LAX93FA186

NTSB accident investigation · Beech 58 · Tucson, AZ · April 26, 1993

Accident · FatalField investigationFinal report
Date
April 25, 1993, 17:38 local (Apr 26, 1993, 00:38 UTC)
Place
Tucson, AZ
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N158WBBeech 58
Weather
Visual (VMC) · Day
Status
Completed · report November 19, 1993
Report
Approved by Office Director
FAA report
19930425010419A
Case key
27831

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 pilots improper preflight inspection, his failure to compeltely secure the aft utility door, and his failure to reconfigure the trim tabs to a takeoff setting. The utility door's sudden opening just after rotation and the effect of the nose up trim setting led to an inadvertent stall during the takeoff initial climb.

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 flightTakeoff - initial climb
Door,cargo/baggage - not securedCause
Aircraft preflight - inadequatePilot in commandCause
Aircraft control - not maintainedPilot in commandCause
Stall/spin - inadvertentPilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The pilot had recently purchased the twin engine airplane and had accumulated about 123 total hours of multi engine time, with about 115 hours in the accident airplane. Witnesses stated that just after rotation the airplane pitched up abruptly and rotated to the right impacting the ground about 2000 feet beyond the approximate point of rotation and about 1500 feet to the right of the runway center line. Post crash examination of the wreckage revealed that the aft utility doors were unlatched, with the aft door rotated rearward against the fuselage and the extension limiting hinges sheared at the hinge pin. The elevator trim tabs were found in the landing configuration with tab deflections at about 9 degrees down. The rudder trim tab was found 20 degrees left deflection. Both engines were removed to an engine overhaul facility for detailed examination. No mechanical discrepancies were found and power and rotation signatures were evident. The airplane was departing on runway 11L from taxiway 6 with a nine knot tailwind and 9950 feet of runway

Aircraft

Registration
N158WB
Reported as
Beech 58
Category
Airplane
Serial number
TH-396
Airframe hours
2,310
Engine
Continental IO-520-C, 285 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Operator
Jay M. Supkoff, doing business as S & H Aircraft Leasing
Registered owner
Supkoff, Jay
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 6, 1992 · 115 hours before
Destination
SJC · San Jose, CA
Airport
TUS · Tucson, runway 11, 10,994 × 150 ft, concrete

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
64
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
1,090 total · 123 in this make and model · 29 in the last 90 days · 5 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 9 knots
Visibility
40 statute miles
Lowest ceiling
None
Temperature
88 °F, dew point 25 °F
Altimeter
29.00 inHg
Observed at
TUS, 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.