PIPER PA-34-220T near Ankeny, IA — 2010-06-09
- Date
- 2010-06-09
- Location
- Ankeny, IA, USA
- Airport
- IKV
- Aircraft
- PIPER PA-34-220T
- Registration
- N104NW
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Approach
Probable cause
The failure of the stabilator control cable due to wear. Contributing to the accident was the inadequate maintenance inspection of the stabilator control cable.
NTSB narrative
The pilot reported that when he pulled back on the control yoke during the landing flare the nose of the airplane did not pitch up. The airplane landed hard on the nosewheel and bounced several times before stopping on the runway. A postaccident examination of the airplane revealed that the stabilator control cable had fractured in two pieces. The location of the fracture was in the unobstructed area in the tail cone; the location of the fracture was not associated with a pulley, fairlead, or bulkhead, and no rubbing or chaffing was found in the area of the fracture. The entire length of the cable was covered with dried black grease and the majority of the fractured ends of the individual wires exhibited wear damage with the exposed surfaces of the wires covered in grease. The ends of the fractured wires exhibited features typical of overstress separation, with no evidence of fatigue cracking. Federal Aviation Administration guidance states that the inspection and repair of control cables should be accomplished during annual inspections. The aircraft maintenance logbooks indicated that the last annual maintenance inspection was conducted about three months prior to the accident, equating to 17 flight hours. The logbook entry for that inspection indicated that the control cables were checked for correct rigging and cable tensions. The logbook entry stated, “Stabilator OK.” There was no indication of any repair or replacement of the stabilator control cable.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Inspection and maintenance of control cables not performed as per FAA recommendations.
NTSB coding
Evidence available
- Photos
- 17 docket documents
Docket documents17
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Aircraft Logbook Pagesother
- FAA SAIB No. CE-01-30other
- Figure of Stabilator Control Installationother
- Piper Maintenance Manual, Chapter 27 "Flight Controls"other
- Piper Service Bulletin - 1048other
- Piper Service Letter - 1069other
- Photo 1. View of cable run in tailphotos
- Photo 2. View of debris in tailphotos
- Photo 3. View of fractured cablephotos
- Photo 4. View of fractured cablephotos
- Photo 5. View of entire cablephotos
- Photo 6. View of fractured cablephotos
- Photo 7. View of fractured cablephotos
- Materials Laboratory Factual Report 10-072report
Related mishaps
- CUB CRAFTERS INC CC19-215
2026-06-09 · Plymouth, NH
- COSTRUZIONI AERONAUTICHE TECNA P-MENTOR
2026-06-09 · Pompano Beach, FL
- PIPER PA-28-180
2026-05-28 · Chesapeake, VA
- CESSNA 182
2026-05-28 · Dickinson, ND
- CESSNA 172
2026-05-27 · Naubinway, MI
- CESSNA R182
2026-05-26 · Fitchburg, MA