BEECH A36 near San Gabriel, CA — 2009-11-15
- Date
- 2009-11-15
- Location
- San Gabriel, CA, USA
- Aircraft
- BEECH A36
- Registration
- N17803
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Descent
Probable cause
Failure of the exhaust band V-clamp during cruise flight, which resulted in an in-flight fire and a subsequent forced landing.
NTSB narrative
About 15 minutes after takeoff, witnesses observed the airplane make a forced landing adjacent to a railroad track. The airplane touched down partially on the track and bounced several times before coming to rest about 500 yards beyond the initial point of impact. The witnesses reported that the engine was at idle power during the shallow approach. The fuselage and engine area were thermally damaged and the pilot suffered fatal injuries due to a fire. A postaccident examination revealed that a section of the upper left cowling had localized fire damage that was not attributed to the postimpact fire. The left cowling was placed in its normal position just forward of the airplane fuselage. A matching thermal pattern was noted in a small section of the airplane skin just aft of the firewall. Further examination revealed that the left exhaust system transition pipe and V-band clamp had separated from the engine and that the V-band clamp exhibited evidence of corrosion. A metallurgical examination of the V-band clamp revealed that it had fractured through the strap adjacent to a gap between the V-shaped clamping segments. The separation was a result of an overstress fracture of the strap, which was already weakened due to localized oxidation. It is likely that the failure of this clamp resulted in the initiation of an in-flight fire in the engine compartment area.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have opted for a different landing area before forced landing.
NTSB coding
Evidence available
- Photos
- 16 docket documents
Docket documents16
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Release of Aircraft Wreckage, NTSB Form 6120.15 (Return of Clamps)form
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Exerpt Aircraft Logbook Copiesother
- Lycoming Service Bulletin 240 and V-band Clamp Torquing Requirementsother
- Map of Accident Areaother
- Materials Laboratory 15 - Factual Report 10-008 (6 Embedded Images)photos
- Photo 1 - Initial Impact (LASO)photos
- Photo 2 - Main Wreckage (LASO)photos
- Photo 3 - Main Wreckage (LASO)photos
- Photo 4 - Separated Engine (LASO)photos
- Photo 5 - Upper left cowl with fire damage (NTSB)photos
- Photo 6 - Underside of left cowl (NTSB)photos
- Report from Lycoming (6 Embedded Images)photos
- Toxicological Reportreport
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