# Bell Helicopter Textron Canada 206L-3

- Type: Aircraft model (FAA registry)
- Registry code: 1182156
- Manufacturer (registry): BELL HELICOPTER TEXTRON CANADA
- Model: 206L-3
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 5
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (OpenAirDocs)
- Holder: Bell Textron Canada Limited
- Registered aircraft: 4
- Page: https://openairdocs.org/model/bell-helicopter-textron-canada-206l-3

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 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 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 2023-06-05](https://openairdocs.org/ad/2023-06-05): Tail Rotor Drive Shaft · Bell Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective May 19, 2023
- [AD 2022-22-08](https://openairdocs.org/ad/2022-22-08): Main Rotor Blades · Main rotor blade assembly P/N 20633000-101 (Van Horn STC SR02684LA). Effective Dec 23, 2022
- [AD 2022-20-04](https://openairdocs.org/ad/2022-20-04): Tail Rotor Drive Shaft · Bell Textron Canada 206, 206A, 206A-1 (OH-58A) and 6 more. Effective Dec 23, 2022
- [AD 2021-24-15](https://openairdocs.org/ad/2021-24-15): Tail Rotor Drive Shaft · Bell Textron Canada 206L-1, 206L-3 and 206L-4 with STC SH2750NM. Effective Jan 18, 2022
- [AD 2021-19-01](https://openairdocs.org/ad/2021-19-01): Cabin Equipment/Furnishings · Shoulder harness restraint system (Bell Helicopter Textron STC SH2073SO or SH2751SO). Effective Oct 13, 2021
- [AD 2021-15-06](https://openairdocs.org/ad/2021-15-06): Tail Rotor Drive · Bell Textron Canada 206A, 206B, 206L and 3 more. Effective Aug 27, 2021
- [AD 2021-10-08](https://openairdocs.org/ad/2021-10-08): Fuel Quantity Sensor · Bell Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective Jun 11, 2021
- [AD 2019-08-10](https://openairdocs.org/ad/2019-08-10): Main Rotor Drive System · Bell Helicopter Textron Canada 206A, 206B, 206L and 4 more. Effective Jun 24, 2019
- [AD 2018-25-17](https://openairdocs.org/ad/2018-25-17): Air Conditioning System Wiring · Airbus Helicopters 206A, 206B, 206L and 13 more. Effective Jan 22, 2019
- [AD 2017-05-04](https://openairdocs.org/ad/2017-05-04): Tension Torsion Strap · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Mar 17, 2017
- [AD 2015-12-02](https://openairdocs.org/ad/2015-12-02): Turbine Section · Bell Helicopter Textron Canada 206L-1, 206L-3 and 206L-4. Effective Jul 14, 2015
- [AD 2014-02-02](https://openairdocs.org/ad/2014-02-02): Main Rotor Blades · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective Mar 7, 2014
- [AD 2013-25-10](https://openairdocs.org/ad/2013-25-10): Rotorcraft Tailboom · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective Jan 31, 2014
- [AD 2013-22-21](https://openairdocs.org/ad/2013-22-21): Emergency Flotation Section · Apical Industries, Inc. Emergency Float Kits (Dart Aerospace ULC STC SR01535LA). Effective Dec 13, 2013
- [AD 2013-18-06](https://openairdocs.org/ad/2013-18-06): Main Rotor Control · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Oct 17, 2013
- [AD 2013-02-01](https://openairdocs.org/ad/2013-02-01): Rotorcraft Servo System · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective Feb 7, 2013
- [AD 2012-12-11](https://openairdocs.org/ad/2012-12-11): Engine EFT/TOT Indicating System · Supplemental lighting system (Aviation Specialties Unlimited STC SR01383SE). Effective Jul 24, 2012
- [AD 2012-02-51](https://openairdocs.org/ad/2012-02-51): Main rotor blades · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective May 4, 2012
- [AD 2011-25-01](https://openairdocs.org/ad/2011-25-01): Liferafts · Agusta AB412, AB412 EP, 206A and 23 more. Effective Jan 17, 2012
- [AD 2010-26-51](https://openairdocs.org/ad/2010-26-51): Tail rotor blade · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Mar 25, 2011
- [AD 96-18-05 R1](https://openairdocs.org/ad/96-18-05-R1): Tailboom · Bell Helicopter Textron Canada 206L, 206L-1 and 206L-3. Effective Dec 21, 2010
- [AD 2009-07-52](https://openairdocs.org/ad/2009-07-52): Cyclic control lever assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 7 more. Effective May 1, 2009
- [AD 2008-14-06](https://openairdocs.org/ad/2008-14-06): Horizontal stabilizers · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 2 more. Effective Aug 14, 2008
- [AD 2008-14-03](https://openairdocs.org/ad/2008-14-03): Tailboom attachment · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Aug 14, 2008
- [AD 2007-01-06](https://openairdocs.org/ad/2007-01-06): Tail rotor blade (blade) · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Feb 13, 2007
- [AD 2005-21-03](https://openairdocs.org/ad/2005-21-03): Tail rotor blade (blade) root doublers (doublers) · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective Nov 21, 2005
- [AD 2004-22-13](https://openairdocs.org/ad/2004-22-13): Magnetic brake assembly · Bell Helicopter Textron Canada 206L-1 and 206L-3. Effective Dec 7, 2004
- [AD 2003-13-14](https://openairdocs.org/ad/2003-13-14): Chip detector · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective Aug 12, 2003
- [AD 2002-25-07](https://openairdocs.org/ad/2002-25-07): Tailboom skins · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective Jan 27, 2003
- [AD 2002-20-05](https://openairdocs.org/ad/2002-20-05): Rescue hoists · Agusta A109, A109A, A109A II and 31 more. Effective Nov 7, 2002
- [AD 2001-02-03](https://openairdocs.org/ad/2001-02-03): Raised Forging Boss · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Mar 9, 2001
- [AD 99-17-19](https://openairdocs.org/ad/99-17-19): Mast And Trunnion · Bell Helicopter Textron Canada 206L, 206L-1, 206L-3 and 1 more. Effective Sep 24, 1999
- [AD 95-11-14](https://openairdocs.org/ad/95-11-14): Crosstubes · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective Jun 30, 1995
- [AD 95-09-06](https://openairdocs.org/ad/95-09-06): Fuel Valve Switch · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Jun 8, 1995
- [AD 94-24-11](https://openairdocs.org/ad/94-24-11): Tail Rotor Drive Shaft · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Jan 6, 1995
- [AD 94-20-03](https://openairdocs.org/ad/94-20-03): Main Rotor Hub Trunnion · Bell Helicopter Textron Canada 206A, 206B, 206B-1 and 4 more. Effective Oct 11, 1994
- [AD 94-19-02](https://openairdocs.org/ad/94-19-02): Swashplate Support Assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Sep 28, 1994
- [AD 94-15-07](https://openairdocs.org/ad/94-15-07): Main Rotor Blades · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Aug 26, 1994
- [AD 92-06-12](https://openairdocs.org/ad/92-06-12): Transmission Failure · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Apr 13, 1992
- [AD 92-01-05](https://openairdocs.org/ad/92-01-05): Main Rotor Blades · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Feb 5, 1992
- [AD 90-13-01 R1](https://openairdocs.org/ad/90-13-01-R1): Tail Rotor Blade Assembly · Bell Helicopter Textron Canada 206B, 206L, 206L-1 and 1 more. Effective Oct 17, 1991
- [AD 89-20-13](https://openairdocs.org/ad/89-20-13): Horizontal Stabilizer · Bell Helicopter Textron Canada 206L, 206L-1 and 206L-3. Effective Oct 15, 1991
- [AD 90-21-03](https://openairdocs.org/ad/90-21-03): Tail Rotor Blade Assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Aug 14, 1991
- [AD 91-03-12](https://openairdocs.org/ad/91-03-12): Emergency Float Bags · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Feb 28, 1991
- [AD 88-23-03](https://openairdocs.org/ad/88-23-03): Tail Rotor Yoke Assembly · Bell Helicopter Textron Canada 206A, 206B, 206B-1 and 3 more. Effective Jul 25, 1989
- [AD 78-11-02 R1](https://openairdocs.org/ad/78-11-02-R1): Rotor Blade Straps · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Dec 15, 1988
- [AD 87-10-11](https://openairdocs.org/ad/87-10-11): Main Rotor Mast Assemblies · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Aug 8, 1988
- [AD 87-15-01](https://openairdocs.org/ad/87-15-01): Stabilizer Assembly · Bell Helicopter Textron Canada 206L-1 and 206L-3. Effective Aug 6, 1987

Historical (superseded or no longer in force):

- [AD 2021-26-08](https://openairdocs.org/ad/2021-26-08) (historical): Tail Rotor Drive Shaft · Bell Textron Canada 206, 206A, 206A-1 and 7 more. Effective Jan 27, 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 2009-08-03](https://openairdocs.org/ad/2009-08-03) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Apr 24, 2009
- [AD 2009-07-51](https://openairdocs.org/ad/2009-07-51) (historical): Lever assembly bearing · Bell Helicopter Textron 206A, 206A-1 (OH-58A), 206B and 7 more
- [AD 2007-19-52](https://openairdocs.org/ad/2007-19-52) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Dec 5, 2007
- [AD 2004-24-08](https://openairdocs.org/ad/2004-24-08) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 3 more. Effective Dec 16, 2004
- [AD 99-13-12](https://openairdocs.org/ad/99-13-12) (historical): Tailboom Skin For Cracks Inspection · Bell Helicopter Textron 206L, 206L-1, 206L-3 and 1 more. Effective Jul 9, 1999
- [AD 96-18-05](https://openairdocs.org/ad/96-18-05) (historical): Tailboom  Inspection · Bell Helicopter Textron Canada 206L, 206L-1 and 206L-3. Effective Sep 16, 1996

All 63: https://openairdocs.org/model/bell-helicopter-textron-canada-206l-3/ads.md

## Information bulletins (advisory) (8)

- [SAIB SW-19-05](https://openairdocs.org/saib/SW-19-05): Tail Rotor Drive System, Spline Damage. Issued Apr 4, 2019
- [SAIB SW-18-02](https://openairdocs.org/saib/SW-18-02): Loss of Hardware  Tail Rotor Drive Shaft Couplings. Issued Nov 2, 2017
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012
- [SAIB SW-10-42R1](https://openairdocs.org/saib/SW-10-42R1): Emergency Float Kits. Issued Aug 11, 2010
- [SAIB SW-10-42](https://openairdocs.org/saib/SW-10-42) (historical): Emergency Float Kits. Issued Aug 5, 2010
- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008
- [SAIB SW-05-24](https://openairdocs.org/saib/SW-05-24): . Issued Dec 22, 2004
- [SAIB SW-04-92](https://openairdocs.org/saib/SW-04-92): . Issued Sep 30, 2004

## Registered aircraft (4)

- [N17TL](https://openairdocs.org/aircraft/N17TL): [Turbines Ltd](https://openairdocs.org/faa-owner/TURBINES%20LTD), [West Point, NE](https://openairdocs.org/faa-place/NE/West%20Point), built 1992, S/N 51603
- [N313HP](https://openairdocs.org/aircraft/N313HP): [Mshr Helicopter Services LLC](https://openairdocs.org/faa-owner/MSHR%20HELICOPTER%20SERVICES%20LLC), [Chehalis, WA](https://openairdocs.org/faa-place/WA/Chehalis), built 1990, S/N 51341
- [N4KA](https://openairdocs.org/aircraft/N4KA): [Ambrose Group Inc](https://openairdocs.org/faa-owner/AMBROSE%20GROUP%20INC), [Bellevue, WA](https://openairdocs.org/faa-place/WA/Bellevue), built 1992, S/N 51578
- [N979HB](https://openairdocs.org/aircraft/N979HB): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), S/N 51403

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN25LA408](https://openairdocs.org/ntsb/CEN25LA408), Aug 22, 2025: Bell Helicopter Textron Canada 206L-3 (N17TL), Picayune, MS, substantial damage, investigation ongoing
- [NTSB FTW94FA152](https://openairdocs.org/ntsb/FTW94FA152), May 10, 1994: Bell 206L-3 (N5844), Intracoastl Cty, LA, destroyed, 5 fatal. Probable cause: THE PILOT'S FAILURE TO MAINTAIN AIRCRAFT CONTROL FOR UNDETERMINED REASONS.

## 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, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 19940510010489A](https://openairdocs.org/incident/19940510010489A), May 10, 1994: Bell 206L3 (N5844), Intercoastal Ci, LA, Destroyed, 5 fatal. Helicopter en route to oil rig with crew change impacted in gulf one mile from shore. No anomalies.

## Service difficulty reports (2,927, newest 50)

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

- [SDR EVCA2026100126](https://openairdocs.org/sdr/EVCA2026100126), Sep 30, 2026: BLOWER MOTOR. UNSERVICEABLE. ELECTRICAL SMELL WHEN AIR CONDITIONER IS TURNED ON. AFT BLOWER MOTOR WAS THE CAUSE. SYSTEM MEL'ED UNTIL A REPLACEMENT ARRIVES.
- [SDR EVCA20250623001](https://openairdocs.org/sdr/EVCA20250623001), Jun 23, 2025: PUMP. FAILED. HYDRAULIC FAILURE
- [SDR EVCA202503250001](https://openairdocs.org/sdr/EVCA202503250001), Mar 19, 2025: ANGLE. CRACKED. LH & RH FS 145 & STIFFENER CLIP CRACKED
- [SDR EVCA20250228001](https://openairdocs.org/sdr/EVCA20250228001), Feb 27, 2025: STIFFENER. CRACKED. UPPER BOX BEAM FWD STIFFENERS CRACKED. PN 206-033-110-229 & 206-033-110-197
- [SDR EVCA20241204001](https://openairdocs.org/sdr/EVCA20241204001), Dec 4, 2024: STIFFENER. CRACKED. VERTICAL TUNNEL AFT RH STIFFENER CRACKED. VERTICAL TUNNEL SKIN CRACKED AT WL 65.0
- [SDR EVCA202406240002](https://openairdocs.org/sdr/EVCA202406240002), Jun 24, 2024: BLADE. CRACKED. M/R BLADE INBOARD TRIM TABS CRACKED
- [SDR EVCA202406240001](https://openairdocs.org/sdr/EVCA202406240001), Jun 24, 2024: BLADE. CRACKED. M/R BLADE INBOARD TRIM TABS CRACKED
- [SDR EVCA202404220002](https://openairdocs.org/sdr/EVCA202404220002), Apr 22, 2024: HEATER. ODOR. BURNING SMELL FROM HEATER, COULD NOT DUPLICATE.
- [SDR EVCA202402190024](https://openairdocs.org/sdr/EVCA202402190024), Feb 17, 2024: UNKNOWN. ODOR. STRONG FUEL SMELL IN AIRCRAFT ON STARTUP. AMT PULLED HAT RACK AND FUEL VALVE COVER, PERFORMED VISUAL INSPECTION AND NO LEAKS DETECTED. PERFORMED GROUND RUN AND 
- [SDR EVCA202308220002](https://openairdocs.org/sdr/EVCA202308220002), Aug 22, 2023: STIFFENER. CRACKED. R/H FS 145 STIFFENER CLIP CRACKED.
- [SDR EVCA202308220001](https://openairdocs.org/sdr/EVCA202308220001), Aug 22, 2023: FRAME. CRACKED. L/H FS 145 FRAME CRACKED.
- [SDR EVCA08222023](https://openairdocs.org/sdr/EVCA08222023), Aug 22, 2023: STIFFENER. CRACKED. L/H FS 145 STIFFENER CLIP CRACKED.
- [SDR EVCA03102023](https://openairdocs.org/sdr/EVCA03102023), Mar 9, 2023: BLADE. UNSERVICEABLE. MR BLADE TRIM TAB CTRACKED
- [SDR EVCA20230119001](https://openairdocs.org/sdr/EVCA20230119001), Jan 19, 2023: STIFFENER. CRACKED. LEFT HAND VERTICAL TUNNEL STIFFENER IS CRACKED ON UPPER END
- [SDR EVCA01122023](https://openairdocs.org/sdr/EVCA01122023), Jan 6, 2023: FUEL CONTROL. LEAKING. FUEL SMELL IN CABIN UPON TAKE OFF. FOUND FUEL SEEP AT FUEL CONTROL UNIT.
- [SDR EVCA010320233](https://openairdocs.org/sdr/EVCA010320233), Jan 2, 2023: RING. CRACKED. 1/2 INCH CRACK AT UPPER LH INBOARD SIDE OF TAILBOOM RING.
- [SDR EVCA2023010300001](https://openairdocs.org/sdr/EVCA2023010300001), Jan 2, 2023: HOSE. CRACKED. HOSE CRACKED AT THE ATTACHMENT FITTING CAUSING A LOSS OF HYDRAULIC FLUID AND THE LOSS OF HYDRAULIC ASSISTED FLIGHT CONTROLS.
- [SDR EVCA202212200001](https://openairdocs.org/sdr/EVCA202212200001), Dec 18, 2022: UNKNOWN. ODOR. FUEL SMELL IN CABIN UPON TAKE OFF. NO DISCREPANCIES NOTED DURING INSPECTION. COULD NOT DUPLICATE.
- [SDR EVCA202211230022](https://openairdocs.org/sdr/EVCA202211230022), Nov 23, 2022: STIFFENER. CRACKED. STIFFENER AT FORWARD EDGE OF BOX BEAM IS CRACKED ON RH SIDE (.2 INCH).
- [SDR 2022FA0000299](https://openairdocs.org/sdr/2022FA0000299), Jun 17, 2022: NONE. MALFUNCTIONED. PILOT REPORTED THE FOLLOWING: "AT ROUGHLY 230 P.M., I WAS MAKING MY WAY BACK FROM A NORTH CANYON TOUR LANDING SOUTH TAKEOFF WEIGHT 3767 POUNDS. WINDS WERE ABOUT
- [SDR EVCA102921](https://openairdocs.org/sdr/EVCA102921), Oct 29, 2021: ANGLE. CRACKED. DOING A VISUAL INSPECTION FOUND THE RH 145 BULKHEAD UPPER ANGLE CRACKED AROUND FASTENERS.
- [SDR EVCA102521(2)](https://openairdocs.org/sdr/EVCA102521(2)), Oct 25, 2021: BRACKET. CRACKED. LH PASSENGER DOOR OPENER BRACKET IS CRACKED.
- [SDR EVCA102521](https://openairdocs.org/sdr/EVCA102521), Oct 25, 2021: RING. CRACKED. UPPER LH ATTACHMENT FITTING ON TAILBOOM RING IS CRACKED
- [SDR EVCA08192021](https://openairdocs.org/sdr/EVCA08192021), Aug 19, 2021: BULKHEAD. CRACKED. WHILE DOING THE 300 HOUR PERIODIC INSPECTIONS WE NOTICED WORKING RIVETS AT STA. 145. WE OPENED ON THE BULKHEAD PANELS AND USED A BORESCOPE AND FOUND A CRACK ON 
- [SDR EVCA06182021](https://openairdocs.org/sdr/EVCA06182021), Jun 18, 2021: BLADE. DAMAGED. MAIN ROTOR BLADE SPAN-WISE WEIGHT COVER SEPARATED FROM BLADE IN FLIGHT.
- [SDR EVCA06022021](https://openairdocs.org/sdr/EVCA06022021), May 29, 2021: BLADE. DAMAGED. MAIN ROTOR BLADE SPAN-WISE WEIGHT COVER SEPARATED FROM BLADE IN FLIGHT.
- [SDR EVCA051720212](https://openairdocs.org/sdr/EVCA051720212), May 17, 2021: PANEL. CRACKED. PILOT'S CRUSH PANEL IS CRACKED AT THE CENTER NUTPLATE. WE WILL REPLACE THE CRUSH PANEL.
- [SDR EVCA0517211](https://openairdocs.org/sdr/EVCA0517211), May 17, 2021: SKIN. DEBONDED. LEFT HAND ELEVATOR TRAILING EDGE IS DEBONDED THE ENTIRE LENGTH OF THE ELEVATOR. WE WILL REPLACE THE PART.
- [SDR EVCA2020093003](https://openairdocs.org/sdr/EVCA2020093003), Sep 29, 2020: DISC PACK. CORRODED. DURING ROUTINE INSPECTION, NR 6 TAIL ROTOR DRIVE SHAFT DISC PACK HAS CORROSION BETWEEN DISCS.
- [SDR EVCA202009183](https://openairdocs.org/sdr/EVCA202009183), Sep 17, 2020: COMBUSTION LINER. CRACKED. DURING INSPECTION, CRACKS WERE VISUALLY FOUND ON THE ENGINE COMBUSTION LINER.
- [SDR EVCA2020031611](https://openairdocs.org/sdr/EVCA2020031611), Mar 16, 2020: ATTACH FITTING. CRACKED. UPPER L/H TAILBOOM ATTACH FITTING CRACKED. REMOVED DAMAGED FITTING PN 206-032-409-001P AND INSTALLED NEW FITTING PN 206-032-409-001P IAW BHT-206-SRM-1 6-3-1.
- [SDR EVCA2020011700000](https://openairdocs.org/sdr/EVCA2020011700000), Jan 17, 2020: BULKHEAD. CRACKED. DURING PERIODIC INSPECTION, FOUND LT BULKHEAD AT FS 145 UPPER FLANGE CRACKED AT RIVET ATTACHMENT.
- [SDR IAVA2019101600001](https://openairdocs.org/sdr/IAVA2019101600001), Oct 16, 2019: SKIN. CRACKED. CRACK ON UPPER TAIL BOOM SKIN AT STATION 172 FROM 3RD RIVET FORWARD OF CASTING ON SKIN SPLICE SEAM TO 4TH RIVET AT TAIL ROTOR GEARBOX CASTING ATTACHMENT RIVET L
- [SDR EVCA201910100003](https://openairdocs.org/sdr/EVCA201910100003), Oct 10, 2019: BLADE. CORRODED. BOTH RED & WHITE MR BLADES HAVE CORROSION IN BLADE PIN RETENTION RECEPTACLES. REMOVED MR BLADE ASSY(S). PN: 206-015-001-115, SN(S) BH482876 & BH482878, AND REPL
- [SDR W7OA20200204001](https://openairdocs.org/sdr/W7OA20200204001), May 16, 2019: BLADE. DAMAGED. THIS IS OUR SECOND SET OF VAN HORN AVIATION TAIL ROTOR BLADES PN 2062200-301 THAT WE HAVE ENCOUNTERED CRACKS/DEBONDING IN THE LOWER/UPPER LEADING EDGES AND SKIN
- [SDR EVCA2019050800001](https://openairdocs.org/sdr/EVCA2019050800001), May 8, 2019: CONNECTOR. BURNED. CREW REPORTS ELECTRICAL BURNT SMELL IN REAR CABIN WHEN AIR CONDITIONING TURN ON. REPLACED 2 EACH WIRE CONNECTORS ON AIR CONDITIONER COMPRESSOR RELAY P/N RC10-25
- [SDR EVCA2019050200000](https://openairdocs.org/sdr/EVCA2019050200000), May 2, 2019: STRUCTURE. CRACKED. ONE INCH CRACK FOUND ON UPPER TOP DECK. IT IS LOCATED AT STA 147, WL 72, AND BL 11.
- [SDR 2019FA0000069](https://openairdocs.org/sdr/2019FA0000069), Mar 13, 2019: BULKHEAD. CRACKED. DURING AN OAS INSPECTION A SMALL CRACK WAS FOUND ON THE TOP RIGHT HAND SIDE OF THE AFT FUSELAGE BULKHEAD P/N 206-032-308-003, NEXT TO THE TAILBOOM ATTACHMENT BO
- [SDR EVCA201809052](https://openairdocs.org/sdr/EVCA201809052), Sep 4, 2018: ATTACH FITTING. CRACKED. TAILBOOM ATTACHMENT FITTING UPPER LEFT TAILBOOM SIDE CRACKED. AMT'S REMOVED AND REPLACED TAILBOOM FITTING.
- [SDR EVCA20180618181](https://openairdocs.org/sdr/EVCA20180618181), Jun 12, 2018: STRUCTURE. CRACKED. DURING INSPECTION, A CRACK WAS SUSPECTED IN EXTRUSION NEAR BS 73 OVER THE RT FWD LANDING GEAR FITTING. REMOVED AND REPLACED THE CRACKED EXTRUSION.
- [SDR EVCA20180523211](https://openairdocs.org/sdr/EVCA20180523211), May 21, 2018: MOUNT FLANGE. CRACKED. WHILE PERFORMING A SCHEDULED 100 HR INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM MOUNTING RING PN: 206-032-400-027 APPROXIMATELY 3 INCHES IN LENGTH BELOW THE U
- [SDR EVCA201803090001](https://openairdocs.org/sdr/EVCA201803090001), Mar 8, 2018: STRUCTURE. CORRODED. PILOT DISCOVERED A CRACK IN WING WALK COMPOUND LOCATED ON THE RT CABIN ROOF. INVESTIGATED AND FOUND CORROSION UNDER THE WING WALK COMPOUND.
- [SDR EVCA201802061](https://openairdocs.org/sdr/EVCA201802061), Feb 6, 2018: ATTACH FITTING. CRACKED. DURING SCHEDULED INSPECTION AND COMPLIANCE WITH FAA AD 2013-25-10 MAINTENANCE TECHNICIAN FOUND A 1.125" CRACK IN UPPER LEFT HAND TAILBOOM ATTACH FITTING PN: 206
- [SDR EVCA201708260001](https://openairdocs.org/sdr/EVCA201708260001), Aug 26, 2017: CONNECTOR. BURNED. FLIGHT CREW REPORTED A BURNING ODOR EMANATING FROM THE AFT CABIN. DURING INSPECTION, IT WAS DISCOVERED THAT THE CONNECTOR TO THE TRANSPONDER CONTROL UNIT IN THE
- [SDR EVCA201705301](https://openairdocs.org/sdr/EVCA201705301), May 30, 2017: TUBE. DAMAGED. WHILE PERFORMING INSPECTION OF THE AIRCRAFT, FOUND ONE CYCLIC TUBE TO HAVE THE FIXEDAND NON ADJUSTABLE CLEVIS ON THE TRANSMISSION BELLCRANK END OF THE CONTROL T
- [SDR EVCA201611021](https://openairdocs.org/sdr/EVCA201611021), Nov 2, 2016: BLOWER MOTOR. BURNED. DURING FINAL APPROACH TO SCHEDULED LANDING PILOT AND FLIGHT CREW REPORTED SMELLING A STRONG ELECTRICAL BURNING SMELL. UPON MAINTENANCE INSPECTION FOUND THE ARMA
- [SDR AC2R2016052301](https://openairdocs.org/sdr/AC2R2016052301), May 23, 2016: STRUCTURE. CRACKED. CRACK ON LT SIDE OF ACFT AFT LOWER SHELL, AT BS 140-150. CRACK IS FROM WL 35-54, BL 26. CRACK IS ADJACENT TO TIEDOWN, STEP WHICH IS MOUNTED TO AIRFRAME. CRACK W
- [SDR EVCA20160215001](https://openairdocs.org/sdr/EVCA20160215001), Feb 12, 2016: ANGLE. CRACKED. FOUND CRACKS AT BOX BEAM INTERFACE WITH FWD VERTICAL CONTROL TUNNEL ON RT SIDE. FOUND ANGLE, PN 206-033-110-229 & WEB PN 206-033-110-183, CRACKED. MAXIMUM CRACK
- [SDR EVCA201512281](https://openairdocs.org/sdr/EVCA201512281), Dec 24, 2015: BLOWER MOTOR. INOPERATIVE. IN FLIGHT CREW REPORTED ELEC BURNING SMELL. ACFT RETURNED TO BASE. UPON INSPECTION FOUND FAIL AFT AIR CONDITIONER BLOWER MOTOR.
- [SDR CA160119009](https://openairdocs.org/sdr/CA160119009), Oct 15, 2015: ROTOR. SEPARATED. (CAN) ACFT WAS ON AN AERIAL APPLICATION MISSION WHEN IT WAS REQUIRED TO MAKE A FORCED LANDING. INITIAL REPORTS STATE THE TAIL ROTOR SEPARATED FROM THE ACFT.

All 2,927: https://openairdocs.org/model/bell-helicopter-textron-canada-206l-3/reports.md

## STCs that may be installed (OpenAirDocs) (465, 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 SH2750NM](https://openairdocs.org/stc/SH2750NM): Installation of a Freon type cabin air conditioning system with engine-driven compressor. Air Comm Corporation
- [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [STC SR00643SE](https://openairdocs.org/stc/SR00643SE): Installation of Geneva Aviation Video System. Turbolyft USA Corporation
- [STC SR12375NY](https://openairdocs.org/stc/SR12375NY): Demonstration of Aircraft Equipment Configurations Tolerance to Transmitting Portable Electronic Devices (TPED) in Part 27 Aircraft in accordance with the FAA-approved Rotorcraft Equipment Compatibility List (RECL). Kilroy Aviation, LLC
- [STC SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc
- [STC SR00521SE](https://openairdocs.org/stc/SR00521SE): Installation of Geneva Aviation Audio System. AEM USA Inc
- [STC SR02301SE](https://openairdocs.org/stc/SR02301SE): Installation of Geneva Aviation 28 - 14 VDC Power Converter. AEM USA Inc
- [STC SR02445SE](https://openairdocs.org/stc/SR02445SE): Installation of P178 Failsafe Audio Mixer. AEM USA Inc
- [STC SR02684LA](https://openairdocs.org/stc/SR02684LA): Installation of main rotor blade assembly P/N 20633000-101. Van Horn Aviation LLC
- [STC SH2617SO](https://openairdocs.org/stc/SH2617SO): Installation of a hat rack safety net assembly, P/N 206-432. Bell Helicopter Textron Inc
- [STC SR11898NY](https://openairdocs.org/stc/SR11898NY): Installation of Outerlink Corporation Air IP system. Sterling Helicopter
- [STC SR04845NY](https://openairdocs.org/stc/SR04845NY): Installation of a Helifab East Equipment Mount. Helifab East LLC
- [STC SR04842NY](https://openairdocs.org/stc/SR04842NY): Installation of RMCI Inc. Expandable Rotorcraft Diagnostic System (XRDS). Sterling Helicopter
- [STC SR02809SE](https://openairdocs.org/stc/SR02809SE): Installation of Isolair Inc. Spray System model 3900-206L. Isolair Inc
- [STC SR00532SE](https://openairdocs.org/stc/SR00532SE): Installation of Certified Technology quick release door pins. Certified Technology
- [STC SH3761SW](https://openairdocs.org/stc/SH3761SW): Installation of enlarged instrument panel. Safran Electronics & Defense Avionics USA LLC
- [STC SR00853DE](https://openairdocs.org/stc/SR00853DE): Installation of Fibrotek survey stinger. Upper Limit Aviation
- [STC SR04548CH](https://openairdocs.org/stc/SR04548CH): Installation of Appareo Systems AIRS-400 Flight Monitoring System. Appareo Systems
- [STC SR00425SE](https://openairdocs.org/stc/SR00425SE): Installation of a satellite phone. Turbolyft USA Corporation
- [STC SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd
- [STC SR00891LA](https://openairdocs.org/stc/SR00891LA): Installation of aft utility mount. Airfilm Camera Systems LLC
- [STC SR01688LA](https://openairdocs.org/stc/SR01688LA): Installation of Aero Pacific Belly Utility Mount. Airfilm Camera Systems LLC
- [STC SR04637CH](https://openairdocs.org/stc/SR04637CH): Replacement of existing main ship battery with Lithium Ion Battery and installation of Annunciator Control Panel. Airwolf Aerospace LLC
- [STC SH1244SO](https://openairdocs.org/stc/SH1244SO): Fabrication and installation of camera mount and photographer's seat. Ephraim Nowak
- [STC SH1661SO](https://openairdocs.org/stc/SH1661SO): Fabrication and installation of wind sceen. Ephraim Nowak
- [STC SH3899NM](https://openairdocs.org/stc/SH3899NM): Installation of cabin accessory steps. Dart Aerospace USA Inc
- [STC SH5220NM](https://openairdocs.org/stc/SH5220NM): Installation of Freon air conditioning system. Dart Aerospace USA Inc
- [STC SH5231NM](https://openairdocs.org/stc/SH5231NM): Installation of external pod, camera mount, and 12 volt power provision. Dart Aerospace USA Inc
- [STC SR00106DE](https://openairdocs.org/stc/SR00106DE): Installation and provisions for a nose mounted mini-video camera system and controls. Dart Aerospace USA Inc
- [STC SR00196DE](https://openairdocs.org/stc/SR00196DE): Installation of quick-mount snow pads. Dart Aerospace USA Inc
- [STC SR00326DE](https://openairdocs.org/stc/SR00326DE): Installation of stabilized camera system. Dart Aerospace USA Inc
- [STC SR00611DE](https://openairdocs.org/stc/SR00611DE): Installation of a ram air vent control cable kit in. Dart Aerospace USA Inc
- [STC SR00682DE](https://openairdocs.org/stc/SR00682DE): Installation of Augmented Reality System. Dart Aerospace USA Inc
- [STC SR02120SE](https://openairdocs.org/stc/SR02120SE): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc
- [STC SR00010DE](https://openairdocs.org/stc/SR00010DE): Installation of anti-torque pedal extensions. Dart Aerospace USA Inc
- [STC SR00011DE](https://openairdocs.org/stc/SR00011DE): Installation of a monitor mount assembly to mount a video monitor. (206B S/N 914 and subs). Dart Aerospace USA Inc
- [STC SR00159DE](https://openairdocs.org/stc/SR00159DE): Installation of Spectrolab SX-16 searchlight under cargo compartment. Dart Aerospace USA Inc
- [STC SR00449DE](https://openairdocs.org/stc/SR00449DE): Installation of removable dual pedal system. Dart Aerospace USA Inc
- [STC SR00516DE](https://openairdocs.org/stc/SR00516DE): Installation of mounting hardware. Dart Aerospace USA Inc
- [STC SR00654DE](https://openairdocs.org/stc/SR00654DE): Installation of Rotary Latch Seat Belts. Dart Aerospace USA Inc
- [STC SH5243NM](https://openairdocs.org/stc/SH5243NM): Installation of hard point for mounting of a Forward Looking Infrared imaging unit or similar external gimbal. Dart Aerospace USA Inc
- [STC SR00014DE](https://openairdocs.org/stc/SR00014DE): Installation of Inframetrics IRTV-445G infrared imaging system. Dart Aerospace USA Inc
- [STC SR00025DE](https://openairdocs.org/stc/SR00025DE): Installation of a shelf panel. Dart Aerospace USA Inc
- [STC SR00033DE](https://openairdocs.org/stc/SR00033DE): Installation of an external mirror. Dart Aerospace USA Inc
- [STC SR00169DE](https://openairdocs.org/stc/SR00169DE): Installation of a fuel cap hinge and hardware. (206B S/N 3567 and subsquent). Dart Aerospace USA Inc
- [STC SR00375DE](https://openairdocs.org/stc/SR00375DE): Installation of laser mapping system. Dart Aerospace USA Inc
- [STC SR00489DE](https://openairdocs.org/stc/SR00489DE): Installation of Paravion Technology PR-206SC-100 engine start counter system. Dart Aerospace USA Inc
- [STC SR00104DE](https://openairdocs.org/stc/SR00104DE): Installation of 6 large area cabin windows. DV Aviation Inc
- [STC SR01980WI](https://openairdocs.org/stc/SR01980WI): Installation of Garmin GI 275 Multi-Function Instrument. Garmin International Inc
- [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

All 465: https://openairdocs.org/model/bell-helicopter-textron-canada-206l-3/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.

- [206EC-206-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191900160820260923123949.0001): Instl-Air Cond – Dual Fwd Evap (206L,L1&L3) – (General Arrangement-206L, L1 & L3 Air Cond Sys (Torq-Loc). Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [MDLDL-206V](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184905881020260923124149.0001): Cabin Ventilation System. Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [206EC-206-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182732151920260923123948.0001): Instl-Air Cond – Single Fwd Evap (LH) (206L,L1&L3) – (General Arrangement-206L, L1 & L3 Air Cond Sys (Torq-Loc). Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [206EC-206-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121020261420260923123948.0001): Instl-Air Cond – Single Fwd Evap (RH) (206L,L1&L3) – (General Arrangement-206L, L1 & L3 Air Cond Sys (Torq-Loc). Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [MDLDL-206H](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107083244720260923124149.0001): Cabin Heater System. Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [23511-02VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124645630220260728184230.0001): Screw Cap Socket Head. Vision Air Services, LLC · PMA PQ2075NM · Replaces 23511-02 · Jul 8, 2026
- [206-011-132-113A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157029258720260618165544.0001): Main Rotor Grip Assembly. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-011-132-113A · May 27, 2026
- [ATBY5V14VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117318159020260527183058.0001): Bearing. Vision Air Services, LLC · PMA PQ2075NM · Replaces C42642-68 · May 11, 2026
- [41001912VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145872229320260501132544.0001): Rod End, Spherical. Vision Air Services, LLC · PMA PQ2075NM · Replaces 41001912 · Apr 15, 2026
- [98020206-5025](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129220331020260325205944.0001): Bell Helicopter 206 NVG Modification Kit. REB Technologies Inc · PMA PQ1018SW · Modification part · Mar 23, 2026
- [109090-000325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198569213920260202232903.0001): INDUSTRIAL SD CARD, 512GB. Appareo Systems LLC · PMA PQ4000CE · Modification part · Jan 15, 2026
- [67574VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168293892820260120135233.0001): Bearing. Vision Air Services, LLC · PMA PQ2075NM · Replaces 67574 · Jan 7, 2026
- [67560VA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137424716420260120135232.0001): Bearing Ball. Vision Air Services, LLC · PMA PQ2075NM · Replaces 67560 · Jan 7, 2026
- [2AA-310-700-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191327412620260107201328.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-310-700-101 · Jan 5, 2026
- [2AA-040-032-105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169845768820260107201329.0001): Duplex Bearing. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-040-032-105 · Jan 5, 2026
- [2AA-040-272-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166278269320260107201327.0001): Seal Assy. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-040-272-101 · Jan 5, 2026
- [2AA-010-443-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161373427620260107201329.0001): Duplex Bearing. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-010-443-001 · Jan 5, 2026
- [2AA-340-206-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155802986620260107201328.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-340-206-101 · Jan 5, 2026
- [2AA-011-111-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135822418020260107201329.0001): Bearing. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-011-111-001 · Jan 5, 2026
- [2AA-340-104-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123478311420260107201328.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 206-340-104-101 · Jan 5, 2026
- [535639AA-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115535228420260107201330.0001): Seal. Able Aerospace Services, Inc. · PMA PQ2487NM · Replaces 535639-10 · Jan 5, 2026
- [RMA-000032-160](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199691214320260225193403.0001): TRACKER CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-220](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196747860220260225193405.0001): MAIN GEARBOX CASE, INTL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-180](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193182969620260225193404.0001): GROUND CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMMD-000116-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192330602920260225193406.0001): BELL 206 TGB TACH BRACKET. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-230](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189845645320260225193405.0001): MAIN ROTOR SWASH-PLATE, INTL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-00032-150](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176505659720260225193403.0001): ETHERNET CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-140](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176414415920260225193403.0001): TAIL ROTOR TACH CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-110](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175930578120260225193402.0001): MAIN ROTOR SWASH-PLATE ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-190](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169897018120260225193404.0001): CABIN VERTICAL ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMMD-000095-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169003899220260225193359.0001): GPS ANTENNA BRACKET. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-90](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168276412620260225193401.0001): MAINGEARBOX FORWARD ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-40](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164889868220260225193400.0001): HANGER BEARING 4 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMED-000080-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163533474020260225193358.0001): KEY FOB. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-210](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158150502720260225193404.0001): MAIN GEARBOX FORWARD, INTL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-130](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156226701220260225193402.0001): MAIN ROTOR TACH CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-250](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151555606020260225193405.0001): MAIN ROTOR TACH, INTL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147874050920260225193401.0001): HANGER BEARING 7 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-20](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143714288420260225193400.0001): HANGER BEARING 2 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-170](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137996134820260225193403.0001): POWER CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-80](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131362320320260225193401.0001): TAIL GEARBOX ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-50](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129849570720260225193400.0001): HANGER BEARING 5 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-60](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127640891220260225193401.0001): HANGER BEARING 6 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126079299920260225193402.0001): MAIN GEARBOX CASE ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116043965120260225193400.0001): HANGER BEARING 3 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-120](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112670640120260225193402.0001): ENGINE GEARBOX ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109659436520260225193359.0001): HANGER BEARING 1 ACCEL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMMD-000139-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109509477720260225193359.0001): EPU LITE ASSEMBLY. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107314285720260225193404.0001): GPS CABLE. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025
- [RMHA-000032-240](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104716139520260225193405.0001): ENGINE GEARBOX,  INTL. Sterling Helicopter · PMA PQ10048NE · Modification part · Dec 22, 2025

All of them: https://openairdocs.org/model/bell-helicopter-textron-canada-206l-3/pma.md

## The same model under other registry codes

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

- [Bell 206L-3](https://openairdocs.org/model/bell-206l-3): 159 registered aircraft, registry code 1182108

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.