LAX93FA097

NTSB accident investigation · Beech A35 · Tulare, CA · January 21, 1993

Accident · FatalField investigationFinal report
Date
January 20, 1993, 18:05 local (Jan 21, 1993, 02:05 UTC)
Place
Tulare, CA
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N595BBeech A35
Weather
Visual (VMC) · Night/dark
Status
Completed · report May 4, 1994
Report
Approved by Office Director
FAA report
19930120000609A
Case key
27821

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 installation of an unapproved wing tip fuel tank system; an inadequate annual inspection which did not note, or correct, the unapproved fuel system addition; a wing tank fuel selector valve installation without adequate placards to show position or operation; and incorrect instructions to the pilots by the owner and mechanic on positioning fuel selector valves which led to inadvertent mispositioning by the pilots and subsequent fuel starvation. In addition, the pilot at the controls failed to maintain adequate airspeed following the power loss which resulted in an inadvertent stall/spin. A factor which contributed to the loss of control was the dark night light condition.

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(partial) - nonmechanicalTakeoff - initial climb
Fuel system - improperCause
Maintenance,installation - improperOther maintenance personnelCause
Maintenance,annual inspection - inadequateOther maintenance personnelCause
Fuel system,selector/valve - inadequateCause
Instructions,written/verbal - inadequateOther personCause
Instructions,written/verbal - inadequateOther maintenance personnelCause
Fluid,fuel - starvationCause
Fuel tank selector position - inadvertentPilot in command(cfi)
Loss of control - in flightTakeoff - initial climb
Light condition - dark nightFactor
Airspeed(vs) - not maintainedPilot in command(cfi)Cause
Stall/spin - inadvertentPilot in command(cfi)
In flight collision with terrain/waterTakeoff - initial climb

Analysis

The CFI in the right seat was giving dual to the left seat CFI, who had no experience in type. During the initial climb, at about 400-500 ft AGL, witnesses heard the engine lose power or surge. The airplane was seen to roll to one side and descend steeply to impact. The airplane had been extensively modified with an unapproved wing tip fuel tank system addition. The fuel selector valve for the tip tanks did not have any placards showing position or operation. Both cfi's had been given incorrect instructions on how to position the fuel system selector valves by the owner and a mechanic who signed off the annual inspection. Post-crash examination revealed that the standard factory fuel selector was in the aux position, and the tip tanks fuel selector valve was in a half-on/half-off position. The airplane also had a powerplant modification for increased horsepower and other airframe modifications, not all of which were documented or approved. This was the first flight since the annual inspection.

Aircraft

Registration
N595B
Reported as
Beech A35
Category
Airplane
Serial number
D-1616
Airframe hours
4,950
Engine
Continental E-225-8, 225 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Instructional · Part 91
Operator
Rent And Lease Programs
Registered owner
Rent And Lease Programs
Airworthiness certificate
Standard, Normal
Last inspection
Annual · December 29, 1992 · 1 hours before

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
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Toxicology
Performed
Flight hours
7,100 total · 44 in this make and model · 117 in the last 90 days · 34 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
57 °F, dew point 48 °F
Altimeter
30.00 inHg
Observed at
VIS, 11 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.