What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On July 21, 2001, at 1215 central daylight time, a Cessna T210N airplane, N6114A, was substantially damaged during landing at the Amarillo International Airport near Amarillo, Texas. The airplane was registered to and operated by the pilot. The private pilot, and sole occupant, was not injured. Visual meteorological conditons prevailed, and no flight plan was filed for the 14 CFR part 91 personal flight. Preliminary information indicates the pilot put the landing gear control switch to the down position. The nose landing gear extended, but the main landing gear did not extend. As the airplane was touching down on runway 22, the gear warning horn sounded. After touch down, the left wing dropped and struck the runway damaging the wing tip, left horizontal stabilizer and elavator. Subsequent inspection revealed a tripped gear motor circuit breaker; however, the main gear was capable of manual extension. (.4) on July 21, 2001, at 1215 central daylight time, a Cessna T210N single-engine airplane, N6114A, was substantially damaged during landing at the Amarillo International Airport near Amarillo, Texas. The airplane was regist ered to and operated by the pilot. The private pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the 14 code of federal regulations part 91 personal flight. The flight originated from sugar land, Texas, at 0900. According to the pilot, he put the landing gear control switch to the down position when he was 5 miles from landing. Prior to turning final, he "verified" that the gear was extended by looking out the window and into the mirror under the right wing. As the airplane was touching down on runway 22, the gear warning horn sounded. After touchdown, the main landing gear collapsed, and the nose landing gear remained extended. When the "wings lost lift," the airplane tilted to the left, the left wing struck the runway, and the airplane turned 90 degrees and exited the runway. The pilot stated in the recommendation (how could this accident have been prevented) section of the pilot/operator aircraft accident report, NTSB form 6120.1/2, that the accident could have been prevented by better training for the pilot on the failure of the gear to extend and lock, and practice of manual gear extension. An examination of the airplane by the FAA inspector, who responded to the accident site, revealed that the left wing tip, left horizontal stabilizer and left elevator were damaged. A subsequent examination of the cockpit revealed "a tripped [landing] gear motor circuit breaker." The circuit breaker was reset, and the gear was successfully pumped down by hand using the emergency gear extension mechanism.
As the FAA filed it
(-23) ON JULY 21, 2001, AT 1215 CENTRAL DAYLIGHT TIME, A CESSNA T210N AIRPLANE, N6114A, WAS SUBSTANTIALLY DAMAGED DURING LANDING AT THE AMARILLO INTERNATIONAL AIRPORT NEAR AMARILLO, TEXAS. THE AIRPLANE WAS REGISTERED TO AND OPERATED BY THE PILOT. THE PRIVATE PILOT, AND SOLE OCCUPANT, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITONS PREVAILED, AND NO FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 91 PERSONAL FLIGHT. PRELIMINARY INFORMATION INDICATES THE PILOT PUT THE LANDING GEAR CONTROL SWITCH TO THE DOWN POSITION. THE NOSE LANDING GEAR EXTENDED, BUT THE MAIN LANDING GEAR DID NOT EXTEND. AS THE AIRPLANE WAS TOUCHING DOWN ON RUNWAY 22, THE GEAR WARNING HORN SOUNDED. AFTER TOUCH DOWN, THE LEFT WING DROPPED AND STRUCK THE RUNWAY DAMAGING THE WING TIP, LEFT HORIZONTAL STABILIZER AND ELAVATOR. SUBSEQUENT INSPECTION REVEALED A TRIPPED GEAR MOTOR CIRCUIT BREAKER; HOWEVER, THE MAIN GEAR WAS CAPABLE OF MANUAL EXTENSION. (.4) ON JULY 21, 2001, AT 1215 CENTRAL DAYLIGHT TIME, A CESSNA T210N SINGLE-ENGINE AIRPLANE, N6114A, WAS SUBSTANTIALLY DAMAGED DURING LANDING AT THE AMARILLO INTERNATIONAL AIRPORT NEAR AMARILLO, TEXAS. THE AIRPLANE WAS REGIST ERED TO AND OPERATED BY THE PILOT. THE PRIVATE PILOT, SOLE OCCUPANT OF THE AIRPLANE, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED FOR THE 14 CODE OF FEDERAL REGULATIONS PART 91 PERSONAL FLIGHT. THE FLIGHT ORIGINATED FROM SUGAR LAND, TEXAS, AT 0900. ACCORDING TO THE PILOT, HE PUT THE LANDING GEAR CONTROL SWITCH TO THE DOWN POSITION WHEN HE WAS 5 MILES FROM LANDING. PRIOR TO TURNING FINAL, HE "VERIFIED" THAT THE GEAR WAS EXTENDED BY LOOKING OUT THE WINDOW AND INTO THE MIRROR UNDER THE RIGHT WING. AS THE AIRPLANE WAS TOUCHING DOWN ON RUNWAY 22, THE GEAR WARNING HORN SOUNDED. AFTER TOUCHDOWN, THE MAIN LANDING GEAR COLLAPSED, AND THE NOSE LANDING GEAR REMAINED EXTENDED. WHEN THE "WINGS LOST LIFT," THE AIRPLANE TILTED TO THE LEFT, THE LEFT WING STRUCK THE RUNWAY, AND THE AIRPLANE TURNED 90 DEGREES AND EXITED THE RUNWAY. THE PILOT STATED IN THE RECOMMENDATION (HOW COULD THIS ACCIDENT HAVE BEEN PREVENTED) SECTION OF THE PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT, NTSB FORM 6120.1/2, THAT THE ACCIDENT COULD HAVE BEEN PREVENTED BY BETTER TRAINING FOR THE PILOT ON THE FAILURE OF THE GEAR TO EXTEND AND LOCK, AND PRACTICE OF MANUAL GEAR EXTENSION. AN EXAMINATION OF THE AIRPLANE BY THE FAA INSPECTOR, WHO RESPONDED TO THE ACCIDENT SITE, REVEALED THAT THE LEFT WING TIP, LEFT HORIZONTAL STABILIZER AND LEFT ELEVATOR WERE DAMAGED. A SUBSEQUENT EXAMINATION OF THE COCKPIT REVEALED "A TRIPPED [LANDING] GEAR MOTOR CIRCUIT BREAKER." THE CIRCUIT BREAKER WAS RESET, AND THE GEAR WAS SUCCESSFULLY PUMPED DOWN BY HAND USING THE EMERGENCY GEAR EXTENSION MECHANISM.
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 N6114A · 1
Matched to the same aircraft by N-number and date.