Accident Beechcraft 58 Baron N9253A,
ASN logo
ASN Wikibase Occurrence # 34976
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Friday 7 July 1989
Time:12:12
Type:Silhouette image of generic BE58 model; specific model in this crash may look slightly different    
Beechcraft 58 Baron
Owner/operator:Central Sales & Leasing
Registration: N9253A
MSN: TH-45
Total airframe hrs:4750 hours
Engine model:CONTINENTAL IO-520-C
Fatalities:Fatalities: 3 / Occupants: 4
Aircraft damage: Destroyed
Category:Accident
Location:Battle Creek, MI -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Executive
Departure airport:(BTL)
Destination airport:Newburgh, NY (SWF)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
DURING THE INITIAL CLIMB AFTER TAKEOFF, ONE OF THE CREW MEMBERS REPORTED THAT THE RIGHT ENGINE LOST POWER & THAT THEY WOULD RETURN FOR A LANDING. THE AIRCRAFT WAS OBSERVED TO CIRCLE TO THE LEFT WITH THE RIGHT PROP FEATHERED. DURING THE TURN TO THE AIRPORT, THE AIRCRAFT DESCENDED & CRASHED IN A SWAMPY AREA THAT WAS SURROUNDED BY TREES. A POST IMPACT FIRE ERUPTED & DESTROYED THE AIRCRAFT. SUBSEQUENT INVESTIGATION VERIFIED THAT THE RIGHT ENGINE PROPELLER HAD BEEN FEATHERED. THE FUEL SELECTOR FOR THE RIGHT ENGINE WAS FOUND POSITIONED BETWEEN 'OFF' & 'ON.' THE MAGNETO SWITCH FOR THE LEFT ENGINE WAS FOUND IN THE 'OFF' POSITION, WHILE THE MAGNETO SWITCH FOR THE RIGHT ENGINE WAS IN THE 'BOTH' POSITION. REMNANTS OF THE THROW-OVER YOKE SHOWED THAT IT WAS POSITIONED TO THE COPILOT'S SIDE. THE COPILOT'S FLIGHT TIME IN THE BEECH 58 WAS NOT VERIFIED. BOTH ENGS WERE REMOVED & PREPARED FOR OPERATIONAL CHECKS. AFTER WATER CONTAMINATION WAS CLEANED FROM THE ENGINES, BOTH WERE STARTED & RAN SUCCESSFULLY. CAUSE: THE FLIGHT CREW INADVERTENTLY SHUT DOWN THE LEFT ENGINE AFTER THE RIGHT ENGINE LOST POWER, AND THE COPILOT FAILED TO MAINTAIN CONTROL OF THE AIRCRAFT WHILE MANEUVERING THE AIRCRAFT BACK TOWARD THE RUNWAY. FACTORS RELATED TO THE ACCIDENT WERE: IMPROPER POSITIONING OF THE FUEL SELECTOR (PROBABLY) BY THE COPILOT AND IMPROPER MONITORING BY THE OTHER PILOT, WHICH RESULTED IN FUEL STARVATION TO THE RIGHT ENGINE.

Sources:

NTSB: https://www.ntsb.gov/ntsb/brief.asp?ev_id=20001213X28755

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org