MIA87FA091

NTSB accident investigation · Beech A36TC · Orlando, FL · February 21, 1987

Accident · Serious injuriesField investigationFinal report
Date
February 21, 1987, 14:56 local (19:56 UTC)
Place
Orlando, FL
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N47EEBeech A36TC
Weather
Visual (VMC) · Day
Status
Completed · report August 19, 1988
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19870221003119A
Case key
31752

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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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 powerTakeoff
Reason for occurrence undeterminedFactor
Exhaust system,manifold/pipe - cracked
Loss of engine power(total) - nonmechanicalTakeoff - initial climb
Emergency procedure - improperPilot in commandCause
Fuel boost pump selector position - improperPilot in commandCause
Forced landingManeuvering - turn to landing area (emergency)
Loss of control - in flightManeuvering - turn to landing area (emergency)
Airspeed - not maintainedOther crewmemberCause
Stall - inadvertentOther crewmemberCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Drg the takeoff roll, lgt colored smoke was seen trailing the the acft. The plt rprtd that at 100 to 200 ft AGL, the englost partial pwr. He said he checked all ctls & raised the lndg gear. Witnesses rprtd that at about that time, heavy smoke bgn trailing the acft & the eng backfired & quit. The plt said the safety plt then took ctl & atmtd to return to the arpt. At about that time, the acft stalled, dscndd out of ctl & crashed at the edge of a lake. Rsn for the initial pwr loss was not determined. The elec boost pump was fnd in the hi psn after the acdnt. The flt manual warned that the hi boost pump must not be used unless the eng driven fuel pump had failed; otherwise, increased pressure fm the hi boostpump would result in eng roughness; in some cases, eng combustion may cease. The eng operated normally in a test cell after the acdnt. When another eng was tested, loss of pwr occurred 3 to 5 sec after the hi boost pump was activated. Also, a crack was fnd in the turbocharger inlet pipe, but duplication of this resulted in only a minor pwr loss.

Aircraft

Registration
N47EE
Reported as
Beech A36TC
Category
Airplane
Serial number
EA-272
Airframe hours
830
Engine
Continental TSIO-520-UB, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Raymond C. Barget
Airworthiness certificate
Standard, Utility
Last inspection
Annual · July 23, 1986 · 64 hours before
Destination
MLB · Melbourne, FL
Flight plan
IFR
Airport
ORL · Orlando Executive, runway 7, 6,000 × 150 ft, water

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
63
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
2,000 total · 278 in this make and model · 20 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
50° at 8 knots
Visibility
7 statute miles
Lowest ceiling
5,000 ft overcast
Altimeter
29.00 inHg
Observed at
ORL, 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.