19980324008469A

Accident · Substantial damage

FAA accident report · Piper PA-22 · Kalispell, MT · March 24, 1998

Date
March 24, 1998 · 09:30 local
Place
Kalispell, MT
Airport
Glacier Park International
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1770A
NTSB investigation
NTSBSEA98LA051
Reported as
Piper PA22
Reported engine
Lycoming O320A2B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
390 total12 in this make and model12 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.

Ground looped during touch and go. Collapsed right main gear. Damaged wing PA22 had been converted to tail wheel. (.4)the pilot was landing with a left crosswind. He reported that while landing the airplane, which had been modified with a tailwheel installation and a short-takeoff-and-landing (stol) modification, he did not keep full left aileron in. He stated that when he relaxed wheel input, the wind picked up his left wing, at which point the right main landing gear folded and the right wing struck the ground. (-23)the pilot reported he was practicing takeoff and landings with approximately a 7 to 8 knot crosswind when he lost control and ground looped the aircraft. The aircraft received substantial damage when the right gear collapsed bending the spars in the right wing. There were no injuries.

As the FAA filed it

GROUND LOOPED DURING TOUCH AND GO. COLLAPSED RIGHT MAIN GEAR. DAMAGED WING PA22 HAD BEEN CONVERTED TO TAIL WHEEL. (.4)THE PILOT WAS LANDING WITH A LEFT CROSSWIND. HE REPORTED THAT WHILE LANDING THE AIRPLANE, WHICH HAD BEEN MODIFIED WITH A TAILWHEEL INSTALLATION AND A SHORT-TAKEOFF-AND-LANDING (STOL) MODIFICATION, HE DID NOT KEEP FULL LEFT AILERON IN. HE STATED THAT WHEN HE RELAXED WHEEL INPUT, THE WIND PICKED UP HIS LEFT WING, AT WHICH POINT THE RIGHT MAIN LANDING GEAR FOLDED AND THE RIGHT WING STRUCK THE GROUND. (-23)THE PILOT REPORTED HE WAS PRACTICING TAKEOFF AND LANDINGS WITH APPROXIMATELY A 7 TO 8 KNOT CROSSWIND WHEN HE LOST CONTROL AND GROUND LOOPED THE AIRCRAFT. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE WHEN THE RIGHT GEAR COLLAPSED BENDING THE SPARS IN THE RIGHT WING. THERE WERE NO INJURIES.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.