FTW91FA080

NTSB accident investigation · Beech V35B · Manor, TX · May 16, 1991

Accident · FatalField investigationFinal report
Date
May 16, 1991, 10:20 local (15:20 UTC)
Place
Manor, TX
Injuries
4 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N9435QBeech V35B
Weather
Visual (VMC) · Day
Status
Completed · report December 4, 1992
Report
Approved by Office Director
FAA report
19910516016219A
Case key
23260

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 NTSB’s determination of the probable cause, and any contributing factors.

The pilot's operation of the aircraft at a gross weight and center of gravity which exceeded the certificated operating limitations, resulting in loss of control and structural overload. Turbulence was a related factor.

Analysis

The plt lost ctl of the acft in IFR conds as the plane was dscndg thru abt 6000' MSL, in an area of convective activity with moderate to severe turbc & up/down drafts. Both wings sepd fm the acft & wreckage was scattered over an area of aprx 1.5 mi. Calculations showed that at the time of the acdnt, the acft's gross wt was 29 lbs over its max limit, and the center-of-gravity (CG) was abt 3.3 to 5.3 inches behind the aft limit. Under these conds, the acft's maneuvering stability & stick force per 'g' characteristics would have been seriously degraded. In turn, this would have allowed the plt to exceed the structural design limits of the acft with little or no effort. An exam of the wreckage disclosed evidence of apparent flap asymmetry, a cond which way have occurred drg the in-flt breakup of the acft.

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 flightDescent - normal
Aircraft weight and balance - exceededPilot in commandCause
Weather condition - turbulence in cloudsFactor
Airframe/component/system failure/malfunctionDescent - uncontrolled
Flight control,flap - asymmetrical
Design stress limits of aircraft - exceededPilot in commandCause
Wing - overload
In flight collision with terrain/waterDescent - uncontrolled

Aircraft

Registration
N9435Q
Reported as
Beech V35B
Category
Airplane
Serial number
D-9317
Airframe hours
3,883
Engine
Continental IO-520-BA, 285 horsepower, reciprocating
Damage
Destroyed
Flight
Business · Part 91
Operator
Bonanza 9435 Quebec
Registered owner
Bonanza 9435 Quebec
Airworthiness certificate
Standard, Utility
Last inspection
Annual · April 26, 1991 · 7 hours before
Departed
ADS · Addison, TX
Destination
AUS · Austin, TX
Flight plan
IFR

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
36
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
315 total · 38 in this make and model · 241 as pilot in command · 5 in the last 90 days · 2 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 9 knots
Visibility
5 statute miles
Lowest ceiling
1,700 ft broken
Temperature
81 °F, dew point 73 °F
Altimeter
29.00 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 N9435Q · 1

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