Accident Beechcraft G35 Bonanza N32TS,
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ASN Wikibase Occurrence # 43428
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Date:Monday 9 January 1995
Time:18:50 LT
Type:Silhouette image of generic BE35 model; specific model in this crash may look slightly different    
Beechcraft G35 Bonanza
Owner/operator:Jose Pineda
Registration: N32TS
MSN: D4643
Year of manufacture:1956
Total airframe hrs:4116 hours
Engine model:CONTINENTAL E-225-8
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Location:West Palm Beach, FL -   United States of America
Phase: En route
Departure airport:Pahokee, FL (KPHK)
Destination airport:Wellington, FL
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
The airplane was seen flying erratically, in a rapid descent, with smoke coming from the engine compartment and flames coming from the airplane's right side. Subsequently, the airplane crashed/landed and burned. An investigation revealed that the #1 cylinder had separated from the engine. Examination of the #1 cylinder revealed the upper crankcase thru-bolt at the 10 o'clock position had failed in fatigue below the cylinder deck surface. The lower thru-bolt at the cylinder pad's 8 o'clock position was intact; however, the nut was missing and the threads were battered and polished. The cylinder had 6 deck studs in addition to the thru-bolts. The studs at the 11 and 1 o'clock positions were missing; the studs at the 5 and 7 o'clock positions failed in fatigue; and the studs at the 2 and 4 o'clock positions were fractured with the fractured ends battered. Also, a silicon sealant (RTV) had been used on the thru-bolt threads, though not recommended by the manufacturer. The remaining thru-bolts were examined for tightness using a torque wrench; all were found undertorqued. During a top overhaul of the engine, about 85 flight hours before the accident, all of the cylinders had been removed and reinstalled.

Probable Cause: Improper top overhaul by maintenance personnel, and improperly torqued crackcase thru-bolts and cylinder deck studs at the number one cylinder, which led to fatigue failure of four of the bolts, failure and/or separation of the number one cylinder, and a subsequent fire.

Accident investigation:
Investigating agency: NTSB
Report number: NYC95FA049
Status: Investigation completed
Duration: 1 year and 5 months
Download report: Final report




Revision history:

24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
09-Apr-2024 17:08 ASN Update Bot Updated [Time, Cn, Other fatalities, Departure airport, Source, Narrative, Category, Accident report]

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