FTW91FA043

NTSB accident investigation · Mitsubishi MU-2B-60 · Tulsa, OK · February 22, 1991

Accident · FatalField investigationFinal report
Date
February 22, 1991, 15:19 local (21:19 UTC)
Place
Tulsa, OK
Injuries
3 fatal
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N274MAMitsubishi MU-2B-60
Weather
Visual (VMC) · Day
Status
Completed · report January 28, 1993
Report
Approved by Office Director
FAA report
19910222003339A
Case key
23250

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 shutdown of one engine for undetermined reasons, and the pilot's failure to maintain vmca during a critical phase of flight. A factor in the accident was the pilot's improper emergency procedure.

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(total) - nonmechanicalTakeoff - initial climb
1 engine
Reason for occurrence undeterminedCause
Propeller feathering - performedPilot in command
Loss of control - in flightTakeoff - initial climb
Airspeed(vmc) - not maintainedPilot in commandCause
Emergency procedure - improperPilot in commandFactor
In flight collision with terrain/waterTakeoff - initial climb

Analysis

Airplane was departing on a required maintenance test flight following replacement of both engines. Witnesses stated that the takeoff roll and initial climb appeared normal, but that at about 500 ft AGL, the airplane entered a right bank which continued until the wings were vertical and the nose fell through. Airplane impacted in an inverted steep nose down attitude. Examination of wreckage revealed that the right engine had been secured and feathered. Subsequent investigation did not reveal any evidence of pre-impact failure or malfunction of either engine or any of the airframe systems. Engine mounting/rigging continuity could not be established due to impact damage. The pilot was a principal in the operator's organization and not one of the regular line pilots. Evidence indicated that the gear was up and that the left spoiler was deployed at impact. Emerg procedure taught in transition training is to use rudder trim as soon as possible after eng failure to preclude deployment of spoilers. Rudder trim found in neutral position.

Aircraft

Registration
N274MA
Reported as
Mitsubishi MU-2B-60
Category
Airplane
Serial number
786SA
Airframe hours
6,094
Engine
Garrett TPE-331-10, 715 horsepower, turbo prop
Damage
Destroyed
Flight
Part 91
Operator
Corp. Aviation Services, Inc.
Registered owner
Scope Leasing, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · February 22, 1991 · 1 hours before
Airport
TUL · Tulsa International, runway 35L, 6,101 × 150 ft

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
58
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
4,910 total · 445 in this make and model · 4,531 as pilot in command · 27 in the last 90 days · 11 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
20° at 13 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 30 °F
Altimeter
30.00 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 N274MA · 1

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