DEN92FA035

NTSB accident investigation · Swearingen SA-26AT · Glenwood Spring, CO · February 14, 1992

Accident · Serious injuriesField investigationFinal report
Date
February 13, 1992, 20:55 local (Feb 14, 1992, 03:55 UTC)
Place
Glenwood Spring, CO
Injuries
3 serious, 1 minor, 1 uninjured
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N26JBSwearingen SA-26AT
Weather
Instrument (IMC) · Night/dark
Status
Completed · report August 26, 1993
Report
Approved by Office Director
FAA report
19920213005749A
Case key
18147

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

Malfunction of the right engine fuel control that caused the engine to flame out, and delamination of the left engine compressor shroud. Factors were: the pilot became disoriented, the mountainous terrain, the dark night, and the weather conditions.

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) - mech failure/malfCruise - normal
1 engine
Fuel system,fuel control - movement restrictedCause
Propeller feathering - performedPilot in command
Loss of engine power(partial) - mech failure/malfCruise - normal
1 engine
Turbine assembly,shroud - delaminationCause
In flight collision with terrain/waterDescent - emergency
Became lost/disoriented - inadvertentPilot in commandFactor
Weather condition - obscurationFactor
Light condition - dark nightFactor
Terrain condition - mountainous/hillyFactor

Analysis

The pilot of the air ambulance feathered the right propeller after reporting 'a bit of a problem' with the right engine. He attempted to divert to the nearest suitable airport, but after receiving its latest weather report, elected to return to base. The airplane made a left turn, reentered IMC, and impacted a mountainside on a magnetic heading of 092 degrees. The heading to the airport of intended landing was 272 degrees. The accident occurred during a snow storm at night. All five occupants survived and were rescued the following afternoon. Thick grease on the right engine fuel control cam shaft prevented a Spring from returning the 3D cam to a lower altitude position. The cam was found struck on the shaft at a position equating to an altitude of approximately 15,000 feet. The fuel flow schedule for flight idle was below specifications. In addition, shroud material was found delaminated from the left engine second stage compressor housing.

Aircraft

Registration
N26JB
Reported as
Swearingen SA-26AT
Category
Airplane
Serial number
T26-163
Airframe hours
3,988
Engine
Garrett TPE331-1-151G, 665 horsepower, turbo prop
Damage
Destroyed
Flight
Part 135
Registered owner
Fowler, Richard L.
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · December 23, 1991 · 27 hours before
Departed
GJT · Grand Junction, CO
Destination
DEN · Denver, CO
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
37
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
8,600 total · 750 in this make and model · 8,550 as pilot in command · 85 in the last 90 days · 30 in the last 30 days

Weather

Conditions
Instrument (IMC) · Night/dark
Wind
Calm
Visibility
2 statute miles
Lowest ceiling
300 ft
Temperature
34 °F, dew point 27 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.