N141UE

MINR
None

BEECH 1900C S/N: UC141

Accident Details

Date
Wednesday, April 27, 1994
NTSB Number
FTW94IA139
Location
CHEYENNE, WY
Event ID
20001206X01093
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
21
Total Aboard
21

Probable Cause and Findings

A PARTIAL FAILURE OF THE LEADING EDGE TIP PORTION OF ONE OF THE LEFT ENGINE PROPELLER BLADES DUE TO PREVIOUS IMPACT DAMAGE FROM AN UNKNOWN SOURCE.

Aircraft Information

Registration
N141UE
Make
BEECH
Serial Number
UC141
Engine Type
Turbo-shaft
Year Built
1991
Model / ICAO
1900C B190
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
RAYTHEON AIRCRAFT CREDIT CORP
Address
8300 E THORN DR STE 100
Status
Deregistered
City
WICHITA
State / Zip Code
KS 67226-2715
Country
United States

Analysis

On April 27, 1994, at 0800 mountain daylight time, a Beech 1900C, N141UE, operating as United Express Flight 5840, sustained minor damage while in cruise flight when a portion of a propeller blade separated from the number one engine. The 2 crew members and 19 passengers were not injured. The flight was on an IFR flight plan and was operating under 14 CFR Part 135 when the incident occurred. The flight departed Bismarck, North Dakota, at 0555 and was in the vicinity of Cheyenne, Wyoming, en route to Denver, Colorado.

According to the crew, the flight was at 15,000 feet msl in clear air when the propeller failure occurred. Following the loss, the crew stated they secured the engine and proceeded to Denver due to unfavorable weather for an emergency landing in Cheyenne.

The propeller was a Hartzell HC-B4MP-3A/MI0877K. It was removed and shipped to Hartzell for examination. The Hartzell report is attached and provides information that the leading edge tip end of the number three blade separated in a jagged manner and the tip was not recovered. The trailing edge of the blade remained intact almost to the tip; however, the outer shin laminates had separated. No other discrepancies were noted.

Following the examination by Hartzell, the failed blade was sent to Wright Patterson Air Force Base for further examination by the composite section of their materials laboratory. The Wright Patterson report is attached and provides information that the blade failed due to apparent impact damage on the leading edge. The source of the impact damage was not discovered.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94IA139