Accident Beechcraft D55 Baron N222JJ,
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ASN Wikibase Occurrence # 290334
 
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Date:Saturday 27 September 2014
Time:13:45 LT
Type:Silhouette image of generic BE55 model; specific model in this crash may look slightly different    
Beechcraft D55 Baron
Owner/operator:Jld Conyngham Ltd
Registration: N222JJ
MSN: TE-639
Year of manufacture:1968
Total airframe hrs:3463 hours
Engine model:Continental IO 520 SERIES
Fatalities:Fatalities: 0 / Occupants: 4
Aircraft damage: Substantial
Category:Accident
Location:Hazleton, PA -   United States of America
Phase: Landing
Nature:Private
Departure airport:Hazleton Airport, PA (HZL/KHZL)
Destination airport:Hazleton Airport, PA (HZL/KHZL)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
After an uneventful 30 minute flight the pilot returned to the airport and entered the traffic pattern for a full stop landing on runway 28; the wind at the time was variable at 3 knots. He reported the touchdown was normal, but about 5 to 10 seconds after touchdown, "the plane started rumbling and pulling hard to the left"; he confirmed he was not on the airplane's brakes at that time. He reported the nose steering was not effective, and when the left main landing gear wheel was in the grass, he advanced the left throttle in an attempt to overcome the left turning tendency. The airplane then contacted a temporary rock road and both main landing gears collapsed. All occupants exited the airplane uninjured, and when he deemed it safe, he reentered the airplane and secured the fuel selectors.

Postaccident inspection of the airplane by several FAA inspectors revealed the left tire was deflated and a hole was completely worn through the casing on an area of the tread, and also through the tube. Postaccident operational testing of the airplane's brake system revealed no evidence of preimpact failure or malfunction. The brakes released with release of pressure on the brake pedals; no sticking was noted. Damage to a portion of the left wing at the leading edge and main spar was noted. Damage was also noted the main spar of the left aileron, and to structure on the lower fuselage aft of the wing trailing edge.

Probable Cause: The brake application for unknown reasons resulting in rupture of the left main landing gear tire and tube, and subsequent loss of directional control.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA14CA463
Status: Investigation completed
Duration: 3 months
Download report: Final report

Sources:

NTSB ERA14CA463

Location

Revision history:

Date/timeContributorUpdates
06-Oct-2022 13:53 ASN Update Bot Added
06-Jun-2023 04:04 Ron Averes Updated

Corrections or additions? ... Edit this accident description

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