- Date
- July 21, 2001, 07:20 local (14:20 UTC)
- Place
- Winslow, AZ
- Injuries
- 1 minor, 4 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N222RWWatkins Velocity
- Weather
- Visual (VMC) · Day
- Status
- Completed · report October 24, 2002
- Report
- Approved by Office Director
- Parties
- FAA - FLIGHT STANDARDS DIST OFFICE
- FAA report
- 20010721017839A
- Case key
- 52789
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 separation of the number three cylinder head from the barrel resulting in a loss of engine oil during flight. Factors were the lack of suitable terrain for the forced landing, and the rough uneven ground of the forced landing site.
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
During cruise flight, the engine lost power, followed by an off-airport forced landing. The airplane collided with obstacles on the ground. The pilot, who was receiving flight following advisories, reported a loss of engine oil pressure to the air traffic controller. During the flight's diversion to an airport, the engine continued to lose power and the pilot was unable to maintain altitude and reach the divert airport. Local police reported that the pilot subsequently returned to the airplane, chopped it up with an axe, and transported it from the site in a truck. Subsequently, repair personnel examined the engine noting that the number three cylinder head had separated from the cylinder barrel allowing the engine oil to drain from the engine during flight. Engine records indicated the last engine overhaul was January 1988. The pilot reported the engine had 1,275 hours since overhaul with 38 hours since the airplane's last annual inspection in May 2001.
Factual narrative
On July 21, 2001, at 0720 hours mountain standard time, an experimental Velocity, N222RW, reported a loss of engine oil pressure and made an emergency forced landing 8 to 10 miles north of Winslow, Arizona. The airplane was substantially damaged during the ensuing ground obstacle collision sequence. One passenger received minor injuries, and the certificated private pilot and remaining three passengers were not injured. The airplane was being operated as a personal flight by a private owner under the provisions of 14 CFR Part 91 when the accident occurred. The flight had originated earlier that morning from Grand Canyon, Arizona, and was en route to Albuquerque, New Mexico, at the time of the accident. Visual meteorological conditions prevailed at the time and an IFR flight plan had been filed, but not activated.
According to Albuquerque center air traffic controllers, at 0720, the pilot, who had been flight following with center, requested airport location information as the result of an in-flight maintenance problem. At 0729, the pilot reported that he had experienced a loss of engine oil pressure, and that he was proceeding to the Winslow-Lindbergh Regional Airport. At 0733, he advised air traffic controllers that he would be unable to reach Winslow, and that he was "going down." Controllers advised the pilot the location of an emergency landing strip 15 miles north of the airport. Subsequently, controllers lost all radio and radar contact with the airplane.
At 0919, Arizona Department of Public Safety Air Range No. 42 located the accident site. All the occupants were transported to Winslow Memorial Hospital, Winslow, treated, and released.
Navajo County sheriff deputies reported that the pilot later returned to the site with a pickup truck and an ax. He chopped up the airplane, loaded it in the truck, and departed the area.
On November 19, 2001, the Safety Board hired a representative from D and B Aircraft Engines of Bethany, Oklahoma, to travel to Cashion, Oklahoma, and inspect the wreckage at its storage location. The examination revealed that the engine number three cylinder head had separated from the cylinder barrel, causing a gradual loss of engine oil. The details of the examination are included in this report.
Aircraft
- Registration
- N222RW
- Reported as
- Watkins Velocity
- Category
- Airplane, amateur-built
- Serial number
- DM101
- Airframe hours
- 1,130
- Engine
- Avco Lycoming IO-360-C1C, 200 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Billy Ray Watkins, Jr.
- Airworthiness certificate
- Special, Experimental (Special)
- Last inspection
- Annual · May 18, 2001 · 38 hours before
- Departed
- GCN · Grand Canyon, AZ
- Destination
- ABQ · Albuquerque, NM
- Flight plan
- IFR
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
- 43
- Injuries
- None
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--no waivers/lim.
- Last flight review
- October 26, 1999
- Seat
- Left
- Flight hours
- 1,677 total · 1,130 in this make and model · 1,533 as pilot in command · 39 in the last 90 days · 21 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 4 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 70 °F, dew point 52 °F
- Altimeter
- 30.14 inHg
- Observed at
- INW
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.