20090318005089A

Accident · Substantial damage

FAA accident report · Cessna 310K · Ocala, FL · March 18, 2009

Date
March 18, 2009 · 13:21 local
Place
Ocala, FL
Airport
Ocala International-Jim Taylor Field
Phase of flight
Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6901L
NTSB investigation
NTSBERA09LA210
Reported as
Cessna 310K
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
6,997 total71 in this make and model15 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.

(-23) Aircraft departed Ocala on a training flight, landed at williston and fueled aircraft. Aircraft departed williston for dunnellon and performed one touch and go landing and one full stop landing. After departing dunnellon pilot noticed that he did not have a gear up and locked light. Pilot cycled landing gear and still did not have an up and locked light. After cycling gear aircraft felt as if the landing gear had not fully retracted. Prior to landing at Ocala aircraft conducted a fly-by to verify position of landing gear. Ground personnel reported that left gear appeared to be partially retracted. Pilot cycled landing gear circuit breaker and received a green light for the left main and nose gear. Another pass was made and ground personnel reported that the landing gear appeared to be down. Instructor pilot performed landing and upon roll out the right gear collapsed. Inspection of the aircraft revealed that the u bolts securing the forward pivot shaft to the landing gear strut assembly were missing, the shaft remained in the bearing housing. The aft pivot shaft remained attached to the strut assembly but was bent down at a 90 degree angle and pulled out of the bearing housing.

As the FAA filed it

(-23) AIRCRAFT DEPARTED OCALA ON A TRAINING FLIGHT, LANDED AT WILLISTON AND FUELED AIRCRAFT. AIRCRAFT DEPARTED WILLISTON FOR DUNNELLON AND PERFORMED ONE TOUCH AND GO LANDING AND ONE FULL STOP LANDING. AFTER DEPARTING DUNNELLON PILOT NOTICED THAT HE DID NOT HAVE A GEAR UP AND LOCKED LIGHT. PILOT CYCLED LANDING GEAR AND STILL DID NOT HAVE AN UP AND LOCKED LIGHT. AFTER CYCLING GEAR AIRCRAFT FELT AS IF THE LANDING GEAR HAD NOT FULLY RETRACTED. PRIOR TO LANDING AT OCALA AIRCRAFT CONDUCTED A FLY-BY TO VERIFY POSITION OF LANDING GEAR. GROUND PERSONNEL REPORTED THAT LEFT GEAR APPEARED TO BE PARTIALLY RETRACTED. PILOT CYCLED LANDING GEAR CIRCUIT BREAKER AND RECEIVED A GREEN LIGHT FOR THE LEFT MAIN AND NOSE GEAR. ANOTHER PASS WAS MADE AND GROUND PERSONNEL REPORTED THAT THE LANDING GEAR APPEARED TO BE DOWN. INSTRUCTOR PILOT PERFORMED LANDING AND UPON ROLL OUT THE RIGHT GEAR COLLAPSED. INSPECTION OF THE AIRCRAFT REVEALED THAT THE U BOLTS SECURING THE FORWARD PIVOT SHAFT TO THE LANDING GEAR STRUT ASSEMBLY WERE MISSING, THE SHAFT REMAINED IN THE BEARING HOUSING. THE AFT PIVOT SHAFT REMAINED ATTACHED TO THE STRUT ASSEMBLY BUT WAS BENT DOWN AT A 90 DEGREE ANGLE AND PULLED OUT OF THE BEARING HOUSING.

NTSB investigation

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