20100407032049I

Incident · Minor damage

FAA incident report · Cessna 310Q · Clanton, AL · April 7, 2010

Date
April 7, 2010 · 05:50 local
Place
Clanton, AL
Airport
Clanton
Phase of flight
Takeoff: Departure Roll
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N69827
Reported as
Cessna 310Q
Reported engine
Continental I0-470 series
People aboard
3
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,569 total2,569 in this make and model9 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.

On April 07, 2010, at 0630 CST, a Cessna 310Q operated as a 14 code of federal regulations part 91, personal flight at Clanton, AL (02A). The pilot stated that during takeoff roll the windshield fogged over with dew, and he lost directional control of the aircraft. The aircraft ran off of the north side of the runway. Upon returning to the runway the front gear collapsed causing the aircraft to skid to a stop. The pilot and the passengers sustained no injuries, and the aircraft incurred minor damaged. The on scene investigation confirmed that the aircraft nose gear collapsed and was torn off of the aircraft. Both engine propellers were damaged; the nose of the aircraft was damaged, but there was no damage to the aircraft bulkhead. The aircraft flight controls continuity check was performed and no discrepancy found. The aircraft electrical system was operational; fuel was present in all tanks, and the main landing gear continuity check was good. There was no visible damage to the aircraft wings and fuselage section.

As the FAA filed it

ON APRIL 07, 2010, AT 0630 CST, A CESSNA 310Q OPERATED AS A 14 CODE OF FEDERAL REGULATIONS PART 91, PERSONAL FLIGHT AT CLANTON, AL (02A). THE PILOT STATED THAT DURING TAKEOFF ROLL THE WINDSHIELD FOGGED OVER WITH DEW, AND HE LOST DIRECTIONAL CONTROL OF THE AIRCRAFT. THE AIRCRAFT RAN OFF OF THE NORTH SIDE OF THE RUNWAY. UPON RETURNING TO THE RUNWAY THE FRONT GEAR COLLAPSED CAUSING THE AIRCRAFT TO SKID TO A STOP. THE PILOT AND THE PASSENGERS SUSTAINED NO INJURIES, AND THE AIRCRAFT INCURRED MINOR DAMAGED. THE ON SCENE INVESTIGATION CONFIRMED THAT THE AIRCRAFT NOSE GEAR COLLAPSED AND WAS TORN OFF OF THE AIRCRAFT. BOTH ENGINE PROPELLERS WERE DAMAGED; THE NOSE OF THE AIRCRAFT WAS DAMAGED, BUT THERE WAS NO DAMAGE TO THE AIRCRAFT BULKHEAD. THE AIRCRAFT FLIGHT CONTROLS CONTINUITY CHECK WAS PERFORMED AND NO DISCREPANCY FOUND. THE AIRCRAFT ELECTRICAL SYSTEM WAS OPERATIONAL; FUEL WAS PRESENT IN ALL TANKS, AND THE MAIN LANDING GEAR CONTINUITY CHECK WAS GOOD. THERE WAS NO VISIBLE DAMAGE TO THE AIRCRAFT WINGS AND FUSELAGE SECTION.

Other reports on N69827 · 2

Matched to the same aircraft by N-number and date.