Service difficulty report · Frame · Boeing 7474R7F

Difficulty date
July 8, 2010
Submitted
August 16, 2010
Operation
Air carrier
Aircraft
N581UP
Make and model
Boeing 7474R7F
Aircraft serial
25866
Aircraft time
82,754 hours, 14,396 cycles
Engine
Ge CF680C2B1F
Part
Frame
Condition
Cracked
Location
Bs 2598 Bulkhead
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

INSPECTION TYPE:C EMP- TAIL COMPT STA 2598 LT BHD INNER CHORD CRACK AT LWR TORSION BOX AREA AS MARKED. (CHORD CRACK LENGTH 0.915"), ( WEB CRACK LENGTH 0.030" ) CHORD & WEB REPAIRED IAW HX RS R53-80-36775, REV A AND EO 747- 5310-38966-A, ORG MAT'L:BAC1505-100859, 7075T6(INNER CHORD), CLAD 7075T6-0.050" BONDED WEB ASSY CHORD CUTOUT SIZE: 0.99" X 0.863", WEB FINAL HOLE SIZE: 0.309", THIS IS CLASSIFIED AS A MAJOR REPAIR THE REPAIR TIME LIMITED TO 17396 FLT CYC PENDING A (DTA).

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