LAX08CA021

NTSB accident investigation · Beech A36 · Camarillo, CA · October 26, 2007

Accident · No injuriesData collectionFinal report
Date
October 26, 2007, 12:05 local (19:05 UTC)
Place
Camarillo, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N16SFBeech A36
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2007
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20071026826969A
Case key
66977

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 failure to maintain an adequate airspeed during a go-around, which resulted in a stall.

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 control - in flightGo-around (vfr)
Go-around - attemptedPilot in command
Airspeed - not obtained/maintainedPilot in commandCause
Stall - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - runway

Analysis

The airplane impacted the ground during an attempted go-around. The pilot flew the approach at a higher altitude than anticipated but decided to continue. Prior to landing, about 30 feet agl, the local air traffic controller instructed the pilot to perform a go-around. The pilot initiated the procedure with application of full throttle, and he increased the airplane's pitch attitude. When the pilot saw he was gaining altitude, he retracted the landing gear and the flaps. The airplane then stalled and impacted the runway.

Factual narrative

On October 26, 2007, about 1205 Pacific daylight time, a Beech A36, N16SF, stalled and impacted the runway at Camarillo Airport, Camarillo, California. Flying A36 LLC was operating the airplane under the provisions of 14 CFR Part 91. The private pilot and one passenger were not injured. The airplane sustained substantial damage during the attempted go-around maneuver. The personal flight departed Paso Robles Municipal Airport, Paso Robles, California, about 1115, with a planned destination of Camarillo. Visual meteorological conditions prevailed, and no flight plan had been filed.

In a written report to the National Transportation Safety Board, the pilot stated he flew a traffic pattern approach for landing and he entered on the downwind leg. After turning final, he realized he was at a higher altitude than anticipated but he decided to continue the approach. Prior to landing, about 30 feet agl, the local air traffic controller instructed the pilot to perform a go-around. The pilot initiated the procedure with application of full throttle, and increased the pitch attitude of the airplane. When the pilot saw he was gaining altitude, he retraced the landing gear and the flaps. The airplane stalled and impacted the runway.

The pilot reported no preimpact mechanical malfunctions or failures with the airframe or engine. The airplane sustained damage to the landing gear structure and fuselage.

Aircraft

Registration
N16SF
Reported as
Beech A36
Category
Airplane
Serial number
E-635
Engine
Teledyne Continental IO-520, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 1, 2007
Departed
PRB · Paso Robles, CA
Destination
CMA · Camarillo, CA
Airport
CMA · Camarillo Airport, runway 26, 6,013 × 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
41
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Without waivers/limitations
Last flight review
October 1, 2006
Seat
Left
Flight hours
349 total · 225 in this make and model · 319 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 6 knots
Visibility
6 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 54 °F
Altimeter
29.90 inHg
Observed at
CMA

FAA reports on this event · 1

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