Service difficulty report · Frame · Beech 1900D

Difficulty date
November 18, 2014
Submitted
March 12, 2015
Operation
General aviation
Make and model
Beech 1900D
Aircraft time
39,448 hours
Engine
Pwa PT6A67D
Part
Frame
Condition
Cracked
Location
Bs 288
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

(CAN) DURING ABC STRUCTURAL INSPECTION MAINTENANCE NOTICED A 0.500" CRACK FOUND ON LT FRAME BS 288 AT STRINGER 11L LOCATION. REFERENCE "A" CHECK ITEM #37, FIGURE 27. "A HIGH FREQUENCY CURRENT SURFACE SCAN (EDDY CURRENT) WAS CARRIED OUT ON REPAIR OF STATION 288 FRAME AT WING BOX ATTACHMENT RIB AFTER DAMAGE WAS CUT OUT. NO FURTHER DEFECTS FOUND." REPAIRS CARRIED OUT IAW CAS ENGINEERING B1900-53-002. TUB FITTING INSTALLED WET WITH PS870 USING ALL LOCK FASTENER PINS AND COLLARS. ALL EFFECTED AREA PREPED/EPOXY PRIMED IAW AMM 20-08-00.

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