LAX86LA184

NTSB accident investigation · Cessna 310N · Fullerton, CA · April 21, 1986

Accident · No injuriesLimited investigationFinal report
Date
April 21, 1986, 10:44 local (18:44 UTC)
Place
Fullerton, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N4162QCessna 310N
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19860421014439A
Case key
25127

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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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.

Miscellaneous/otherTakeoff - roll/run
Flight control,elevator - vibrationFactor
Aircraft preflight - inadequatePilot in commandCause
ComplacencyPilot in commandCause
Flight manuals - not followedPilot in commandCause
OverrunLanding - roll
Landing gear,normal brake system - overtemperatureFactor
Preflight planning/preparation - inadequatePilot in commandFactor
In-flight planning/decision - delayedPilot in commandCause
Aborted takeoff - delayedPilot in commandCause

Analysis

The acft overran the rwy during an aborted takeoff. The plt had flown the acft the day prior on his bfr and conducted a 'thorough preflight' insp. On the day of the accident, he preflighted the acft again and flew it without incident. He then refueled the acft and left it unattended for aprx 90MINS. When the plt returned he 'did a visual walk around' before entering the acft. During the takeoff ground run, at 95 mph, he heard 'excessive wind noise.' He then started to rotate and felt a vibration. The takeoff was aborted and the acft ran off the end of the rwy. The plt stated the brakes fadded the last 100 ft of travel. The acft was examined and the inspection panel was found hanging from the right horizontal stabilizer. The panel had 1 screw holding it in place and 1 screw was in the nut plate, but not through the panel. The operators manual states to make an exterior inspection prior to starting the engines. The accelerate stop distance was aprx 2,600 ft. rwy length at the arpt is 3,121 ft.

Aircraft

Registration
N4162Q
Reported as
Cessna 310N
Category
Airplane
Serial number
310N-0062
Airframe hours
1,986
Engine
Continental IO-470-V, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Norman A. Takaki
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 8, 1985 · 40 hours before
Departed
FUL · Fullerton, CA
Destination
LAS · Las Vegas, NV
Airport
FUL · Fullerton, runway 24, 3,121 × 75 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
51
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
1,565 total · 382 in this make and model · 1,333 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 6 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 55 °F
Altimeter
29.00 inHg
Observed at
FUL

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.