20000126036069A

Accident · Substantial damage

FAA accident report · Piper PA-28-181 · Key Largo, FL · January 26, 2000

Date
January 26, 2000 · 09:50 local
Place
Key Largo, FL
Airport
Ocean Reef Club Airport
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9578C
NTSB investigation
NTSBMIA00LA075
Reported as
Piper PA28181
Reported engine
Lycoming O360A4M
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,650 total20 in this make and model4 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.

(.4)The pilot stated that while on the downwind leg of the traffic pattern to land, he was advised that the wind was from 330 degrees with gusts to 18 knots. The flight continued and while either on base or final approach, he heard the flightcrew of a falcon airplane announce that the flight was 10 miles out, inbound. The pilot of the accident airplane landed uneventfully and while back taxiing on the runway at a reported speed of 4-5 mph, the airplane turned to the left. He applied right aileron but the airplane traveled off the runway and collided with hedges. Examination of the runway by an FAA inspector revealed continuous skid marks measuring 45 feet in length from both main landing gear to the point where the airplane exited the runway. The skid marks begin before a 10 foot by 12 foot discolored portion of the runway. Following temporary repairs to the airplane, it was flown to where it was based and no discrepancies pertaining to the brakes were noted by the pilot; the brakes were not worked on following the accident. Additionally, examination of the fractured nose steering components revealed no evidence of preimpact failure or malfunction.

As the FAA filed it

(.4)THE PILOT STATED THAT WHILE ON THE DOWNWIND LEG OF THE TRAFFIC PATTERN TO LAND, HE WAS ADVISED THAT THE WIND WAS FROM 330 DEGREES WITH GUSTS TO 18 KNOTS. THE FLIGHT CONTINUED AND WHILE EITHER ON BASE OR FINAL APPROACH, HE HEARD THE FLIGHTCREW OF A FALCON AIRPLANE ANNOUNCE THAT THE FLIGHT WAS 10 MILES OUT, INBOUND. THE PILOT OF THE ACCIDENT AIRPLANE LANDED UNEVENTFULLY AND WHILE BACK TAXIING ON THE RUNWAY AT A REPORTED SPEED OF 4-5 MPH, THE AIRPLANE TURNED TO THE LEFT. HE APPLIED RIGHT AILERON BUT THE AIRPLANE TRAVELED OFF THE RUNWAY AND COLLIDED WITH HEDGES. EXAMINATION OF THE RUNWAY BY AN FAA INSPECTOR REVEALED CONTINUOUS SKID MARKS MEASURING 45 FEET IN LENGTH FROM BOTH MAIN LANDING GEAR TO THE POINT WHERE THE AIRPLANE EXITED THE RUNWAY. THE SKID MARKS BEGIN BEFORE A 10 FOOT BY 12 FOOT DISCOLORED PORTION OF THE RUNWAY. FOLLOWING TEMPORARY REPAIRS TO THE AIRPLANE, IT WAS FLOWN TO WHERE IT WAS BASED AND NO DISCREPANCIES PERTAINING TO THE BRAKES WERE NOTED BY THE PILOT; THE BRAKES WERE NOT WORKED ON FOLLOWING THE ACCIDENT. ADDITIONALLY, EXAMINATION OF THE FRACTURED NOSE STEERING COMPONENTS REVEALED NO EVIDENCE OF PREIMPACT FAILURE OR MALFUNCTION.

NTSB investigation

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

Other reports on N9578C · 2

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