20010629039899A

Accident · Substantial damage

FAA accident report · Piper PA18A150 · Palmer, AK · June 29, 2001

Date
June 29, 2001 · 13:50 local
Place
Palmer, AK
Airport
Palmer Municipal Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6881B
NTSB investigation
NTSBANC01LA078
Reported as
Piper PA18A150
Reported engine
Lycoming IO320*
Fatal injuries
0
Pilot’s flight hours
120 total65 in this make and model14 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) Departure was from a private airstrip. Windsock indicated wind to be about 8 knots from the south. Shortly after takeoff the engine started running rough and lost power. Pilot stated he decided to return to the strip rather than go into the trees at the end. Aircraft impacted the surface and sustained substantial damage. Right wing was separated from the fuselage. Both fuel tanks were intact. Left tank was about 2/3 full and right tank had drained down due to separation. Fuel selector indicated right tank selection. Carburetor was broken from flange. Exhaust cone in place and intact. Fuel selector valve examined and found right port and outlet about 1/3 occluded. Plastic cone ears broken for counter clockwise rotation.

As the FAA filed it

(-23) DEPARTURE WAS FROM A PRIVATE AIRSTRIP. WINDSOCK INDICATED WIND TO BE ABOUT 8 KNOTS FROM THE SOUTH. SHORTLY AFTER TAKEOFF THE ENGINE STARTED RUNNING ROUGH AND LOST POWER. PILOT STATED HE DECIDED TO RETURN TO THE STRIP RATHER THAN GO INTO THE TREES AT THE END. AIRCRAFT IMPACTED THE SURFACE AND SUSTAINED SUBSTANTIAL DAMAGE. RIGHT WING WAS SEPARATED FROM THE FUSELAGE. BOTH FUEL TANKS WERE INTACT. LEFT TANK WAS ABOUT 2/3 FULL AND RIGHT TANK HAD DRAINED DOWN DUE TO SEPARATION. FUEL SELECTOR INDICATED RIGHT TANK SELECTION. CARBURETOR WAS BROKEN FROM FLANGE. EXHAUST CONE IN PLACE AND INTACT. FUEL SELECTOR VALVE EXAMINED AND FOUND RIGHT PORT AND OUTLET ABOUT 1/3 OCCLUDED. PLASTIC CONE EARS BROKEN FOR COUNTER CLOCKWISE ROTATION.

NTSB investigation

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