid Valves of the Power Control Unit (Flap)Removal of the Filters of the Valve BlocksInstallation of the Valve Blocks 23CV, 24CV of the Power Control Unit (Flap)Installation of the Solenoid Valves of the Power Control Unit (Flap)Installation of the Filters of the Valve Blocks
R (1) Make sure that the Post Flight Report does not show any hydraulic R system faults. R
 (2) Move the flaps (Ref. AMM TASK 27-50-00-866-008) (Ref. AMM TASK 27-50-00-866-009).
R (a) Examine the SFCC, FLP ON GROUND FAULTS page for a valveblock R message. R
R (b) If a valveblock message is shown, or the A/C has had this fault R before, do the fault isolation procedure.
 4. Fault Isolation
_______________
R A. Procedure
R (1) Interchange the SFCC1 and SFCC2 (Ref. AMM TASK 27-51-34-000-001) and R (Ref. AMM TASK 27-51-34-400-001).
R (2) Move the flaps, Ref. Para. 3.A. (2).
 「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 ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 202
 Nov 01/98 CES

 

R  (3) If the fault moves to the other system, replace the applicable SFCC-1 
R  (21CV) or SFCC-2 (22CV), (Ref. AMM TASK 27-51-34-000-001) and (Ref. 
R  AMM TASK 27-51-34-400-001). 
R  (4) If the fault does not move: 
R  - and the fault message includes the FIN 23CV or 24CV go to Para. (7) 
R  - and the fault message does not include the FIN 23CV or 24CV 
R  continue this procedure. 
R  (5) Do a check of the circuit resistance and circuit isolation of the 
R  extend and retract solenoid valves as follows: 
R  CAUTION: DO NOT SHORT CIRCUIT THE WIRING TO THE SOLENOID VALVES. 
R  DAMAGE TO THE SFCC CAN OCCUR. 
R  NOTE : A test is not available for the LVDT.____ 
R  (a) Get access to the electrical connector at the applicable VALVE 
R  BLOCK-FLAP 1 (23CV) or VALVE BLOCK-FLAP 2 (24CV), (Ref. AMM TASK
 27-54-53-000-001). 
R  (b) Use a Multimeter and at the connector do a check and make a note 
R  of the resistance values between: 
R  - for SFCC1/VALVE BLOCK-FLAP 1 (23CV), (EXTEND) pins T and U, 
R  (RETRACT) pins J and H (Ref. ASM 27-51/02) 
R  - For SFCC2/VALVE BLOCK-FLAP 2 (24CV), (EXTEND) pins T and U, 
R  (RETRACT) pins J and H (Ref. ASM 27-51/03). 
R  (c) The resistance values must be as follows: 
R  - for solenoid valves with Part No. 667C0000-02, between 71 Ohms 
R  and 84 Ohms. 
R  - for solenoid valves with Part No. 903A0000-01, between 53 Ohms 
R  and 60 Ohms. 
R  - for solenoid valves with Part No. 1106A0000-01 or 1111A0000-01, 
R  between 53 Ohms and 60 Ohms. 
R  (d) At the valveblock electrical connector, do a check for circuit 
R  isolation: 
R  1_  For the EXTEND solenoid connect the pins U and T together.
R  2_  For the RETRACT solenoid connect the pins J and H together.
 
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本文链接地址:A320 Trouble Shooting Manual 排故手册 飞行操纵 1(83)