# Tail rotor drive shaft

- Type: NTSB finding subsection
- Path: [Aircraft](https://openairdocs.org/ntsb-findings/01) › [Aircraft propeller/rotor](https://openairdocs.org/ntsb-findings/0104) › [Tail rotor drive system](https://openairdocs.org/ntsb-findings/010465) › Tail rotor drive shaft
- NTSB code: 01046510
- Cases: 25
- In the probable cause: 20
- Fatal cases: 2
- All cases: https://openairdocs.org/ntsb-findings/01046510/cases.md
- Cases with it in the probable cause: https://openairdocs.org/ntsb-findings/01046510/cases.md?cause=1
- Page: https://openairdocs.org/ntsb-findings/01046510

## Cases per year (in the probable cause / all)

- 2008: 1 / 2
- 2009: 0 / 1
- 2011: 3 / 3
- 2012: 1 / 3
- 2013: 1 / 1
- 2015: 5 / 5
- 2017: 1 / 1
- 2021: 3 / 3
- 2022: 2 / 2
- 2024: 3 / 4

## Defining events in these cases

- [Sys/Comp malf/fail (non-power)](https://openairdocs.org/ntsb-events/330): 10 cases
- [Flight control sys malf/fail](https://openairdocs.org/ntsb-events/333): 7 cases
- [Loss of control in flight](https://openairdocs.org/ntsb-events/240): 2 cases
- [Miscellaneous/other](https://openairdocs.org/ntsb-events/900): 1 cases
- [External load event (Rotorcraft)](https://openairdocs.org/ntsb-events/480): 1 cases
- [Part(s) separation from AC](https://openairdocs.org/ntsb-events/338): 1 cases
- [Aircraft structural failure](https://openairdocs.org/ntsb-events/337): 1 cases
- [Loss of tail rotor effectiveness](https://openairdocs.org/ntsb-events/242): 1 cases
- [Low altitude operation/event](https://openairdocs.org/ntsb-events/220): 1 cases

## Aircraft models (registry)

- [Robinson Helicopter R22 BETA](https://openairdocs.org/model/robinson-helicopter-r22-beta): 2 cases
- [Bell 206L-3](https://openairdocs.org/model/bell-206l-3): 2 cases
- [Sikorsky S-92A](https://openairdocs.org/model/sikorsky-s-92a): 1 cases
- [Robinson Helicopter R44 II](https://openairdocs.org/model/robinson-helicopter-r44-ii): 1 cases
- [Hughes Helicopters HUGHES 369D](https://openairdocs.org/model/hughes-helicopters-hughes-369d): 1 cases
- [Hughes 269B](https://openairdocs.org/model/hughes-269b): 1 cases
- [Hiller UH-12A](https://openairdocs.org/model/hiller-uh-12a): 1 cases
- [Enstrom Helicopter 280C](https://openairdocs.org/model/enstrom-helicopter-280c): 1 cases
- [Mcdonnell Douglas Heli 369FF](https://openairdocs.org/model/mcdonnell-douglas-heli-369ff): 1 cases
- [Continental Copters 47G](https://openairdocs.org/model/continental-copters-47g): 1 cases

## Other findings in the same cases

- [Aircraft control](https://openairdocs.org/ntsb-findings/02063040) (Personnel issues): 3 cases
- [Directional control](https://openairdocs.org/ntsb-findings/01062020) (Aircraft): 3 cases
- [Not determined, general](https://openairdocs.org/ntsb-findings/05000000) (Not determined): 2 cases
- [Installation](https://openairdocs.org/ntsb-findings/02062035) (Personnel issues): 2 cases
- [Yaw control](https://openairdocs.org/ntsb-findings/01062024) (Aircraft): 2 cases
- [Maintenance records](https://openairdocs.org/ntsb-findings/04033025) (Organizational issues): 1 cases
- [Initial training](https://openairdocs.org/ntsb-findings/04031010) (Organizational issues): 1 cases
- [Training, general](https://openairdocs.org/ntsb-findings/04031000) (Organizational issues): 1 cases
- [Adequacy of policy/proc](https://openairdocs.org/ntsb-findings/04021015) (Organizational issues): 1 cases
- [Debris/dirt/foreign object](https://openairdocs.org/ntsb-findings/03022055) (Environmental issues): 1 cases

## Newest cases

- [NTSB ERA25LA040](https://openairdocs.org/ntsb/ERA25LA040), Nov 5, 2024: Hughes 369D (N11AS), Waycross, GA, substantial damage. Probable cause: An encounter with a foreign object, which resulted in a loss of control and collision with terrain.
- [NTSB ERA24LA263](https://openairdocs.org/ntsb/ERA24LA263), Jun 14, 2024: Rotorway Exec (N99TE), Alva, FL, substantial damage. Probable cause: A loss of tail rotor control as a result of unsecured tail rotor drive belt tensioner bolts.
- [NTSB ERA24LA205](https://openairdocs.org/ntsb/ERA24LA205), May 1, 2024: Airbus Helicopters AS350B3 (N413JM), Plant City, FL, substantial damage. Probable cause: The pilot’s inadequate yaw control of the helicopter while maneuvering at a low altitude and airspeed, which resulted in a hard landing.
- [NTSB ANC24LA013](https://openairdocs.org/ntsb/ANC24LA013), Feb 11, 2024: Robinson Helicopter R44 II (N74868), Glacier View, AK, substantial damage. Probable cause: A sudden stoppage of the tail rotor for unknown reasons, which resulted in the tortional overload failure of the tail rotor driveshaft.
- [NTSB WPR23LA004](https://openairdocs.org/ntsb/WPR23LA004), Oct 1, 2022: Bell 206B (N284CA), Fresno, CA, substantial damage. Probable cause: The disbond of a tail rotor drive shaft splined adapter, which resulted in a loss of tail rotor drive and a subsequent hard landing.
- [NTSB WPR22LA340](https://openairdocs.org/ntsb/WPR22LA340), Sep 10, 2022: Bell Helicopter Textron 206L-1 (N242BH), Banning, CA, substantial damage. Probable cause: The improper attachment of the tail rotor drive shaft to the air conditioner drive pulley without a drive ring, which resulted in the failure of the hardware, a loss of tail rotor drive, and the loss…
- [NTSB CEN21LA389](https://openairdocs.org/ntsb/CEN21LA389), Aug 27, 2021: Robinson Helicopter R22 Beta (N827SH), Arnaudville, LA, substantial damage. Probable cause: The loss of tail rotor drive due to a fatigue failure of the tail rotor gearbox output shaft, which resulted in a loss of control during landing.
- [NTSB ERA21LA339](https://openairdocs.org/ntsb/ERA21LA339), Aug 21, 2021: Enstrom 280 (N9285), Port Orange, FL, substantial damage. Probable cause: The failure of the tail rotor drive shaft at the coupling due to torsionally applied shear stress.
- [NTSB ERA21FA195](https://openairdocs.org/ntsb/ERA21FA195), Apr 28, 2021: Bell Helicopter Textron Canada 429 (N53DE), Eden, NC, destroyed, 1 fatal. Probable cause: The impact of the main rotor blades with the tail boom during low-altitude maneuvers, which severed the tail rotor drive shaft and resulted in a loss of control and impact with terrain.
- [NTSB CEN17LA375](https://openairdocs.org/ntsb/CEN17LA375), Sep 11, 2017: Hiller UH 12A (N2686), Griffith, IN, substantial damage. Probable cause: The loss of tail rotor thrust due to a failed tail rotor driveshaft, which resulted in a loss of tail rotor control and a hard landing.

NTSB has coded findings and defining events since 2008; earlier cases used its older occurrence and cause codes and aren't counted.

Findings: https://openairdocs.org/ntsb-findings.md. Defining events: https://openairdocs.org/ntsb-events.md. Phases of flight: https://openairdocs.org/ntsb-phases.md. Every investigation, filtered by finding, event, phase, state, year or model: https://openairdocs.org/ntsb.md (for example ?state=MI&fatal=1).

NTSB's definitions: Accident and incident, 49 CFR 830.2 (https://www.ecfr.gov/current/title-49/subtitle-B/chapter-VIII/part-830/subpart-A/section-830.2), CICTT occurrence categories (PDF) (https://www.ntsb.gov/safety/data/Documents/datafiles/OccurrenceCategoryDefinitions.pdf), CICTT phases of flight (PDF) (https://www.ntsb.gov/safety/data/Documents/datafiles/PhaseofFlightDefinitions.pdf), and NTSB coding manual, before 2008 (PDF) (https://www.ntsb.gov/GILS/Documents/codman.pdf). NTSB publishes no definitions for its findings, only their names.

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