LAX89LA177

NTSB accident investigation · Cessna 310C · Jackson, CA · May 3, 1989

Accident · No injuriesLimited investigationFinal report
Date
May 3, 1989, 11:00 local (18:00 UTC)
Place
Jackson, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N1798HCessna 310C
Weather
Visual (VMC) · Day
Status
Completed · report October 24, 1990
Report
Approved by Office Director
FAA report
19890503010699A
Case key
26396

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 failure of the instructor pilot (pilot in command) to reject the takeoff after the loss of power on one engine when sufficient runway remained to stop the aircraft. Contributing to the accident was the disregard of the aircraft manual, failure to use the fuel boost pump and exceeding the aircraft single engine performance capability.

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 - roll/run
1 engine - failure,total
Fuel boost pump selector position - not selectedPilot in command(cfi)Factor
Flight manuals - disregardedPilot in command(cfi)Factor
Aborted takeoff - not performedPilot in command(cfi)Cause
Loss of control - in flightTakeoff - initial climb
Aircraft performance,engine out capability - exceededFactor
Forced landingDescent - emergency
Terrain condition - none suitable
On ground/water collision with objectLanding - roll
Object - pole

Analysis

The acft owner was taking MEL training for a class rating. He stated that the CFI told him to not use the aux electric fuel pumps during takeoff, a procedure in contradiction to the flight manual. During the takeoff ground roll, the student said the right engine quit at a speed just below rotation. The CFI assumed control of the acft and continued the takeoff, lost control of the acft and landed in a field off the departure end of the runway. The student said the acft was halfway down the 3,400 ft runway when the engine quit. The flight manual lists VMC as 82 mph, and, vyse as 109 mph. The takeoff and landing ground roll distance charts in the flight manual state that 960 feet is required to accelerate to 86 mph, and 650 ft is required to decelerate from that speed. Exam of the acft revealed that the right propeller was not feathered, and no reason was found for the right engine power loss.

Aircraft

Registration
N1798H
Reported as
Cessna 310C
Category
Airplane
Serial number
35898
Airframe hours
3,381
Engine
Continental IO-470-D, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Mason, Richard I.
Registered owner
Richard I Mason
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 1, 1989 · 12 hours before
Departed
O70 · Jackson, CA
Destination
O70
Airport
070 · Westover, runway 10, 3,400 × 60 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
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
12,068 total · 2,205 in this make and model · 11,872 as pilot in command · 72 in the last 90 days · 45 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
330° at 10 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
79 °F
Altimeter
30.00 inHg

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 N1798H · 1

Matched to the same aircraft by N-number and date.