Service difficulty report · Skin · Boeing 747212B

Difficulty date
June 2, 2004
Submitted
July 1, 2004
Operation
Air carrier
Aircraft
N808MC
Make and model
Boeing 747212B
Aircraft serial
21048
Engine
Ge CF650E2
Part
Skin
Condition
Cracked
Location
Nr 2 Nacelle
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

(D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE AND EXPOSED WINDOW STRAP SURFACE, ALONG WITH FASTENER HOLES, HFEC INSPECTED TO ENSURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .254. RIB INSTALLATION AT NAC STA .248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON NR 3 STIFFENER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS.

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