# N433JS: 2015 Bell Helicopter Textron Canada 407

- Status: Valid registration
- Airframe: Bell Helicopter Textron Canada 407 (registry code 1182154, TCDS H2SW (OpenAirDocs match))
- Engine: Rolls-Royce 250-C47B (registry code 54585, TCDS E1GL (OpenAirDocs match))
- Serial number: 54613
- Year built: 2015
- Type: Rotorcraft
- Airworthiness: Standard, normal
- Airworthiness date: December 3, 2015
- Certificate issued: January 5, 2016
- Expires: January 31, 2029
- Mode S code: A52F1C
- Registered owner: Scott J B
- Location: Boise, ID
- Owner's area on the map: 43.5548° N, 116.2214° W: Placed by OpenAirDocs at the center of ZIP code 83705, within about 2 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N433JS

ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs matched by airframe (Bell Helicopter Textron Canada 407) (OpenAirDocs)

- [AD 2026-14-07](https://openairdocs.org/ad/2026-14-07): Main rotor control · Bell Textron Canada 407. Effective Aug 21, 2026
- [AD 2026-10-04](https://openairdocs.org/ad/2026-10-04): Electrical connectors · Bell Textron Canada 407. Effective Jun 25, 2026
- [AD 2025-13-01](https://openairdocs.org/ad/2025-13-01): Main Rotor Blades · Bell Textron Canada 407 and 427. Effective Jul 8, 2025
- [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 2024-10-12](https://openairdocs.org/ad/2024-10-12): Fuel system wiring · Bell Textron Canada 407. Effective Aug 22, 2024
- [AD 2023-17-51](https://openairdocs.org/ad/2023-17-51): Tail Rotor Blades · Bell Textron Canada 407. Effective Sep 21, 2023
- [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 2022-27-08](https://openairdocs.org/ad/2022-27-08): Rotorcraft Tail Boom · Bell Textron Canada 407. Effective Jan 12, 2023
- [AD 2022-23-02](https://openairdocs.org/ad/2022-23-02): Fuselage Structure · Bell Textron Canada 407. Effective Jan 3, 2023
- [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 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 2018-10-06](https://openairdocs.org/ad/2018-10-06): Tail Rotor Drive Shaft · Bell Helicopter Textron Canada 407. Effective Jun 25, 2018
- [AD 2015-17-02](https://openairdocs.org/ad/2015-17-02): Main Rotor Drive System · Bell Helicopter Textron Canada 206L-4, 407, 427 and 1 more. Effective Sep 24, 2015
- [AD 2015-05-04](https://openairdocs.org/ad/2015-05-04): Fuselage Main, Longeron/Stringer · Bell Helicopter Textron Canada 407. Effective Apr 20, 2015
- [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 2013-22-01](https://openairdocs.org/ad/2013-22-01): Main Rotor Drive System · Bell Helicopter Textron Canada 206L-4 and 407. Effective Dec 5, 2013
- [AD 2013-20-05](https://openairdocs.org/ad/2013-20-05): Turbine Section · Bell Helicopter Textron Canada 407. Effective Dec 5, 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 2012-18-09](https://openairdocs.org/ad/2012-18-09): Rotorcraft tailboom · Bell Helicopter Textron Canada 407. Effective Oct 22, 2012
- [AD 2012-14-07](https://openairdocs.org/ad/2012-14-07): Rotorcraft Servo System · Bell Helicopter Textron Canada 407 and 427. Effective Aug 3, 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 2009-25-08](https://openairdocs.org/ad/2009-25-08): Hydraulic pump driveshaft assembly · Bell Helicopter Textron Canada 407 and 427. Effective Dec 28, 2009
- [AD 2009-22-11](https://openairdocs.org/ad/2009-22-11): Swashplate link assembly bearing · Bell Helicopter Textron Canada 407 and 427. Effective Nov 16, 2009
- [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 2004-10-07](https://openairdocs.org/ad/2004-10-07): Oil cooler blower bearings · Bell Helicopter Textron Canada 407. Effective Jun 4, 2004
- [AD 2003-05-11](https://openairdocs.org/ad/2003-05-11): Swashplate outer ring · Bell Helicopter Textron Canada 407. Effective Apr 2, 2003
- [AD 2003-02-06](https://openairdocs.org/ad/2003-02-06): Tailboom gearbox support castings · Bell Helicopter Textron Canada 407. Effective Feb 10, 2003
- [AD 2002-22-10](https://openairdocs.org/ad/2002-22-10): Horizontal stabilizer slat (slat) · Bell Helicopter Textron Canada 407. Effective Nov 21, 2002
- [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 2002-17-03](https://openairdocs.org/ad/2002-17-03): Fuel Filler Cap · Bell Helicopter Textron Canada 407. Effective Sep 20, 2002
- [AD 2002-11-09](https://openairdocs.org/ad/2002-11-09): Forward Bearing Hanger Bracket · Bell Helicopter Textron Canada 407. Effective Jul 16, 2002
- [AD 2001-13-02](https://openairdocs.org/ad/2001-13-02): Cockpit Warning Horns · Bell Helicopter Textron Canada 407. Effective Aug 1, 2001
- [AD 2001-01-52 R1](https://openairdocs.org/ad/2001-01-52-R1): Tail Rotor Blades · Bell Helicopter Textron Canada 407. Effective Jul 25, 2001
- [AD 2000-14-16](https://openairdocs.org/ad/2000-14-16): Tail Rotor System · Bell Helicopter Textron Canada 407. Effective Aug 29, 2000
- [AD 2000-04-25](https://openairdocs.org/ad/2000-04-25): Door Latch Assembly · Bell Helicopter Textron Canada 407. Effective Apr 12, 2000
- [AD 2000-04-20](https://openairdocs.org/ad/2000-04-20): Hydraulic Relief Valve · Bell Helicopter Textron Canada 407. Effective Apr 5, 2000
- [AD 99-22-13](https://openairdocs.org/ad/99-22-13): Fin Assembly For Reduced Skin Thickness Inspection · Bell Helicopter Textron Canada 407. Effective Dec 2, 1999
- [AD 98-19-13](https://openairdocs.org/ad/98-19-13): Driveshaft · Bell Helicopter Textron Canada 407. Effective Jan 27, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-12-22](https://openairdocs.org/ad/98-12-22): Tail Rotor Drive System Bearing Supports · Bell Helicopter Textron Canada 407. Effective Jul 15, 1998
- [AD 97-24-17](https://openairdocs.org/ad/97-24-17): Tail Rotor Drive Coupling Disc Pack · Bell Helicopter Textron Canada 407. Effective Apr 16, 1998

Historical (superseded or no longer in force): AD 2021-23-13, AD 2014-04-07, AD 2013-12-07, AD 2011-15-51, AD 2009-08-03, AD 2009-07-51, AD 2007-19-52, AD 2005-03-07, AD 2003-05-03, AD 2002-23-51, AD 2002-06-52, AD 2001-13-51, AD 2001-01-52, AD 2000-20-18, AD 2000-06-10, AD 2000-02-12, AD 99-23-18, AD 99-06-15, AD 96-21-12 PL

## ADs matched by engine (Rolls-Royce 250-C47B) (OpenAirDocs)

- [AD 2006-20-07](https://openairdocs.org/ad/2006-20-07): Adds an additional life limit for third- and fourth-stage turbine wheels · Rolls-Royce 250-C30, 250-C30G, 250-C30G/2 and 11 more. Effective Nov 2, 2006
- [AD 2006-16-04](https://openairdocs.org/ad/2006-16-04): Inspection of the fuel nozzle screen · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 43 more. Effective Sep 7, 2006
- [AD 2004-24-04](https://openairdocs.org/ad/2004-24-04): Hydromechanical unit (HMU) Power Lever Angle (PLA) potentiometer · Rolls-Royce 250-C30R/3, 250-C30R/3M, 250-C47B and 1 more. Effective Jan 3, 2005
- [AD 98-10-03](https://openairdocs.org/ad/98-10-03): Hydromechanical Unit · Rolls-Royce 250-C47B. Effective May 26, 1998
- [AD 82-24-05](https://openairdocs.org/ad/82-24-05): Control Assembly and Power Turbine Governor Assembly · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 43 more. Effective Nov 26, 1982

Historical (superseded or no longer in force): AD 2004-24-09, AD 2003-13-10, AD 97-21-09, AD 96-24-09

## Information bulletins (advisory)

- [SAIB SW-15-20](https://openairdocs.org/saib/SW-15-20): Air Conditioning System Wiring
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System
- [SAIB SW-10-42R1](https://openairdocs.org/saib/SW-10-42R1): Emergency Float Kits
- [SAIB SW-10-42](https://openairdocs.org/saib/SW-10-42): Emergency Float Kits
- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits)
- [SAIB SW-05-70](https://openairdocs.org/saib/SW-05-70): 
- [SAIB SW-04-92](https://openairdocs.org/saib/SW-04-92): 
- [SAIB NE-06-12R1](https://openairdocs.org/saib/NE-06-12R1): 
- [SAIB NE-06-12](https://openairdocs.org/saib/NE-06-12): 

## Service difficulty reports (59)

- [SDR VNAA0311003](https://openairdocs.org/sdr/VNAA0311003), Nov 11, 2003: PSEU. DURING FLIGHT, THE CREW FELT A VIBRATION AND RETURNED TO YUL.  MAINTENANCE INSPECTED AND FOUND THE FORWARD NOSE LANDING GEAR DOOR LATCHED OPEN.  MAINTENANCE THE
- [SDR VNAA0310022](https://openairdocs.org/sdr/VNAA0310022), Oct 29, 2003: CONTROL PANEL. SMOKE IN AIRCRAFT FROM AUTOPILOT CONTROL PANEL.  SMOKE CLEARED AFTER AP/YD TURNED OFF.  MAINTENANCE INSPECTED AND REPLACED THE AP CONTROL PANEL IN ACCORDANCE WI
- [SDR VNAA0305011](https://openairdocs.org/sdr/VNAA0305011), May 17, 2003: BATTERY. THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROWS 7 - 9 WERE NOT ILLUMINATING.  MAINTENANCE INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY IN ACCORD
- [SDR VNAA0305006](https://openairdocs.org/sdr/VNAA0305006), May 11, 2003: CONNECTOR. DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL MESSAGE AND ABORTED TAKEOFF.  MAINTENANCE INSPECTED AND CLEANED THE CANNON PLUG ON THE IB
- [SDR VNAA0304024](https://openairdocs.org/sdr/VNAA0304024), Apr 27, 2003: BATTERY. THE CREW REPORTED THAT THE LAST ROW OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING.  THE AIRCRAFT WAS THEN FERRIED TO PIT.  MAINTENANCE INSPECTED AND REPLACED
- [SDR VNAA0304001](https://openairdocs.org/sdr/VNAA0304001), Apr 4, 2003: ACTUATOR. EN ROUTE, THE CREW RECEIVED A RIGHT HAND FUEL SHUTOFF VALVE ACTUATOR CLOSED CAS MESSAGE AND RETURNED TO PIT.  MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND 
- [SDR VNAA0303033](https://openairdocs.org/sdr/VNAA0303033), Mar 30, 2003: DAU. DURING FLIGHT CONTROL CHECK THE ELEVATOR CONTROLS BECAME STUCK. MAINTENANCE INSPECTED THE ELEVATOR CONTROL SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 
- [SDR VNAA0303009](https://openairdocs.org/sdr/VNAA0303009), Mar 7, 2003: PROXIMITY SENSOR. EN ROUTE, THE EMERGENCY DOOR WARNING LIGHT WAS DISPLAYED.  THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED TO RIC.  THE AIRCRAFT WAS THEN FERRIED TO
- [SDR VNAA0302024](https://openairdocs.org/sdr/VNAA0302024), Feb 26, 2003: INDICATOR. AFTER THE CREW LOWERED THE LANDING GEAR, THE CREW RECEIVED GREEN DOWN AND LOCKED LIGHTS FOR THE MAIN GEAR BUT RED FOR THE NOSE GEAR.  THE CAPTAIN CYCLED THE GEA
- [SDR VNAA0302013](https://openairdocs.org/sdr/VNAA0302013), Feb 16, 2003: BRUSH BLOCK. DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND PROP DE-ICE FAIL CAS MESSAGE AND ABORTED TAKEOFF.  MAINTENANCE INSPECTED, CLEANED, AND REPOSITIONED THE RT BRUSH 

## Reports on N433JS not matched to an aircraft (1)

They name N433JS, but no registry record covers the event date, or the aircraft registered then was built later.

- [Incident 20031029027549I](https://openairdocs.org/incident/20031029027549I), Oct 29, 2003: Dorner DO328100 (N433JS), Pittsburgh, PA. (-23) Flight 2473 was climbing through 6000 feet from Pittsburgh international airport. The crew noticed smoke coming from the GP-300 auto-pilot. ATC was…

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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.