# N405SW: 2013 Bell Helicopter Textron Canada 407

- Status: Valid registration
- Airframe: [Bell Helicopter Textron Canada 407](https://openairdocs.org/model/bell-helicopter-textron-canada-407) (registry code 1182154, 8 seats)
- Engine: [Rolls-Royce 250-C47B](https://openairdocs.org/engine/rolls-royce-250-c47b) (registry code 54585)
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (Bell Textron Canada Limited), [TCDS E1GL](https://openairdocs.org/tcds/E1GL) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 54391
- Year built: 2013
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: February 11, 2013
- Certificate issued: September 10, 2024
- Expires: September 30, 2031
- Mode S code: A4C0D9
- Registered owner: [Sw Aviation LLC](https://openairdocs.org/faa-owner/SW%20AVIATION%20LLC)
- Location: [Norman, OK](https://openairdocs.org/faa-place/OK/Norman)
- Owner type: LLC
- Owner's area on the map: 35.2560° N, 97.4668° W: Placed by OpenAirDocs at the center of ZIP code 73069, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=405SW
- Page: https://openairdocs.org/aircraft/N405SW

From the FAA registry file of October 21, 2026. 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 that may apply (OpenAirDocs): 49 in force

### Matched by airframe (Bell Helicopter Textron Canada 407)

- [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

### Matched by engine (Rolls-Royce 250-C47B)

- [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 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 2014-04-07](https://openairdocs.org/ad/2014-04-07) (historical): Rotorcraft Tail Boom and Middle Section · Bell Helicopter Textron Canada 407. Effective Jul 28, 2014
- [AD 2013-12-07](https://openairdocs.org/ad/2013-12-07) (historical): Rotorcraft tailboom · Bell Helicopter Textron Canada 407. Effective Aug 1, 2013
- [AD 2011-15-51](https://openairdocs.org/ad/2011-15-51) (historical): Hydraulic servo actuators · Bell Helicopter Textron Canada 407 and 427. Effective Nov 14, 2011
- [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 2005-03-07](https://openairdocs.org/ad/2005-03-07) (historical): Crosstube assembly · Bell Helicopter Textron Canada 407. Effective Mar 17, 2005
- [AD 2003-05-03](https://openairdocs.org/ad/2003-05-03) (historical): Tailboom · Bell Helicopter Textron Canada 407. Effective Apr 17, 2003
- [AD 2002-23-51](https://openairdocs.org/ad/2002-23-51) (historical): Swashplate drive link cup washers · Bell Helicopter Textron 407
- [AD 2002-06-52](https://openairdocs.org/ad/2002-06-52) (historical): Oil Cooler Blower Bearings · Bell Helicopter Textron 407. Effective May 2, 2002
- [AD 2001-13-51](https://openairdocs.org/ad/2001-13-51) (historical): Driveshafts · Bell Helicopter Textron Canada 206L-4, 407 and 427. Effective Oct 9, 2001
- [AD 2001-01-52](https://openairdocs.org/ad/2001-01-52) (historical): Airspeed · Bell Helicopter Textron 407. Effective Feb 21, 2001
- [AD 2000-20-18](https://openairdocs.org/ad/2000-20-18) (historical): Horizontal Stabilizer Slat · Bell Helicopter Textron 407. Effective Nov 22, 2000
- [AD 2000-06-10](https://openairdocs.org/ad/2000-06-10) (historical): Tail Boom · Bell Helicopter Textron 407. Effective Apr 14, 2000
- [AD 2000-02-12](https://openairdocs.org/ad/2000-02-12) (historical): Engine Oil Cooler Blower Shaft Bearings · Bell Helicopter Textron 407. Effective Mar 3, 2000
- [AD 99-23-18](https://openairdocs.org/ad/99-23-18) (historical): Revised Life Limit · Bell Helicopter Textron Canada 407. Effective Nov 30, 1999
- [AD 99-06-15](https://openairdocs.org/ad/99-06-15) (historical): Tail Rotor Blades · Bell Helicopter Textron 407. Effective Apr 22, 1999
- [AD 96-21-12 PL](https://openairdocs.org/ad/96-21-12-PL) (historical): Placard -- Inflight Engine Shut-downs · Bell Helicopter Textron 407
- [AD 2004-24-09](https://openairdocs.org/ad/2004-24-09) (historical): Fuel nozzle · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 40 more. Effective Jan 5, 2005
- [AD 2003-13-10](https://openairdocs.org/ad/2003-13-10) (historical): Hydromechanical unit (HMU) power lever angle (PLA) · 250-C30R/3, 250-C30R/3M, 250-C47B and 1 more. Effective Jul 15, 2003
- [AD 97-21-09](https://openairdocs.org/ad/97-21-09) (historical): Engine Main Electrical Harness Assembly · 250-C47B. Effective Dec 3, 1997
- [AD 96-24-09](https://openairdocs.org/ad/96-24-09) (historical): Engine Main Electrical Harness Assembly · 250-C47B. Effective Nov 25, 1996

## Information bulletins (advisory) (7 in force)

- [SAIB SW-15-20](https://openairdocs.org/saib/SW-15-20): Air Conditioning System Wiring. Issued Aug 13, 2015
- [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-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008
- [SAIB SW-05-70](https://openairdocs.org/saib/SW-05-70): . Issued Jul 21, 2005
- [SAIB SW-04-92](https://openairdocs.org/saib/SW-04-92): . Issued Sep 30, 2004
- [SAIB NE-06-12R1](https://openairdocs.org/saib/NE-06-12R1): . Issued Jan 13, 2006
- [SAIB SW-10-42](https://openairdocs.org/saib/SW-10-42) (historical): Emergency Float Kits. Issued Aug 5, 2010
- [SAIB NE-06-12](https://openairdocs.org/saib/NE-06-12) (historical): . Issued Dec 2, 2005

## NTSB investigations

None matched to N405SW.

## FAA accident and incident reports

None matched to N405SW.

## Reports on N405SW not matched to an aircraft (4)

They name N405SW, but no registry record covers the event date, or the aircraft registered then was built later.

- [Incident 20070813830629I](https://openairdocs.org/incident/20070813830629I), Aug 13, 2007: Cndair CL6002B19 (N405SW), Winnipeg Man, CN, Minor damage. (-23) Aircraft reportedly was parked at the gate with wheel chocks installed. A sudden gust of wind caused aircraft to jump chocks and contact a tug. Aircraft…
- [Incident 20020323006589I](https://openairdocs.org/incident/20020323006589I), Mar 23, 2002: Cndair CL6002B19 (N405SW), Salt Lake City, UT, Minor damage. (-23) On March 23, 2002, at approximately 1741 MST, skywest (swia) flight #3964, a CL-600-2B19, N405SW, enroute from msp-slc, sustained a left wing tip strike…
- [Incident 19941212045639I](https://openairdocs.org/incident/19941212045639I), Dec 12, 1994: Cndair CL6002B19 (N405SW), Salt Lake City, UT. Flap problem on approach. Had history of flap defects. Replaced entire system. Returned to service.
- [Incident 19941207045629I](https://openairdocs.org/incident/19941207045629I), Dec 7, 1994: Cndair CL6002B19 (N405SW), Salt Lake City, UT. Unable extend flaps for landing. Replaced flap actuators.

## Service difficulty reports (170, newest 50)

As reported by operators and repair stations.

- [SDR SWIA201333804](https://openairdocs.org/sdr/SWIA201333804), Jun 24, 2013: SELECTOR VALVE. FAILED. GEAR DISAGREE WARNING MESSAGE, COMPLIED WITH QRH & RECEIVED 3 DOWN & LOCKED INDICATIONS. HOWEVER, UNABLE TO STOW LANDING GEAR MANUAL RELEASE HANDLES, CYCLING GE
- [SDR SWIA201333770](https://openairdocs.org/sdr/SWIA201333770), Jun 21, 2013: LIGHT. INOPERATIVE. FORWARD EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5482 RELAMPED.
- [SDR SWIA201332930](https://openairdocs.org/sdr/SWIA201332930), Mar 5, 2013: LIGHT. INOPERATIVE. LEFT WING FORWARD EXTERIOR EMERGENCY EXIT LIGHT BURNED OUT. (FLT 5485) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232226](https://openairdocs.org/sdr/SWIA201232226), Nov 21, 2012: LIGHT. INOPERATIVE. NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 6498) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231848](https://openairdocs.org/sdr/SWIA201231848), Sep 26, 2012: WINDOW. CRACKED. FIRST OFFICERS SIDE WINDOW CRACKED. (FLT 4776) REPLACED RIGHT SIDE WINDOW IN REFERENCE TO CRJ 200 MM. P/N: NP-139322-12 S/N OFF: 93046H5242.
- [SDR SWIA201231847](https://openairdocs.org/sdr/SWIA201231847), Sep 21, 2012: WINDSHIELD. DAMAGED. SMOKE IN THE COCKPIT. ISOLATED THE SMOKE TO THE PHENOLIC BLOCK ON THE FIRST OFFICER'S SIDE. (FLT 4762) REPLACED CO-PILOTS WINDSHIELD IN REFERENCE TO CRJ MM. P/N
- [SDR SWIA201231321](https://openairdocs.org/sdr/SWIA201231321), Jul 21, 2012: BATTERY. DISCHARGED. EMERGENCY LIGHTS ARE OUT. (FLT 6299) CHARGED BATTERIES.
- [SDR SWIA201231286](https://openairdocs.org/sdr/SWIA201231286), Jul 17, 2012: SWITCHING UNIT. FAILED. MULTIPLE GEAR INDICATION MESSAGES. (FLT 5492) REPLACED THROTTLE QUADRANT ADJUSTABLE CAM SWITCHING UNIT. PN: FE210-302, SN OFF: FR1008.
- [SDR SWIA201231206](https://openairdocs.org/sdr/SWIA201231206), Jul 4, 2012: SKIN. DAMAGED. LEFT FUSELAGE SKIN AT STATION 411 BETWEEN STR 19 AND 20 LEFT IS DAMAGED. (FLT 4468) REPAIRED PER SRM.
- [SDR SWIA201231128](https://openairdocs.org/sdr/SWIA201231128), Jun 22, 2012: LIGHT. INOPERATIVE. NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4446) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201230875](https://openairdocs.org/sdr/SWIA201230875), Jun 2, 2012: COUNTERBALANCE. OUT OF RIG. MAIN CABIN DOOR IS BINDING WHEN OPENING. (FLT 4623) ADJUSTED UPPER LATCH CAM ROD AND RIGGED DOOR COUNTER BALANCE FORWARD AND AFT IN REFERENCE TO AMM.
- [SDR SWIA201230072](https://openairdocs.org/sdr/SWIA201230072), Mar 15, 2012: RELAY. FAILED. EMERGENCY LIGHTS CAME ON IN FLIGHT, WERE ON WHENEVER LIGHTS WERE ARMED, WENT OFF WHEN SWITCH WAS OFF. (FLT 4665) REPLACED AC ESSENTIAL BUS RELAY IN REF TO AMM. 
- [SDR SWIA201229728](https://openairdocs.org/sdr/SWIA201229728), Feb 16, 2012: ATTACH BRACKET. CRACKED. OUTBOARD SIDE ATTACH BRACKET OF LEFT INBOARD WING LEADING EDGE IS CRACKED. REPLACED OUTBOARD SIDE ATTACH BRACKET AT LEFT WING INBOARD LEADING EDGE.
- [SDR SWIA201229727](https://openairdocs.org/sdr/SWIA201229727), Feb 16, 2012: ANGLE. CRACKED. RIGHT WING UPPER MID LEADING EDGE ANGLE CRACKED. REPLACED RIGHT WING UPPER MID LEADING EDGE ANGLE.
- [SDR SWIA201229726](https://openairdocs.org/sdr/SWIA201229726), Feb 16, 2012: ANGLE. CRACKED. LEFT WING UPPER MID LEADING EDGE ANGLE CRACKED. REPLACED ANGLE AT LEFT WING UPPER MID AREA.
- [SDR SWIA201229158](https://openairdocs.org/sdr/SWIA201229158), Jan 5, 2012: OIL SYSTEM. OVERSERVICED. RETURNED TO THE FIELD WITH LEFT ENGINE HIGH OIL TEMPERATURE. (FLT 6403) INSPECTED LEFT ENGINE OIL LEVEL FOUND TO BE OVERSERVICED, REMOVED 2 QTS OF OIL.
- [SDR SWIA201129114](https://openairdocs.org/sdr/SWIA201129114), Dec 31, 2011: HANDLE. DIRTY. MAIN CABIN DOOR HARD TO OPEN FROM THE EXTERIOR. (FLT 5441) CLEANED AND LUBED EXTERIOR DOOR HANDLE.
- [SDR SWIA201128084](https://openairdocs.org/sdr/SWIA201128084), Sep 29, 2011: BRAKE. LOCKED. NR 2 MLG BRAKE LOCKED UP AND NR 2 MLG TIRE IS FLAT. (FLT 5819) REPLACED BOTH NR 1 AND NR 2 MAIN LANDING GEAR WHEEL ASSEMBLIES AND REPLACED NR 2 BRAKE ASSEMBLY P
- [SDR SWIA201127411](https://openairdocs.org/sdr/SWIA201127411), Aug 28, 2011: SHAFT. DEFECTIVE. MCD IS DIFFICULT TO OPEN. (FLT 5819) REPLACED THE MAIN CABIN DOOR FORWARD COUNTER-BALANCE GUIDE SHAFT.
- [SDR SWIA201126290](https://openairdocs.org/sdr/SWIA201126290), Apr 3, 2011: INTERCOSTAL. CRACKED. FLOOR INTERCOSTAL AT FS 484.0 CRACKED UNDER FLOOR. (C-CHECK) REPLACED FLOOR INTERCOSTAL AT FS 484.0 RIGHT OUTBOARD INTERCOSTAL.
- [SDR SWIA201024760](https://openairdocs.org/sdr/SWIA201024760), Aug 23, 2010: MOUNT. DAMAGED. RIGHT ENGINE FWD YOKE MOUNT UPPER END DAMAGED AND LOWER BUSHING PITTED. (ENGINE CHANGE) REMOVED AND REPLACED.
- [SDR SWIA201024725](https://openairdocs.org/sdr/SWIA201024725), Aug 18, 2010: BUSHING. CORRODED. LEFT ENGINE FORWARD MOUNT LINK CLAMP-UP BUSHING HAS PITTING CORROSION. (ENGINE CHANGE) REPLACED BUSHING.
- [SDR SWIA201024724](https://openairdocs.org/sdr/SWIA201024724), Aug 18, 2010: BUSHING. CORRODED. LEFT ENGINE FORWARD MOUNT LINK HAS PITTING CORROSION ON BUSHINGS. (C-CHECK) REPLACED BUSHINGS.
- [SDR SWIA201024691](https://openairdocs.org/sdr/SWIA201024691), Aug 12, 2010: DOOR. BINDING. MAIN CABIN DOOR WAS DIFFICULT TO OPEN. (FLT 4761) REPOSITIONED AIRCRAFT TO LEVEL GROUND.
- [SDR SWIA201024500](https://openairdocs.org/sdr/SWIA201024500), Jul 3, 2010: ROLLER. OUT OF ADJUST. MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6518) ADJUSTED MAIN DOOR TOP SPIGOT ROLLERS AND ALL LATCH PINS PER AMM.
- [SDR SWIA201024485](https://openairdocs.org/sdr/SWIA201024485), Jun 27, 2010: CAM. OUT OF ADJUST. MAIN CABIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. (FLT 4656) RIGGED LOWER CAM LOCK.
- [SDR SWIA201024382](https://openairdocs.org/sdr/SWIA201024382), Jun 1, 2010: HINGE. WORN. OUTER DOOR HANDLE ON MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6900) REPLACED DOOR HINGE.
- [SDR SWIA201024062](https://openairdocs.org/sdr/SWIA201024062), Apr 18, 2010: FASTENER. BROKEN. WHEN DOING CONTROL CHECKS, THE LEFT ELEVATOR WILL NOT RETURN TO NEUTRAL. (FLT 4458) REPLACED HI-LOK PIN ON PCU/ELEVATOR INTERCONNECT BRACKET.
- [SDR SWIA201023943](https://openairdocs.org/sdr/SWIA201023943), Mar 31, 2010: LIGHT. MALFUNCTIONED. MAIN CABIN DOOR AND SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. (FLT 6311) OPERATIONAL CHECK NORMAL.
- [SDR SWIA201023750](https://openairdocs.org/sdr/SWIA201023750), Feb 26, 2010: HANDLE. OBSTRUCTED. UNABLE TO OPEN MAIN CABIN DOOR FROM OUTSIDE. (FLT 3094) REMOVED DEBRIS AND CLEANED AROUND MAIN CABIN DOOR OUTER HANDLE.
- [SDR SWIA201023475](https://openairdocs.org/sdr/SWIA201023475), Jan 15, 2010: CIRCUIT BREAKER. TRIPPED. FLT 5880 - EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. RESET TRIPPED CIRCUIT BREAKER, OPERATION CHECK NORMAL.
- [SDR SWIA200922700](https://openairdocs.org/sdr/SWIA200922700), Sep 24, 2009: LIGHT. INOPERATIVE. AFT RED ARROW ON EMERGENCY FLOOR STRIP IS NOT ILLUMINATED AT ROWS 9 AND 11. (FLT 5791) REPLACED FLOOR TRACK EMERGENCY LIGHT AT ROW 9 AND 11 IAW AMM 33-51-01.
- [SDR SWIA200922607](https://openairdocs.org/sdr/SWIA200922607), Sep 12, 2009: INVERTER. FAILED. MAIN AND SERVICE DOOR EMERGENCY LIGHTS INOP. (FLT 6723) REPLACED NR 1 INVERTER.
- [SDR SWIA200922562](https://openairdocs.org/sdr/SWIA200922562), Sep 3, 2009: TORQUE SHAFT. OUT OF RIG. MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4435) INSTALLED SHIMS ON INNER HANDLE TORQUE SHAFT.
- [SDR SWIA200922505](https://openairdocs.org/sdr/SWIA200922505), Sep 1, 2009: HANDLE. LACK OF LUBE. MAIN DOOR HARD TO OPEN FROM OUTSIDE. (FLT 4530) LUBED LATCH PINS AND HANDLE.
- [SDR SWIA200922424](https://openairdocs.org/sdr/SWIA200922424), Aug 22, 2009: HANDLE. OUT OF POSITION. MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 6157) FOUND OUTER HANDLE IMPROPERLY STOWED. OPERATIONAL CHECKS NORMAL.
- [SDR SWIA200922219](https://openairdocs.org/sdr/SWIA200922219), Jul 25, 2009: DOOR. BINDING. MAIN DOOR WILL NOT OPEN FROM OUTSIDE. (FLT 5800) OPERATIONAL CHECK NORMAL.
- [SDR SWIA200921648](https://openairdocs.org/sdr/SWIA200921648), May 12, 2009: LATCH. OUT OF RIG. FLT 6015 - MCD OUTER HANDLE WOULD NOT OPEN. RIGGED LATCH CAM ASSEMBLY.
- [SDR SWIA200921586](https://openairdocs.org/sdr/SWIA200921586), May 2, 2009: DOOR. STIFF. FLT 4794 - MAIN CABIN DOOR VERY DIFFICULT TO OPEN. DOOR OPERATES NORMALLY.
- [SDR SWIA200921323](https://openairdocs.org/sdr/SWIA200921323), Jan 30, 2009: SKIN. CORRODED. C-CHECK, INNER SKIN OF PASSENGER DOOR CORRODED. REPAIRED PER REO.
- [SDR SWIA200921322](https://openairdocs.org/sdr/SWIA200921322), Jan 30, 2009: SEAT TRACK. CORRODED. C-CHECKM, SIDEWALL SEAT TRACK CORRODED. REPLACED TRACK SECTIONS PER SRM.
- [SDR SWIA200921321](https://openairdocs.org/sdr/SWIA200921321), Jan 30, 2009: WINDOW POST. CRACKED. C-CHECK, RIGHT WINDSHIELD SIDE POST LOWER OUTBOARD CLIPS CRACKED. REPLACED PER SRM.
- [SDR SWIA200921320](https://openairdocs.org/sdr/SWIA200921320), Jan 30, 2009: PRESSURE BLKHD. CRACKED. C-CHECK, AFT SIDE OF PRESSURE BULKHEAD HAS NUMEROUS CRACKS. REPAIRED PER REO.
- [SDR SWIA200921319](https://openairdocs.org/sdr/SWIA200921319), Jan 30, 2009: BULKHEAD. CRACKED. C-CHECK, FS 621 AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.
- [SDR SWIA200921318](https://openairdocs.org/sdr/SWIA200921318), Jan 30, 2009: DOOR FRAME. CRACKED. C-CHECK, PASSENGER DOOR FRAME AT FS 338 CRACKED. REPAIRED PER REO.
- [SDR SWIA200921317](https://openairdocs.org/sdr/SWIA200921317), Jan 30, 2009: FLOORBEAM. CRACKED. C-CHECK, FS 280 FLOOR SUPPORT BEAM CRACKED. REPAIRED PER REO.
- [SDR SWIA200921316](https://openairdocs.org/sdr/SWIA200921316), Jan 30, 2009: FLOORBEAM. CRACKED. C-CHECK, FS 280 FORWARD FLOOR SUPPORT AT LBL9 AND RBL9 CRACKED. REPAIRED PER SRM.
- [SDR SWIA200820639](https://openairdocs.org/sdr/SWIA200820639), Dec 11, 2008: SKIN. DENTED. FLT 1010 - TWO DENTS ON RIGHT LEADING EDGE AT WS 201.0 EXCEED LIMITS OF SRM. REPLACED LEADING EDGE SKIN PER SRM.
- [SDR SWIA200819949](https://openairdocs.org/sdr/SWIA200819949), Aug 7, 2008: ACCESS PANEL. CORRODED. PASSENGER DOOR SHOWS SIGNS OF CORROSION AROUND UPPER ACCESS PANELS. REPAIRED PAX DOOR PER REO 601R-52-11-1520. 
- [SDR SWIA200819627](https://openairdocs.org/sdr/SWIA200819627), May 11, 2008: SELECTOR VALVE. MALFUNCTIONED. FLT 6377 - WHEN EXTENDING GEAR ON APPROACH, RECEIVED A "GEAR DISAGREE" MESSAGE. MANUALLY EXTENDED THE GEAR. REPLACED MAIN GEAR SELECTOR VALVE IAW 32-32-10.

All 170: https://openairdocs.org/aircraft/N405SW/reports.md

## Related

- Other Bell Helicopter Textron Canada 407 aircraft: https://openairdocs.org/model/bell-helicopter-textron-canada-407/aircraft.md
- STCs for the Bell Helicopter Textron Canada 407: https://openairdocs.org/model/bell-helicopter-textron-canada-407/stcs.md
- The Rolls-Royce 250-C47B engine: https://openairdocs.org/engine/rolls-royce-250-c47b.md

---
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.