LAX98LA101

NTSB accident investigation · Cessna 310C · Lancaster, CA · March 2, 1998

Accident · Minor injuriesLimited investigationFinal report
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.

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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.

Loss of engine power(total) - nonmechanicalTakeoff - initial climb
Mixture - improper use ofPilot in commandCause
Forced landingTakeoff - initial climb
Terrain condition - rough/unevenFactor

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.