19970913026479A

Accident · Destroyed

FAA accident report · Amtrth THORP T-18 · Wagoner, OK · September 13, 1997

Date
September 13, 1997 · 13:40 local
Place
Wagoner, OK
Airport
Wagoner Airstrip Airport
Phase of flight
In Traffic Pattern-Circling
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N16LE
NTSB investigation
NTSBFTW97LA346
Reported as
Amtrth THORPT18
People aboard
1
Fatal injuries
1
Pilot’s flight hours
2,450 total

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.

Entered accelerated stall in steep bank to realign with runway. Type has relatively high stalling speed. Hit lake. (.19) on September 13, 1997, at 1340 central daylight time, a reilly thorp T-18 experimental airplane, N16LE, registered to the pilot (builder of the airplane), impacted a shallow lake following a loss of control during approach for landing at Wagoner Airstrip, Wagoner, Oklahoma. The private pilot was fatally injured, and the pilot-rated passenger sustained serious injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the title 14 CFR part 91 demonstration flight. The flight, which originated from Wagoner Airstrip at 1300, was intended for the owner/pilot to demonstrate the aircraft to the passenger who was a potential buyer. Several witnesses observed the airplane in a left traffic pattern on the base leg for runway 17. The witnesses then observed the airplane in a left traffic pattern on the base leg for runway 17. The witnesses then observed the airplane make a "very steep" left turn toward the runway. During the turn, the airplane's left wing "seemed to drop dramatically," and the airplane quickly lost altitude. Subsequently , the airplane descended uncontrolled into a lake, located southeast of the approach end of runway 17. During recovery the right wing was found separated from the fuselage. The instrument panel buckled downward, and the underside of the fuselage was extensively damaged. (.4) after about 40 minutes of local flight, the airplane entered into a left downwind for runway 17. Reported winds were from 130 at 10 knots. Several witnesses observed the airplane in a left traffic pattern on the base leg for runway 17. One of the witnesses, who was a pilot, stated that he observed the airplane 'overshoot' the runway on base leg, saw the left wing go 'down', and then saw the airplane 'stall.' The other witness observed the airplane make a 'very steep' left turn toward the runway, heard the engine 'power up' during the turn, and then saw the airplane's left wing 'drop dramatically.' Subsequently, the airplane descended uncontrolled into a lake, located southeast of the approach end of runway 17. A stall strip was not found installed on the aircraft. (-23) on September 13, 1997, at approximately 1:40 p.m. central standard daylight saving time, N16LE, an amateur built model thorp T18, aircraft was destroyed when it collided with the water at fort gibson lake while attempting to land at Wagoner Airstrip, Wagoner, OK. The airplane was owned by Mr. Leland reilly and was on a demonstration flight flown by the potential buyer/pilot. Visual meteorological conditions prevailed throughout the area. The owner/co-pilot received fatal injuries, the pilot received serious injuries. The flight originated and was to have terminated at Wagoner Airstrip, after a left downwind for runway 17, N16LE, turned left base, while turning final the pilot realized he had overshot final and continued to steepen the turn, until the aircraft stalled and crashed in the water.

As the FAA filed it

ENTERED ACCELERATED STALL IN STEEP BANK TO REALIGN WITH RUNWAY. TYPE HAS RELATIVELY HIGH STALLING SPEED. HIT LAKE. (.19) ON SEPTEMBER 13, 1997, AT 1340 CENTRAL DAYLIGHT TIME, A REILLY THORP T-18 EXPERIMENTAL AIRPLANE, N16LE, REGISTERED TO THE PILOT (BUILDER OF THE AIRPLANE), IMPACTED A SHALLOW LAKE FOLLOWING A LOSS OF CONTROL DURING APPROACH FOR LANDING AT WAGONER AIRSTRIP, WAGONER, OKLAHOMA. THE PRIVATE PILOT WAS FATALLY INJURED, AND THE PILOT-RATED PASSENGER SUSTAINED SERIOUS INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED FOR THE TITLE 14 CFR PART 91 DEMONSTRATION FLIGHT. THE FLIGHT, WHICH ORIGINATED FROM WAGONER AIRSTRIP AT 1300, WAS INTENDED FOR THE OWNER/PILOT TO DEMONSTRATE THE AIRCRAFT TO THE PASSENGER WHO WAS A POTENTIAL BUYER. SEVERAL WITNESSES OBSERVED THE AIRPLANE IN A LEFT TRAFFIC PATTERN ON THE BASE LEG FOR RUNWAY 17. THE WITNESSES THEN OBSERVED THE AIRPLANE IN A LEFT TRAFFIC PATTERN ON THE BASE LEG FOR RUNWAY 17. THE WITNESSES THEN OBSERVED THE AIRPLANE MAKE A "VERY STEEP" LEFT TURN TOWARD THE RUNWAY. DURING THE TURN, THE AIRPLANE'S LEFT WING "SEEMED TO DROP DRAMATICALLY," AND THE AIRPLANE QUICKLY LOST ALTITUDE. SUBSEQUENTLY , THE AIRPLANE DESCENDED UNCONTROLLED INTO A LAKE, LOCATED SOUTHEAST OF THE APPROACH END OF RUNWAY 17. DURING RECOVERY THE RIGHT WING WAS FOUND SEPARATED FROM THE FUSELAGE. THE INSTRUMENT PANEL BUCKLED DOWNWARD, AND THE UNDERSIDE OF THE FUSELAGE WAS EXTENSIVELY DAMAGED. (.4) AFTER ABOUT 40 MINUTES OF LOCAL FLIGHT, THE AIRPLANE ENTERED INTO A LEFT DOWNWIND FOR RUNWAY 17. REPORTED WINDS WERE FROM 130 AT 10 KNOTS. SEVERAL WITNESSES OBSERVED THE AIRPLANE IN A LEFT TRAFFIC PATTERN ON THE BASE LEG FOR RUNWAY 17. ONE OF THE WITNESSES, WHO WAS A PILOT, STATED THAT HE OBSERVED THE AIRPLANE 'OVERSHOOT' THE RUNWAY ON BASE LEG, SAW THE LEFT WING GO 'DOWN', AND THEN SAW THE AIRPLANE 'STALL.' THE OTHER WITNESS OBSERVED THE AIRPLANE MAKE A 'VERY STEEP' LEFT TURN TOWARD THE RUNWAY, HEARD THE ENGINE 'POWER UP' DURING THE TURN, AND THEN SAW THE AIRPLANE'S LEFT WING 'DROP DRAMATICALLY.' SUBSEQUENTLY, THE AIRPLANE DESCENDED UNCONTROLLED INTO A LAKE, LOCATED SOUTHEAST OF THE APPROACH END OF RUNWAY 17. A STALL STRIP WAS NOT FOUND INSTALLED ON THE AIRCRAFT. (-23) ON SEPTEMBER 13, 1997, AT APPROXIMATELY 1:40 P.M. CENTRAL STANDARD DAYLIGHT SAVING TIME, N16LE, AN AMATEUR BUILT MODEL THORP T18, AIRCRAFT WAS DESTROYED WHEN IT COLLIDED WITH THE WATER AT FORT GIBSON LAKE WHILE ATTEMPTING TO LAND AT WAGONER AIRSTRIP, WAGONER, OK. THE AIRPLANE WAS OWNED BY MR. LELAND REILLY AND WAS ON A DEMONSTRATION FLIGHT FLOWN BY THE POTENTIAL BUYER/PILOT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED THROUGHOUT THE AREA. THE OWNER/CO-PILOT RECEIVED FATAL INJURIES, THE PILOT RECEIVED SERIOUS INJURIES. THE FLIGHT ORIGINATED AND WAS TO HAVE TERMINATED AT WAGONER AIRSTRIP, AFTER A LEFT DOWNWIND FOR RUNWAY 17, N16LE, TURNED LEFT BASE, WHILE TURNING FINAL THE PILOT REALIZED HE HAD OVERSHOT FINAL AND CONTINUED TO STEEPEN THE TURN, UNTIL THE AIRCRAFT STALLED AND CRASHED IN THE WATER.

NTSB investigation

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