SDR AU010065

Service difficulty report · Fitting · Airbus A320211

Difficulty date
January 23, 2001
Submitted
March 20, 2001
Operation
General aviation
Make and model
Airbus A320211
Engine
Cfmint CFM565A1
Part
Fitting
Condition
Cracked
Location
Mlg
Stage of operation
IN
How discovered
E
Nature of condition
O
Precautionary procedure
K

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

What was found

(AUS) RT MAIN LANDING GEAR DOOR ACTUATOR FITTING AND CONNECTING STRIP CRACKED IN TWO PLACES. CRACK LENGTHS 20MM (0.78IN) IN FORWARD FLANGE AND 28MM (1.102IN) IN AFT FLANGE. CONNECTION STRAP CRACKED FROM FASTENER HOLE. CRACK LENGTH 5MM (0.196IN). FOUND DURING NDI INSPECTION IAW SB A320-53A1135 AND AN ENGINEERING RELEASE A32-53-40-9B.

More about the Airbus A320-211