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20010926035799I

Incident · Minor damage
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FAA incident report · Cessna 310P · Lakeland, FL · September 26, 2001

FAA Aviation Safety Information Portal

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Date
September 26, 2001 · 12:30 local
Place
Lakeland, FL
Airport
Lakeland Regional Airport
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N69HS
Reported as
Cessna 310P
People aboard
2
Fatal injuries
0
Pilot’s flight hours
3,500 total1,200 in this make and model50 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) While taxiing in from a check ride at Lakeland linder regional airport, the left landing gear separated from the aircraft. During the investigation the left aft shaft pin (Cessna p/n 5041107-2) was found, undamaged, rolling around in the wing area aft of the landing gear attach point. The slotted pin (p/n NAS561P4-28) was found intact, installed in the strut assembly. The left forward shaft pin was found broken, with one half in the airframe fitting and the other half properly locked in the strut assembly.

As the FAA filed it

(-23) WHILE TAXIING IN FROM A CHECK RIDE AT LAKELAND LINDER REGIONAL AIRPORT, THE LEFT LANDING GEAR SEPARATED FROM THE AIRCRAFT. DURING THE INVESTIGATION THE LEFT AFT SHAFT PIN (CESSNA P/N 5041107-2) WAS FOUND, UNDAMAGED, ROLLING AROUND IN THE WING AREA AFT OF THE LANDING GEAR ATTACH POINT. THE SLOTTED PIN (P/N NAS561P4-28) WAS FOUND INTACT, INSTALLED IN THE STRUT ASSEMBLY. THE LEFT FORWARD SHAFT PIN WAS FOUND BROKEN, WITH ONE HALF IN THE AIRFRAME FITTING AND THE OTHER HALF PROPERLY LOCKED IN THE STRUT ASSEMBLY.