Service difficulty report · Panel · Doug DC871F

Difficulty date
February 24, 2005
Submitted
December 9, 2005
Operation
Air carrier
Aircraft
N821BX
Make and model
Doug DC871F
Aircraft serial
45811
Aircraft time
85,895 hours, 36,255 cycles
Part
Panel
Condition
Cracked
Location
Ws 74.869
Part time
85,895 hours, 36,255 cycles
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

DURING A ROUTINE C-CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AT STA XRS 74.869, S-2. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER + FILLER PLUG. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW SEMAN DRAWING ED-3831 AND FAA FORM 8110-3 05020, DC8 SRM 51-1-11, 51-1-20D, 51-1-22, 51-1-26, 51-3-1, 51-3-2.

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