20001219036499I

Incident · Minor damage

FAA incident report · Cessna 310N · Turlock, CA · December 19, 2000

Date
December 19, 2000
Place
Turlock, CA
Airport
Turlock Airpark Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N4184Q
Reported as
Cessna 310N
Reported engine
Continental IO470VO
People aboard
1
Fatal injuries
0

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) On 02/28/01, a request for a special flight permit to fly with the gear down was investigated and it was found that the subject aircraft was involved in an incident that occurred during the landing phase. Further research revealed that the aircraft's landing gear collapsed upon landing causing damage to both propellers, some lower fuselage structural stringers and sheet metal skins. There was other evidence of flap damage located on the right wing and nose gear doors had severe scrapes and dents at their aft sections. The propellers were removed for overhaul and both crankshafts were inspected for further damage. It is the opinion of the reporting ASI, based on the visual evidence of the aircraft, it appears the gear for some unknown reason retracted upon landing. This problem is certainly electrically related and further troubleshooting is required. The aircraft was issued a special flight permit to accomplish further maintenance repairs. (See attached sheet)

As the FAA filed it

(-23) ON 02/28/01, A REQUEST FOR A SPECIAL FLIGHT PERMIT TO FLY WITH THE GEAR DOWN WAS INVESTIGATED AND IT WAS FOUND THAT THE SUBJECT AIRCRAFT WAS INVOLVED IN AN INCIDENT THAT OCCURRED DURING THE LANDING PHASE. FURTHER RESEARCH REVEALED THAT THE AIRCRAFT'S LANDING GEAR COLLAPSED UPON LANDING CAUSING DAMAGE TO BOTH PROPELLERS, SOME LOWER FUSELAGE STRUCTURAL STRINGERS AND SHEET METAL SKINS. THERE WAS OTHER EVIDENCE OF FLAP DAMAGE LOCATED ON THE RIGHT WING AND NOSE GEAR DOORS HAD SEVERE SCRAPES AND DENTS AT THEIR AFT SECTIONS. THE PROPELLERS WERE REMOVED FOR OVERHAUL AND BOTH CRANKSHAFTS WERE INSPECTED FOR FURTHER DAMAGE. IT IS THE OPINION OF THE REPORTING ASI, BASED ON THE VISUAL EVIDENCE OF THE AIRCRAFT, IT APPEARS THE GEAR FOR SOME UNKNOWN REASON RETRACTED UPON LANDING. THIS PROBLEM IS CERTAINLY ELECTRICALLY RELATED AND FURTHER TROUBLESHOOTING IS REQUIRED. THE AIRCRAFT WAS ISSUED A SPECIAL FLIGHT PERMIT TO ACCOMPLISH FURTHER MAINTENANCE REPAIRS. (SEE ATTACHED SHEET)