Service difficulty report · Sill · Airbus A310

Difficulty date
March 26, 2009
Submitted
March 26, 2009
Operation
Air carrier
Aircraft
N813FD
Make and model
Airbus A310
Aircraft serial
500
Aircraft time
43,113 hours, 18,640 cycles
Part
Sill
Condition
Corroded
Location
Fuselage
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

MAIN DECK, R-2 DOOR SILL AREA HAS A STRINGER ANGLE CORRODED AT FRAME 74, BS 3998 THRU 4005; STRINGER 26R. REMOVED CORROSION IN REF TO SRM 51-74-40. ORIGINAL MATERIAL THICKNESS 0.118 IAW DWG A539800712. MATERIAL REMOVED 0.026. MATERIAL REMANING 0.092 AND FOUND TO BE WITHIN LIMITS IAW DWG A537800712 AND SRM 53-10-00 FIG 104. ALODINED IN REF TO SRM 561-21-10. PRIMED & TOP COATED IAW SRM 51-23-10. REAPPLIED CIC IAW AMM 51-22-00-0; FIG 001.

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