20050702015849A

Accident · Destroyed

FAA accident report · Piper PA-28-180 · Yuma, AZ · July 2, 2005

Date
July 2, 2005 · 11:30 local
Place
Yuma, AZ
Airport
Yuma Mcas - Yuma International
Phase of flight
Forced Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9254J
NTSB investigation
NTSBLAX05LA223
Reported as
Piper PA28180
Reported engine
Lycoming O360*
People aboard
4
Fatal injuries
0
Pilot’s flight hours
94 total94 in this make and model20 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) While on short final for landing, aircraft landed short of runway on airport access road and ran through closed gate in airport perimeter fence. Both wings completely severed from aircraft and nose gear partially collapsed rearward. Aircraft came to rest 3/4 inverted resting on left upper fuselage section. No injuries to pilot or passengers. Available information indicates aircraft was below max gross weight but substantially forward of allowable CG limit during entire flight. During aircraft recovery it was noted that fuel lines leading to gas collator contained fuel. Post accident engine test run was conducted with no anomalies or discrepancies in operation noted.

As the FAA filed it

(-23) WHILE ON SHORT FINAL FOR LANDING, AIRCRAFT LANDED SHORT OF RUNWAY ON AIRPORT ACCESS ROAD AND RAN THROUGH CLOSED GATE IN AIRPORT PERIMETER FENCE. BOTH WINGS COMPLETELY SEVERED FROM AIRCRAFT AND NOSE GEAR PARTIALLY COLLAPSED REARWARD. AIRCRAFT CAME TO REST 3/4 INVERTED RESTING ON LEFT UPPER FUSELAGE SECTION. NO INJURIES TO PILOT OR PASSENGERS. AVAILABLE INFORMATION INDICATES AIRCRAFT WAS BELOW MAX GROSS WEIGHT BUT SUBSTANTIALLY FORWARD OF ALLOWABLE CG LIMIT DURING ENTIRE FLIGHT. DURING AIRCRAFT RECOVERY IT WAS NOTED THAT FUEL LINES LEADING TO GAS COLLATOR CONTAINED FUEL. POST ACCIDENT ENGINE TEST RUN WAS CONDUCTED WITH NO ANOMALIES OR DISCREPANCIES IN OPERATION NOTED.

NTSB investigation

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