ASN Wikibase Occurrence # 296394
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 27 November 2002 |
Time: | 19:00 LT |
Type: | Cessna TR182 |
Owner/operator: | Peter Geier |
Registration: | N4929S |
MSN: | R18201468 |
Year of manufacture: | 1980 |
Total airframe hrs: | 3448 hours |
Engine model: | Lycoming O-540-L3C5D |
Fatalities: | Fatalities: 0 / Occupants: 4 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Willoughby, Ohio -
United States of America
|
Phase: | Unknown |
Nature: | Private |
Departure airport: | Willoughby Lost Nation Municipal Airport, OH (LNN/KLNN) |
Destination airport: | Cincinnati Municipal Airport, OH (LUK/KLUK) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:Shortly after departing, the pilot started to experience an electrical problem, and then a complete loss of electrical power. While maneuvering to land at his departure airport, the pilot selected the landing gear to the "DOWN" position, and ultimately "FULL" flaps. The airplane touched down on runway 05, with the landing gear partially extended approximately 3,700 feet down the 5,028-foot long runway, and overran the end by approximately 100 feet. Examination of the airplane confirmed flight control continuity to all the flight control surfaces, and a landing gear operational check revealed no anomalies. An engine run was then performed. The engine functioned normally and engine control continuity was confirmed. The electrical master switch was a split rocker type, the left side controlled the alternator, and the right controlled the battery. With the engine operating, the alternator was turned off. It quit charging, and the battery picked up the load. The alternator was then turned back on. It picked up the load, and started charging the battery. The alternator was required to be in the "ON" position during normal operations. Winds were reported to be from 270 degrees at 20 knots.
Probable Cause: The pilot's failure to select the alternator to the "ON" position before initiating the flight. A factor in the accident was the tailwind which resulted in the overrun.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | NYC03LA026 |
Status: | Investigation completed |
Duration: | 1 year 1 month |
Download report: | Final report |
|
Sources:
NTSB NYC03LA026
Revision history:
Date/time | Contributor | Updates |
14-Oct-2022 05:52 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation