- Date
- May 17, 1998, 11:30 local (18:30 UTC)
- Place
- Richvale, CA
- Injuries
- 1 uninjured
- Damage
- Destroyed
- Phase of flight
- Initial climb
- Aircraft
- N8177KSchweizer G164D
- Weather
- Visual (VMC) · Day
- Status
- Completed · report February 11, 2000
- Report
- Approved by Office Director
- FAA report
- 19980517009779A
- Case key
- 30088
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 four compressor/turbine blades resulting in a sudden loss of engine power with a subsequent forced landing into unsuitable terrain.
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
On takeoff, the pilot experienced a loss of engine power preceded by the sound of loud 'pop.' He completed a forced landing on soft ground and the aircraft nosed over. During the post-accident teardown inspection of the engine, it was noted that four compressor/turbine blades had failed at the blade/butt interface. The failed blades were not standard manufacturer's replacement parts.
Factual narrative
On May 17, 1998, at 1130 hours Pacific daylight time, a Schweizer G164D, N8177K, was destroyed when it nosed over during a forced landing following a total loss of engine power on takeoff. The commercial pilot was not injured and there was no property damage. At the time of the accident, the flight was departing the Doc Thompson airstrip which is located 9 miles north-northwest of Richvale, California. Visual meteorological conditions prevailed and no flight plan was filed for the 14 CFR Part 137 agricultural application flight.
The operator stated in his accident report that, approximately 15 feet agl, he heard a loud "pop" in the engine compartment followed by an immediate loss of engine power. He made a forced landing to a soft dirt field about 800 feet from the end of the runway.
During a teardown inspection of the engine, it was noted that four compressor/turbine blades were broken off at the blade/butt interface. The parting surface on the butt side of the break was clean and did not show evidence of progressive failure. It was also noted that the four broken blades were not standard manufacturer's replacement parts.
Aircraft
- Registration
- N8177K
- Reported as
- Schweizer G164D
- Category
- Airplane
- Serial number
- 8D
- Airframe hours
- 9,628
- Engine
- P&W PT6A-34AG, 750 horsepower, turbo prop
- Damage
- Destroyed
- Flight
- Aerial application · Part 137
- Registered owner
- Avag, Incorporated
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- Annual · April 25, 1998 · 62 hours before
- Departed
- PVT · CA
- Airport
- Thompson Strip, runway 16, 2,000 × 30 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
- 57
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Front
- Flight hours
- 37,000 total · 8,000 in this make and model · 50 in the last 90 days · 50 in the last 30 days · 8 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 280° at 8 knots
- Visibility
- 60 statute miles
- Lowest ceiling
- None
- Temperature
- 70 °F, dew point 46 °F
- Altimeter
- 30.00 inHg
- Observed at
- CIC, 18 nm away
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.