19991110043339A

Accident · Substantial damage

FAA accident report · Cessna T310Q · Jacksonville, FL · November 10, 1999

Date
November 10, 1999 · 17:30 local
Place
Jacksonville, FL
Airport
Craig Municipal Airport
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N310GC
NTSB investigation
NTSBATL00LA010
Reported as
Cessna T310Q
People aboard
1
Fatal injuries
0
Pilot’s flight hours
4,500 total200 in this make and model75 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(.4)The pilot had completed a local personal flight and was on taxiway 'c,' and was returning to the parking ramp, when without warning the left main landing gear collapsed. Examination of the airplane and the landing gear assembly showed that the left main landing gear down-lock end fitting assembly and the retention bolt had broken. The landing gear examination of the locking linkage failed to establish installation specification prior to the accident. A visual examination of the failed bolt assembly also failed to disclose pre-existing cracking in the bolt structure. A review of the maintenance logbooks revealed that recent maintenance had been performed on the landing gear assembly 18 hours before the accident. (-23)while taxing to hanger left MLG collasped causing substantial damage to left wing and left stabilizer. FAA inspection of aircraft found left MLG downlock end fitting assembly and retention bolt broken. (-23) while taxiing to hangar left MLG collapsed causing substantial damage to left wing and left stabilizer. FAA inspection of aircraft found left MLG downlock end fitting assembly and retention bolt broken.

As the FAA filed it

(.4)THE PILOT HAD COMPLETED A LOCAL PERSONAL FLIGHT AND WAS ON TAXIWAY 'C,' AND WAS RETURNING TO THE PARKING RAMP, WHEN WITHOUT WARNING THE LEFT MAIN LANDING GEAR COLLAPSED. EXAMINATION OF THE AIRPLANE AND THE LANDING GEAR ASSEMBLY SHOWED THAT THE LEFT MAIN LANDING GEAR DOWN-LOCK END FITTING ASSEMBLY AND THE RETENTION BOLT HAD BROKEN. THE LANDING GEAR EXAMINATION OF THE LOCKING LINKAGE FAILED TO ESTABLISH INSTALLATION SPECIFICATION PRIOR TO THE ACCIDENT. A VISUAL EXAMINATION OF THE FAILED BOLT ASSEMBLY ALSO FAILED TO DISCLOSE PRE-EXISTING CRACKING IN THE BOLT STRUCTURE. A REVIEW OF THE MAINTENANCE LOGBOOKS REVEALED THAT RECENT MAINTENANCE HAD BEEN PERFORMED ON THE LANDING GEAR ASSEMBLY 18 HOURS BEFORE THE ACCIDENT. (-23)WHILE TAXING TO HANGER LEFT MLG COLLASPED CAUSING SUBSTANTIAL DAMAGE TO LEFT WING AND LEFT STABILIZER. FAA INSPECTION OF AIRCRAFT FOUND LEFT MLG DOWNLOCK END FITTING ASSEMBLY AND RETENTION BOLT BROKEN. (-23) WHILE TAXIING TO HANGAR LEFT MLG COLLAPSED CAUSING SUBSTANTIAL DAMAGE TO LEFT WING AND LEFT STABILIZER. FAA INSPECTION OF AIRCRAFT FOUND LEFT MLG DOWNLOCK END FITTING ASSEMBLY AND RETENTION BOLT BROKEN.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.