Fuel exhaustion Accident Piper PA-25-235 Pawnee N8808L,
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ASN Wikibase Occurrence # 166588
 
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Date:Wednesday 28 May 2014
Time:15:00
Type:Silhouette image of generic PA25 model; specific model in this crash may look slightly different    
Piper PA-25-235 Pawnee
Owner/operator:Soaring Society of Boulder Inc.
Registration: N8808L
MSN: 25-5306
Year of manufacture:1971
Total airframe hrs:8847 hours
Engine model:Lycoming O-540-B2C5
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:WNW of Boulder Municipal Airport (KBDU), Boulder, Colorado -   United States of America
Phase: Approach
Nature:Banner and glider towing
Departure airport:Boulder, CO (BDU)
Destination airport:Boulder, CO (BDU)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that the accident occurred during his fifth glider aero-tow flight since the airplane had last been refueled. He stated that the aero-tow and glider release were uneventful. However, as he was returning to the departure airport, the engine began to run intermittently before it eventually experienced a total loss of engine power. During the subsequent forced landing, the airplane became entangled with a chain-link fence and impacted a road before it slid into a drainage ditch.
A postaccident examination of the airplane’s single fuel tank established that it was undamaged and void of any usable fuel. Before the first flight of the day, the airplane was refueled, and the total usable fuel was about 32.5 gallons. The airplane recording tachometer indicated that 2.2 tachometer hours had been accumulated since that time. Although the airplane operator reported that, according to historical fueling and flight data, the airplane’s average fuel consumption rate was about 10.2 gallons per tachometer hour, the calculated average fuel consumption rate was 14.8 gallons per tachometer hour since the last refueling. Although the total loss of engine power was caused by fuel exhaustion, the investigation could not determine the reason for the above-normal fuel consumption rate. However, if the pilot had determined the actual fuel consumption rate between flights, he should have identified that insufficient fuel was available to complete the accident flight.

Probable Cause: The pilot's failure to adequately monitor the airplane's actual fuel consumption rate, which resulted in a total loss of engine power due to fuel exhaustion.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN14LA261
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB

History of this aircraft

Other occurrences involving this aircraft
31 July 1995 N8808L Private 0 Shelley, ID sub

Location

Images:


Photo taken at the crash site ~30 minutes after the incident.

Media:

Revision history:

Date/timeContributorUpdates
28-May-2014 22:44 Geno Added
28-May-2014 22:46 Geno Updated [Aircraft type]
28-May-2014 22:52 Geno Updated [Source]
29-May-2014 05:37 harro Updated [Embed code]
30-May-2014 04:59 Geno Updated [Time, Source, Embed code, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
29-Nov-2017 14:24 ASN Update Bot Updated [Operator, Other fatalities, Nature, Departure airport, Destination airport, Source, Embed code, Narrative]
23-Sep-2020 20:08 Anon. Updated [Embed code, Photo]

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