# TCDS H3SW: Brantly International Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Brantly International Inc.
- Revision: 10
- Revised: October 17, 1990
- Product: Aircraft, Rotorcraft
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B186D0C98F70D3438525671500566016.0001
- Page: https://openairdocs.org/tcds/H3SW

## Models (1)

- 305

## ADs (5)

- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 2021-26-09](https://openairdocs.org/ad/2021-26-09): Tail Rotor Head · Brantly International 305, B-2, B-2A and 1 more. Effective Jan 19, 2022
- [AD 76-08-06](https://openairdocs.org/ad/76-08-06): Main Rotor Hub Clevis Bearing · Brantly International 305. Effective May 25, 1976
- [AD 68-05-02](https://openairdocs.org/ad/68-05-02): Tail Rotor Drive Shaft · Brantly International 305, B-2, B-2A and 1 more. Effective Mar 30, 1968
- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.