Cessna 177A accident near Hanksville, Utah, May 8, 2012
On May 8, 2012 at about 4:45 pm local time, a Cessna 177A, registered N28WF, was substantially damaged in an accident during maneuvering (low-alt flying) near Hanksville, Utah. It was a personal flight under general aviation rules (Part 91). 2 people had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain adequate airspeed while maneuvering at a low altitude in high density altitude conditions, which resulted in the airplane’s inability to climb or maintain clearance from terrain.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- May 8, 2012 · about 4:45 pm local time
- Place
- Hanksville, Utah · map
- Type
- Accident
- Injuries
- 2 people had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna 177A · all 177As on the register
- Registration
- N28WF · registry record · serial 17700876
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that about 1 hour into a local flight, he made a low fly-by over a remote airstrip. When he applied power to climb, the engine responded normally. However, about 15 seconds later, after he raised the flaps, the airplane’s airspeed slowed, and the airplane stopped climbing. The pilot stated that he was in a mountainous canyon and, believing that the airplane would not climb satisfactorily, he performed a forced landing in the canyon. During the forced landing, the airplane’s nosewheel dug into the soft, sandy terrain, the nose landing gear separated, and the main landing gear collapsed. The pilot reported having taken off with full tanks and stated that he should have had about 40 gallons of fuel remaining after the 1-hour flight. When the airplane was recovered, no fuel was found in the left tank and only 1/3 gallon of fuel was found in the right tank. However, the fuel system lines around the fuel selector and the fuel shut-off valve were compromised, and it is likely that any remaining fuel leaked out of the tanks during the several days that passed between the accident and recovery of the wreckage. Examination of the airplane and its engine found no evidence of any preimpact mechanical malfunctions or failures that would have prevented normal operation. At the calculated density altitude of 6,000 feet, the normally aspirated engine’s maximum output of 150 horsepower (hp) would be reduced to 120 hp. Aircraft performance can become marginal in high density altitude conditions, and both maneuvering at low altitude and operating at high density altitude require pilot vigilance to maintain adequate airspeed during climb.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of control in flight during maneuvering (low-alt flying) defining event
- Collision with terrain or object (not controlled flight into terrain) during landing (landing roll)
- Off-field or emergency landing during landing
The NTSB's findings
- cause Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Effect on operation
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Environmental issues › Physical environment › Terrain › Rough terrain › Effect on equipment
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 985 hours in all; 91 in this make and model; 45 in the last 90 days; 14 in the last 30 days; 930 as pilot in command; 240 on instruments
- Last flight review: April 20, 2012
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: rgt
- Injury: minor injuries
The aircraft
- Airframe total time: 4,261 hours
- Last inspection: annual inspection, August 22, 2011
- Maximum gross weight: 2,350 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-320 (piston); 0 hours total
- Operator: Ame High LLC
The flight
- Departed from: U77 Spanish Fork UT at 3:45 pm
- Destination: U77 Spanish Fork UT
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 60 statute miles
- Sky: scat at 2,000 ft
- Temperature: 61°F (16°C), dew point 30°F (-1°C)
- Altimeter: 30.06 inHg
- Observation at 4:30 pm from HVE, 15 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
