PIPER PA-34-200T near Tallahassee, FL — 2013-06-03
- Date
- 2013-06-03
- Location
- Tallahassee, FL, USA
- Airport
- TLH
- Aircraft
- PIPER PA-34-200T
- Registration
- N633TC
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Climb
Probable cause
The failure of the elevator trim cable due to fatigue cracking, which resulted from maintenance personnel’s repeated inadequate inspection of the cable.
NTSB narrative
According to the flight instructor, during the initial climb, the student pilot noticed a problem with the elevator trim wheel. The flight instructor moved the trim wheel and noted no resistance. He then looked down at the wheel and observed the trim cable protruding from its side. The flight instructor assumed control of the airplane, advised the tower air traffic controller of the emergency, and landed the airplane without incident. Examination of the elevator trim cable assembly revealed that the trim cable failed due to fatigue cracking of the individual wires. The wire breaks were so numerous and over such a sizable length that they should have been detectable by a visual inspection. However, a review of the aircraft logbooks revealed that maintenance personnel did not detect the fatigue cracking of the wires during the most recent 100-hour and annual inspections nor during compliance with an airworthiness directive (AD) that required, in part, that all control cables be inspected for broken wires strands and that any broken wire strands be replaced; the inspections and AD were accomplished less than 2 months before the incident.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Inspection failure to detect trim cable issues during recent maintenance.
NTSB coding
- Flight control sys malf/fail · Initial climb
- Maintenance
Evidence available
- Photos
- 12 docket documents
Docket documents12
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- CFI Statement Trim Tab Malfunctioninterview
- Aircraft Logbook Annual excerpt pageother
- FAA Advisory Circular 43.13-1B excerptother
- N633TC Stabilator Cable Replacement Log excerptother
- Piper Seneca II Service Diagramother
- Stabilator Control System Inspection Service Bulletin 1245Aother
- Stabilator Inspection AD Sign Offother
- Trim Cable Airworthiness Directive 2013-02-13other
- Photo 1 - Broken Cable (Photo Courtesy of FAA)photos
- Photo 2 - Baggage Compartment (Photo Courtesy of FAA)photos
- Materials Laboratory Factual report 14-048report
Related mishaps
- PYKA INC PELICAN
2025-03-28 · Dixon, CA
- CESSNA 172
2024-12-20 · Cintrona, PR · 1 fatality
- CUB CRAFTERS CARBON CUB
2024-10-27 · Ogallala, NE
- BEECH 95
2023-11-18 · Yuma, AZ
- CESSNA 172
2023-05-26 · Lake Worth, FL · 2 fatalities
- CIRRUS DESIGN CORP SF50
2022-11-25 · Mount Comfort, IN