Accident Piper PA-30 Twin Comanche N7350Y,
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ASN Wikibase Occurrence # 167623
 
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Date:Wednesday 25 June 2014
Time:17:00
Type:Silhouette image of generic PA30 model; specific model in this crash may look slightly different    
Piper PA-30 Twin Comanche
Owner/operator:Ridgeaire Inc
Registration: N7350Y
MSN: 30-404
Year of manufacture:1964
Total airframe hrs:4862 hours
Engine model:Lycoming IO-320 SERIES
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Glacier Park International Airport, Kalispell, Montana -   United States of America
Phase: Take off
Nature:Private
Departure airport:Kalispell, MT (GPI)
Destination airport:Eureka, MT (88M)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The commercial pilot reported that, during takeoff for the cross-country flight, the right engine lost power. The airplane, which was about 10 ft above the ground, then veered right away from the runway. The pilot immediately switched fuel tanks, raised the landing gear, and feathered both propellers. Subsequently, the airplane entered about an 80-degree right bank, and the pilot was able to get the airplane nearly level, applying full left aileron and rudder, just before it contacted the ground. The airplane came to rest about 500 ft off the right side of the runway. During the accident sequence, the right engine separated from the fuselage. After the accident, the pilot shut off the fuel valves; he did not recall which position the fuel selectors were set to for takeoff. Postaccident examination of the airframe and right engine did not reveal any anomalies or failures that would have precluded normal operation.
Postaccident examination of the airplane revealed that the main fuel tanks appeared to be empty but that the auxiliary tanks, which have a total capacity of 30 gallons, appeared to be almost full. The pilot reported taking off with a total fuel quantity of 30 gallons; therefore, most of the usable fuel was in the auxiliary tanks. The airplane flight manual states that, for takeoff, the fuel selectors should be selected “on” to the main fuel tanks. It is likely that the pilot followed these procedures, which led to the fuel starvation of the right engine. The Pilot’s Operating Handbook preflight check included a step to visually check each tank’s fuel quantity on the gauge and to visually check the fuel quantity in each tank during the walkaround inspection. Based on the evidence, it is likely that the pilot did not adequately follow these procedures before the flight.


Probable Cause: The pilot’s inadequate preflight planning and checks, during which he failed to determine the quantity and distribution of the fuel, which resulted in the loss of right engine power during takeoff due to fuel starvation.


Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR14LA269
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB
FAA register: 2. FAA: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?omni=Home-N-Number&nNumberTxt=7350Y

5. https://uk.flightaware.com/resources/registration/N7350Y

Location

Revision history:

Date/timeContributorUpdates
28-Jun-2014 00:55 Geno Added
28-Feb-2016 21:11 Dr.John Smith Updated [Time, Departure airport, Destination airport, Source, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
17-Apr-2017 21:36 Dr.John Smith Updated [Time, Location, Departure airport, Destination airport, Source, Narrative]
29-Nov-2017 15:02 ASN Update Bot Updated [Time, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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