- Date
- May 1, 1998, 15:00 local (22:00 UTC)
- Place
- Monroe, WA
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Approach
- Aircraft
- N5157WPiper PA-28-160
- Weather
- Visual (VMC) · Day
- Status
- Completed · report July 12, 2000
- Report
- Approved by Office Director
- FAA report
- 19980501008299A
- Case key
- 42779
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
Fuel starvation due to the flight instructor's improper in-flight decision to simulate an engine failure by pulling the mixture control toward the lean position until the engine shut down, and his failure to return the mixture to the rich position until after the aircraft had reached a low altitude and the propeller had stopped turning. Factors include the rough/uneven terrain within the construction area in which the aircraft was landed.
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 the instructor simulated an engine failure by pulling out the mixture control until the engine shut down, the student attempted to maneuver for a landing at a paved private airstrip. Just after turning a close-in final, with the mixture still pulled out almost to the full-lean position, the student raised the aircraft's nose, and the propeller stopped turning. The instructor then returned the mixture control to the full rich position and instructed the student to engage the starter. After two unsuccessful attempts to get the engine to start, the student landed the aircraft in an area where the terrain had been torn up by construction workers. Just after touchdown, the aircraft impacted rough/uneven terrain and sustained substantial damage.
Factual narrative
On May 1, 1998, approximately 1500 Pacific daylight time, a Piper PA-28-160, N5157W, collided with rough terrain during a forced landing off the approach end of FirstAir Field, Monroe, Washington. The certified flight instructor and the student pilot were not injured, but the aircraft, which was owned by the student, sustained substantial damage. The 14 CFR Part 91 instructional flight, which departed Harvey Field, Snohomish, Washington, about 30 minutes earlier, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation.
According to the instructor, while approximately 4,000 feet AGL, he pulled out the mixture control until the engine stopped firing in order to simulate an engine failure in flight. Then as the student maneuvered toward FirstAir Field, the instructor occasionally "cleared" the engine by returning the mixture to the full rich position. After turning onto a close-in final approach, with the mixture still pulled nearly all the way out, the student raised the nose of the aircraft a few degrees, and the propeller stopped turning. The instructor then returned the mixture control to the full rich position, and told the student to engage the starter. According to the instructor, the student attempted twice to get the propeller to rotate using the starter, but there were "no results." When the engine did not start, the instructor pushed the nose down to prevent a stall, and the student completed a landing in an area where the terrain had been torn up by construction crews. Just after touchdown, the aircraft collided with the rough/uneven terrain created by the construction.
In a post-accident interview, the instructor said that in the past he had always used the throttle to simulate an engine failure (instead of the mixture), and was not sure why he had used the mixture this time instead.
A post-accident inspection of the engine revealed no anomalies, and using the battery that was in the aircraft at the time of the accident, the engine was successfully started on the first attempt and run to 1,500 rpm. A higher rpm run was not attempted because of the vibrations generated by the bent propeller.
Aircraft
- Registration
- N5157W
- Reported as
- Piper PA-28-160
- Category
- Airplane
- Serial number
- 28-188
- Airframe hours
- 2,253
- Engine
- Lycoming O-320-B2B, 160 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Registered owner
- Keith S. Sudac
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · October 22, 1997
- Departed
- S43 · Snohomish, WA
- Destination
- O9S · Monroe, WA
- Airport
- WA38 · Firstair Field, runway 25, 2,092 × 34 ft, asphalt
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
- 26
- Certificates
- Flight instructor, Commercial
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Right
- Flight hours
- 653 total · 17 in this make and model · 539 as pilot in command · 185 in the last 90 days · 58 in the last 30 days · 2 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 270° at 10 knots
- Visibility
- 20 statute miles
- Lowest ceiling
- None
- Temperature
- 75 °F
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.