Stall / Spin · NTSB CEN09LA331

GENTRY JOHN K CHINOOK PL — Bridgeport, TX

1 fatal High-time pilotLow altitude
DateMay 29, 2009
LocationBridgeport, TX
AircraftGENTRY JOHN K CHINOOK PL
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceManeuvering Aerodynamic stall/spin
Pilot age76
Pilot total time2,125 hrs · Experienced
Time in typeUnknown
Fatalities1, 1 serious

Probable cause

The flight instructor and pilot's decision to take off with known control deficiencies with the aircraft which resulted in a loss of control.

NTSB findings

  • Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C

What happened

The flight instructor said that when he arrived at the private pilot's private airstrip they both conducted a preflight inspection of the ultralight airplane. The instructor then proceeded to taxi up and down the runway before he departed on a short solo flight. During this flight, he performed basic turns and discovered that when a small amount of aileron input was applied he needed to apply a much larger input of rudder to maintain coordinated flight. After landing, the instructor informed the private pilot about the rudder/aileron relationship and that it would be too noisy for him to provide any instruction. The private pilot, who had never flown the ultralight before, still wanted to fly it around the airstrip and asked the instructor to go with him. The instructor agreed and they departed. The instructor said that when they were on downwind, the private pilot turned around and said something, but that he was unable to hear what the pilot said and that he then immediately saw a tree. Two witnesses reported seeing the airplane make a sharp left bank and nose over. One of the witnesses said the engine was running at the time. Examination of the ultralight revealed that it had sustained substantial damage to the airframe, wings and tail section. The fuel in the fuel tank had a foul odor, but the reason for the foul odor was not determined.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →