Accident Beechcraft C55 Baron N282JL,
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ASN Wikibase Occurrence # 176649
 
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Date:Wednesday 28 April 2004
Time:15:20
Type:Silhouette image of generic BE55 model; specific model in this crash may look slightly different    
Beechcraft C55 Baron
Owner/operator:Private
Registration: N282JL
MSN: TE-355
Total airframe hrs:3948 hours
Engine model:Continental IO-550
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Rifle, CO -   United States of America
Phase: Landing
Nature:Private
Departure airport:Telluride Regional Airport, CO (TEX/KTEX)
Destination airport:Glenwood Springs Municipal Airport, CO (GWS/KGWS)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
According to the pilot, while en route to his home base, he experienced an electrical system malfunction. Due to the wind gust conditions at his home base, he elected to divert to a second airport. While on approach to the second airport, the airplane's electrical system became more erratic, which included the illumination of all warning lights on the digital exhaust gas temperature (EGT) gauge and the indication of "extreme" engine temperatures of over 1,650 degrees. Shortly thereafter, the electrical system failed. He immediately attempted to lower the flaps and landing gear, but the flaps only partially lowered. The pilot hand cranked the landing gear half way down, but because of the severe turbulence, asked his passenger to assist him while he flew the airplane. When the passenger finished, the pilot verified that the landing gear crank had "quit turning." The pilot stated that, due to the "extreme danger" of a possible engine fire, he elected not to attempt a fly-by to verify that the landing gear was extended. When he attempted to land on runway 26, he felt both propellers strike the runway. When he "cut" the power to both engines, the airplane settled onto the runway, and slid approximately 1,000 feet before coming to a stop on the grass just off the right side of the runway. The pilot realized that the passenger had inadvertently raised the landing gear, resulting in an unintentional gear-retracted landing. Later, it was determined that several fractured propeller pieces had impacted the fuselage resulting in substantial damage to several fuselage bulkheads. An examination of the airplane's electrical system, which included a 2-hour ferry flight, showed no anomalies.


Probable Cause: the pilot's failure to verify the manual extension of the landing gear resulting in an inadvertent wheels up landing. Contributing factors include the electrical systems failure for undetermined reasons, the pilot's diverted attention and the pilot's improper in-flight planning and decision making.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DEN04LA075
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20040615X00791&key=1

Revision history:

Date/timeContributorUpdates
04-Jun-2015 20:52 Noro Added
21-Dec-2016 19:30 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
07-Dec-2017 17:54 ASN Update Bot Updated [Cn, Other fatalities, Departure airport, Destination airport, Source, Narrative]
07-Jun-2023 06:04 Ron Averes Updated [[Cn, Other fatalities, Departure airport, Destination airport, Source, Narrative]]

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