20020628019689I

Incident

FAA incident report · Aviat A-1B · Orlando, FL · June 28, 2002

Date
June 28, 2002 · 11:00 local
Place
Orlando, FL
Airport
Orlando Sanford Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Aircraft
N628RA
Reported as
Aviat A1B
Reported engine
Lycoming O360A1D
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,100 total372 in this make and model40 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) Left main wheel, on float plane, would not extend three other wheels did extend. Pilot landed on grass area within airport. No damage was reported by pilot or airport authority. On July 2, 2002, an inspection of the aircraft right landing gear revealed that the axle shock strut attached to the gear actuator was binding against the right main gear track. Evidence of debris consisting of dirt and sand may have caused the shock strut to bind against the main gear track. Also, a pressure switch disconnects the landing gear hydraulic system once the pressure reaches 250 PSI. The husky A-1B maintenance manual requires a 25 hour lubricant inspection which was complied with.

As the FAA filed it

(-23) LEFT MAIN WHEEL, ON FLOAT PLANE, WOULD NOT EXTEND THREE OTHER WHEELS DID EXTEND. PILOT LANDED ON GRASS AREA WITHIN AIRPORT. NO DAMAGE WAS REPORTED BY PILOT OR AIRPORT AUTHORITY. ON JULY 2, 2002, AN INSPECTION OF THE AIRCRAFT RIGHT LANDING GEAR REVEALED THAT THE AXLE SHOCK STRUT ATTACHED TO THE GEAR ACTUATOR WAS BINDING AGAINST THE RIGHT MAIN GEAR TRACK. EVIDENCE OF DEBRIS CONSISTING OF DIRT AND SAND MAY HAVE CAUSED THE SHOCK STRUT TO BIND AGAINST THE MAIN GEAR TRACK. ALSO, A PRESSURE SWITCH DISCONNECTS THE LANDING GEAR HYDRAULIC SYSTEM ONCE THE PRESSURE REACHES 250 PSI. THE HUSKY A-1B MAINTENANCE MANUAL REQUIRES A 25 HOUR LUBRICANT INSPECTION WHICH WAS COMPLIED WITH.