- Date
- March 2, 1998, 12:30 local (20:30 UTC)
- Place
- Lancaster, CA
- Injuries
- 2 minor
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N608GCessna 310C
- Weather
- Visual (VMC) · Day
- Status
- Completed · report February 15, 2001
- Report
- Approved by Office Director
- FAA report
- 19980302002299A
- Case key
- 30041
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 pilot's improper use of the mixture controls.
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
The pilot attempted takeoff with the mixture controls in an intermediate lean position. The right engine stopped running approximately 300 feet agl, and the pilot elected to land straight ahead rather than attempt a single engine return for landing. When asked about the lean mixture setting for takeoff, the pilot stated that her mechanic had told her to do it that way.
Factual narrative
On March 2, 1998, at 1230 hours Pacific standard time, a Cessna 310C, N608G, was substantially damaged when it impacted terrain following takeoff from the William J. Fox Airport, Lancaster, California. There were minor injuries to the commercial pilot and one passenger and no damage to ground structures or surrounding terrain.
The pilot stated to the Federal Aviation Administration (FAA) inspector that after the right engine stopped at an altitude of approximately 300 feet agl, the decision was made to land straight ahead with the gear down rather than attempt a single engine closed traffic pattern.
Upon examination of the aircraft cockpit following the forced landing, the FAA inspector found both mixture controls in an intermediate lean position. When he interviewed the pilot as to why that position was used for takeoff, she stated that her aircraft mechanic had told her to do it that way. No other airframe discrepancies were noted and the aircraft had been refueled prior to takeoff.
An examination of the aircraft engines was conducted and no evidence of mechanical malfunction was found in either engine. Both rotated freely, had thumb compression on all cylinders with corresponding valve action, and ignition was verified to all sparkplugs. There was no contamination found in the fuel systems and the engine oil was clear for both. The spline drive on the right engine driven fuel pump was found partially severed and there was rust on the inside of the pump housing. However, the pump was flow tested using an electric drill to turn it and it pumped a solid stream of fuel with no cavitation bubbles visible.
Aircraft
- Registration
- N608G
- Reported as
- Cessna 310C
- Category
- Airplane
- Serial number
- 35941
- Airframe hours
- 6,128
- Engine
- Continental IO-470-D, 240 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Anna M. Hagen
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · February 4, 1998 · 3 hours before
- Departed
- WJF
- Destination
- L15 · Henderson, NV
- Airport
- WJF · William J. Fox, runway 24, 5,001 × 150 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
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 3, Valid Medical--w/ waivers/lim
- Seat
- Left
- Flight hours
- 625 total · 435 in this make and model · 565 as pilot in command · 9 in the last 90 days · 6 in the last 30 days · 2 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 230° at 5 knots
- Visibility
- 40 statute miles
- Lowest ceiling
- None
- Temperature
- 63 °F, dew point 39 °F
- Altimeter
- 29.00 inHg
- Observed at
- WJF, 1 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.
Other investigations on N608G · 1
Matched to the same aircraft by N-number and date.