N51816

Substantial
None

CESSNA 402B S/N: 402B0816

Accident Details

Date
Saturday, July 29, 1995
NTSB Number
SEA95LA159
Location
WENATCHEE, WA
Event ID
20001207X04103
Coordinates
47.490337, -120.190612
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

IMPROPER INSTALLATION (FAILURE TO INSTALL COTTER KEY) BY COMPANY MAINTENANCE PERSONNEL.

Aircraft Information

Registration
Make
CESSNA
Serial Number
402B0816
Engine Type
Reciprocating
Year Built
2002
Model / ICAO
402B C402
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
182T

Registered Owner (Current)

Name
BARR AIR PATROL LLC
Address
1442 AIRPORT BLVD STE 11
City
MESQUITE
State / Zip Code
TX 75181-1339
Country
United States

Analysis

On July 28, 1995, approximately 2100 Pacific daylight time, a Cessna 402B, N51816, impacted the terrain while attempting an emergency landing at Pangborn Memorial Airport, Wenatchee, Washington. The commercial pilot, who was the sole occupant, was not injured, but the aircraft sustained substantial damage. The Part 135 cargo flight, which had just departed Pangborn Airport for Boeing Field, Seattle, Washington, was being operated in visual meteorological conditions at the time of the accident. The pilot had filed an IFR flight plan, and there was no report of an ELT activation.

According to the operator, the elevator trim actuator rod failed during the takeoff sequence when the aircraft was about 100 feet above ground level. The rod then became jammed in a manner that resulted in a nose-down trim greater than the normal full nose-down position. The pilot therefore immediately attempted an emergency landing on the runway from which he had just departed. During this attempted landing, the aircraft impacted the terrain about 300 feet short of the runway threshold.

The pilot stated that he estimated about 150 pounds down force on the yoke. He let go of the yoke with one hand to retard the throttles, and was unable to keep the aircraft from impacting short of the runway threshold.

FAA investigators found that the elevator trim tab was in the extreme nose-down trim position, while the cockpit trim wheel was found in the extreme nose-up trim position. The trim was tested with no effect. Inspectors then noted that the attaching bolt, nut, and cotter key for the trim-tab push rod to the trim-tab actuator-assembly was missing. The disconnected end of the trim- tab push rod was wedged behind the elevator spar, forcing the trim tab into its extreme nose-down trim position. Maintenance logs showed that the right elevator had been replaced on July 15, 1995, 24.9 flight hours prior to the accident. The mechanic performing the repair stated that he had used the old hardware to perform the installation, but he was certain he had installed the cotter key.

The operator provided an incomplete portion of the NTSB form 6120.1/2, which is attached.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA95LA159