- Date
- December 6, 1998, 12:00 local (17:00 UTC)
- Place
- Garner, VA
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N31253Univair 7GC-AA
- Weather
- Visual (VMC) · Day
- Status
- Completed · report December 1, 1999
- Report
- Approved by Office Director
- FAA report
- 19981206032779A
- Case key
- 45472
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
A jammed right wheel for undetermined reasons.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
After releasing a glider, the pilot preformed a left spiral to lose altitude, and entered the traffic pattern. After completing the downwind and base legs of the traffic pattern, the pilot established the airplane on an offset final for the runway. The airplane touched down on the first 1/3 of the runway and started to roll out. During rollout, the pilot 'tapped' the brakes and felt the airplane pull to the right. The pilot then 'tapped' the left brake and the airplane straightened out, but when the left brake pressure was removed the airplane once again turned to the right. Because of a right crosswind, the pilot thought the right turn was the airplane trying to weathervane, so he added full left rudder, which had no effect. With full left rudder, the tailwheel off the ground, and approximately 35 mph of airspeed, the pilot reapplied the left brake. When the left brake was applied, the airplane stopped abruptly and nosed over. After the accident, while the airplane was still inverted maintenance personnel had difficulty rotating the right tire by hand, but once it started to rotate, it did so freely. There were no mechanical failures with the right wheel assembly.
Factual narrative
On December 6, 1998, about 1200 eastern standard time, a Univair 7GC-AA, N31253, was substantially damage while landing at a private airstrip near Garner, Virginia. The certificated airline transport pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the glider tow conducted under 14 CFR Part 91.
The pilot stated that the purpose of the flight was to tow a glider to 3,000 feet above mean sea level (MSL), release it, and return. Prior to the accident flight the pilot conducted two similar flights and noticed no mechanical problems with the airplane. On the accident flight, the pilot towed a glider to 3,000 feet MSL, released the glider, preformed a left spiral to lose altitude, and entered the traffic pattern via a left crosswind. The pilot then completed the downwind and base legs of the traffic pattern, before establishing the airplane on an offset final for runway 20. The pilot flew an offset final because of the tow rope and a small building on the approach end of runway.
The airplane touched down on the first 1/3 of the runway and started to rollout. While the airplane was rolling out, the pilot "tapped" the brakes and felt the airplane pull to the right. The pilot then "tapped" the left brake and the airplane straightened out, but when the left brake pressure was removed the airplane once again turned to the right. Because of a right crosswind, the pilot thought the right turn was the airplane trying to weathervane, so he added full left rudder, which had no effect. With full left rudder, the tailwheel off the ground, and approximately 35 mph of airspeed, the pilot reapplied the left brake. When the left brake was applied, the airplane stopped abruptly and nosed over.
The pilot stated that the runway was approximately 2,500 feet long and orientated on a magnetic heading of 200 degrees. He added that the winds were out of the southwest at 8 to 10 knots, and "weather was not a factor in the accident."
After the accident, while the airplane was still inverted maintenance personnel had difficulty rotating the right tire by hand, but once it started to rotate, it did so freely.
A Federal Aviation Administration Airworthiness Inspector examined the right wheel assembly and found no anomalies.
Aircraft
- Registration
- N31253
- Reported as
- Univair 7GC-AA
- Category
- Airplane
- Serial number
- 250-72
- Airframe hours
- 4,193
- Engine
- Lycoming O-320, 150 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Tidewater Soaring Society
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · March 5, 1998 · 60 hours before
- Departed
- NONE
- Airport
- NONE · Garner Field, runway 20, 2,500 × 75 ft, grass/turf
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 60
- Certificates
- Flight engineer, Airline transport, Flight instructor, Commercial
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 1, Valid Medical--w/ waivers/lim
- Seat
- Front
- Flight hours
- 24,538 total · 203 in this make and model · 20,050 as pilot in command · 1,893 in the last 90 days · 22 in the last 30 days · 1 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 279° at 10 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 75 °F, dew point 63 °F
- Altimeter
- 30.00 inHg
- Observed at
- ORF, 27 nm away
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.