Service difficulty report · Skin · Beech 1900D

Difficulty date
September 24, 2008
Submitted
October 7, 2008
Operation
Air carrier
Aircraft
N100UX
Make and model
Beech 1900D
Aircraft serial
UE100
Part
Skin
Condition
Cracked
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

MAJOR REPAIR CONFORMITY CHECK OF REPAIR ABOVE AIRSTAIR DOOR PERFORMED. MX FOUND STOP DRILLED CRACKS AROUND 2 RIVETS BOTH 1.25 FROM LT AND RT CENTERLINE OF STRINGER 1 AT 163.975. MX REMOVED OLD PATCH, REMOVED DAMAGED AREAS BY CUTTING OUT .75" SKIN IN BOTH AREAS. MX INSTALLED SHIM MADE FROM ORIGINAL SKIN MATERIAL, THEN INSTALLED COVER PATCH IAW BEECH 1900 SRM 51-70-06. COVER PATCH MADE FROM NEW FACTORY SKIN MATERIAL 6.2" BY 4.1". RII INSPECTION COMPLIED WITH AT STATION 163.975 PER TASKCARD 8.2.1 MX PERFORMED A PRESSURIZATION CHECK THAT WAS REQUIRED FOR MAJOR REPAIR OF FUSELAGE SKIN IN AW BMM 21-30. ALL CHECKS FOUND TO BE WITHIN LIMITS.

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