20010804024069I

Incident · Minor damage

FAA incident report · Piper PA-32RT-300 · Abilene, TX · August 4, 2001

Date
August 4, 2001 · 23:37 local
Place
Abilene, TX
Airport
Abilene Regional Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N39540
Reported as
Piper PA32RT300
People aboard
6
Fatal injuries
0
Pilot’s flight hours
20,000 total200 in this make and model35 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) Pilot over rotated during a night takeoff, stalled and settled back hard on the left main gear and tail. One arm of the left main landing gear casting fractured and the tail cone was deformed and damaged. The pilot had loaded the aircraft to 100 pounds below gross weight, topping the left wing fuel tank and partially filling the right wing fuel tank to manage weight and balance. He knew he was heavy so he used a faster airspeed for rotation. When he made the rotation he put too much elevator input into the maneuver, plus the center of gravity (CG) was in the aft portion of the envelope. The pilot, 58 inches tall, had difficulty seeing over the instrument panel in the darkness and the vertical adjustment of the seat was inoperative, so the seat was in the full down position.

As the FAA filed it

(-23) PILOT OVER ROTATED DURING A NIGHT TAKEOFF, STALLED AND SETTLED BACK HARD ON THE LEFT MAIN GEAR AND TAIL. ONE ARM OF THE LEFT MAIN LANDING GEAR CASTING FRACTURED AND THE TAIL CONE WAS DEFORMED AND DAMAGED. THE PILOT HAD LOADED THE AIRCRAFT TO 100 POUNDS BELOW GROSS WEIGHT, TOPPING THE LEFT WING FUEL TANK AND PARTIALLY FILLING THE RIGHT WING FUEL TANK TO MANAGE WEIGHT AND BALANCE. HE KNEW HE WAS HEAVY SO HE USED A FASTER AIRSPEED FOR ROTATION. WHEN HE MADE THE ROTATION HE PUT TOO MUCH ELEVATOR INPUT INTO THE MANEUVER, PLUS THE CENTER OF GRAVITY (CG) WAS IN THE AFT PORTION OF THE ENVELOPE. THE PILOT, 58 INCHES TALL, HAD DIFFICULTY SEEING OVER THE INSTRUMENT PANEL IN THE DARKNESS AND THE VERTICAL ADJUSTMENT OF THE SEAT WAS INOPERATIVE, SO THE SEAT WAS IN THE FULL DOWN POSITION.