- Date
- July 22, 2017, 12:00 local (17:00 UTC)
- Place
- Denison, TX
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Takeoff
- Aircraft
- N91JGGilbert Thomas Jeffrey Lancair 235
- Defining event
- Takeoff: Loss of control on ground
- Weather
- Visual (VMC) · Day
- Status
- Completed · report October 31, 2017
- Report
- Approved by Office Director
- NTSB office
- General Aviation Accidents
- Parties
- FAA
- FAA report
- 20170722010719A
- Case key
- 95650
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The pilot’s failure to maintain directional control during the takeoff roll.
Findings · 3
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot of the experimental, amateur-built airplane reported that he was unfamiliar with the airplane and that, during a prepurchase flight, he was accompanied by an aircraft mechanic/pilot familiar with the airplane. The mechanic, seated in the right seat, instructed him to anticipate adding right rudder when increasing power during takeoff. During takeoff, the pilot applied right rudder; however, he reported that, once full power was applied, the airplane continued to veer to the left. The pilot added that he and the mechanic verbally communicated that they "both were applying right rudder and simultaneous aileron." The pilot then pulled the mixture control to shut off the engine; however, the airplane continued off the left side of the runway. The pilot heard a loud "pop," and the airplane then veered to the right, the landing gear collapsed, and the airplane came to rest off the right side of the runway. The airplane sustained substantial damage to the fuselage and rudder. The pilot reported that he believed a "mechanical" failure caused the airplane to not respond to inputs from the right rudder, right brake, and right aileron and that the left brake or bearing seized, causing enough friction to overcome the control inputs. The mechanic stated that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. According to the mechanic, the airplane was not equipped with rudder/brake pedals on the right side, and before the flight, the pilot had used the brakes effectively to taxi for takeoff. He further stated, "all brakes were in good shape, and everything was in good operational condition." The automated weather observation system on the airport reported that, about the time of the accident, the wind was from 190° at 7 knots. The pilot was departing on runway 17L.
Factual narrative
The pilot of the experimental amateur-built airplane reported that, he was unfamiliar with the airplane, and that during a pre-purchase flight, he was accompanied by an aircraft mechanic/pilot familiar with the airplane. The mechanic, seated in the right seat, instructed him to anticipate adding right rudder when increasing power during takeoff. During takeoff, the pilot applied right rudder; however, he reported that once full power was applied the airplane continued to veer to the left. The pilot added that, there was a verbal communication shared between the two pilots that they "both were applying right rudder and simultaneous aileron." The pilot then pulled the mixture control to shutoff the engine, however, the airplane continued off the left side of the runway, he heard a loud "pop," the airplane then veered to the right, the landing gear collapsed, and the airplane came to rest off the right side of the runway. The airplane sustained substantial damage to the fuselage and rudder. The pilot reported that he believed there was a "mechanical" failure, causing the airplane to not respond to inputs from the right rudder, right brake, and right aileron; and that the left brake or bearing seized causing enough friction to overcome the control inputs. According to the mechanic, the airplane was not equipped with rudder/brake pedals on the right side, and that prior to the flight the pilot had used the brakes effectively to taxi for takeoff. He further stated, "all brakes were in good shape, and everything was in good operational condition." The mechanic added that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation system on the accident airport reported, that about the time of the accident, the wind was 190° at 7 knots. The pilot was departing on runway 17L.
Aircraft
- Registration
- N91JG
- Reported as
- Gilbert Thomas Jeffrey Lancair 235 (NO SERIES)
- Category
- Airplane, amateur-built
- Serial number
- 090
- Built
- 1990
- Airframe hours
- 327
- Engine
- Lycoming O-235, 125 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Special, Experimental (Special)
- Departed
- GYI · Denison, TX
- Destination
- GYI · Denison, TX
- Airport
- GYI · North Texas Rgnl/Perrin Field, runway 17L, 9,000 × 150 ft, concrete
- Equipment
- Unknown
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew · 2
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 37
- Injuries
- None
- Certificates
- Commercial, Flight instructor
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, With waivers/limitations
- Last flight review
- February 1, 2017
- Seat
- Left
- Restraint
- 4-point
- Flight hours
- 2,405 total · 1,672 as pilot in command · 42 in the last 90 days · 21 in the last 30 days · 4 in the last 24 hours
- Role
- Check pilot
- Injuries
- None
- Certificates
- Flight instructor, Flight engineer, Airline transport
- Airplane ratings
- Single-engine land, Multi-engine land
- Medical
- Class 2
- Seat
- Right
- Restraint
- 4-point
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 190° at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 95 °F, dew point 72 °F
- Altimeter
- 29.95 inHg
- Observed at
- KGYI
Docket · 3
The files NTSB released with the investigation on October 3, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.9 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.