Service difficulty report · Stabilator · Beech C24R

Difficulty date
October 26, 2000
Submitted
November 9, 2000
Operation
General aviation
Aircraft
N6710D
Make and model
Beech C24R
Aircraft serial
MC709
Part
Stabilator
Part number
16962000165
Condition
Cracked
Location
Aft
Part time
2,000 hours
Component
Stabilator
Component part number
169620001603
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 INSPECTIONS OF UNDERSIDES OF STABILATORS ON BEECH SIERRAS, SUNDOWNERS, HAVE FOUND DEFECTS RANGING FROM WORKING RIVETS TO CRACKS IN LOWER SKINS. PROBLEM IS CENTERED APPROX 6 INCHES OUT FROM FUSELAGE ON BOTH SIDES. MECHANICS HAVE INSTALLED OVERSIZED RIVETS, ADDITIONAL RIVETS, PATCHES. BEECH ADDRESSES THIS PROBLEM IN SI 1167, OFFERS A P/N FOR IMPROVED AFT CENTER SPAR CALLING FOR NEW SPAR TO BE BONDED TO SKINS. REPLACED AFT CENTER SPARS, AFT LOWER SKINS ON 2 SIERRAS, IN ONE, SPARS CRACKED WEAKENED BY 0.250 INCH CHERRY MAX RIVETS AND TRIPPLING OF RIVETS. ORIG SPAR DOES NOT OFFER ENOUGH SUPPORT TO CONTROL OIL CANNING EVEN THOUGH EXISTING SPAR MAY NOT BE CRACKED, WORKING, OR OVERSIZED. (X)

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