CESSNA 560XL near Nantucket, MA — 2012-10-19
- Date
- 2012-10-19
- Location
- Nantucket, MA, USA
- Airport
- ACK
- Aircraft
- CESSNA 560XL
- Registration
- N576QS
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Initial climb
Probable cause
The incorrect installation of the left main gear aft trunnion pivot pin by maintenance personnel, which resulted in separation of the aft portion of the left main gear trunnion from the aft trunnion fitting and minor damage to the airplane.
NTSB narrative
Shortly after takeoff, a tower air traffic controller notified the flight crew that fuel was pouring from the left wing. The crew also noted hydraulic and flight control annunciator messages and a gear unlocked indication. The flight remained in the traffic pattern and the airplane landed with a fuel imbalance of about 1,000 pounds. An examination of the airplane after the incident revealed minor damage in the left wing and gear well areas. The left main gear aft trunnion pivot pin was not in place, resulting in separation of the aft portion of the left main gear trunnion from the aft trunnion fitting. The end of the aft trunnion punctured the interior of the gear well, resulting in damage to surrounding structure and damage to the fuel cell and hydraulic line. The damage resulted in the fuel leak and the flight control and hydraulic messages. The pin was later found loose and undamaged in the flap track area of the left wing. The aft trunnion pivot pin retaining bolt that was intended to restrain the pivot pin was in place and secured with a nut and cotter pin. A review of maintenance records for the airplane revealed that the left main gear trunnion was removed and replaced with a new unit about six weeks before the incident. The maintenance was performed by an outside vendor. According to the airplane maintenance manual, when installing the aft main landing gear trunnion, the trunnion pivot pin must be slid forward, aligning a hole in the trunnion with a hole in the pivot pin. The trunnion pivot pin is then secured in place with the retaining bolt, washers, nut, and cotter pin. It is likely that the incorrect installation of the left main gear aft trunnion allowed the aft trunnion pivot pin to eventually exit the trunnion and attach fitting. This allowed the aft trunnion to puncture the interior of the gear well.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Proper installation of the left main gear trunnion pivot pin could have prevented the failure.
NTSB coding
- Miscellaneous/other · Initial climb
- Maintenance
Evidence available
- Photos
- 8 docket documents
Docket documents8
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Statement of Party Representatives to NTSB Investigationinterview
- 560XL Maintenance Manual Excerptsother
- Aircraft Maintenance Recordsother
- Photo 1: Damage to Interior of Gear Well (Netjets Digital Photo)photos
- Photo 2: Main Gear Trunnion Pin, Near Location Found in Gear Well (Netjets Digital Photo)photos
- Photo 3: Aft Trunnion with Retaining Bolt and Nut Installed (FAA Digital Photo)photos
- Cessna Structures Reportreport
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