20030414008829I

Incident · Minor damage

FAA incident report · Piper PA-28-161 · Plattsmouth, NE · April 14, 2003

Date
April 14, 2003 · 13:35 local
Place
Plattsmouth, NE
Airport
Plattsmouth Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Operator
HE8S
Damage
Minor damage
Aircraft
N83416
Reported as
Piper PA28161
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) On April 14, 2003, at approximately 1335 CDT, Piper PA-28-161, N83416, experienced a failure of the LH MLG strut during landing rollout on runway 16 at the Plattsmouth, Nebraska municipal airport. The aircraft, owned and operated by the lemay flight training center, sustained minor damage, with no injury reporting by the crewmembers. Subsequent investigation disclosed a failure of the LH MLG drag brace attach fittings located on the outboard casting. The strut housing assembly will be shipped to the united states air force research laboratory at wright-patterson afb for analysis. An FAA malfunction or defect report, FAA form 8010-4 has been submitted to AFS-640.

As the FAA filed it

(-23) ON APRIL 14, 2003, AT APPROXIMATELY 1335 CDT, PIPER PA-28-161, N83416, EXPERIENCED A FAILURE OF THE LH MLG STRUT DURING LANDING ROLLOUT ON RUNWAY 16 AT THE PLATTSMOUTH, NEBRASKA MUNICIPAL AIRPORT. THE AIRCRAFT, OWNED AND OPERATED BY THE LEMAY FLIGHT TRAINING CENTER, SUSTAINED MINOR DAMAGE, WITH NO INJURY REPORTING BY THE CREWMEMBERS. SUBSEQUENT INVESTIGATION DISCLOSED A FAILURE OF THE LH MLG DRAG BRACE ATTACH FITTINGS LOCATED ON THE OUTBOARD CASTING. THE STRUT HOUSING ASSEMBLY WILL BE SHIPPED TO THE UNITED STATES AIR FORCE RESEARCH LABORATORY AT WRIGHT-PATTERSON AFB FOR ANALYSIS. AN FAA MALFUNCTION OR DEFECT REPORT, FAA FORM 8010-4 HAS BEEN SUBMITTED TO AFS-640.