Accident RotorWay Exec 162F N929BL,
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ASN Wikibase Occurrence # 386166
 
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Date:Saturday 3 March 2001
Time:15:30 LT
Type:Silhouette image of generic EXEC model; specific model in this crash may look slightly different    
RotorWay Exec 162F
Owner/operator:Bradley Lenart
Registration: N929BL
MSN: 6246
Total airframe hrs:36 hours
Engine model:Rotorway RI 162F
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Wallingford, CT -   United States of America
Phase: Take off
Nature:Training
Departure airport:Wallingford, CT (NONE)
Destination airport:Seymour, CT (NONE)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
In preparation for an instructional flight, the flight instructor flew the helicopter from the student pilot/builder's yard to an open field across the street for the purpose of added take-off room with two people on board. Prior to this relocation, the forward ballast weight required for solo operations remained on the front right skid. The flight instructor and student agreed that the student would move the ballast weight from the forward right skid to the tail boom before getting into the helicopter. When the student met the instructor across the street, he was concerned about the skids being in the dirt. The instructor reassured the student that the ground was solid. The instructor then slid from the left seat to the right seat and the student got into the helicopter and sat in the left seat. Both occupants forgot about repositioning the ballast weight. When the instructor lifted the helicopter to hover, the nose pitched down and the helicopter accelerated forward into trees. The instructor stated that he did not use the pre-take off checklist, which would have reminded him about repositioning the ballast weight. Examination of the flight manual revealed that in the weight and balance section, it stated: "SOLO flight is performed ONLY FROM THE LEFT SEAT, and must have the ballast weight placed on the front passenger skid. DUAL flight requires the ballast weight be placed on the rear mount tube under the tail boom." There were no mechanical deficiencies.

Probable Cause: flight instructor's failure to follow published checklist procedures, which resulted in the forward ballast weight not being moved to the tailboom prior to departure.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: IAD01LA036
Status: Investigation completed
Duration: 6 months
Download report: Final report

Sources:

NTSB IAD01LA036

Location

Revision history:

Date/timeContributorUpdates
05-Apr-2024 11:52 ASN Update Bot Added

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