Service difficulty report · Spar · Beech A100

Difficulty date
January 1, 2010
Submitted
March 1, 2010
Operation
General aviation
Make and model
Beech A100
Aircraft time
17,122 hours
Engine
Pwa PT6A28
Propeller
Hartzl HCB4TN3
System (JASC)
5711 · Wing Spar
Part
Spar
Part number
5011002628
Condition
Cracked
Location
Ws 110 .11
Part time
17,121 hours
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN) THE OTBD WING REAR SPAR WEB WAS FOUND CRACKED AT THE LAP JOIINT WS 110.11, THE LOCATION OF THE OTBD FLAP, INBD TRACK. THE RIVETS SECURING THE LOWER CLIPS TO THE FLAP TRACK FAILED. THE FORCES APPLIED TO THE FLAP TRACK WHEN THE FLAPS WERE LOWERED PULLED ON THE WEB, AND IT CRACKED, ALSO ANGLE PN 50-110034-4. THE REPAR WAS COMPLETED IAW MFG REPAIR DWG NR FR-KA-03494 AND SRM CHAPTER 20-50-01 CHART 203. REPLACED ALSO WERE PN 50-110034-4 ANGLE, 35-15398-3 STIFFENER, 2 CLIPS ACFT RETURNED TO SERVICE. PN`S 35-11596-3 & 4. (TC 20100209010)

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