CONVAIR CV-580 near Columbus, OH — 2008-09-01
- Date
- 2008-09-01
- Location
- Columbus, OH, USA
- Airport
- LCK
- Aircraft
- CONVAIR CV-580
- Registration
- N587X
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 3
- Phase of flight
- Initial climb
Probable cause
The improper (reverse) rigging of the elevator trim cables by company maintenance personnel, and their subsequent failure to discover the misrigging during required post-maintenance checks. Contributing to the accident was the captain’s inadequate post-maintenance preflight check and the flight crew’s improper response to the trim problem.
Contributing factors
Contributing to the accident was the captain’s inadequate post-maintenance preflight check and the flight crew’s improper response to the trim problem.
NTSB narrative
The accident flight was the first flight following maintenance that included flight control cable rigging. The flight was also intended to provide cockpit familiarization for the first officer and the pilot observer, and as a training flight for the first officer. About one minute after takeoff, the first officer contacted the tower and stated that they needed to return to land. The airplane impacted a cornfield about one mile southwest of the approach end of the runway, and 2 minutes 40 seconds after the initiation of the takeoff roll. The cockpit voice recorder (CVR) indicated that, during the flight, neither the captain nor the first officer called for the landing gear to be raised, the flaps to be retracted, or the power levers to be reduced from full power. From the time the first officer called "rotate" until the impact, the captain repeated the word "pull" about 27 times. When the observer pilot asked, "Come back on the trim?" the captain responded, "There's nothing anymore on the trim." The inspection of the airplane revealed that the elevator trim cables were rigged improperly, which resulted in the trim cables being reversed. As a result, when the pilot applied nose-up trim, the elevator trim system actually applied nose-down trim. The flight crew was briefed on the maintenance work that had been performed on the airplane; therefore, when the captain’s nose-up trim inputs were affecting his ability to control the airplane, at a minimum, he should have stopped making additional inputs and returned the airplane to the configuration it was in before the problem worsened. An examination of the maintenance instruction cards used to conduct the last inspection revealed that the inspector's block on numerous checks were not signed off by the Required Inspection Item (RII) inspector. The RII inspector did not sign the item that stated: "Connect elevator servo trim tab cables and rig in accordance with Allison Convair [maintenance manual]...” The item had been signed off by the mechanic, but not by the RII inspector. The card also contained a NOTE, which stated in bold type, "A complete inspection of all elevator controls must be accomplished and signed off by an RII qualified inspector and a logbook entry made to this effect." The RII inspector block was not signed off.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Properly sign off maintenance checks before flight.
NTSB coding
Evidence available
- CVR
- FDR / data
- ADS-B / radar
- Photos
- 53 docket documents
Docket documentsshowing 50 of 53
- ATC Packageatc
- Cockpit Voice Recorder 12 - Factual Report of Group Chairmancvr
- Cockpit Voice Recorder 12 - Sound Spectrum Studycvr
- Flight Data Recorder 10 - Specialist's Factual Reportfdr
- Aircraft Informationform
- Pilot Informationform
- Pilot Training Informationform
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- FAA Interview Notesinterview
- NTSB Interview Notesinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Aircraft Maintenance Manualother
- Aircraft Maintenance Recordsother
- Convair 580 Checklistother
- E-mail From Operator's Vice-president of Maintenanceother
- Final Response to Petition for Reconsiderationother
- Fuel Receiptother
- Incoming Petition for Reconsiderationother
- Photo 1. Aerial View of Wreckage Path Looking to the Southphotos
- Photo 10. Lower Skin Panel of Right Wingphotos
- Photo 11. View of Main Wreckage in Debris Pathphotos
- Photo 12. Left Wing Sectionphotos
- Photo 13. Left Engine and Nacellephotos
- Photo 14. Right Engine and Nacellephotos
- Photo 15. Burned Empennagephotos
- Photo 16. Burned Empennagephotos
- Photo 17. Right Wing and Fuselagephotos
- Photo 18. Cockpit Instrumentsphotos
- Photo 19. Cockpit Instruments and Debrisphotos
- Photo 2. Aerial View of Main Wreckagephotos
- Photo 20. Forward Section of Fuselagephotos
- Photo 21. Propeller Hubphotos
- Photo 22. Inside of Fuselage Looking Forwardphotos
- Photo 23. Inside of Fuselage with Floorboards Removedphotos
- Photo 24. Elevator Trim Cables at FS 798 Floor Beamphotos
- Photo 25. Inboard Elevator Trim Cable Turnbucklephotos
- Photo 26. Inboard Elevator Trim Cable Through the Bottom Holephotos
- Photo 27. Elevator Trim Drum (Top View)photos
- Photo 28. Elevator Trim Drum (Bottom View)photos
- Photo 3. Aerial View of Main Wreckagephotos
- Photo 4. Cut Going Through Corn Stalksphotos
- Photo 5. View of Wreckage Path Looking Southphotos
- Photo 6. Propeller Blade in Debris Pathphotos
- Photo 7. Piece of Propeller Gearboxphotos
- Photo 8. Propeller Blade in Debris Pathphotos
- Photo 9. Section of Right Wing in Debris Pathphotos
- Radar Plots on Mapradar
- Kelowna Flightcraft Reportreport
- Original Brief Reportreport
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