FTW89DPJ07

NTSB accident investigation · Beech T-34 · Haskell, OK · June 24, 1989

Accident · FatalFinal report
Date
June 24, 1989, 15:35 local (20:35 UTC)
Place
Haskell, OK
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Other
Aircraft
N34CJBeech T-34
Weather
Visual (VMC) · Day
Status
Completed · report June 19, 1991
Report
Approved by Office Director
FAA report
19890624017329A
Case key
22701

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

Failure of the pilot to maintain adequate airspeed, which resulted in an inadvertent stall. Factors related to the accident were: a leak in the pitot system, failure of the pilot to obtain adequate maintenance/inspection of the pitot system, and his lack of familiarity with the aircraft.

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.

Airframe/component/system failure/malfunctionOther
Pitot/static system - leakFactor
Maintenance,inspection - inadequatePilot in commandFactor
Loss of control - in flightManeuvering
Procedures/directives - not followedPilot in command
Stall warning system - not installed
Airspeed - not maintainedPilot in commandCause
Stall - inadvertentPilot in commandCause
Lack of familiarity with aircraftPilot in commandFactor
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The airspeed indcr was malfunctioning on a previous flt. Bfr taking off again, the plt was seen to disassemble the pitottube as if the remove foreign matter. On the next flt, he bgn a hi spd/low pass ovr rwy 35. At abt midfield, the acft entered a climb to aprx 800 to 1000 ft AGL. Nr the peak of the climb, there was a reduction of pwr & the acft mnvrd (turned left, then rgt, as if to enter a base turn for rwy 17). The lndg gear was extdd at abt 300 to 500 ft AGL, flwd by a turn (south) twd the rwy. After abt 45 deg of turn, the acft entered a steep dscnt & crashed. An exam revealed a rubber pitot line, pn 35-324323, was deteriorated & leaked. No otr preimpact part failure was fnd. Experimental categoryacft with svrl limitations: flts rstrd to TX; exhibition only; PIC was required to have an instructor's logbook endorse-ment or letter of authorization (loa) to oper the acft. Neither an endorsement nor loa was fnd. Plt had abt 1 hr in T-34ACFT; cannabinoids detected in plt's urine, but none fnd in his blood. Acft was not equipped with stall warning sys.

Aircraft

Registration
N34CJ
Reported as
Beech T-34
Category
Airplane
Serial number
CG-211
Airframe hours
5,550
Engine
Continental IO-470-N, 260 horsepower, reciprocating
Damage
Destroyed
Flight
Part 91
Registered owner
Red Stevenson
Airworthiness certificate
Special, Experimental (Special)
Last inspection
100 hour · January 3, 1989 · 10 hours before
Departed
00K7
Airport
0OK7 · Haskell, runway 17, 3,710 × 30 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
40
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Rear
Toxicology
Performed
Flight hours
778 total · 1 in this make and model · 653 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 8 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
88 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
TUL, 23 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.