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19940312006809I

Incident · Minor damage
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FAA incident report · Piper PA28180 · Islip, NY · March 12, 1994

FAA Aviation Safety Information Portal

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Date
March 12, 1994 · 13:01 local
Place
Islip, NY
Airport
Long Island Mac Arthur
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N3299R
Reported as
Piper PA28180
People aboard
2
Fatal injuries
0
Pilot’s flight hours
600 total500 in this make and model31 in the last 90 days
N3299RRegistered now · Piper PA-28R-180S/N 28R-31270 · Built 1970Airframe modelPiper PA-28R-180Engine modelLycoming I0360 seriesReciprocating

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.

Narrative: as determined from pilot interviews and examination of the airplane, it appears that the safety pilot, ian britton , lost control of the airplane during landing rollout when the airplane exited runway 06 to the right in the vicinity of runway 10. The left landing gear collapsed as additional centrifugal force applied excesive side loads to the gear in a right turn at a speed of about 50 tp 60 mph. The aircraft sustained minor damage with no injuries to the pilots . A records check indicated that the aircraft was airworthy and the airman current and qualified at the time of the mishap.

As the FAA filed it

NARRATIVE: AS DETERMINED FROM PILOT INTERVIEWS AND EXAMINATION OF THE AIRPLANE, IT APPEARS THAT THE SAFETY PILOT, IAN BRITTON , LOST CONTROL OF THE AIRPLANE DURING LANDING ROLLOUT WHEN THE AIRPLANE EXITED RUNWAY 06 TO THE RIGHT IN THE VICINITY OF RUNWAY 10. THE LEFT LANDING GEAR COLLAPSED AS ADDITIONAL CENTRIFUGAL FORCE APPLIED EXCESIVE SIDE LOADS TO THE GEAR IN A RIGHT TURN AT A SPEED OF ABOUT 50 TP 60 MPH. THE AIRCRAFT SUSTAINED MINOR DAMAGE WITH NO INJURIES TO THE PILOTS . A RECORDS CHECK INDICATED THAT THE AIRCRAFT WAS AIRWORTHY AND THE AIRMAN CURRENT AND QUALIFIED AT THE TIME OF THE MISHAP.