Service difficulty report · Bulkhead · Beech 200BEECH

Difficulty date
December 2, 2005
Submitted
June 6, 2006
Operation
General aviation
Make and model
Beech 200BEECH
Aircraft time
9,542 hours
Engine
Pwa PT6A41
Part
Bulkhead
Condition
Cracked
Location
Fuselage
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

WHILE TROUBLESHOOTING A PRESSURIZATION SNAG ON THE AIRCRAFT UNDERGOING MAINTENANCE AT OUR FACILITY, DISCOVERED AN APPROXIMATELY 3.5 LONG CRACK IN A SECTION OF THE BULKHEAD LOWER FLANGE ATTACHED AT THE REAR SPAR AT FS 227. THE CRACK WAS CAUSING A MAJOR PRESSURIZATION LEAK THAT COULD BE FELT OUTSIDE OF THE AFT SPAR BOX ON THE EXTERIOR OF THE AIRCRAFT. NO SPECIFIC REPAIR INSTRUCTIONS ARE PROVIDED IN THE MAINTENANCE MANUAL FOR THIS DAMAGE. A CANADIAN DAR WAS CONTRACTED TO PROVIDE A REPAIR DESIGN FOR THE ABOVE AND REPAIRS WERE COMPLETED AS PER APPROVAL. UPON COMPLETION OF REPAIRS A PRESSURIZATION TEST WAS COMPLETED.