20070215006079I

Incident · Minor damage

FAA incident report · Piper PA-28R-200 · Atwater, CA · February 15, 2007

Date
February 15, 2007 · 17:41 local
Place
Atwater, CA
Airport
Castle Afb
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Operator
YMOS
Damage
Minor damage
Aircraft
N9350K
Reported as
Piper PA28R200
People aboard
2
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) The aircraft experienced a gear malfunction after takeoff, which was the aircraft's first flight after maintenance. The maintenance involved a related gear problem that resulted in replacing some hydraulic components. According to the pilot, the in-transit light stayed illuminated all through the flight with the right main gear not retracting completely into the wheel well. The gear handle was cycled down and the nose and left main gear operated normally indicating down and locked with their respective green lights "on." There were attempts made to get the right gear down such as: conducting flight turning maneuvers and bouncing on the runway hoping to dislodge the gear, which all attempts failed. After approximately two (2) hours, the pilot landed the aircraft on the remaining gear holding it up until finally touching the right wing, which caused the aircraft to spin onto a soft dirt area. There was minimal damage to the right flap and lower aileron control areas.

As the FAA filed it

(-23) THE AIRCRAFT EXPERIENCED A GEAR MALFUNCTION AFTER TAKEOFF, WHICH WAS THE AIRCRAFT'S FIRST FLIGHT AFTER MAINTENANCE. THE MAINTENANCE INVOLVED A RELATED GEAR PROBLEM THAT RESULTED IN REPLACING SOME HYDRAULIC COMPONENTS. ACCORDING TO THE PILOT, THE IN-TRANSIT LIGHT STAYED ILLUMINATED ALL THROUGH THE FLIGHT WITH THE RIGHT MAIN GEAR NOT RETRACTING COMPLETELY INTO THE WHEEL WELL. THE GEAR HANDLE WAS CYCLED DOWN AND THE NOSE AND LEFT MAIN GEAR OPERATED NORMALLY INDICATING DOWN AND LOCKED WITH THEIR RESPECTIVE GREEN LIGHTS "ON." THERE WERE ATTEMPTS MADE TO GET THE RIGHT GEAR DOWN SUCH AS: CONDUCTING FLIGHT TURNING MANEUVERS AND BOUNCING ON THE RUNWAY HOPING TO DISLODGE THE GEAR, WHICH ALL ATTEMPTS FAILED. AFTER APPROXIMATELY TWO (2) HOURS, THE PILOT LANDED THE AIRCRAFT ON THE REMAINING GEAR HOLDING IT UP UNTIL FINALLY TOUCHING THE RIGHT WING, WHICH CAUSED THE AIRCRAFT TO SPIN ONTO A SOFT DIRT AREA. THERE WAS MINIMAL DAMAGE TO THE RIGHT FLAP AND LOWER AILERON CONTROL AREAS.

Other reports on N9350K · 2

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