What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.19) On April 6, 2001, at 1000 hours MST, a Cessna 210, N126RA, sustained substantial damage when it lost power and landed in a field near cordes junction, AZ. The airplane was operated under the provisions of CFR 14 part 91 by an airline transport pilot who, along with his one passenger, was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight, which originated from camarillo, CA., at 0800 PDT, and was enroute to payson, AZ. The pilot stated that he reduced power to descend from 11,500 feet to land at payson. When he reached approx. 7,000 feet he tried to increase power but the engine did not respond. He stated the engine continued to run at a reduced power as he tried switching fuel tanks. He originally intended to land on a highway but could not find a clear area due to traffic on the road. He elected to land in a field near the highway. The airplane sustained damage to the propeller, nose gear, left wing, and main gear. (-23)during descent pilot retarded throttle until he reached the necessary altitude at which time he advanced the throttle levers to maintain his alti tude. The pilot then noticed that the engine didn't respond. The pilot stated that he tried to switch fuel tanks, but he still had no response. He then tried to make an emergency landing on interstate 17. The pilot reported that he almost had traffic clear expect for one car, he then decided to make a landing in a field next to the interstate. During landing the aircraft sustained substantial damage with no injuries on board. During examination of the aircraft at the salvage yard it was noted that the throttle linkage was disconnected from the throttle body. (.4) on April 6, 2001, at 1020 hours mountain standard time, a Cessna 210B, N126RA, sustained substantial damage when it lost power and landed in a pasture near Camp Verde, Arizona. The airplane was operated under the provisions of 14 CFR part 91 by an airline transport pilot who, along with his one passenger, was not injured. Visual metrological conditions prevailed and no flight plan was filed for the personal flight, which originated from camarillo, California, at 0800 pacific daylight time, and was en route to payson, Arizona. The pilot stated that he reduced power to descend from 11,500 f eet to land at payson. When he reached approximately 7,000 feet he tried to increase power but the engine did not respond. He stated the engine continued to run at a reduced power as he pushed the mixture fully rich, turned the fuel boost pump to high, and switched fuel tanks. He originally intended to land on a highway but could not find a clear area due to traffic on the road. He elected to land in a field near the highway. Upon touchdown, the nose gear dug in. The airplane slid to a stop, sustaining damage to the propeller, nose gear, firewall, left wing, and main gear. A postaccident inspection by the pilot revealed that the throttle linkage disconnected, allowing the engine to go to idle power. This was confirmed by an federal aviation administration inspector.
As the FAA filed it
(.19) ON APRIL 6, 2001, AT 1000 HOURS MST, A CESSNA 210, N126RA, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT LOST POWER AND LANDED IN A FIELD NEAR CORDES JUNCTION, AZ. THE AIRPLANE WAS OPERATED UNDER THE PROVISIONS OF CFR 14 PART 91 BY AN AIRLINE TRANSPORT PILOT WHO, ALONG WITH HIS ONE PASSENGER, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED FOR THE PERSONAL FLIGHT, WHICH ORIGINATED FROM CAMARILLO, CA., AT 0800 PDT, AND WAS ENROUTE TO PAYSON, AZ. THE PILOT STATED THAT HE REDUCED POWER TO DESCEND FROM 11,500 FEET TO LAND AT PAYSON. WHEN HE REACHED APPROX. 7,000 FEET HE TRIED TO INCREASE POWER BUT THE ENGINE DID NOT RESPOND. HE STATED THE ENGINE CONTINUED TO RUN AT A REDUCED POWER AS HE TRIED SWITCHING FUEL TANKS. HE ORIGINALLY INTENDED TO LAND ON A HIGHWAY BUT COULD NOT FIND A CLEAR AREA DUE TO TRAFFIC ON THE ROAD. HE ELECTED TO LAND IN A FIELD NEAR THE HIGHWAY. THE AIRPLANE SUSTAINED DAMAGE TO THE PROPELLER, NOSE GEAR, LEFT WING, AND MAIN GEAR. (-23)DURING DESCENT PILOT RETARDED THROTTLE UNTIL HE REACHED THE NECESSARY ALTITUDE AT WHICH TIME HE ADVANCED THE THROTTLE LEVERS TO MAINTAIN HIS ALTI TUDE. THE PILOT THEN NOTICED THAT THE ENGINE DIDN'T RESPOND. THE PILOT STATED THAT HE TRIED TO SWITCH FUEL TANKS, BUT HE STILL HAD NO RESPONSE. HE THEN TRIED TO MAKE AN EMERGENCY LANDING ON INTERSTATE 17. THE PILOT REPORTED THAT HE ALMOST HAD TRAFFIC CLEAR EXPECT FOR ONE CAR, HE THEN DECIDED TO MAKE A LANDING IN A FIELD NEXT TO THE INTERSTATE. DURING LANDING THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE WITH NO INJURIES ON BOARD. DURING EXAMINATION OF THE AIRCRAFT AT THE SALVAGE YARD IT WAS NOTED THAT THE THROTTLE LINKAGE WAS DISCONNECTED FROM THE THROTTLE BODY. (.4) ON APRIL 6, 2001, AT 1020 HOURS MOUNTAIN STANDARD TIME, A CESSNA 210B, N126RA, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT LOST POWER AND LANDED IN A PASTURE NEAR CAMP VERDE, ARIZONA. THE AIRPLANE WAS OPERATED UNDER THE PROVISIONS OF 14 CFR PART 91 BY AN AIRLINE TRANSPORT PILOT WHO, ALONG WITH HIS ONE PASSENGER, WAS NOT INJURED. VISUAL METROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED FOR THE PERSONAL FLIGHT, WHICH ORIGINATED FROM CAMARILLO, CALIFORNIA, AT 0800 PACIFIC DAYLIGHT TIME, AND WAS EN ROUTE TO PAYSON, ARIZONA. THE PILOT STATED THAT HE REDUCED POWER TO DESCEND FROM 11,500 F EET TO LAND AT PAYSON. WHEN HE REACHED APPROXIMATELY 7,000 FEET HE TRIED TO INCREASE POWER BUT THE ENGINE DID NOT RESPOND. HE STATED THE ENGINE CONTINUED TO RUN AT A REDUCED POWER AS HE PUSHED THE MIXTURE FULLY RICH, TURNED THE FUEL BOOST PUMP TO HIGH, AND SWITCHED FUEL TANKS. HE ORIGINALLY INTENDED TO LAND ON A HIGHWAY BUT COULD NOT FIND A CLEAR AREA DUE TO TRAFFIC ON THE ROAD. HE ELECTED TO LAND IN A FIELD NEAR THE HIGHWAY. UPON TOUCHDOWN, THE NOSE GEAR DUG IN. THE AIRPLANE SLID TO A STOP, SUSTAINING DAMAGE TO THE PROPELLER, NOSE GEAR, FIREWALL, LEFT WING, AND MAIN GEAR. A POSTACCIDENT INSPECTION BY THE PILOT REVEALED THAT THE THROTTLE LINKAGE DISCONNECTED, ALLOWING THE ENGINE TO GO TO IDLE POWER. THIS WAS CONFIRMED BY AN FEDERAL AVIATION ADMINISTRATION INSPECTOR.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N126RA · 1
Matched to the same aircraft by N-number and date.