# Airworthiness directives that may apply: Brantly B-2A

A list on [Brantly B-2A](https://openairdocs.org/model/brantly-b-2a.md).

Matched by model name and maker. Each AD’s applicability may narrow it by serial number, part number or configuration.

- [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07.md): Ground Proximity System · Effective Jun 22, 2023 · Supersedes AD 2021-23-13
- [AD 2021-26-09](https://openairdocs.org/ad/2021-26-09.md): Tail Rotor Head · Effective Jan 19, 2022
- [AD 2014-20-16](https://openairdocs.org/ad/2014-20-16.md): Main Rotor Blade · Effective Nov 12, 2014
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07.md): ECi cylinder assemblies · Effective Jul 11, 2006 · Supersedes AD 2005-26-10
- [AD 2006-08-07](https://openairdocs.org/ad/2006-08-07.md): Upper tail rotor vertical gearbox (gearbox) · Effective May 2, 2006
- [AD 68-04-04 R2](https://openairdocs.org/ad/68-04-04-R2.md): Tail Rotor Blade · Effective Feb 14, 1983
- [AD 81-17-01](https://openairdocs.org/ad/81-17-01.md): Starting Vibrator Assemblies · Effective Aug 13, 1981
- [AD 72-21-02](https://openairdocs.org/ad/72-21-02.md): Pylon Bearing Shaft · Effective Dec 8, 1972
- [AD 71-17-05](https://openairdocs.org/ad/71-17-05.md): Main Rotor Mast · Effective Nov 26, 1971
- [AD 68-05-02](https://openairdocs.org/ad/68-05-02.md): Tail Rotor Drive Shaft · Effective Mar 30, 1968
- [AD 67-09-02](https://openairdocs.org/ad/67-09-02.md): Main Rotor Mast · Effective Apr 20, 1967
- [AD 65-28-01](https://openairdocs.org/ad/65-28-01.md): Tail Rotor Blades · Effective Dec 14, 1965
- [AD 62-06-01](https://openairdocs.org/ad/62-06-01.md): Seat Back Adjustment · Effective Mar 23, 1962
- [AD 62-05-02](https://openairdocs.org/ad/62-05-02.md): Fuel Pump Seals · Effective Feb 28, 1962
- [AD 61-23-01](https://openairdocs.org/ad/61-23-01.md): Rotor Blade Bond Separation · Effective Nov 4, 1961
- [AD 61-18-02](https://openairdocs.org/ad/61-18-02.md): Tail Rotor Modification · Effective Aug 29, 1961
- [AD 61-16-04](https://openairdocs.org/ad/61-16-04.md): Transmission Mount Lug · Effective Aug 14, 1961
- [AD 61-16-03](https://openairdocs.org/ad/61-16-03.md): Seat Modification · Effective Aug 4, 1961
- [AD 61-11-02](https://openairdocs.org/ad/61-11-02.md): Oil System Modification · Effective Aug 4, 1961
- [AD 61-11-01](https://openairdocs.org/ad/61-11-01.md): Landing Gear Drag Brace · Effective May 31, 1961
- [AD 61-04-01](https://openairdocs.org/ad/61-04-01.md): Clutch Bolts · Effective Feb 22, 1961
- [AD 60-26-03](https://openairdocs.org/ad/60-26-03.md): Drive Shaft Coupling · Effective Dec 20, 1960
- [AD 60-10-02](https://openairdocs.org/ad/60-10-02.md): Main Rotor Blade
- [AD 60-07-02](https://openairdocs.org/ad/60-07-02.md): Tail Rotor Drive Shaft
- [AD 60-06-03](https://openairdocs.org/ad/60-06-03.md): Tail Rotor Guard
- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13.md): Ground Proximity System · Historical · Effective Dec 9, 2021 · Replaced by AD 2023-11-07

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT d.ad_number, d.status, d.subject, d.effective_date
FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
WHERE d.ad_id IN (SELECT ad_id FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_directive.parquet' WHERE aircraft_model_code IN ('1440504'))
ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_number DESC
```

This list as a web page: https://openairdocs.org/model/brantly-b-2a/ads

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