Service difficulty report · Support · Doug MD88

Difficulty date
September 18, 2016
Submitted
November 7, 2016
Operation
Air carrier
Aircraft
N907DE
Make and model
Doug MD88
Aircraft serial
53416
Aircraft time
62,721 hours, 45,586 cycles
Part
Support
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

CORROSION ON CEILING SUPPORT ON STA Y= 1231 BTW X=17 LT TO X= 34 LT, STA Y= 1309 BTW X=35 LT TO 35 RT, BTW STA Y= 1231 TO 1309 X= 17 LT, BTW STA Y=1250 TO 1309 X=0 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED PER SRM 51-10-3 PAR 26 AND SUPPORTS WERE REPLACED PER SRM 53-24-0D FIG 11. MEASURE UT WAS ACCOMPLISHED PER NDTSPM 04-00-07 PAR 5, FIG 3 SHEET 1 AND 2. ORIGINAL THICKNESS ON STA Y= 1231 BTW X=17 LT TO X= 34 LT IS 0.040" AND REMAINING IS 0.038". ORIGINAL THICKNESS ON STA Y= 1309 BTW X=35 LT TO X=-25 RT IS .040" AND REMAINING IS .039", ORIGINAL THICKNESS ON STA Y= 1231 TO 1250 X=17LH .032" AND REMAINING IS .030" AND ORIGINAL THICKNESS ON STA Y=1250 TO 1309 X=0 ORIGINAL THICKNESS IS .063" AND REMAINING IS .062" THEREFORE IS WITHIN LIMITS, AREAS OUT OF LIMITS ON STA Y= 1309 BTW X=-25 X=-35 ORIGINAL THICKNESS IS .040" AND REMAINING IS .020", Y=1250 TO Y=1309 ORIGINAL THICKNESS IS .032" AND REMAINING IS .018" THEREFORE ITS OUT LIMITS PER ER/A 511165-14MA REV C AND SRM 53-01 FIG 1 SHEET 3.

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