ASN Wikibase Occurrence # 355685
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Wednesday 25 June 1997 |
Time: | 22:15 LT |
Type: | Cessna 172N |
Owner/operator: | Great Lakes Aeronautical Club |
Registration: | N7031Q |
MSN: | 172-60331 |
Total airframe hrs: | 4399 hours |
Engine model: | Lycoming O-360-A4M |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Canton, MI -
United States of America
|
Phase: | Unknown |
Nature: | Private |
Departure airport: | Grand Haven, MI (3GM |
Destination airport: | (1D2) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:According to the pilot, he was established on final approach for a landing on runway 36 without the flaps lowered, when he realized that he was too high, and he made a decision to go around. The engine did not respond to throttle movement. The pilot knew of an open field north of the runway, but he thought it was not long enough to stop the aircraft so he executed a steep left turn to land on a nearby road that was perpendicular to the runway. During the turn, the left wing contacted the ground. Winds were reported as 180 degrees at 7 knots at Detroit Metropolitan Wayne County Airport, ten miles to the southeast. Inspection of the carburetor disclosed that the throttle arm was installed out of position such that when the throttle was pulled fully closed the arm was pointing straight back at the cable. In this position, when the throttle was advanced in the cockpit, the cable and housing would bind and could allow the throttle arm on the carburetor to move upward instead of down and forward through the normal arch.
Probable Cause: A loss of engine power due to fuel starvation from a binding throttle/power lever cable. Also causal was the improper maintenance, installation of the throttle arm. Contributing to the accident were the dark night and unsuitable terrain for the forced landing.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CHI97FA188 |
Status: | Investigation completed |
Duration: | 3 years and 2 months |
Download report: | Final report |
|
Sources:
NTSB CHI97FA188
Location
Revision history:
Date/time | Contributor | Updates |
12-Mar-2024 14:32 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation