20000910013939A

Accident · Substantial damage

FAA accident report · Piper PA-28-180 · Payson, AZ · September 10, 2000

Date
September 10, 2000 · 13:30 local
Place
Payson, AZ
Airport
Payson Airport
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4208T
NTSB investigation
NTSBLAX00LA333
Reported as
Piper PA28180
Reported engine
Lycoming O360A3A
People aboard
4
Fatal injuries
0
Pilot’s flight hours
75 total27 in this make and model31 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) Airmand was departin pan,da of 7300 ffet, just under gross weight. According to the performance chart that he used (for a PA-28-161) he would have had a ground roll of 2000 feet. (Rwy is 5500") airman stated that at approx 50 mph the nose gear began to shimmy (after 1000' ground roll so FAR) at the same time directional control became difficult. He rotated at about this time and the tail struck the rwy. A/c became airborne to approx 10 feet and went immediately left, then right, striking heavy bushes to the right side of the runway shearing the right wing. A/c made a 180 degree turn and skidded backwards coming to a stop in a ravine off the right side of the runway. Pilot and 3 pax escaped uninjured. (.4) with three passengers and 30 gallons of fuel in the tanks, the pilot commenced the takeoff roll on a 5,500-foot-long runway, elevation 5,157 feet mean sea level. The density altitude was about 7,650 feet. As the airplane accelerated, it veered left and right, the nose pitched up, and the tail tie down ring scraped on the runway. Directional control was lost, and the airplane overran runway lights and came to rest upon colliding with a tree. The pilot reported that no mechanical malfunctions were experienced with his airplane during the flight. The pilot's total flying experience was 75.3 hours. He was issued a pilot certificate 17 days prior to the mishap.

As the FAA filed it

(-23) AIRMAND WAS DEPARTIN PAN,DA OF 7300 FFET, JUST UNDER GROSS WEIGHT. ACCORDING TO THE PERFORMANCE CHART THAT HE USED (FOR A PA-28-161) HE WOULD HAVE HAD A GROUND ROLL OF 2000 FEET. (RWY IS 5500") AIRMAN STATED THAT AT APPROX 50 MPH THE NOSE GEAR BEGAN TO SHIMMY (AFTER 1000' GROUND ROLL SO FAR) AT THE SAME TIME DIRECTIONAL CONTROL BECAME DIFFICULT. HE ROTATED AT ABOUT THIS TIME AND THE TAIL STRUCK THE RWY. A/C BECAME AIRBORNE TO APPROX 10 FEET AND WENT IMMEDIATELY LEFT, THEN RIGHT, STRIKING HEAVY BUSHES TO THE RIGHT SIDE OF THE RUNWAY SHEARING THE RIGHT WING. A/C MADE A 180 DEGREE TURN AND SKIDDED BACKWARDS COMING TO A STOP IN A RAVINE OFF THE RIGHT SIDE OF THE RUNWAY. PILOT AND 3 PAX ESCAPED UNINJURED. (.4) WITH THREE PASSENGERS AND 30 GALLONS OF FUEL IN THE TANKS, THE PILOT COMMENCED THE TAKEOFF ROLL ON A 5,500-FOOT-LONG RUNWAY, ELEVATION 5,157 FEET MEAN SEA LEVEL. THE DENSITY ALTITUDE WAS ABOUT 7,650 FEET. AS THE AIRPLANE ACCELERATED, IT VEERED LEFT AND RIGHT, THE NOSE PITCHED UP, AND THE TAIL TIE DOWN RING SCRAPED ON THE RUNWAY. DIRECTIONAL CONTROL WAS LOST, AND THE AIRPLANE OVERRAN RUNWAY LIGHTS AND CAME TO REST UPON COLLIDING WITH A TREE. THE PILOT REPORTED THAT NO MECHANICAL MALFUNCTIONS WERE EXPERIENCED WITH HIS AIRPLANE DURING THE FLIGHT. THE PILOT'S TOTAL FLYING EXPERIENCE WAS 75.3 HOURS. HE WAS ISSUED A PILOT CERTIFICATE 17 DAYS PRIOR TO THE MISHAP.

NTSB investigation

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