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时间:2011-03-28 13:44来源:蓝天飞行翻译 作者:航空
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R  (2) If the fault continues: - do a check and repair the wiring of the 28VDC signal from the pressure transducer (2065GN) to the first terminal block, (Ref. ASM 27-92/28). 
R  (3) If the fault continues: - do a check and repair the wiring of the DC SIGNAL from the pressure transducer (2065GN) to the first terminal block, (Ref. ASM 27-92/28).
 B. Do the BITE test given in Para. 3.
 5. Close-up________
 A. Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).

 

 Failure of the Green Hydraulic Pressure Switch (1151GN)
 1. Possible Causes
_______________
 - PRESS SW-FLT CTL, G (1151GN)

 - wiring from the pressure switch (1151GN) pin A/B to the first terminal block


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
31-32-00-810-932 Failure of the Discrete Links
R  AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-863-001 Pressurize the Green Hydraulic System AMM 29-10-00-864-001 Depressurize the Green Hydraulic System AMM 29-32-12-000-001 Removal of the System Pressure Switch (1151GN) AMM 29-32-12-400-001 Installation of the System Pressure Switch (1151GN) ASM 27-92/27
 3. Fault Confirmation
__________________
 A. Job Set-Up
 (1) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001).
 B. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
 C. Test
 (1) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).

 4. Fault Isolation
_______________

 A. If the BITE test gives the maintenance message:
 G HYD PRESS SW1

 - do the trouble shooting procedure (Ref. TASK 31-32-00-810-932) . related to the DSI 17 discret input signal of the SEC 1, . related to the DSI 42 discret input signal of the ELAC 1 COM and ELAC 2 COM (Ref. ASM 27-92/27)
 - open and close the circuit breakers 20CE1 and 20CE2.
 (1) If the fault continues:
 - replace the PRESS SW-FLT CTL, G (1151GN), (Ref. AMM TASK 29-32-12-
000-001) and (Ref. AMM TASK 29-32-12-400-001). - open and close the circuit breakers 20CE1 and 20CE2.
 (a) If the fault continues:
 - do a check and repair the wiring from the pressure switch (1151GN) pin A/B to the first terminal block, (Ref. ASM 27-92/27).
 - open and close the circuit breakers 20CE1 and 20CE2.
 B. Do the BITE test given in Para. 3.
 5. Close-up
________
 A. Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
 「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 ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 214
 Aug 01/99R
 CES  Failure of the Green Hydraulic Pressure Switch (10CE2)


 1. Possible Causes
_______________
 - PRESS SW-G HYD, FLT CTL (10CE2)

 - wiring from the pressure switch (10CE2) pin A/B to the first terminal block


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
31-32-00-810-932 Failure of the Discrete Links AMM 27-92-17-000-001 Removal of the Flight Control Pressure Switch (10CE2) AMM 27-92-17-400-001 Installation of the Flight Control Pressure Switch
 (10CE2)
R  AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-863-001 Pressurize the Green Hydraulic System AMM 29-10-00-864-001 Depressurize the Green Hydraulic System ASM 27-92/27
 3. Fault Confirmation
__________________
 A. Job Set-Up
 (1) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001).
 B. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
 
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