N1763U

Substantial
Minor

Cessna 207 S/N: 20700363

Accident Details

Date
Friday, July 17, 1998
NTSB Number
ANC98LA099
Location
KING SALMON, AK
Event ID
20001211X10452
Coordinates
58.749328, -156.540176
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The disconnection of the mixture control cable from the mixture control arm. Factors associated with this accident were the inadequate 100 hour inspections performed by company mechanics.

Aircraft Information

Registration
N1763U
Make
CESSNA
Serial Number
20700363
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
207 C07T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
YUTE AIR ALASKA INC
Address
PO BOX 190169
Status
Deregistered
City
ANCHORAGE
State / Zip Code
AK 99519-0169
Country
United States

Analysis

On July 16, 1998, at 1725 Alaska daylight time, a Cessna 207 airplane, N1763U, sustained substantial damage when it nosed over during a forced landing 7 miles south of the King Salmon Airport, King Salmon, Alaska. The solo commercial pilot sustained minor injuries. The flight was operated under 14 CFR Part 135 by Yute Air Alaska, Inc., of Anchorage, Alaska, as a nonscheduled cargo flight. The flight departed King Salmon at 1720, transporting bypass mail to Egegik, Alaska. Visual meteorological conditions prevailed at the time of the accident, and a company VFR flight plan was filed.

The pilot told the NTSB investigator on July 16, 1998, that he leveled off to cruise at 700 feet msl, and began to lean the engine's mixture control. He said that about 10 miles south of King Salmon, the mixture control stopped having an effect on engine operation, and the engine began to lose power. While turning towards the airport, the engine lost total power, and he performed an emergency landing. During landing, the airplane nosed over.

Postaccident inspection revealed that the mixture control arm had unscrewed from the mixture control cable. The Cessna 207 Service Manual specifies the jam nuts which attach the cable to the control be torqued to 15 inch-pounds, plus or minus 2 inch-pounds. There is no safety wire required in the installation.

A review of the engine maintenance records indicated that the engine had received 100 hour inspections 44 hours, and 142 hours, prior to the accident. On both these occasions, Service Bulletin SEB95-15R1 (Throttle Control Lever Inspection) was performed. This lever is located next to the disconnected mixture control arm linkage. The mixture control cable was replaced 238 hours prior to the accident.

Inspection of a representative C-207 installation by the NTSB investigator-in-charge revealed that if the mixture control arm becomes disconnected, gravity allows the arm to fall to the lean / idle-cutoff position.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA099