Service difficulty report · Floorbeam · Airbus A310

Difficulty date
March 21, 2005
Submitted
March 24, 2005
Operation
Air carrier
Aircraft
N419FE
Make and model
Airbus A310
Aircraft serial
345
Aircraft time
38,799 hours, 18,108 cycles
Part
Floorbeam
Condition
Damaged
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

FR 38 MDCC FLOORBEAM LT OF CTR AT 38 INCHES, AFTER REMOVAL OF CLS ADAPTER TO FACILITATE FRAME REPAIR, FASTENER HOLES FOUND TO BE OUT OF ROUND, FWD INBOARD HOLE ON CLS ADAPTOR AFT OUTBD, AND ALSO 2 DRILL STARTS. BLENDED OUT DRILL STARTS PER A310 SRM 51-73-10, NDT FOR CRACKS NONE FOUND PER A310 NTM 51-10-08, MEASURED DEPTH FOUND A .019 LOSS AND WITHIN LIMITS PER A310 SRM 53-10-15 FIG 101 SHEET 2, DRILLED 2 EA HOLES TO 2ND OVER 1/4 INCH HILOCKS AND ALL OTHER HOLE DRILLED TO .247 NOMENIAL 1/4" HILOCK IN CONJUCTION WITH N00681 FLOORBEAM REPAIR AND CLS ADAPTER REMOVAL AND REPLACEMENT PER A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 6A.

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