ASN Wikibase Occurrence # 40661
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Date: | Friday 6 June 1997 |
Time: | 18:00 |
Type: | Lockheed P-38L Lightning |
Owner/operator: | Private |
Registration: | N7973 |
MSN: | 8006 |
Fatalities: | Fatalities: 1 / Occupants: 1 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | Tillamook, OR -
United States of America
|
Phase: | Approach |
Nature: | Private |
Departure airport: | Tillamook Municipal Airport, OR (KTMK) |
Destination airport: | Tillamook Municipal Airport, OR (KTMK) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:On June 6, 1997, approximately 1800 Pacific daylight time, a Lockheed P-38L "Lightning," retaining a limited airworthiness registration, N7973, registered to Bruce L. Pruett, and being flown by a commercial pilot, was destroyed during collision with terrain following a loss of control while on visual approach to the Tillamook airport, Tillamook, Oregon. The pilot was fatally injured and a post crash fire destroyed a portion of the aircraft. Visual meteorological conditions existed, and no flight plan had been filed. The flight, which was a practice run for an upcoming P-38 pilot convention (including the pilot's father, a World War II P-38 pilot), was to have been operated under 14CFR91.
The aircraft (P-38) had been topped off with full reserve & main fuel tanks (44 US gal/engine reserve tanks & 72 gal/engine main tanks). The pilot took off with about 20 minutes fuel having been already consumed. Operating with another P-38 within the airport area, the 2 aircraft flew about 20 to 25 minutes each. The fuel consumption was reported nominally at 60 gallons/hour/engine (1 gal/minute). With 44 gallons of fuel in each RESERVE tank for the duration of both flights, the engines would have exhausted all available fuel in each RESERVE tank after about 44 minutes. Both fuel selectors were found on the RESERVE setting at the site. No mechanical malfunction was found with either propeller or engine. The flaps & landing gear were retracted. According to the Pilot's Manual (flight manual), if one engine fails below 120 mph (safe single-engine airspeed), the pilot is to 'close both throttles and land straight ahead.' The flight manual did not provide any information for aircraft minimum control speeds with the flaps fully retracted. Several witnesses reported the aircraft was slow while turning base. Since this was a single-seat aircraft, there was no provision for 'dual' instructional training in single-engine procedures or spin recovery. The pilot was reported to have flown 6 or 7 hours in another P-38, which included practice simulated single-engine maneuvers, but no actual in-flight shut down & feathering of an engine.
Probable Cause: Failure of the pilot to maintain minimum control speed (VMC), after loss of power in one engine, which resulted in a loss of aircraft control and collision with terrain. Related factors were: the pilot's improper fuel management and failure to change the fuel selector position before a fuel tank had emptied, which led to fuel starvation and loss of power in one engine; and the pilot's lack of familiarity with the aircraft, relative to single-engine minimum airspeeds.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | |
Status: | Investigation completed |
Duration: | 1 year and 4 months |
Download report: | Final report |
|
Sources:
NTSB:
http://www.ntsb.gov/ntsb/brief.asp?ev_id=20001208X08240 Images:
Photo: NTSB
Revision history:
Date/time | Contributor | Updates |
24-Oct-2008 10:30 |
ASN archive |
Added |
07-Dec-2010 15:28 |
harro |
Updated [Aircraft type] |
21-Dec-2016 19:23 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
18-Oct-2022 17:44 |
Captain Adam |
Updated [Operator, Nature, Departure airport, Destination airport, Narrative, Accident report, Photo] |
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