SEA98LA068

NTSB accident investigation · Piper PA-28-160 · Monroe, WA · May 1, 1998

Accident · No injuriesLimited investigationFinal report
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.

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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.

Loss of engine power(total) - nonmechanicalApproach - vfr pattern - final approach
In-flight planning/decision - improperPilot in command(cfi)Cause
Remedial action - delayedPilot in command(cfi)Cause
Fluid,fuel - starvationCause
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - construction areaFactor
Terrain condition - rough/unevenFactor

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.