Service difficulty report · Door Frame · Boeing 717200

Difficulty date
August 23, 2016
Submitted
August 25, 2016
Operation
Air carrier
Aircraft
N906AT
Make and model
Boeing 717200
Aircraft serial
55087
Aircraft time
40,249 hours, 28,112 cycles
Part
Door Frame
Condition
Cracked
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

AFT CARGO INTERNAL FUSELAGE CUT OUT, LOWER DOOR JAMB PAN HAS NUMEROUS AREAS OF CORROSION THAT IS AROUND THE AFT CAM LATCH FITTING AND LOWER AFT STOP ASSY TO THE FWD LOWER AFT STOP AND FWD CAM LATCH FITTINGS INCLUDING SPLICES. AROUND BARREL NUTS, AND THE 2 LOWER ANGLES, AFT ANGLE IS BENT AND CRACKED. AFT CARGO DOOR JAMB PAN WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. ORIGINAL T=.050" REMAINING T=.000". THE OUT OF LIMITS PAN WAS REPLACED FROM THE AFT CARGO DOOR CUTOUT IAW SRM 53-20-15, REPAIR 7, THE SPLICE, 1 EA THAT WAS FOUND CORRODED SHOWED 100 PERCENT MATERIAL LOSS. THE NEW FWD DOOR JAMB SPLICE WAS FABRICATED IAW DWG J060228. IT WAS THEN ALODINED, PRIMED, AND PAINTED IAW AMM 51-10-00-370-803. THE NEW SPLICE WAS INSTALLED IAW SRM 51-41-02 & 51-41-05, ALSO ORNRC 70486-0100-0218 AND 70486-0100-0201.

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