20091018020049A

Accident · Destroyed

FAA accident report · Cessna P210N · Rifle, CO · October 18, 2009

Date
October 18, 2009
Place
Rifle, CO
Airport
Garfield County Regional
Phase of flight
Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N7217S
NTSB investigation
NTSBCEN10FA021
Reported as
Cessna P210N
Reported engine
Allison 250B17F2
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
1,423 total169 in this make and model36 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.

Upon takeoff from Rifle, Colorado, an undiscovered issue with the engine caused it to operate only at max power of flight idle. Pilot decided to return to land at Rifle, CO. As pilot manuevered to land alternating between flight idle and max power to control engine RPM and allow his descent, after putting gear and flaps down he realized he was getting low, put max power in but got no response. Aircraft struck the ground hitting the tail first, then the main landing gear, followed by the nosewheel. The nosewheel then dug into the ground and the momentum caused the aircraft to flip over. Post impact examination of the engine showed a dislodged power cable pulled from the swedge area in the linkage. It is unknown whether this was caused by the impact or a causal factor in the accident. The NTSB has sent the parts out for further examination.

As the FAA filed it

UPON TAKEOFF FROM RIFLE, COLORADO, AN UNDISCOVERED ISSUE WITH THE ENGINE CAUSED IT TO OPERATE ONLY AT MAX POWER OF FLIGHT IDLE. PILOT DECIDED TO RETURN TO LAND AT RIFLE, CO. AS PILOT MANUEVERED TO LAND ALTERNATING BETWEEN FLIGHT IDLE AND MAX POWER TO CONTROL ENGINE RPM AND ALLOW HIS DESCENT, AFTER PUTTING GEAR AND FLAPS DOWN HE REALIZED HE WAS GETTING LOW, PUT MAX POWER IN BUT GOT NO RESPONSE. AIRCRAFT STRUCK THE GROUND HITTING THE TAIL FIRST, THEN THE MAIN LANDING GEAR, FOLLOWED BY THE NOSEWHEEL. THE NOSEWHEEL THEN DUG INTO THE GROUND AND THE MOMENTUM CAUSED THE AIRCRAFT TO FLIP OVER. POST IMPACT EXAMINATION OF THE ENGINE SHOWED A DISLODGED POWER CABLE PULLED FROM THE SWEDGE AREA IN THE LINKAGE. IT IS UNKNOWN WHETHER THIS WAS CAUSED BY THE IMPACT OR A CAUSAL FACTOR IN THE ACCIDENT. THE NTSB HAS SENT THE PARTS OUT FOR FURTHER EXAMINATION.

NTSB investigation

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