CESSNA 172RG near Kissimmee, FL — 2011-11-08
- Date
- 2011-11-08
- Location
- Kissimmee, FL, USA
- Airport
- ISM
- Aircraft
- CESSNA 172RG
- Registration
- N5095V
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Landing
Probable cause
A fatigue failure of the right main landing gear pivot assembly, which prevented the landing gear from extending.
NTSB narrative
The pilot was not able to obtain a positive gear down-and-locked indication and noticed that the right main landing gear (MLG) only extended about halfway down. After unsuccessful troubleshooting efforts, he performed an emergency gear-up landing, which resulted in substantial damage to the underside of the fuselage. Examination of the landing gear system revealed that the stub shaft of the right MLG pivot assembly was fractured and exhibited characteristics consistent with a torsional fatigue fracture containing multiple origins. Before the accident flight, a company mechanic observed some hydraulic fluid on the MLG leg and assumed that there was a leak from the pivot gear O-rings, which he replaced. The Federal Aviation Administration previously issued an airworthiness directive (AD), which included an inspection of MLG pivot assemblies for cracks, in accordance with a manufacturer's service bulletin. The AD did not call for repetitive inspections. At the time of the accident, the airplane had been operated for about 7,755 total hours and about 1,800 hours since the time of AD compliance. The airplane service manual contained a supplemental inspection that included initial visual and eddy current inspections of the MLG pivot assembly for cracks in the spline area at 3,000 hours in service with repeated inspections every 500 hours thereafter. The visual and eddy current inspections had not been nor were they required to be performed on the accident airplane.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Failure to perform required inspections on landing gear pivot assembly.
NTSB coding
Evidence available
- Photos
- 13 docket documents
Docket documents13
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Pilot and Airport Personnel Statementsinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Cessna 172RG Parts Catalog Excerpt Depicting Fracture Locationother
- Cessna 172RG Service Manual Supplemental Inspection Number: 32-10-01other
- Cessna Service Bulletin SEB90-1other
- Excerpts of Email Communicationsother
- FAA Airworthiness Directive AD 2001-06-06other
- Photograph # 1 – Partial view of the damage to the underside of the fuselage after recovery (Provided by the Operator)photos
- Photograph # 2 – View of fractured landing gear pivot assembly while installed on the airframe (Provided by the Operator)photos
- Photograph # 3 – View of fractured portion of the pivot assembly splined gear (Provided by the FAA)photos
- Foreign Authority Report Pertaining to Cessna 172RG Pivot Assembly Failure that occurred in Spainreport
- Materials Laboratory Report 12-075report
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