19970817022609A

Accident · Substantial damage

FAA accident report · Piper PA-32R-301 · Jefferson City, MO · August 17, 1997

Date
August 17, 1997 · 19:09 local
Place
Jefferson City, MO
Airport
Jefferson City Memorial
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8147B
NTSB investigation
NTSBCHI97LA262
Reported as
Piper PA32R301
Reported engine
Lycoming IO540K1G5
People aboard
1
Fatal injuries
0
Pilot’s flight hours
5,235 total7 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.

Premature liftoff behind power curve. Settled stall mushed to impact. Helicopter pilot. Minimum fixed wing time. (.4)the pilot said that they had just taken off and were 'approximately 20 to 25 feet in the air when the engine RPM dropped from 2,700 to 400.' As the airspeed decreased, the airplane began to roll to the left. The pilot said that he kept the nose of the airplane up, and leveled the wings. 'As the airplane began to settle, the RPM zoomed to 700. The airplane touched down and then bounced back into the air.' The airplane was about 20 feet above the ground when the RPM dropped to zero and the left wing dropped again. The pilot again leveled the wings. By this time the airplane was left of the runway. The pilot decided to land in the dirt along-side the runway. 'The airplane touched down hard and then slid for a short distance.' The passenger in the right front seat said that after a short takeoff roll, the airplane got airborne, came down, bounced back in the air, and then came down very fast hitting left wing first. The passenger in the right rear sea t said that it was loud when they took off and that the airplane was vibrating and seemed very rough. Exmination of the airplane's stabilizer trim showed an almost full nose up trim setting. The rudder trim was set at full nose left. No other anomalies were revealed with the airplane.

As the FAA filed it

PREMATURE LIFTOFF BEHIND POWER CURVE. SETTLED STALL MUSHED TO IMPACT. HELICOPTER PILOT. MINIMUM FIXED WING TIME. (.4)THE PILOT SAID THAT THEY HAD JUST TAKEN OFF AND WERE 'APPROXIMATELY 20 TO 25 FEET IN THE AIR WHEN THE ENGINE RPM DROPPED FROM 2,700 TO 400.' AS THE AIRSPEED DECREASED, THE AIRPLANE BEGAN TO ROLL TO THE LEFT. THE PILOT SAID THAT HE KEPT THE NOSE OF THE AIRPLANE UP, AND LEVELED THE WINGS. 'AS THE AIRPLANE BEGAN TO SETTLE, THE RPM ZOOMED TO 700. THE AIRPLANE TOUCHED DOWN AND THEN BOUNCED BACK INTO THE AIR.' THE AIRPLANE WAS ABOUT 20 FEET ABOVE THE GROUND WHEN THE RPM DROPPED TO ZERO AND THE LEFT WING DROPPED AGAIN. THE PILOT AGAIN LEVELED THE WINGS. BY THIS TIME THE AIRPLANE WAS LEFT OF THE RUNWAY. THE PILOT DECIDED TO LAND IN THE DIRT ALONG-SIDE THE RUNWAY. 'THE AIRPLANE TOUCHED DOWN HARD AND THEN SLID FOR A SHORT DISTANCE.' THE PASSENGER IN THE RIGHT FRONT SEAT SAID THAT AFTER A SHORT TAKEOFF ROLL, THE AIRPLANE GOT AIRBORNE, CAME DOWN, BOUNCED BACK IN THE AIR, AND THEN CAME DOWN VERY FAST HITTING LEFT WING FIRST. THE PASSENGER IN THE RIGHT REAR SEA T SAID THAT IT WAS LOUD WHEN THEY TOOK OFF AND THAT THE AIRPLANE WAS VIBRATING AND SEEMED VERY ROUGH. EXMINATION OF THE AIRPLANE'S STABILIZER TRIM SHOWED AN ALMOST FULL NOSE UP TRIM SETTING. THE RUDDER TRIM WAS SET AT FULL NOSE LEFT. NO OTHER ANOMALIES WERE REVEALED WITH THE AIRPLANE.

NTSB investigation

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