# Schweizer 269A

- Type: Aircraft model (FAA registry)
- Registry code: 8059506
- Manufacturer (registry): SCHWEIZER
- Model: 269A
- Aircraft type: Rotorcraft
- Engines: 1
- Seats: 2
- Data sheet: TCDS 4H12
- Registered aircraft: 1
- Page: https://openairdocs.org/model/schweizer-269a

## ADs that may apply

- [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 2017-14-06](https://openairdocs.org/ad/2017-14-06): Main Rotor Drive System · Sikorsky 269A, 269A-1, 269B and 3 more. Effective Aug 25, 2017
- [AD 2015-23-01](https://openairdocs.org/ad/2015-23-01): Tail Rotor Drive · Sikorsky 269A, 269A-1, 269B and 3 more. Effective Dec 15, 2015
- [AD 2011-12-16](https://openairdocs.org/ad/2011-12-16): Rotorcraft Tailboom · Schweizer 269A, 269A-1, 269B and 2 more. Effective Jul 21, 2011
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2003-13-15 R1](https://openairdocs.org/ad/2003-13-15-R1): Aft cluster fittings · Schweizer 269A, 269A-1, 269B and 1 more. Effective Aug 10, 2004
- [AD 2000-16-05](https://openairdocs.org/ad/2000-16-05): Tail Rotor Swashplate Shaft · Schweizer 269A, 269A-1, 269B and 3 more. Effective Sep 19, 2000
- [AD 98-18-11](https://openairdocs.org/ad/98-18-11): Main Rotor Blade · Schweizer 269A, 269A-1, 269B and 2 more. Effective Oct 7, 1998
- [AD 97-23-06](https://openairdocs.org/ad/97-23-06): Ring Gear Teeth Inspection · Schweizer 269A, 269A-1, 269B and 1 more. Effective Dec 10, 1997
- [AD 97-05-06](https://openairdocs.org/ad/97-05-06): Main Rotor Thrust Bearing · Schweizer 269A, 269A-1 and 269B. Effective Apr 7, 1997
- [AD 95-21-02](https://openairdocs.org/ad/95-21-02): Main Rotor Drive Shaft · Schweizer 269A, 269A-1, 269B and 1 more. Effective Nov 17, 1995
- [AD 95-03-12](https://openairdocs.org/ad/95-03-12): Clutch Control Spring Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective Mar 1, 1995
- [AD 94-16-04](https://openairdocs.org/ad/94-16-04): Tail Rotor Pedal support Structure · Schweizer 269A, 269A-1, 269B and 1 more. Effective Oct 5, 1994
- [AD 94-12-06](https://openairdocs.org/ad/94-12-06): Lower Pulley Bearings · Schweizer 269A, 269A-1, 269B and 1 more. Effective Sep 19, 1994
- [AD 94-13-04](https://openairdocs.org/ad/94-13-04): Clutch Control Spring Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective Sep 1, 1994
- [AD 93-21-03](https://openairdocs.org/ad/93-21-03): Magnesium Tailboom Fitting · Schweizer 269A, 269A-1 and 269B. Effective Dec 17, 1993
- [AD 93-05-11](https://openairdocs.org/ad/93-05-11): Fuel Pump Drain Tube Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective May 25, 1993
- [AD 89-20-03 R1](https://openairdocs.org/ad/89-20-03-R1): Tail Rotor Blades · Schweizer 269A, 269A-1, 269B and 1 more. Effective Feb 22, 1991
- [AD 90-06-10](https://openairdocs.org/ad/90-06-10): Throttle Cable Assembly · Schweizer 269A, 269A-1, 269B and 1 more. Effective Apr 6, 1990
- [AD 88-17-04](https://openairdocs.org/ad/88-17-04): Aft Cluster Fittings · Schweizer 269A, 269A-1, 269B and 1 more. Effective Aug 19, 1988
- [AD 82-15-01 R1](https://openairdocs.org/ad/82-15-01-R1): Main Transmission · Schweizer 269A, 269A-1, 269B and 1 more. Effective Oct 4, 1982
- [AD 82-15-03](https://openairdocs.org/ad/82-15-03): Rotor System · Schweizer 269A, 269A-1, 269B and 1 more. Effective Jul 16, 1982
- [AD 81-17-01](https://openairdocs.org/ad/81-17-01): Starting Vibrator Assemblies · Bendix Starting Vibrator Assemblies, B-2, B-2A and 49 more. Effective Aug 13, 1981
- [AD 79-23-03 R1](https://openairdocs.org/ad/79-23-03-R1): Tail Rotor Blades · Schweizer 269A, 269A-1, 269B and 1 more. Effective Nov 19, 1979
- [AD 78-26-04](https://openairdocs.org/ad/78-26-04): Tail Rotor Hub Assembly · Schweizer 269A, 269A-1, 269B and 6 more. Effective Dec 27, 1978
- [AD 78-25-04](https://openairdocs.org/ad/78-25-04): Pinion Assemblies · Schweizer 269A, 269A-1, 269B and 1 more. Effective Dec 18, 1978
- [AD 78-02-02](https://openairdocs.org/ad/78-02-02): Tail Rotor Control Pedals · Schweizer 269A, 269A-1, 269B and 1 more. Effective Jan 24, 1978
- [AD 77-23-08](https://openairdocs.org/ad/77-23-08): Cracks in Main Rotor Blades · Schweizer 269A, 269A-1 and 269B. Effective Dec 27, 1977
- [AD 77-07-01](https://openairdocs.org/ad/77-07-01): Clutch Actuator · Schweizer 269A, 269A-1, 269B and 1 more. Effective Apr 4, 1977
- [AD 76-10-02](https://openairdocs.org/ad/76-10-02): Lateral control · Schweizer 269A, 269A-1, 269B and 1 more. Effective May 21, 1976
- [AD 75-15-02](https://openairdocs.org/ad/75-15-02): Throttle and Engine Power Control · Schweizer 269A, 269A-1 and 269B. Effective Jul 15, 1975
- [AD 74-21-04](https://openairdocs.org/ad/74-21-04): Canopy Slats · Schweizer 269A, 269A-1, 269B and 1 more. Effective Apr 4, 1975
- [AD 75-08-12](https://openairdocs.org/ad/75-08-12): Actuator and Cover · Schweizer 269A, 269A-1, 269B and 1 more. Effective Mar 7, 1975
- [AD 71-20-05](https://openairdocs.org/ad/71-20-05): Idler Pulley Bearings · Schweizer 269A, 269A-1 and 269B. Effective Dec 18, 1971
- [AD 70-08-01](https://openairdocs.org/ad/70-08-01): Flapping Hinge Bolts · Schweizer 269A, 269A-1 and 269B. Effective Apr 14, 1970
- [AD 70-01-06](https://openairdocs.org/ad/70-01-06): Lateral pitch idler bell crank · Schweizer 269A, 269A-1 and 269B. Effective Jan 17, 1970
- [AD 69-04-03](https://openairdocs.org/ad/69-04-03): Rotor Blade · Schweizer 269A, 269A-1 and 269B. Effective Mar 22, 1969
- [AD 68-26-01](https://openairdocs.org/ad/68-26-01): Lower Coupling Drive Shaft · Schweizer 269A, 269A-1 and 269B. Effective Dec 21, 1968
- [AD 64-28-02](https://openairdocs.org/ad/64-28-02): Main Rotor Blade Flapping Hinge Bearing · Schweizer 269A, 269A-1 and 269B. Effective Jul 6, 1968
- [AD 67-21-01](https://openairdocs.org/ad/67-21-01): Air Scoop · Schweizer 269A, 269A-1 and 269B. Effective Jul 3, 1967
- [AD 67-11-03](https://openairdocs.org/ad/67-11-03): Main Rotor Gear Drive · Schweizer 269A, 269A-1 and 269B. Effective Apr 7, 1967
- [AD 66-03-02](https://openairdocs.org/ad/66-03-02): Electrical System · Schweizer 269A, 269A-1 and 269B. Effective Jan 14, 1966
- [AD 64-06-04](https://openairdocs.org/ad/64-06-04): Lower Coupling Drive Shaft · Schweizer 269A, 269A-1 and 269B. Effective Mar 18, 1964
- [AD 62-14-03](https://openairdocs.org/ad/62-14-03): Tail Rotor Blade · Schweizer 269A. Effective Jun 26, 1962
- [AD 62-11-04](https://openairdocs.org/ad/62-11-04): Operating Limitations · Schweizer 269A. Effective May 15, 1962
- [AD 69-21-01](https://openairdocs.org/ad/69-21-01): Failure of Input Pinion Shaft · Schweizer 269A, 269A-1, 269B and 4 more
- [AD 62-21-03](https://openairdocs.org/ad/62-21-03): Modification · Schweizer 269A

Historical (superseded or no longer in force): AD 2021-23-13, AD 2011-01-52, AD 2003-13-15, AD 2001-25-52, AD 99-17-10, AD 93-17-13, AD 76-18-01

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19950331009549I](https://openairdocs.org/incident/19950331009549I), Mar 31, 1995: Hughes 269A (N3075U), St Charles, MO, Minor damage. Narrative: shortly after takeoff the pilot heard a loud "bang" noise, felt a "thump" on his head, then heard loud wind noise. Pilot selected an emergency…

## Complete lists

- aircraft: 1, https://openairdocs.org/model/schweizer-269a/aircraft
- ads: 54, https://openairdocs.org/model/schweizer-269a/ads
- incidents: 1, https://openairdocs.org/model/schweizer-269a/incidents

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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.
