EAGLE PASS, TX, USA
N14RR
BEECH 95-C55
THE WRECKAGE WAS LOCATED APPROXIMATELY 16 MI SE OF EAGLE PASS & WITH THE EXCEPTION OF THE ELEVATORS, ALL MAJOR COMPONENTS OF THE ACFT WERE IDENTIFIED AT THE SCENE. THE OUTBOARD HALF OF THE R ELEVATOR WAS FOUND 2 MI NW & THE COUNTERWEIGHT ON THE ELEV TIP WAS MISSING. THE INBOARD HALF WAS FOUND 3 MI NWW. THE L ELEV AS FOUND 1.7 MI & THE ELEVATOR TIP COUNTERWEIGHT WAS MISSING. THE STABILIZER SKINS, TOP & BOTTOM, WERE RAISED BETWEEN THE RIVETS. THE L STABILIZER SPAR MIDDLE HINGE ATTACHMENT FITTING DISCLOSED EVIDENCE OF A PRE-EXISTING FRACTURE. RED PAINT, SIMILAR TO THE SURROUNDING PAINT, COULD BE SEEN WITHIN THE FRACTURE OF THE INBOARD FITTING. COMPRESSION DAMAGE WAS EVIDENT ON THE TOP OF BOTH ELEVATORS BETWEEN THE HINGE POINTS. PAINT THICKNESS MEASUREMENTS ON THE ELEV RANGED FROM: L UPPER SURFACE 0.0060-0.0120,L BOTTOM SURFACE 0.0050-0.0070; R UPPER SURFACE 0.0048-0.0051, R BOTTOM SURFACE 0.0050-0.0055. ACCORDING TO THE MANUFACTURER PAINT THICKNESS ON ELEVATORS OF NEW ACFT RANGE BETWEEN 0.0018 & 0.0027. NO LOGBOOK RECORD OF BALANCING.
Source: NTSB Aviation Accident Database
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