Accident Taylorcraft F21B N4418U,
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ASN Wikibase Occurrence # 385624
 
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Date:Thursday 12 July 2001
Time:07:45 LT
Type:Taylorcraft F21B
Owner/operator:Flying Wolf Ltd.
Registration: N4418U
MSN: 1518
Total airframe hrs:453 hours
Engine model:Lycoming O-235-L2C
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Simsbury, CT -   United States of America
Phase: Landing
Nature:Training
Departure airport:Simsbury, CT (4B9)
Destination airport:(4B9)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
According to the CFI, the private pilot was executing touch and go's on runway 03. During the third landing, after touchdown, the airplane's tailwheel began to "chatter." The airplane started to veer to the right and did not respond to left rudder or brake inputs by the CFI, who had taken over the controls. The airplane then departed the right side of the runway and nosed over. Examination of the airplane revealed that the high and low frequency anti-shimmy compression springs on the tailwheel assembly "had slack." The "slack" allowed for about 2 inches of rudder movement before the compression springs became effective. Review of the airplane's maintenance records revealed that it had seven annual inspections performed after the installation of the tailwheel assembly. The most recent annual inspection was conducted about four months prior to the accident, and the airplane had accumulated about 15 hours of operation since. According to FAA regulations, Appendix D of Part 43, Scope And Detail Of Items To Be Included In Annual And 100-Hour Inspections, each person performing an annual or 100-hour inspection shall inspect all units of the landing gear group for poor condition and insecurity of attachment. The winds reported at a nearby airport, about the time of the accident, were from 320 degrees at 10 knots.

Probable Cause: **This report was modified on 2/24/2016. Refer to the public docket for this accident for additional details.**

a loose tail wheel assembly and the failure of maintenance personnel to adequately follow annual inspection procedures. A factor in the accident was the crosswind.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: NYC01LA170
Status: Investigation completed
Duration: 10 months
Download report: Final report

Sources:

NTSB NYC01LA170

Location

Revision history:

Date/timeContributorUpdates
05-Apr-2024 06:11 ASN Update Bot Added

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