N4829E

Destroyed
Serious

CESSNA 172N S/N: 17271668

Accident Details

Date
Monday, November 15, 1993
NTSB Number
FTW94FA034
Location
FORT COLLINS, CO
Event ID
20001211X13728
Coordinates
40.549728, -105.059547
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

POWER LOSS DUE TO THROTTLE LINKAGE DISCONNECT. FACTORS WERE MISSING COTTER KEY, IMPROPER MAINTENANCE, AND THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

Aircraft Information

Registration
N4829E
Make
CESSNA
Serial Number
17271668
Engine Type
Reciprocating
Model / ICAO
172N C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
NORTHERN COLORADO AIR CHARTER INC
Address
2200 AIRWAY AVE
Status
Deregistered
City
FORT COLLINS
State / Zip Code
CO 80524
Country
United States

Analysis

HISTORY OF FLIGHT

On November 15, 1993, approximately 1215 mountain standard time, a Cessna 172N, N4829E, was destroyed during a forced landing in a field near Fort Collins, Colorado, after the engine lost power. The pilot was seriously injured. Visual meteorological conditions prevailed, and no flight plan was filed for the instructional flight.

The following is based on interviews with the pilot and the Pilot/Operator Report. This was to be a student solo flight to the Fort Collins-Loveland Airport for touch-and-go landing practice. After takeoff, he made a right 30 degree crosswind noise abatement turn at an altitude between 800 and 1,000 feet above ground level (AGL), engine power decreased to idle. The pilot declared an emergency, attempted to troubleshoot the problem, then committed himself to a forced landing on a snow and ice-covered field. Braking action was nil and the airplane went down a hill and collided with an irrigation ditch.

TESTS AND RESEARCH

During an examination of the airplane, the following was revealed: A cotter pin (p/n 82-14, ref. no. 51) that fits into the lock nut (p/n 81-311, ref. no. 49) on the throttle lever (p/n 12-B57, ref. no. 2) was missing. The serrated surfaces of the throttle lever were not meshed and were riding on top of each other. The throttle valve (p/n 14-190, ref. no. 4) was closed because the throttle opening spring (p/n 24-A10, ref. no. 24), designed to fully open (page number. 11-42) was broken.

The following entry was made in the airplane's Maintenance Discrepancy Log: "11/12/93 DISCREPANCY: Throttle shaft loose. REPAIRED OR DEFERRED: Removed carburetor and removed throttle

shaft from carburetor to inspect for wear. New throttle shaft and bushings on order. Reinstalled throttle shaft with proper torque and safety. Reinstalled carburetor on aircraft. Removal and installation done in accordance with Cessna Service Manual 11-42." Similar entries were made in the airframe and engine logbooks. At the time the work was performed, the airplane;'s total time in service and tachometer reading was 4148.5. At the accident site, the tachometer read 4148.5.

The airplane mechanic was asked if he recalled installing the cotter pin in the throttle lever lock nut. He answered, "I'm almost sure I did."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94FA034