Service difficulty report · Wire · Airbus A320211

Difficulty date
February 13, 2011
Submitted
March 15, 2011
Operation
Air carrier
Make and model
Airbus A320211
Aircraft time
52,284 hours, 8,375 cycles
Engine
Cfmint CFM565A1
Part
Wire
Condition
Shorted
Location
Te Flaps
Stage of operation
CL
How discovered
O
Nature of condition
F
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

AFTER T/O FLAPS FAILED TO RETRACT TO "0" MOC AND DISPATCH CONTACTED QRH PROCEDURE C/O RETURED TO BASE WITH SLATS AT 2, FLAPS" 0" +1 AMBER WIRE NR 2751-5906R BETWEEN CONN. 7540VC & 7504VCA, WIRE NR 2751-5910R BETWEEN CONN 7542VC & 7502VCA FOUND SHORTED TO GRD. BOTH WIRE PAIRS AND CNN. 7504VCA REPLACED IAW ESPM 20-33-11(AWM 27-51-11, 27-51-12). CK SERV IAW AMM 27-54-00-710 ADDITIONAL T/S DETAILS: REMOVE RT FLAP LOWER KINK SEAL. WIRING CHECK CARRIED OUT FOUND: RT SYS 1 FLAP ATTACHMENT SENSOR 38CV WIRE 2751-5906R SHORTED CIRCUIT TO GROUND BETWEEN 7540VC AND 7504 VCA. 2 R SYS 2 FLAP ATTACHMENT SENSOR 40CV WIRE 2751-5910R SHORTED CIRCUIT TO GROUND BETWEEN 7542VC AND 7502VCA. CONNECTORS 7504VC AND 7504VCA CORRODED. REINSTALLED RT FLAP LOWER KINK SEAL. BOTH WIRES (2X TEISTED PAIRS) BETWEEN 7540VC & 7504VCA AND 7542VC & 7502VCA REPLACED WITH CONNECTOR 7504VCA. CONN. 7504VC CLEANED AND INSPECTED OK.

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