ASN Wikibase Occurrence # 188420
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Date: | Monday 27 June 2016 |
Time: | 21:00 |
Type: | Cessna 150L |
Owner/operator: | Air America Aerial Ads |
Registration: | N6622G |
MSN: | 15072122 |
Year of manufacture: | 1970 |
Total airframe hrs: | 9907 hours |
Engine model: | Lycoming O-360-A4M |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Other fatalities: | 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Coleman A Young Municipal Airport (KDET), Detroit, MI -
United States of America
|
Phase: | Landing |
Nature: | Banner and glider towing |
Departure airport: | Detroit, MI (DET) |
Destination airport: | Detroit, MI (DET) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The commercial pilot was conducting a banner-tow flight. He reported that the airplane experienced a total loss of engine power after being airborne for at least 3 hours 9 minutes. He informed the tower controller of his emergency, released the banner, and conducted a forced landing to a nearby street. The airplane collided with a power line during the forced landing. The pilot reported that he had used a higher-than-normal engine power setting to maintain altitude throughout the accident flight.
A postaccident examination of the fuel system established that the left fuel tank was empty, that the right fuel tank contained residual fuel, and that the gascolator contained a few ounces of fuel. A subsequent test run established that there were no anomalies with the engine that would have precluded normal operation.
The operator had a policy that limited all banner-tow flights in the accident airplane to 3 hours or less to avoid fuel exhaustion. The operator also noted that environmental considerations, such as operating at a high-density altitude and/or in windy conditions, could require a higher-than-normal engine power setting and increased fuel consumption. Additionally, the operator told its pilots that banner-tow flights operating in such conditions should be reduced to between 2 hours 30 minutes and 2 hours 45 minutes. The pilot had received a verbal briefing within a month of the accident that covered the operator’s policy regarding the maximum allowable flight duration in the accident airplane while towing banners and acknowledged knowing these procedures.
Probable Cause: The pilot’s disregard of the banner-tow operator's policy regarding the maximum allowable flight duration, which resulted in a total loss of engine power due to fuel exhaustion.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CEN16LA236 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB
FAA register:
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=6622G
History of this aircraft
Other occurrences involving this aircraft
12 February 2011 |
N6622G |
Drake Aerial Enterprises LLC Dba |
0 |
Trenton, Michigan |
|
sub |
Maintenance issues |
Location
Revision history:
Date/time | Contributor | Updates |
28-Jun-2016 13:48 |
Geno |
Added |
28-Jun-2016 13:49 |
Geno |
Updated [Source] |
07-Jul-2016 04:26 |
Geno |
Updated [Other fatalities, Narrative] |
04-Feb-2017 11:07 |
Iceman 29 |
Updated [Source, Narrative] |
05-May-2017 07:31 |
PiperOnslaught |
Updated [Source, Narrative] |
19-Aug-2017 14:56 |
ASN Update Bot |
Updated [Operator, Nature, Departure airport, Destination airport, Source, Narrative] |
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