Accident Beechcraft A100 King Air N30GC,
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ASN Wikibase Occurrence # 321837
 

Date:Tuesday 6 November 2007
Time:09:18
Type:Silhouette image of generic BE10 model; specific model in this crash may look slightly different    
Beechcraft A100 King Air
Owner/operator:RHB-JMJ LLC
Registration: N30GC
MSN: B-177
Year of manufacture:1973
Total airframe hrs:11849 hours
Engine model:Pratt & Whitney Canada PT6A-28
Fatalities:Fatalities: 2 / Occupants: 2
Aircraft damage: Destroyed, written off
Category:Accident
Location:1,2 km W of Chino Airport, CA (CNO) -   United States of America
Phase: Take off
Nature:Executive
Departure airport:Chino Airport, CA (CNO/KCNO)
Destination airport:Visalia Airport, CA (VIS/KVIS)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
A Beechcraft A100 King Air, N30GC, impacted trees about 3/4 mile from the departure end of runway 26R at Chino Airport (CNO), CA. The wreckage came to rest inverted in an open field located on the California Department of Corrections and Rehabilitation (CDCR) facility near the airport. The airplane was destroyed.
The commercial instrument rated pilot and the passenger were fatally injured. Instrument meteorological conditions prevailed for the flight.
The reported weather at the time of the accident was calm winds, a 1/4-mile visibility in fog and a vertical visibility of 100 feet. Shortly after takeoff for the instrument-flight-rules flight, the airplane made a slight turn to the left and impacted the tops of 25-foot trees about a 1/2 mile from the runway. An enhanced ground proximity warning system was installed on the airplane and data extraction from the system indicated that the airplane achieved an initial positive climb profile with a slight turn to the left and then a descent. A witness reported hearing the crash and observed the right wing impact the ground and burst into flames. The airplane then cartwheeled for several hundred feet before coming to rest inverted. The airframe, engines, and propeller assemblies were inspected with no mechanical anomalies noted that would have precluded normal flight.

PROBABLE CAUSE: "The pilot's failure to maintain a positive climb rate during an instrument takeoff. Contributing to the accident was the low visibility."

Accident investigation:
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Investigating agency: NTSB
Report number: LAX08FA026
Status: Investigation completed
Duration: 1 year and 6 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

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