20100724047449A

Accident · Destroyed

FAA accident report · Nadig Paul NADIG · Sandy Creek Tow, PA · July 24, 2010

Date
July 24, 2010 · 11:20 local
Place
Sandy Creek Tow, PA
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N579PN
NTSB investigation
NTSBERA10LA373
Reported as
Nadig Paul Nadig
Reported engine
Bombardier ROTAX (ALL)
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
936 total0 in this make and model0 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.

On July 24, 2010 N579PN, a Nadig avid flyer (experimental) crashed near the intersection of the crosswind/downwind leg at venango regional airport. The temperature was 80.6 degrees f and the dew point was 73.4 degrees f. an investigation was performed whereas flight control continuity was established, a thumb compression test was performed and a detailed inspection of the wreckage revealed no anomalies. Witness statements gathered indicated previous mechanical issues with the engine. Modifications to the cooling system and ignition system may have resulted in the accident. Rotax has agreed under NTSB jurisdiction to run and test the engine. Results are pending.

As the FAA filed it

ON JULY 24, 2010 N579PN, A NADIG AVID FLYER (EXPERIMENTAL) CRASHED NEAR THE INTERSECTION OF THE CROSSWIND/DOWNWIND LEG AT VENANGO REGIONAL AIRPORT. THE TEMPERATURE WAS 80.6 DEGREES F AND THE DEW POINT WAS 73.4 DEGREES F. AN INVESTIGATION WAS PERFORMED WHEREAS FLIGHT CONTROL CONTINUITY WAS ESTABLISHED, A THUMB COMPRESSION TEST WAS PERFORMED AND A DETAILED INSPECTION OF THE WRECKAGE REVEALED NO ANOMALIES. WITNESS STATEMENTS GATHERED INDICATED PREVIOUS MECHANICAL ISSUES WITH THE ENGINE. MODIFICATIONS TO THE COOLING SYSTEM AND IGNITION SYSTEM MAY HAVE RESULTED IN THE ACCIDENT. ROTAX HAS AGREED UNDER NTSB JURISDICTION TO RUN AND TEST THE ENGINE. RESULTS ARE PENDING.

NTSB investigation

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