- Date
- August 2, 2016, 21:05 local (Aug 3, 2016, 05:05 UTC)
- Place
- North Pole, AK
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N8512QHolley Carol L Antares
- Defining event
- Landing: Loss of control on ground
- Weather
- Visual (VMC) · Day
- Status
- Completed · report December 5, 2016
- Report
- Approved by Office Director
- NTSB office
- Alaska Regional Office
- Parties
- FAA Fairbanks FSDO
- FAA report
- 20160802012939A
- Case key
- 93757
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 of the weight-shift control airplane during the landing in a crosswind condition, which resulted in a runway excursion, a tip over of the wing, and a collision with terrain.
Findings · 4
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 reported that while practicing stop-and-go landings with a crosswind condition, the tricycle-geared weight-shift control (WSC) airplane "weathervaned" to the right upon touchdown. In an attempt to correct for the weathervane, the pilot applied right pedal, the airplane departed the runway to the right, and tipped over coming to rest on the right leading edge of the wing. The airplane sustained substantial damage to the wing keel. A Federal Aviation Administration (FAA) aviation safety inspector who responded to the accident site reported that he observed no mechanical malfunctions or failures with airframe and engine that would have precluded normal operation and none was reported to him by the pilot. In the recommendation section of the National Transportation Safety Board Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if he had additional training that concentrated on ground handling and crosswind condition operations. The FAA has published the Weight-Shift Control Aircraft Flying Handbook FAA-H-8083-5 (2008). This handbook discusses crosswind landing procedures for WSC airplanes and states in part: When in final approach, the wind correction angle (crab angle) is established by heading toward the wind with the wings level so that the aircraft's ground track remains aligned with the centerline of the runway. This crab angle is maintained all the way to touchdown, when the rear wheels hit first and rotate the carriage and wing around so the front wheel touches the ground with the carriage going straight. However, if in turbulent air or pitched forward during the touchdown, with the front wheel touching the ground first, the pilot should lightly control the steering of the front wheel to be headed in the direction the carriage is going. WSC carriage front landing gear typically has camber that tends to steer the front wheel naturally in the direction of travel, so a light touch on the front wheel as it touches the ground allows it to find its own direction of travel. Once the front wheel is on the ground, lower the nose to keep the WSC on the ground and steer as required down the center of the runway. The procedure for the wing during the roundout is the same as that for normal and turbulent roundout and touchdowns. The exception is that after touchdown the windward wing should be lowered slightly so the wind cannot get under it to flip the WSC aircraft during later landing roll and taxi.
Factual narrative
The pilot reported that while practicing stop-and-go landings with a crosswind condition, the tricycle-geared weight-shift control (WSC) airplane "weathervaned" to the right upon touchdown. In an attempt to correct for the weathervane, the pilot applied right pedal, the airplane departed the runway to the right, and tipped over coming to rest on the right leading edge of the wing. The airplane sustained substantial damage to the wing keel. A Federal Aviation Administration (FAA) aviation safety inspector who responded to the accident site reported that he observed no mechanical malfunctions or failures with airframe and engine that would have precluded normal operation and none was reported to him by the pilot. In the recommendation section of the National Transportation Safety Board Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if he had additional training that concentrated on ground handling and crosswind condition operations. The FAA has published the Weight-Shift Control Aircraft Flying Handbook FAA-H-8083-5 (2008). This handbook discusses crosswind landing procedures for WSC airplanes and states in part: When in final approach, the wind correction angle (crab angle) is established by heading toward the wind with the wings level so that the aircraft's ground track remains aligned with the centerline of the runway. This crab angle is maintained all the way to touchdown, when the rear wheels hit first and rotate the carriage and wing around so the front wheel touches the ground with the carriage going straight. However, if in turbulent air or pitched forward during the touchdown, with the front wheel touching the ground first, the pilot should lightly control the steering of the front wheel to be headed in the direction the carriage is going. WSC carriage front landing gear typically has camber that tends to steer the front wheel naturally in the direction of travel, so a light touch on the front wheel as it touches the ground allows it to find its own direction of travel. Once the front wheel is on the ground, lower the nose to keep the WSC on the ground and steer as required down the center of the runway. The procedure for the wing during the roundout is the same as that for normal and turbulent roundout and touchdowns. The exception is that after touchdown the windward wing should be lowered slightly so the wind cannot get under it to flip the WSC aircraft during later landing roll and taxi.
Aircraft
- Registration
- N8512Q
- Reported as
- Holley Carol L Antares (MA2)
- Category
- Airplane
- Serial number
- 24150HS
- Built
- 2007
- Airframe hours
- 20.7
- Engine
- Rotax 503, 50 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Special, Experimental light sport (Special)
- Last inspection
- Annual · July 5, 2016
- Departed
- 95Z · North Pole, AK
- Destination
- 95Z · North Pole, AK
- Airport
- 95Z · Bradley Sky-Ranch, runway 15, 4,100 × 60 ft, gravel
- Equipment
- Airframe parachute
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
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 39
- Injuries
- None
- Certificates
- Student, Private, Commercial, Military
- Airplane ratings
- Single-engine land
- Instrument ratings
- Helicopter
- Medical
- Class 3, With waivers/limitations
- Seat
- Front
- Restraint
- 4-point
- Flight hours
- 3,124.8 total · 6.8 in this make and model
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 300° at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- 18,000 ft broken
- Temperature
- 66 °F, dew point 55 °F
- Altimeter
- 29.94 inHg
- Observed at
- PAFB, 7 nm away
Docket · 3
The files NTSB released with the investigation on October 25, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.9 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.