Service difficulty report · Skin · Airbus A310324

Difficulty date
November 16, 2010
Submitted
November 17, 2010
Operation
Air carrier
Aircraft
N812FD
Make and model
Airbus A310324
Aircraft serial
467
Aircraft time
52,428 hours, 11,629 cycles
Engine
Pwa PW4152
Part
Skin
Condition
Corroded
Location
Zone 100
Stage of operation
IN
How discovered
V
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

FUSELAGE SKIN EXTERIOR SURFACE FOUND CORROSION UNDER BULK CARGO DOOR SCUFF PLATE (FWD LWR CORNER). REMOVE THE CORROSION IAW SRM 51-74-10. APPLY ALODINE IAW SRM 51-21-10. MEASURE REMAIN THICKNESS OF THE REWORKED AREA IAW NTM51-10-04 (REMAINING THICKNESS WAS 0.148 INCH). DO AN HFEC INSP OF THE REWORKED AREA IAW NTM51-10-08 (NO CRACK FOUND) THE ORIGINAL THICKNESS IS 0.158 INCH, SO THE REMAINING THICKNESS IT IS WITHIN THE LIMIT PER SRM53-17-12/FIG104 6.RESTORE FINISH TOTHE REWORKED AREA IAW SRM51-75-10 7.THE ALLOWABLE REWORK MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI53-17-12-1- 002-00

More about the Airbus A310-324