# Bell Helicopter Textron 205A-1

- Type: Aircraft model (FAA registry)
- Registry code: 1181548
- Manufacturer (registry): BELL HELICOPTER TEXTRON
- Model: 205A-1
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 15
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS H1SW](https://openairdocs.org/tcds/H1SW) (OpenAirDocs)
- Holder: Bell Textron Inc.
- Registered aircraft: 1
- Page: https://openairdocs.org/model/bell-helicopter-textron-205a-1

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2024-17-02](https://openairdocs.org/ad/2024-17-02): Rotorcraft Tail Boom · Bell Textron 204B, 205B, 205A-1 and 2 more. Effective Nov 8, 2024
- [AD 2024-19-17](https://openairdocs.org/ad/2024-19-17): Rotorcraft flight control · Airwolf Aerospace, LLC Tension-Torsion Strap Assemblies, P/N… (STC SR03408CH). Effective Oct 11, 2024
- [AD 2024-16-01](https://openairdocs.org/ad/2024-16-01): Fuselage structure · Bell Textron 205A, 205A-1, 205B and 4 more. Effective Sep 4, 2024
- [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 2022-20-14](https://openairdocs.org/ad/2022-20-14): Main Rotor Gearbox · Bell Textron 204B, 205A, 205A-1 and 20 more. Effective Dec 27, 2022
- [AD 2022-22-12](https://openairdocs.org/ad/2022-22-12): Nose/Tail Landing Gear Structure/Axle · Replacement crosstubes P/N D212-664 (Dart Aerospace STC SR01298NY). Effective Nov 22, 2022
- [AD 2022-21-11](https://openairdocs.org/ad/2022-21-11): Main rotor blades · Bell Textron 204B, 205A, 205A-1 and 11 more. Effective Nov 16, 2022
- [AD 2022-07-02](https://openairdocs.org/ad/2022-07-02): Rotorcraft Tail Boom · Bell Textron 205A, 205A-1, 205B and 5 more. Effective May 9, 2022
- [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 2022-06-03](https://openairdocs.org/ad/2022-06-03): Main Rotor System · Bell Textron 204B, 205A, 205A-1 and 3 more. Effective Mar 16, 2022
- [AD 2020-19-08](https://openairdocs.org/ad/2020-19-08): Main Rotor · Bell Textron 204B, 205A-1 and 212. Effective Oct 21, 2020
- [AD 2020-16-10](https://openairdocs.org/ad/2020-16-10): Cabin Equipment/Furnishings · Bell Textron 204B, 205A, 205A-1 and 7 more. Effective Sep 3, 2020
- [AD 2020-12-10](https://openairdocs.org/ad/2020-12-10): Tail Rotor Blades · Bell Textron 205A, 205A-1, 205B and 4 more. Effective Jul 16, 2020
- [AD 2018-02-08](https://openairdocs.org/ad/2018-02-08): Main Rotor blades · Bell Helicopter Textron 204B, 205A and 205A-1. Effective Feb 1, 2018
- [AD 2016-22-07](https://openairdocs.org/ad/2016-22-07): Main Rotor Blades · Bell Helicopter Textron 204B, 205A and 205A-1. Effective Nov 30, 2016
- [AD 2015-15-04](https://openairdocs.org/ad/2015-15-04): Main Rotor Blade Grip · Bell Helicopter Textron 204B, 205A, 205A-1 and 1 more. Effective Aug 7, 2015
- [AD 2014-12-04](https://openairdocs.org/ad/2014-12-04): Main Rotor Head · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Jul 24, 2014
- [AD 2013-18-07](https://openairdocs.org/ad/2013-18-07): Tail Rotor Control System · Bell Helicopter Textron 204B and 205A-1. Effective Oct 18, 2013
- [AD 2013-15-02](https://openairdocs.org/ad/2013-15-02): Tail Rotor Blades · Bell Helicopter Textron 205A, 205A-1, 205B and 5 more. Effective Aug 14, 2013
- [AD 2013-03-16](https://openairdocs.org/ad/2013-03-16): Main Rotor Head · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Feb 27, 2013
- [AD 2012-17-08](https://openairdocs.org/ad/2012-17-08): Main Rotor Head · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Feb 27, 2013
- [AD 2012-26-11](https://openairdocs.org/ad/2012-26-11): Electrical power system wiring · Bell Helicopter Textron 205A, 205A-1 and 205B. Effective Feb 13, 2013
- [AD 2012-22-06](https://openairdocs.org/ad/2012-22-06): High Landing Gear Forward Crosstube Assembly · Aeronautical Accessories AB412, AB412 EP, 205A and 7 more. Effective Dec 14, 2012
- [AD 2011-23-02](https://openairdocs.org/ad/2011-23-02): Main rotor blade (blade) assemblies · Bell Helicopter Textron 205A-1, 205B, 210 and 1 more. Effective Nov 21, 2011
- [AD 2010-26-52](https://openairdocs.org/ad/2010-26-52): Tail Rotor Blade · Bell Helicopter Textron 204B, 205A, 205A-1 and 6 more. Effective Nov 15, 2011
- [AD 2010-10-16](https://openairdocs.org/ad/2010-10-16): Crosstube · Agusta AB412, AB412 EP, 205A and 6 more. Effective Jun 8, 2010
- [AD 2007-22-02](https://openairdocs.org/ad/2007-22-02): Tail rotor blade (blade) forward tip weight retention block (tip block) and the aft tip closure (tip closure) · Bell Helicopter Textron 205A, 205A-1, 205B and 4 more. Effective Nov 30, 2007
- [AD 2002-22-14](https://openairdocs.org/ad/2002-22-14): Main rotor tension-torsion (TT) straps · Bell Helicopter Textron 204B, 205A, 205A-1 and 4 more. Effective Dec 13, 2002
- [AD 2002-09-51](https://openairdocs.org/ad/2002-09-51): Tail rotor (T/R) grip · Bell Helicopter Textron 204B, 205A, 205A-1 and 1 more. Effective Aug 22, 2002
- [AD 2001-13-01](https://openairdocs.org/ad/2001-13-01): Tail Rotor Counterweight Bellcrank (bellcrank) Retention Nut (retention nut) · Bell Helicopter Textron 205A-1, 205B, 212 and 3 more. Effective Aug 1, 2001
- [AD 2001-08-04](https://openairdocs.org/ad/2001-08-04): Main Rotor Actuator · Bell Helicopter Textron 205A-1, 205B, 212 and 3 more. Effective May 3, 2001
- [AD 2000-15-52](https://openairdocs.org/ad/2000-15-52): Mast and main rotor trunnions · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Dec 28, 2000
- [AD 99-18-02](https://openairdocs.org/ad/99-18-02): Vertical Fin Spar Cap · Bell Helicopter Textron 205A-1 and 205B. Effective Oct 5, 1999
- [AD 99-17-03](https://openairdocs.org/ad/99-17-03): Tailboom Vertical Fin Spar · Bell Helicopter Textron 204B, 205A and 205A-1. Effective Sep 16, 1999
- [AD 98-11-14](https://openairdocs.org/ad/98-11-14): Tail Rotor Yoke Assembly · Bell Helicopter Textron 205A-1 and 205B. Effective Feb 10, 1999
- [AD 95-10-07](https://openairdocs.org/ad/95-10-07): Tail Rotor Drive Gearbox Assembly · Bell Helicopter Textron 204B, 205A and 205A-1. Effective May 26, 1995
- [AD 94-18-09](https://openairdocs.org/ad/94-18-09): Main Transmission Lower Planetary Spider · Bell Helicopter Textron 205A, 205A-1, 205B and 2 more. Effective Oct 14, 1994
- [AD 93-17-12](https://openairdocs.org/ad/93-17-12): Main Rotor Transmission Lower Planetary Spider · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Jul 29, 1994
- [AD 92-27-21](https://openairdocs.org/ad/92-27-21): Tail Rotor Driveshaft · Bell Helicopter Textron 205A-1 and 205B. Effective Jul 7, 1993
- [AD 92-23-01](https://openairdocs.org/ad/92-23-01): Main Rotor Pillow Blocks · Bell Helicopter Textron 204B, 205A, 205A-1 and 10 more. Effective Apr 23, 1993
- [AD 92-13-10](https://openairdocs.org/ad/92-13-10): Tail Rotor Driveshaft Hanger Bearing · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Feb 23, 1993
- [AD 92-07-08](https://openairdocs.org/ad/92-07-08): Swashplate Support Assembly · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Mar 25, 1992
- [AD 90-03-10](https://openairdocs.org/ad/90-03-10): Tail Rotor Grips · Arrow Falcon Exporters UH-1H, UH-1F, 204B and 33 more. Effective Oct 18, 1991
- [AD 89-20-12](https://openairdocs.org/ad/89-20-12): Tail Rotor Hub Assembly · Overseas Aircraft Support 204B, 205A, 205A-1 and 8 more. Effective Aug 15, 1990
- [AD 90-03-09](https://openairdocs.org/ad/90-03-09): T/R Hub Assembly  (See 90-03-09) · Bell Helicopter Textron 205A, 205A-1, 212 and 1 more. Effective Feb 13, 1990
- [AD 89-08-05](https://openairdocs.org/ad/89-08-05): Transmission Internal Sump Oil Filter · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Jan 3, 1990
- [AD 88-25-05](https://openairdocs.org/ad/88-25-05): Tail Rotor Grip Assembly · AST UH-1F, 204B, 205A and 25 more. Effective Dec 13, 1988
- [AD 80-21-05](https://openairdocs.org/ad/80-21-05): Landing Gear Cross Tubes · Bell Helicopter Textron 205A-1 and 212. Effective Oct 15, 1980
- [AD 80-03-07](https://openairdocs.org/ad/80-03-07): Fuselage Main Beams Splice · Bell Helicopter Textron 205A-1. Effective Feb 5, 1980
- [AD 78-20-07](https://openairdocs.org/ad/78-20-07): Shoulder Radius Fitting · Bell Helicopter Textron 204B, 205A-1 and 212. Effective Oct 25, 1978

Historical (superseded or no longer in force):

- [AD 2022-02-02](https://openairdocs.org/ad/2022-02-02) (historical): Main Rotor System · Bell Textron 204B, 205A, 205A-1 and 3 more. Effective Feb 16, 2022
- [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
- [AD 2021-15-51](https://openairdocs.org/ad/2021-15-51) (historical): Main rotor system · Bell Textron 204B, 205A, 205A-1 and 2 more. Effective Aug 24, 2021
- [AD 2011-12-08](https://openairdocs.org/ad/2011-12-08) (historical): Tail rotor (T/R) blades · Bell Helicopter Textron 205A, 205A-1, 205B and 4 more. Effective Jul 5, 2011
- [AD 2008-10-03](https://openairdocs.org/ad/2008-10-03) (historical): Tail rotor blade assembly · Bell Helicopter Textron 204B, 205A, 205A-1 and 6 more. Effective May 21, 2008
- [AD 2007-19-53](https://openairdocs.org/ad/2007-19-53) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 204B, 205A, 205A-1 and 6 more. Effective Dec 5, 2007
- [AD 2003-01-04](https://openairdocs.org/ad/2003-01-04) (historical): Main rotor grip · New rotor blades (Hillsboro STC SH5132NM). Effective Jan 30, 2003
- [AD 2002-09-04](https://openairdocs.org/ad/2002-09-04) (historical): Tip Block and Tip Closure · Bell Helicopter Textron 205A, 205A-1, 205B and 4 more. Effective Jun 7, 2002
- [AD 2002-08-53](https://openairdocs.org/ad/2002-08-53) (historical): T/R Grip · Bell Helicopter Textron 205A, 205A-1 and 205B
- [AD 2000-25-03](https://openairdocs.org/ad/2000-25-03) (historical): Main Rotor Actuator Locking Washer · Bell Helicopter Textron 205A-1, 205B, 212 and 2 more. Effective Dec 28, 2000
- [AD 2000-08-52](https://openairdocs.org/ad/2000-08-52) (historical): Main Rotor System · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more
- [AD 98-24-15](https://openairdocs.org/ad/98-24-15) (historical): Main Rotor Mast and Trunnion · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Dec 8, 1998
- [AD 81-19-02](https://openairdocs.org/ad/81-19-02) (historical): Main Rotor Yoke · Bell Helicopter Textron 204B, 205A, 205A-1 and 1 more. Effective Sep 30, 1981
- [AD 80-17-09](https://openairdocs.org/ad/80-17-09) (historical): Main Rotor Straps · Bell Helicopter Textron 204B, 205A-1, 212 and 16 more. Effective Sep 15, 1980
- [AD 79-20-05](https://openairdocs.org/ad/79-20-05) (historical): Main Rotor Hub Assembly · Bell Helicopter Textron 204B, 205A-1 and 212. Effective Jan 18, 1980
- [AD 76-12-07](https://openairdocs.org/ad/76-12-07) (historical): Tail Rotor Chains · Bell Helicopter Textron 204B and 205A-1. Effective Oct 29, 1979
- [AD 75-26-05](https://openairdocs.org/ad/75-26-05) (historical): Main Rotor Blades · Bell Helicopter Textron 204B, 205A-1 and 212. Effective Jan 19, 1976

All 85: https://openairdocs.org/model/bell-helicopter-textron-205a-1/ads.md

## Information bulletins (advisory) (4)

- [SAIB SW-12-38](https://openairdocs.org/saib/SW-12-38): Emergency Push Out  Window Retention. Issued Jul 30, 2012
- [SAIB SW-05-10R1](https://openairdocs.org/saib/SW-05-10R1): . Issued Nov 30, 2004
- [SAIB SW-05-10](https://openairdocs.org/saib/SW-05-10) (historical): . Issued Nov 5, 2004
- [SAIB ASW-94-01](https://openairdocs.org/saib/ASW-94-01): . Issued Nov 2, 1994

## Registered aircraft (1)

- [N775BB](https://openairdocs.org/aircraft/N775BB): [Copter Lease LLC Trustee](https://openairdocs.org/faa-owner/COPTER%20LEASE%20LLC%20TRUSTEE), [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque), built 1977, S/N 30252

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (232, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR H4QA20260619001](https://openairdocs.org/sdr/H4QA20260619001), Jun 16, 2026: RELAY. FAILED. ENROUTE TO A DIP SITE FOR ANOTHER BUCKET OF WATER THE PILOT SMELLED ELECTRICAL SMOKE IN THE CABIN OF THE AIRCRAFT. ODOR WAS IMMEDIATELY FOLLOWED BY SMOKE COMING
- [SDR 2022F00378](https://openairdocs.org/sdr/2022F00378), Oct 3, 2022: HOSE. RUPTURED. AT APPROXIMATELY 10501.9 ACTT ON 9-29-22 AT 1530 PM I WAS TOLD THAT THERE HAD BEEN A HYDRAULIC SYSTEM 2 FAILURE ON N456TA. THE PILOT LANDED WITHOUT INCIDENT. AF
- [SDR NKVA2025011500013](https://openairdocs.org/sdr/NKVA2025011500013), Oct 13, 2021: SWASHPLATE. CRACKED. A TECHNICIAN REPORTED THAT DURING HIS DAILY INSPECTION HE FELT SOME "LOOSENESS" IN THE SWASHPLATE THAT HE HAD NOT NOTICE ON PRIOR DAILY INSPECTIONS. HE INVESTIG
- [SDR 2021FA0000284](https://openairdocs.org/sdr/2021FA0000284), Oct 13, 2021: SWASHPLATE. CRACKED. A TECHNICIAN REPORTED THAT DURING HIS DAILY INSPECTION HE FELT SOME "LOOSENESS" IN THE SWASHPLATE THAT HE HAD NOT NOTICED ON PRIOR DAILY INSPECTIONS. HE INVESTI
- [SDR H4QA202007230001](https://openairdocs.org/sdr/H4QA202007230001), Jul 20, 2020: CROSSTUBE. BROKEN. REAR AFT CROSSTUBE FAILED WHILE AIRCRAFT WAS NOT RUNNING. CREW WANTED TO FILL BELLY TANK WITH WATER AND MARK NUMBER OF GALLONS, DURING FILLING OPERATIONS FROM W
- [SDR LJEA2020061600001](https://openairdocs.org/sdr/LJEA2020061600001), Jun 11, 2020: GEARBOX. CRACKED. MAIN GEARBOX CASE CRACKED IN WEBBING ABOVE INPUT QUILL. FERRY PERMIT REQUESTED TO RELOCATE AIRCRAFT TO A LOCATION FOR MAINTENANCE.
- [SDR 2020F00078](https://openairdocs.org/sdr/2020F00078), Nov 20, 2019: GEARBOX. CRACKED. CRACK SUSPECTED IN MAIN GEARBOX CASE ABOVE INPUT QUILL PURSUANT TO GUIDANCE FROM BELL HELICOPTERS IN BELL 205 CR&O FIG 66-37. CRACK APPEARS TO EXTEND THROUGH WE
- [SDR 2016FA0000387](https://openairdocs.org/sdr/2016FA0000387), Aug 23, 2016: FIRE DETECTOR. FAILED. ENROUTE TO A FIRE, FIRE LIGHT CAME ON. NO SMOKE WAS DETECTED. LANDED AIRCRAFT BACK AT BASE. MECHANIC TROUBLESHOT THE SYSTEM AND FOUND BAD FIRE SENSOR PROBE IN E
- [SDR HEAA2016012501](https://openairdocs.org/sdr/HEAA2016012501), Jan 25, 2016: CROSSTUBE. CRACKED. DURING ROUTINE WINTER MAINTENANCE, AN INSPECTION OF THE LANDING GEAR CROSSTUBES WERE ACCOMPLISHED IAW THE MFG 300 HOUR INSPECTION. ONE OF THE SADDLES FOR THE AT
- [SDR H4QA20151028559](https://openairdocs.org/sdr/H4QA20151028559), Oct 27, 2015: SUPPORT. BENT. DURING SCHEDULED MX IT WAS DISCOVERED THAT A BEARING WOULD NOT FIT BETWEEN THE MOUNTING LUGS OF THE SWASHPLATE SUPPORT, PN 204-011-404-125, SN RE18039. THE SWAS
- [SDR CA150929013](https://openairdocs.org/sdr/CA150929013), Sep 25, 2015: SHAFT. SHEARED. (CAN) STARTER GENERATOR SHAFT SHEARED IN FLIGHT UNDER NORMAL LOADS CAUSING LOSS OF DC POWER GENERATION. ACFT RETURNED TO BASE UNEVENTFULLY.
- [SDR 2015FA0000355](https://openairdocs.org/sdr/2015FA0000355), Jul 28, 2015: CONNECTOR. BURNED. PILOT REPORTED BURNED PLASTIC ODOR FROM ENGINE COMPARTMENT. MECHANIC INSPECTED ENGINE COMPARTMENT AND FOUND A BURNED AREA ON THE STARTER/GENERATOR CONNECTOR PLU
- [SDR CA150713024](https://openairdocs.org/sdr/CA150713024), Jul 11, 2015: HYDRAULIC LINE. RUPTURED. (CAN) DURING FLIGHT THE PILOT EXPERIENCED A LOSS OF NR 2 HYD PRESS. PILOT RETURN TO THE BASE AFTER ISOLATING THE SYS. ONCE THE ACFT LANDED SAFELY, THE INVESTIGA
- [SDR CA150421003](https://openairdocs.org/sdr/CA150421003), Apr 18, 2015: BLADE. DAMAGED. (CAN) DURING A MAINTENANCE FLIGHT CHECKING MAIN ROTOR SYS TRACK AND BALANCE, THE ACFT WAS INCREASING AIRSPEED FROM 60 KNOTS TO 100 KNOTS. A LOUD BANG WAS HEARD 
- [SDR CA150316004](https://openairdocs.org/sdr/CA150316004), Mar 15, 2015: BLADE. CRACKED. (CAN) DURING INSPECTION OF ACFT BLOWER FAN, IT WAS NOTED THAT 4 OF THE FAN BLADES WERE CRACKED AT THE BASE.
- [SDR CA150225006](https://openairdocs.org/sdr/CA150225006), Feb 23, 2015: SHIELD. LEAKING. (CAN) DURING DAILY INSPECTION, NOTICED THAT THE HANGER BEARING ASSEMBLY GREASE SHIELD WAS LEAKING. UNIT WAS REPLACED WITH SERVICEABLE, GND RUN CARRIED OUT & NO 
- [SDR CA150121002](https://openairdocs.org/sdr/CA150121002), Jan 20, 2015: SPIDER GEAR. CRACKED. (CAN) LOWER PLANETARY SPIDER ASSEMBLY PART NUMBER 205-040-785-003 FOUND CRACKED DURING ROUTINE OVERHAUL. NO KNOWN CAUSE AND NO OTHER DISCREPANCIES FOUND. PART R
- [SDR CA140819004](https://openairdocs.org/sdr/CA140819004), Aug 7, 2014: SERVO. MALFUNCTIONED. (CAN) WHEN PILOT CARRIED OUT START UP CHECK LIST AT IDLE, A HYDRAULIC SYSTEMS CHECK WAS CARRIED OUT. SYSTEM 2 WAS CLOSED AND CONTROLS FUCTIONED PROPERLY. SYSTEM
- [SDR CA140428004](https://openairdocs.org/sdr/CA140428004), Apr 28, 2014: BEAM. CRACKED. (CAN) PERFORMING A SCHEDULE INSPECTION, A VISUAL INSPECTION WAS DONE ON THE LT MAIN BEAM CAP. THE CAP WAS FOUND TO BE CRACKED COMPLETELY THREW. A NEW CAP, PN 20
- [SDR CA131129010](https://openairdocs.org/sdr/CA131129010), Nov 26, 2013: BLADE. DELAMINATED. (CAN) BLADE WAS REPAIRED IN JULY 2013 TO CORRECT SOME DELAMINATION FROM AN OLDER DENT AT 18" FROM THE BLADE TIP. UPON LANDING AT A REMOTE SITE AND SHUTTING DOWN
- [SDR CA130920009](https://openairdocs.org/sdr/CA130920009), Sep 19, 2013: DIFFUSER. CRACKED. (CAN) DURING A ROUTINE MAINTENANCE ACTION, A CRACK WAS DISCOVERED AROUND THE BLEED VALVE PORT. ACFT HAS BEEN REMOVED FROM SERVICE. UP-DATE: CRACK FOUND ON COMPR
- [SDR CA131009002](https://openairdocs.org/sdr/CA131009002), Aug 24, 2013: BLADE. SEPARATED. (CAN) A SUDDEN MEDIUM FREQUENCY VIBRATION WAS FELT IN FLIGHT. A PRECAUTIONARY LANDING WAS CARRIED OUT. AFTER VISUAL INSPECTION, IT WAS DISCOVERED THAT THE TIP C
- [SDR CA140603003](https://openairdocs.org/sdr/CA140603003), Aug 19, 2013: BEAM. CRACKED. (CAN) WHILE PERFORMING A DA!LY INSPECTION, IT WAS FOUND THAT THE UPPER LT MAIN BEAM CAP PORTION, EXTRUDING FROM THE ENGINE DECK, SOMETIMES REFEREED TO AS THE "I
- [SDR CA130813006](https://openairdocs.org/sdr/CA130813006), Aug 8, 2013: SUPPORT. MISMANUFACTURED. (CAN) UPON REMOVAL OF THE NEW SUPPORT, PN 204-011-404-125 FROM THE PACKAGING THE PART DISPLAYED THE FOLLOWING: SEVERAL AREAS WHERE MACHINING WAS NOT COMPLETE. T
- [SDR CA130705006](https://openairdocs.org/sdr/CA130705006), Jul 3, 2013: FITTING. CRACKED. (CAN) AME WAS PERFORMING POST FLIGHT/DAILY INSPECTION FOLLOWING LAST FLIGHT OF DAY. DURING INSPECTION, A SMALL VERTICAL LINE WAS NOTED ON THE LT LUG OF THE FITT
- [SDR CA130627001](https://openairdocs.org/sdr/CA130627001), Jun 14, 2013: QUILL. BROKEN. (CAN) INPUT QUILL IN-FLIGHT FAILURE, FREEWHEEL UNIT FAILURE, INPUT DRIVESHAFT FAILURE, ENGINE OVERSPEED, AUTOROTATIVE LANDING.
- [SDR CA130528009](https://openairdocs.org/sdr/CA130528009), May 27, 2013: TUBE. CRACKED. (CAN) CRACKED TUBE UNDERNEATH FITTING SLEEVE, TUBE POPPED OUT OF FITTING AND BLEW OUT MOST OF FLUID.
- [SDR CA130323001](https://openairdocs.org/sdr/CA130323001), Mar 21, 2013: SHAFT. SHEARED. (CAN) STARTER GENERATOR FAILED TO TURN OVER ENGINE FOR START. INSPECTION REVEALED THE SHAFT HAD SHEARED.
- [SDR CA120912012](https://openairdocs.org/sdr/CA120912012), Sep 11, 2012: BLADE. DAMAGED. (CAN) MAIN ROTOR BLADE CRACKED FROM L/E TO T/E UPPER AND LOWER SURFACE AT APPROXIMATELY 77" FROM BLADE TIP. ACFT LANDED SAFELY, MAIN ROTOR BLADE INTACT AS 1 PIE
- [SDR CA120817001](https://openairdocs.org/sdr/CA120817001), Aug 7, 2012: LONGERON. CRACKED. (CAN) TOP LT LONGERON ON ACFT LOCATED IN AFT COMPARTMENT WAS CRACKED BEHIND DOUBLER ON TOP LT TAILBOOM ATTACHMENT. CRACK WAS FOUND DURING DAILY INSPECTION, MACH
- [SDR CA120629008](https://openairdocs.org/sdr/CA120629008), Jun 18, 2012: BEARING. DAMAGED. (CAN) DEBRIS, METAL, FOUND ON ENGINE CHIP DETECTOR. 7.7 HRS LATER DEBRIS WAS FOUND AGAIN ON ENGINE CHIP DETECTOR. 1 HR AFTER ENGINE WAS REMOVED FROM ACFT DUE TO
- [SDR CA120629007](https://openairdocs.org/sdr/CA120629007), Jun 18, 2012: NUT. DAMAGED. (CAN) DEBRIS, METAL, FOUND ON ENGINE CHIP DETECTOR. 7.7 HRS LATER DEBRIS WAS FOUND AGAIN ON ENGINE CHIP DETECTOR. 1 HR AFTER ENGINE WAS REMOVED FROM ACFT DUE TO
- [SDR CA120817004](https://openairdocs.org/sdr/CA120817004), Jun 6, 2012: TACHOMETER. FAILED. (CAN) CO-PILOT DUAL TACH N2 ENGINE RPM NEEDLE, FLUCUATES FROM 0 TO 50 PERCENT THEN STICKS.
- [SDR CA120223006](https://openairdocs.org/sdr/CA120223006), Jan 28, 2012: CAP. FRACTURED. (CAN) FAILURE OF CAP, IN ORDER TO EXAMINE THE FRACTURE SURFACE OF A STRUCTURAL LONGERON, HERE-IN REFERRED TO AS A CAP. THE CAP, PN 205-030-207-005 AND THE ASSOC
- [SDR CA120116003](https://openairdocs.org/sdr/CA120116003), Jan 16, 2012: GIMBAL RING. DAMAGED. (CAN) DURING 100 HRS INSPECTION, 2 SMALL DAMAGED SCREWS WHERE FOUND IN THE BOTTOM OF THE MAIN TRANSMISSION BAY STILL ATTACHED WITH LOCKING WIRE. FURTHER INSPECT
- [SDR CA111220005](https://openairdocs.org/sdr/CA111220005), Dec 20, 2011: BLADE. CRACKED. (CAN) 3 CRACKS DEVELOPED ON BOTTOM SIDE OF BLADE SKIN, PN 212-015-501-115, SN A6009 (TSN) 3521.9, 1 CRACK 5.5", THE OTHER 2 CRACKS ARE 2.5" - 3.5" RESPECTIVELY.
- [SDR CA110909011](https://openairdocs.org/sdr/CA110909011), Aug 14, 2011: GOVERNOR. FAILED. (CAN) ACFT LEVELED OFF AFTER CLIMB, A BANG WAS HEARD THEN ACFT YAWED, ROTOR LOW HORN AND LIGHT SOUNDED. ENGINE FAILURE WAS CONFIRMED- N1 WAS AT 25 PERCENT AND T
- [SDR CA110726007](https://openairdocs.org/sdr/CA110726007), Jul 25, 2011: CHANNEL. MISMANUFACTURED. NEW PART DOES NOT FIT ACFT OR FIXTURE PLATE. MANUFACTURED .040 TOO WIDE.
- [SDR CA110711020](https://openairdocs.org/sdr/CA110711020), Jul 8, 2011: COUPLING. FAILED. THE PILOT NOTICED A SLIGHT YAW AS HE WAS TOUCHING DOWN. HE ALSO NOTICED THAT WHEN WHEN APPLYING COLLECTIVE TO TAKEOFF, THERE WAS NO RESPONSE FROM THE PEDALS. TH
- [SDR CA111222011](https://openairdocs.org/sdr/CA111222011), Mar 6, 2011: DIFFUSER. USED. (CAN) UPON LANDING AND PERFORMING A POST FLIGHT VISUAL INSPECTION THE AME FOUND THE BOTTOM STRUT ON THE EXHAUST DIFFUSER CRACKED WITH A SECTION OF MATERIAL MISS
- [SDR CA101122028](https://openairdocs.org/sdr/CA101122028), Nov 22, 2010: BAFFLE. DETACHED. BAFFLE DIVIDING FORWARD AND AFT SECTIONS OF FUEL CELL, FOUND DETACHED. FUEL IS ABLE TO MOVE AROUND POTENTIALLY CAUSING C OF G ISSUES. IN LOW FUEL SITUATIONS, SL
- [SDR CA100901007](https://openairdocs.org/sdr/CA100901007), Aug 16, 2010: BEAM. CRACKED. THE ACA HOLDER WAS DOING HIS DAILY PREFLIGHT WHEN HE NOTICED 2 BLACK LINES THAT APPEARED TO BE CRACKS. THE ACA HOLDER LOOKED CLOSER AND FOUND THE TRANSMISSION 5
- [SDR H4QA2010F00111](https://openairdocs.org/sdr/H4QA2010F00111), May 20, 2010: HOUSING. CRACKED. COMBUSTION CHAMBER HOUSING FOUND CRACKED 8 INCHES LONG FROM (LOOKING FORWARD) 12:30-2:30 POSITION. CRACK WAS FOUND AFTER SHUTDOWN DURING DAILY INSPECTION BY MEC
- [SDR CA091120005](https://openairdocs.org/sdr/CA091120005), Nov 20, 2009: IGNITER. FAILED. (CAN) FOUND IGNITER PLUG 1 OF 4 INSTALLED, FAILED CAUSED BY IGNITER INTERIOR CATHODE BECOMING LOOSE.
- [SDR CA091120004](https://openairdocs.org/sdr/CA091120004), Nov 20, 2009: IGNITER. FAILED. (CAN) FOUND IGNITER PLUG , 2 OF 4 INSTALLED FAILED CAUSED BY IGNITER INTERIOR CATHODE BECOMING LOOSE.
- [SDR CA091109002](https://openairdocs.org/sdr/CA091109002), Nov 6, 2009: BOOT. SEPARATED. (CAN) DURING THE 12 MONTH INSP AND RE-GREASE OF THE INPUT DRIVE SHAFT, IT WAS DISCOVERED THAT THE INNER DIAMETER OF THE BOOT HAD COMPLETELY SEPERATED FROM THE R
- [SDR CA091006004](https://openairdocs.org/sdr/CA091006004), Sep 19, 2009: SHAFT. WORN. (CAN) WHILE FLYING THE PILOT HAD A CAUTION LIGHT. IT WAS THE FUEL PUMP CAUTION LIGHT THAT HAD ILLUMINATED. THE PILOT LANDED AS SOON AS PRACTICAL. THE ENG FUEL C
- [SDR CA090818006](https://openairdocs.org/sdr/CA090818006), Aug 14, 2009: BOLT. BROKEN. WHILE THE ENGINEER WAS CARRYING OUT A DAILY INSP, FOUND HALF A BOLT WITH NUT ATTACHED ON ENG DECK. FURTHER INVESTIGATION REVEALED THAT BOLT (ONE OF TWO) WAS PAR
- [SDR CA090806005](https://openairdocs.org/sdr/CA090806005), Jul 30, 2009: GOVERNOR. UNKNOWN. EXCESSIVE ENGINE DROOP.
- [SDR CA090702013](https://openairdocs.org/sdr/CA090702013), Jul 1, 2009: FITTING. CRACKED. DURING A POST FLIGHT INSP, THE TAIL ROTOR DRIVE FITTING WAS FOUND CRACKED. TIME ON THE FITTING IS UNKNOWN. CRACK WAS FOUND RADIATING FROM THE BORE OF THE BARREL

All 232: https://openairdocs.org/model/bell-helicopter-textron-205a-1/reports.md

## STCs that may be installed (OpenAirDocs) (230, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SR12508IB](https://openairdocs.org/stc/SR12508IB): Installation of Personnel Carrying Devices (PCDs) for Human External Cargo (HEC). Ascent Aerospace Ltd
- [STC SR12457NY](https://openairdocs.org/stc/SR12457NY): Demonstration of Aircraft Equipment Configurations Tolerance to Transmitting Portable Electronic Devices (TPED) in Part 29 Aircraft. Kilroy Aviation, LLC
- [STC SR12427IB](https://openairdocs.org/stc/SR12427IB): Installation of an AEM MTP136D Panel Mount FM Transceiver. Anodyne Electronics Manufacturing Corporation
- [STC SR02736NY](https://openairdocs.org/stc/SR02736NY): Installation of Utility Basket on the right hand side. Alpine Aerotech Ltd
- [STC SR02270SE](https://openairdocs.org/stc/SR02270SE): Fabrication and installation of Geneva Aviation Audio System. AEM USA Inc
- [STC SR02444SE](https://openairdocs.org/stc/SR02444SE): Installation of P178 Failsafe Audio Mixer. AEM USA Inc
- [STC SR12332SE](https://openairdocs.org/stc/SR12332SE): Installation of Mechanical Specialties, LLC Human External Cargo (HEC) and non-HEC Hook System. Mechanical Specialties, LLC
- [STC SH1201SO](https://openairdocs.org/stc/SH1201SO): Installation P/N 364-83300-1 (Standard Skid Gear) or P/N 364-83300-3 (High Skid Gear). This Wire Strike Protection System. Magellan Aerospace
- [STC SR04465NY](https://openairdocs.org/stc/SR04465NY): Installation of the iPad Mount. Avio Design Group Inc
- [STC SR12072IB](https://openairdocs.org/stc/SR12072IB): Manufacturing and Installation of Cargo Hold Nets; Maintenance must be in accordance with ICARUS Aero Inc. Instructions for Continued Airworthiness as shown on the attached FAA AML No. SR12072IB. Icarus Aero Inc
- [STC SH8609SW](https://openairdocs.org/stc/SH8609SW): Fabrication of Isolair Eliminator II Model 4600-205 fire fighting system. Isolair Inc
- [STC SR01776SE](https://openairdocs.org/stc/SR01776SE): Fabrication, installation, and maintenance of the Isolair Helicopters, Inc., Model 9002 High Cross tubes. Isolair Inc
- [STC SR04662CH](https://openairdocs.org/stc/SR04662CH): Installation of Luma Technologies LT-4205 20 Station Integrated LED Display Panel. Luma Technologies LLC
- [STC SR00145IB](https://openairdocs.org/stc/SR00145IB): Installation of LH and RH Vertical Reference Door(s). Transwest Helicopters Ltd
- [STC SR00141IB](https://openairdocs.org/stc/SR00141IB): Installation of the Aft Pedestal Stowage Compartment. Alpine Aerotech LP
- [STC SH4056NM](https://openairdocs.org/stc/SH4056NM): Installation of pneumatic door actuators. Dart Aerospace USA Inc
- [STC SR01865SE](https://openairdocs.org/stc/SR01865SE): Fabrication and installation of FastFin System. BLR Aerospace LLC
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SR09462RC](https://openairdocs.org/stc/SR09462RC): Installation of Night Vision Goggle Compatible Interior Lighting System. REB Technologies Inc
- [STC SR00094IB](https://openairdocs.org/stc/SR00094IB): Installation of Extended Port Seat Rail. Ascent Aerospace Ltd
- [STC SR00080IB](https://openairdocs.org/stc/SR00080IB): Installation of the Garmin GRA 55 Radar Altimeter. Alpine Aerotech LP
- [STC SR00077IB](https://openairdocs.org/stc/SR00077IB): Installation of the Two Place Seat Assembly. Ascent Aerospace Ltd
- [STC SR00075IB](https://openairdocs.org/stc/SR00075IB): Installation of Cabin Furnishings. Ascent Aerospace Ltd
- [STC SH400NW](https://openairdocs.org/stc/SH400NW): Installation of left hand bubble door with or without duplicate engine instruments. WSH, LLC
- [STC SR03832NY](https://openairdocs.org/stc/SR03832NY): Installation of Full Vertical Reference Door P/N D412-761 for Left Hand Vertical Reference Operations. Dart Aerospace Limited
- [STC SR00058IB](https://openairdocs.org/stc/SR00058IB): Installation of J301A Audio Controller. Alpine Aerotech LP
- [STC SR00047IB](https://openairdocs.org/stc/SR00047IB): Installation of VIH Aerospace (VIHA) Pulse Light. VIH Aerospace Inc
- [STC SR04615NY](https://openairdocs.org/stc/SR04615NY): Installation of the Human External Cargo (HEC) Suspension Line Kit. Boost Human External Cargo Systems Inc
- [STC SR04616NY](https://openairdocs.org/stc/SR04616NY): Installation of the Dual HEC Hook System Provisions is to be performed. Boost Human External Cargo Systems Inc
- [STC SR02189SE](https://openairdocs.org/stc/SR02189SE): Installation of a Supplemental Lighting System, manufactured and installed. Aviation Specialties Unlimited Inc
- [STC SR00713SE](https://openairdocs.org/stc/SR00713SE): Installation of Onboard Systems International Cargo Hook Kit. Onboard Systems International
- [STC SR01903NY](https://openairdocs.org/stc/SR01903NY): Installation of a modified co-pilot seat. Transwest Helicopters Ltd
- [STC SR04663NY](https://openairdocs.org/stc/SR04663NY): Installation of the Center Pedestal Riser. Alpine Aerotech LP
- [STC SH5707NM](https://openairdocs.org/stc/SH5707NM): Fabrication of Onboard Systems Model 200-088-03 or 200-088-04 (without Load Weight) or 200-089-03, -04, -05 or -06 (with Load Weight) cargo hook suspension systems. Onboard Systems International
- [STC SH5737NM](https://openairdocs.org/stc/SH5737NM): Replacement of Bell magnesium cargo hook bumper and ring Part Nos. 204-072-901-1 or -3, and 204-072-905-3, respectively, with Onboard bumper ring kit No. 210-092-00. Fabrication of Onboard Systems Model 210-092-00 bumper ring kit. Onboard Systems International
- [STC SH5758NM](https://openairdocs.org/stc/SH5758NM): Fabrication of the Onboard Model 200-095-00 Multi-Channel Electrical Slip-Ring Kit. Onboard Systems International
- [STC SR00277SE](https://openairdocs.org/stc/SR00277SE): Fabrication of Onboard Systems Model 528-002-00 or 528-002-01 cargo hook. Onboard Systems International LLC
- [STC SR00699SE](https://openairdocs.org/stc/SR00699SE): Fabrication of Onboard Systems Model 200-246-00 cargo hook kit. Onboard Systems International
- [STC SR04425NY](https://openairdocs.org/stc/SR04425NY): Installation of the Basic Digital Flight Instrument Kit. Alpine Aerotech LP
- [STC SR04588NY](https://openairdocs.org/stc/SR04588NY): Replacement Cabin Floor Panels. Trinity Aviation Services Limited
- [STC SR04581NY](https://openairdocs.org/stc/SR04581NY): Installation of Mirror and Pulse Light. Ascent Aerospace Canada Ltd
- [STC SR02001SE](https://openairdocs.org/stc/SR02001SE): Fabrication and installation of Model 72448 locking fuel cover assembly. Timberline Aerospace LLC
- [STC SR04593NY](https://openairdocs.org/stc/SR04593NY): Installation of Two Place Seat. Ascent Aerospace Canada Ltd
- [STC SR04579NY](https://openairdocs.org/stc/SR04579NY): Installation of the 212-030-003-049 Nose Assembly. Ascent Aerospace Canada Ltd
- [STC SR04580NY](https://openairdocs.org/stc/SR04580NY): Installation of Public Address Speaker Box. Ascent Aerospace Canada Ltd
- [STC SR04577NY](https://openairdocs.org/stc/SR04577NY): Installation of Cabin Furnishings. Ascent Aerospace Canada Ltd
- [STC SR04578NY](https://openairdocs.org/stc/SR04578NY): Installation of Extended Port Seat Rails. Ascent Aerospace Canada Ltd
- [STC SR04569NY](https://openairdocs.org/stc/SR04569NY): Installation of the Garmin GTX 3x5 ADS-B Transponder. Alpine Aerotech LP
- [STC SR02492LA](https://openairdocs.org/stc/SR02492LA): Installation of a Helicopter Technology Company main rotor blade assembly. Helicopter Technology Co
- [STC SR04517NY](https://openairdocs.org/stc/SR04517NY): The Forward and Aft Crew Door Rod Assembly Replacement. Transwest Helicopters Ltd

All 230: https://openairdocs.org/model/bell-helicopter-textron-205a-1/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [67723VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171720993820260615132356.0001): Bearing Ball. Vision Air Services, LLC · PMA PQ2075NM · Replaces 67723 · May 14, 2026
- [66993VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133968021920260513201202.0001): Bearing Needle. Vision Air Services, LLC · PMA PQ2075NM · Replaces 66993 · May 6, 2026
- [650-430-100-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172240988120260512112135.0001): MECHANICAL SPECIALTIES, LLC MODEL 650-430-100-100ADVANCED DUEL EXTERNAL CARGO HOOK /ADEC™HOOK SYSTEM. Mechanical Specialties LLC · PMA PQ2180NM · Modification part · Apr 29, 2026
- [SL50029-102VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135551302320260501132607.0001): Bolt, Expandable Diameter. Vision Air Services, LLC · PMA PQ2075NM · Replaces SL50029-102 · Apr 14, 2026
- [310598VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115084524120260330121205.0001): Guide - Spring. Vision Air Services, LLC · PMA PQ2075NM · Replaces 310598 · Mar 6, 2026
- [297010VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140116613720260312142108.0001): Bearing-Valve Plate Needle. Vision Air Services, LLC · PMA PQ2075NM · Replaces 297010 · Dec 4, 2025
- [7244872448](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114062648220251119194650.0001): Locking CoverLocking Cover. Timberline Aerospace, LLC · PMA PQ05397NM · Modification part · Nov 10, 2025
- [297018VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164062991920260108162052.0001): Plate    Shoe Bearing. Vision Air Services, LLC · PMA PQ2075NM · Replaces 297018 · Oct 28, 2025
- [571917VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134512459920251216141232.0001): Ring - Retaining. Vision Air Services, LLC · PMA PQ2075NM · Replaces 571917 · Sep 17, 2025
- [WF338110](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187724258220250602133047.0001): Filter Element, Oil. Donaldson Company Inc · PMA PQ2432CE · Replaces 204-040-760-109, Alternate… · May 23, 2025
- [WF335199](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135387472720250602133021.0001): Filter Element, Hydraulic. Donaldson Company Inc · PMA PQ2432CE · Replaces 205-076-034-3, 205-076-034-003… · May 23, 2025
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149218362420250508133539.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [731753VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194830054520250121001131.0001): Shaft Drive. Vision Air Services, LLC · PMA PQ2075NM · Replaces 731753 · Jan 16, 2025
- [21146VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150503868120250121001131.0001): Gasket Retainer. Vision Air Services, LLC · PMA PQ2075NM · Replaces 21146 · Jan 16, 2025
- [41000253VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146232210320250121001131.0001): Clip. Vision Air Services, LLC · PMA PQ2075NM · Replaces 41000253 · Jan 16, 2025
- [67486VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113612412320250121001130.0001): Retainer Plate. Vision Air Services, LLC · PMA PQ2075NM · Replaces 67486 · Jan 16, 2025
- [98020205-1002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178365566620230502200036.0001): Bell Helicopter 205 NVG Modification Kit. REB Technologies Inc · PMA PQ1018SW · Modification part · May 2, 2023
- [APS105-00200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171485037220221020170412.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 105-00200 · Aug 10, 2022
- [APS66-10600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129038959420221020170313.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10600 · Aug 10, 2022
- [528-002-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197744174620220811112041.0001): 6,000 lb Cargo Hook. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [210-092-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179787422320220811112038.0001): Bumper Ring Kit. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [200-246-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171444673920220811112053.0001): 6K Keeperless Hook Kit. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [200-095-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170007928420220811112039.0001): 8-Channel Slip-Ring Kit. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [200-088-03200-088-04200-089-03200-089-04200-089-05200-089-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137647750920220811112036.0001): Suspension System. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [200-088-10200-088-11200-089-10200-089-11200-089-20200-089-21200-089-22200-089-23200-089-24200-089-25200-089-26200-089-27](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122178719620220811112054.0001): UH-1 Suspension System w/ Keeperless Hook. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [AG627000-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173317158220220809130834.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · May 10, 2022
- [AG844000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184493597720220809102509.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · Apr 18, 2022
- [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179433188720220408135727.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022
- [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103311286320220408135659.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022
- [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147138991420220408135626.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021
- [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181376643720220408135739.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138518672920220408140214.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AF1441003-1T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID638103261720211115171053.0001): Titanium Axle – Landing Gear. Airforms LLC · PMA PQ2644CE · Replaces 1441003-1 · Nov 4, 2021
- [AF1441003-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID220260073202111151710530.0001): Axle - Landing Gear. Airforms LLC · PMA PQ2644CE · Replaces 1441003-1 · Nov 4, 2021
- [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID766603459202111101104320.0001): Gasket-UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 9, 2021
- [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID242507537120210727195119.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 2020
- [AG843000-79](https://drs.faa.gov/browse/excelExternalWindow/7C47B4B54B5941DF862586240047DC8E.0001): Gasket - UHF / AM / IFF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2020
- [AG477000-35](https://drs.faa.gov/browse/excelExternalWindow/CAA7A03C831CF5A78625861F004520E1.0001): Gasket - GPS ANTENNA. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 11, 2020
- [AG247000-05](https://drs.faa.gov/browse/excelExternalWindow/A8B3EE75D8E4BBD2862585E5006243CC.0001): Gasket - Security System Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 24, 2020
- [AG843000-19](https://drs.faa.gov/browse/excelExternalWindow/6325AFC5586C8E34862585E500649009.0001): Gasket - VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 24, 2020
- [AG822000-03](https://drs.faa.gov/browse/excelExternalWindow/25D416C8B528F4988625859F003C440E.0001): Gasket - TCAS Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · May 31, 2020
- [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/44F91AF19B0D8D4586258591003A1785.0001): Gasket - UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 1, 2020
- [72448](https://drs.faa.gov/browse/excelExternalWindow/C7FE61192FBCF7B886258569003CFF58.0001): Locking Cover. Timberline Aerospace, LLC · PMA PQ05397NM · Modification part · Aug 27, 2019
- [AG843000-15](https://drs.faa.gov/browse/excelExternalWindow/445335953945E98886258560003BF2F7.0001): Gasket - VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 18, 2019
- [200-089-24](https://drs.faa.gov/browse/excelExternalWindow/FF6B50A8BBBF701486258567005C175F.0001): UH-1 Suspension System w/ Keeperless Hook. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 2, 2019
- [200-089-25](https://drs.faa.gov/browse/excelExternalWindow/5BB30B8E0F9510B586258567005C1794.0001): UH-1 Suspension System w/ Keeperless Hook. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 2, 2019
- [200-088-11](https://drs.faa.gov/browse/excelExternalWindow/49EC6823184C3FE586258567005C1723.0001): UH-1 Suspension System w/ Keeperless Hook. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 2, 2019
- [AG247000-04](https://drs.faa.gov/browse/excelExternalWindow/F4D9B388DAECF53586258553004D4A85.0001): Gasket - L-Band Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 25, 2019
- [AG723000-27](https://drs.faa.gov/browse/excelExternalWindow/0740FB46C2B93B86862585520042A854.0001): Gasket - Radio Altimeter Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 9, 2019
- [72448-107](https://drs.faa.gov/browse/excelExternalWindow/A3835EFF6F7514BC86258550004EBC9A.0001): Hinge, Locking Cover. Timberline Aerospace, LLC · PMA PQ05397NM · Modification part · Apr 29, 2019

All of them: https://openairdocs.org/model/bell-helicopter-textron-205a-1/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Bell 205A-1](https://openairdocs.org/model/bell-205a-1): 56 registered aircraft, registry code 1181414
- [Bell/Southwest Florida Aviatio 205 A1](https://openairdocs.org/model/bell-southwest-florida-aviatio-205-a1): 2 registered aircraft, registry code 11814SF

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