Service difficulty report · Bolt · Boeing 747200

Difficulty date
July 9, 2004
Submitted
August 4, 2004
Operation
Air carrier
Aircraft
N522UP
Make and model
Boeing 747200
Aircraft serial
21936
Aircraft time
68,765 hours, 16,239 cycles
System (JASC)
1430 · Fasteners
Part
Bolt
Condition
Corroded
Location
Lt Wing
Stage of operation
IN
How discovered
9
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

INSPECTION TYPE:C, LT WING CENTER SECTION REAR SPAR WEB AT BS 1241 BULKHEAD FITTING CORROSION REVEALED BETWEEN BOLT NR 7, 8 AND 9. THICKNESS CHECK PER NTM PART 4,57-10-19 RESULT: NR 7 HOLE 0.335 INCH, NR 8 HOLE 0.350 INCH, NR 9 HOLE 0.370 INCH. NR 7, 8 & 9 FASTENER HOLES REAMED TO 0.375 INCH DIA PER UPS EO B747-5710-11129 FIG 6. FASTENER HOLES AREA CORROSION REMOVED AS PER SRM 21-10-01 & REPROTECTED AS PER SRM 51-12-02.

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