# Bell Helicopter Textron Canada 430

- Type: Aircraft model (FAA registry)
- Registry code: 1182151
- Manufacturer (registry): BELL HELICOPTER TEXTRON CANADA
- Model: 430
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 2 · Turbo-shaft
- Seats: 10
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS H9SW](https://openairdocs.org/tcds/H9SW) (OpenAirDocs)
- Holder: Bell Textron Canada Limited
- Registered aircraft: 3
- Page: https://openairdocs.org/model/bell-helicopter-textron-canada-430

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 2026-13-12](https://openairdocs.org/ad/2026-13-12): Main rotor head · Bell Textron Canada 430. Effective Aug 11, 2026
- [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 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 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 2016-21-01](https://openairdocs.org/ad/2016-21-01): Main Rotor Head · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Nov 18, 2016
- [AD 2016-08-17](https://openairdocs.org/ad/2016-08-17): Rotorcraft Servo System · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective May 31, 2016
- [AD 2015-13-11](https://openairdocs.org/ad/2015-13-11): Tail Rotor Control · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Aug 11, 2015
- [AD 2013-20-03](https://openairdocs.org/ad/2013-20-03): Turbine Section · Bell Helicopter Textron, A Division of Textron Canada 430. 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 2013-06-51](https://openairdocs.org/ad/2013-06-51): Equipment/Furnishings · Agusta A109, A109A, A109A II and 43 more. Effective Jul 15, 2013
- [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 2010-10-12](https://openairdocs.org/ad/2010-10-12): Blades · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Jul 16, 2010
- [AD 2008-19-02](https://openairdocs.org/ad/2008-19-02): Main rotor hydraulic actuator support (support) · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Oct 16, 2008
- [AD 2008-15-04](https://openairdocs.org/ad/2008-15-04): Tail rotor pitch · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Sep 3, 2008
- [AD 2008-14-01](https://openairdocs.org/ad/2008-14-01): Fuel valve switch · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Aug 14, 2008
- [AD 2007-26-10](https://openairdocs.org/ad/2007-26-10): Prevent fatigue failure of the bolt and subsequent loss of control of the helicopter. · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Feb 6, 2008
- [AD 2006-13-14](https://openairdocs.org/ad/2006-13-14): Tail rotor counterweight bellcrank (bellcrank) · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Jul 11, 2006
- [AD 2002-20-02](https://openairdocs.org/ad/2002-20-02): Right-hand upper fuel enclosure area · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Nov 7, 2002
- [AD 2002-01-07](https://openairdocs.org/ad/2002-01-07): Electrical Power Distribution System · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Feb 21, 2002
- [AD 2001-05-09](https://openairdocs.org/ad/2001-05-09): Electrical System · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Apr 24, 2001
- [AD 2001-01-51](https://openairdocs.org/ad/2001-01-51): Main Rotor Hydraulic Actuator Support · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Mar 2, 2001
- [AD 2000-22-13](https://openairdocs.org/ad/2000-22-13): Fuel Quantity Indicating System · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Dec 12, 2000
- [AD 2000-16-06](https://openairdocs.org/ad/2000-16-06): Arm Clamp Screws · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Sep 20, 2000
- [AD 2000-16-04](https://openairdocs.org/ad/2000-16-04): Main Rotor Adapter Assembly Inspection · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Sep 19, 2000
- [AD 99-23-03](https://openairdocs.org/ad/99-23-03): Torque Of Vertical Fin Attachment Bolts Inspection · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Nov 19, 1999
- [AD 98-24-31](https://openairdocs.org/ad/98-24-31): Forward Fairing Assembly · Bell Helicopter Textron, A Division of Textron Canada 430. Effective Feb 3, 1999

Historical (superseded or no longer in force):

- [AD 2025-09-03](https://openairdocs.org/ad/2025-09-03) (historical): Main rotor head · Bell Textron Canada 430. Effective May 13, 2025
- [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 2021-24-09](https://openairdocs.org/ad/2021-24-09) (historical): Main Rotor Head · Bell Textron Canada 430. Effective Dec 7, 2021
- [AD 2010-19-51](https://openairdocs.org/ad/2010-19-51) (historical): Corrosion or a nonconforming piston rod · Bell Helicopter Textron, A Division of Textron Canada 222, 222B, 222U and 2 more. Effective Dec 9, 2010
- [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 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 2005-04-09](https://openairdocs.org/ad/2005-04-09) (historical): Tail rotor blades · 222, 222B, 222U and 2 more. Effective Mar 4, 2005
- [AD 2004-26-11](https://openairdocs.org/ad/2004-26-11) (historical): Tail Rotor Blades · 222, 222B, 222U and 2 more. Effective Jan 18, 2005
- [AD 97-15-16](https://openairdocs.org/ad/97-15-16) (historical): Main Rotor Adapter Assemblies · 430. Effective Oct 24, 1997

## Information bulletins (advisory) (1)

- [SAIB SW-03-32](https://openairdocs.org/saib/SW-03-32): . Issued Mar 20, 2003

## Registered aircraft (3)

- [N430VR](https://openairdocs.org/aircraft/N430VR): [Aerotrust Services Corp](https://openairdocs.org/faa-owner/AEROTRUST%20SERVICES%20CORP), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 49002
- [N431LL](https://openairdocs.org/aircraft/N431LL): [Hm Aviation Holdings LLC](https://openairdocs.org/faa-owner/HM%20AVIATION%20HOLDINGS%20LLC), [Fort Pierce, FL](https://openairdocs.org/faa-place/FL/Fort%20Pierce), S/N 49128
- [N991W](https://openairdocs.org/aircraft/N991W): [Tailwinds LLC](https://openairdocs.org/faa-owner/TAILWINDS%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 2007, S/N 49122

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (392, newest 50)

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

- [SDR QMLA2019092619076](https://openairdocs.org/sdr/QMLA2019092619076), Sep 26, 2019: FILTER. ABNORMAL. DURING CLIMB OUT, PILOT TURNED ON AIR CONDITIONING SYSTEM AND CABIN FILLED WITH SMOKE. PILOT IMMEDIATELY RETURNED BACK TO BASE AND MAINTENANCE WAS ON SITE TO IN
- [SDR K2DA2019090600000](https://openairdocs.org/sdr/K2DA2019090600000), Jul 24, 2019: BLADE. DEBONDED. UPON A DAILY / POST FLIGHT INSPECTION THE A&P MECHANICS DISCOVERED THE TAIL ROTOR BLADE DEBONDED AT THE BLADE ROOT. THE TAIL ROTOR BLADE HAD 22.7 HOURS TIME SIN
- [SDR K2DA201811030001](https://openairdocs.org/sdr/K2DA201811030001), Nov 3, 2018: BLADE. DEBONDED. WITH AUTOPILOT ENGAGED AND A COMMANDED CLIMB TO 1500 FT MSL IN PROGRESS, THE PIC EXPERIENCED A LOUD THUMP, IMMEDIATELY FOLLOWED BY A MEDIUM-TO-HIGH FREQUENCY VI
- [SDR QMLA2018101118110](https://openairdocs.org/sdr/QMLA2018101118110), Oct 10, 2018: MOUNT. CRACKED. DURING PREFLIGHT INSPECTION, FOUND RIGHT HAND TRANSMISSION MOUNT ASSEMBLY P/N 230-031-619-101 CRACKED AT THE EAR FOR THE LATERAL ISOLATION MOUNT ATTACH POINT.
- [SDR K2DA2020012220](https://openairdocs.org/sdr/K2DA2020012220), Oct 3, 2018: BLADE. DAMAGED.  AT 1104 HST, WAS AT APPROXIMATELY N19.54`02" W156.06`58" TRANSITIONING THROUGH PHKO CLASS D AIRSPACE AT 1350`MSL AND 125 KIAS ON A HEADING OF 165 DEGREES, EN R
- [SDR 2PJA20180717001](https://openairdocs.org/sdr/2PJA20180717001), Jul 17, 2018: TRANSDUCER. FAILED. ON TAKEOFF, DURING CLIMB NR 2 HYDRAULIC PRESSURE REDUCED TO 0 PSI. PAGE 2 CAUTION WAS ILLUMINATED. AIRCRAFT DIVERTED TO KMTN. MAINTENANCE REMOVED AND REPLACED T
- [SDR Q6HA2016092900001](https://openairdocs.org/sdr/Q6HA2016092900001), Sep 27, 2016: WIRE. BROKEN. WITH LANDING GEAR SELECTED DOWN THE LANDING GEAR DOES NOT EXTEND INTERMITTENTLY. WARNING HORN DOES SOUND WITH GEAR HANDLE DOWN AND GEAR UP. WIRE G11A22 FOUND BR
- [SDR QMLA201601316010](https://openairdocs.org/sdr/QMLA201601316010), Feb 13, 2016: ENGINE. MAKING METAL. ENGINE REMOVAL DUE TO CHIP EVENTS IN SUMP CHIP DETECTOR.
- [SDR QMLA2015092215086](https://openairdocs.org/sdr/QMLA2015092215086), Sep 22, 2015: SUPPORT. CRACKED. DURING ZONE 10 INSPECTION FOUND CRACK IN TAIL BOOM AT SUPPORT ASSEMBLY FOR HORIZONTAL STABILIZER.
- [SDR CA150827010](https://openairdocs.org/sdr/CA150827010), Aug 20, 2015: SHEAR RESTRAINT. DEBONDED. (CAN) ACFT EXPERIENCE HIGH LATERAL VIBRATION IN FLIGHT. ACFT RETURNED TO BASE AND VISUAL INSPECTION REVEALED ELASTOMERIC DEBONDED ON SHEAR RESTRAINT.
- [SDR CA150616001](https://openairdocs.org/sdr/CA150616001), Jun 4, 2015: BEARING SUPPORT. CRACKED. (CAN) THE FOLLOWING HAS BEEN REPORTED. POST A SEAL CHANGE ON THE ACFT, WHEN ROTATING THE ROTOR, THE ENGINEER HEARD A UNUSUAL SOUND IN THE TAIL BOOM AREA. AFTER 
- [SDR CA150505001](https://openairdocs.org/sdr/CA150505001), Apr 26, 2015: SUN GEAR. FAULTY. (CAN) FINDINGS BY STEPS OF OCCURRENCE: A CRACK SOUND DURING HOVER HEARD BY EVERYONE INCLUDING PASSENGERS. BOTH ENGINES NP POWER TURBINE RPM REACHED TO PERCENT 1
- [SDR CA150429014](https://openairdocs.org/sdr/CA150429014), Apr 26, 2015: ENGINE. MALFUNCTIONED. (CAN) ACFT REPORTED TO HAVE SUFFERED A HARD LANDING FOLLOWING A PROBLEM WITH THE NR 1 ENGINE. A/C SKIDS ARE SPLAYED.
- [SDR CA150421007](https://openairdocs.org/sdr/CA150421007), Apr 14, 2015: NUT. DAMAGED. (CAN) TWO ANCHOR NUTS WERE FOUND BROKEN, CRACKED AND MISSING THE RETENTION SPRING.
- [SDR QMLA2015021215010](https://openairdocs.org/sdr/QMLA2015021215010), Feb 12, 2015: STRIP. CRACKED. DURING BLADE REMOVAL, FOR 100HR YOKE INSPECTION, FOUND CRACKS IN ABRASION STRIP ON LE OF BLADE SN A-2180. DETERMINED CRACK IS OUT OF LIMITS IAW THE MM.
- [SDR CA141114012](https://openairdocs.org/sdr/CA141114012), Oct 13, 2014: YOKE. DELAMINATED. (CAN) MAIN ROTOR YOKE ASSY HAS DELAMINATION IN ONE SIDE, 12" LONG, AND 3" WIDE, CENTERED ON THE CENTERLINE, 6" IN EACH DIRECTION. CONFIRMED BY TAP TEST AND BY E
- [SDR Q2HA2014092500001](https://openairdocs.org/sdr/Q2HA2014092500001), Aug 14, 2014: ACTUATOR. MALFUNCTIONED. INCREASED COLLECTIVE FORCES WERE REQUIRED TO CONTROL AIRCRAFT. AN INSPECTION OF THE ENTIRE FLIGHT CONTROL SYS WAS PERFORMED WITH NO ANOMALIES. IT WASN`T UNTIL T
- [SDR Q2HA2014090500001](https://openairdocs.org/sdr/Q2HA2014090500001), Aug 14, 2014: ACTUATOR. MALFUNCTIONED. INCREASED COLLECTIVE FORCES WERE REQUIRED TO CONTROL AIRCRAFT. AN INSPECTION OF THE ENTIRE FLIGHT CONTROL SYSTEM WAS PERFORMED WITH NO ANOMALIES. IT WASN`T UNTI
- [SDR QMLA2014081214101](https://openairdocs.org/sdr/QMLA2014081214101), Aug 12, 2014: TRANSMISSION. MAKING METAL. DURING ZONE INSPECTION AT ACTT 6722+54 IT WAS NOTED OF METAL PARTICLES ON COLLECTOR GEAR CHIP DETECTOR. AT ACTT 6729+01 THE TRANSMISSION SUMP CHIP LIGHT ILLUMIN
- [SDR QMLA2014061614074](https://openairdocs.org/sdr/QMLA2014061614074), Jun 16, 2014: YOKE. CRACKED. UPON INITIAL INSPECTION FOUND FOUR CRACKS IN MAIN ROTOR YOKE LOCATED BETWEEN STATION 26 & 31. CRACKS ARE 2 TO 4.5 INCHES IN LENGTH. AFTER REMOVING SEALANT FROM 
- [SDR QMLA2014050514049](https://openairdocs.org/sdr/QMLA2014050514049), May 5, 2014: YOKE. CRACKED. WHILE PERFORMING SCHEDULED 600 HR RECURRING INSPECTION IAW ASB 430-12-48 & BHT-430-MM-2 SECTION 4.1 ON ACSN 49120, DISCOVERED A TOTAL OF 5 CRACKS LESS THAN 3 IN
- [SDR CA131121001](https://openairdocs.org/sdr/CA131121001), Nov 14, 2013: ENGINE. FAILED. (CAN) DURING AN OFFSHORE FLIGHT, THE NR 1 ENGINE EXPERIENCED A SUMP CHIP LIGHT, THEN A LOUD BANG AND LOSS OF OIL PRESSURE. ENGINE WAS SECURED AND THE ACFT FLOWN
- [SDR QMLA2013110613159](https://openairdocs.org/sdr/QMLA2013110613159), Nov 6, 2013: YOKE. CRACKED. WHILE PERFORMING 150 HR INSPECTION OF MAIN ROTOR YOKE, FOUND SIX NEW CRACKS SINCE LAST INSPECTION. SMALLEST CRACK WAS 0.5 AND LONGEST CRACK 3.375. FOUR ON TOP O
- [SDR QMLA2013090413126](https://openairdocs.org/sdr/QMLA2013090413126), Sep 4, 2013: STUD. BROKEN. STUD HAD SHEARED OFF OF THE TAIL ROTOR GEARBOX MOUNTING FLANGE AT ONE O`CLOCK POSITION. NOTICED POSITIONS THREE, FIVE AND ELEVEN O`CLOCK STUDS WERE LOOSE AS WEL
- [SDR AC2A20130709001](https://openairdocs.org/sdr/AC2A20130709001), Jul 3, 2013: LINE. FAILED. WHILE IN A HOVER, DURING A TRACK AND BALANCE FLIGHT THE NR 1 HYD SYSTEM FAILED. INDICATED BY A MASTER CAUTION LIGHT AND LOSS OF NR 1 SYSTEM HYD PSI AND THE PEDA
- [SDR CA130618008](https://openairdocs.org/sdr/CA130618008), Jun 13, 2013: CONTROL TUBE. CRACKED. (CAN) DURING A ROUTINE ANNUAL INSPECTION, WHILE INSPECTING THE TAIL ROTOR FLIGHT CONTROLS IN THE BELLY OF THE ACFT, SOME CHAFING WAS NOTED ON CONTROL TUBE, PN 4
- [SDR CA130430014](https://openairdocs.org/sdr/CA130430014), Apr 24, 2013: HOSE. DAMAGED. (CAN) ACFT WAS ON APPROACH TO FIELD AND PILOT ATTEMPTED TO EXTEND RETRACTABLE LANDING GEAR AND DID NOT GET GREEN ADVISORY LIGHT FOR LT MLG. AFTER 5 ATTEMPTS WIT
- [SDR CA130325016](https://openairdocs.org/sdr/CA130325016), Mar 24, 2013: CONTROL TUBE. BROKEN. (CAN) PILOT LOST THE TAIL ROTOR CONTROL DURING FLIGHT. ROD END BROKEN.
- [SDR QMLA2013012713014](https://openairdocs.org/sdr/QMLA2013012713014), Jan 27, 2013: SUPPORT. CRACKED. DURING THE BALANCING PROCEDURES OF THE MAIN DRIVE SHAFT AND THE FAN SHAFT ON THE NR 1 ENGINE. TWO CRACKS WERE NOTICED ON THE OIL COOLER BLOWER MOUNTING SUPPORT 
- [SDR Q2HA20121109001](https://openairdocs.org/sdr/Q2HA20121109001), Oct 27, 2012: FITTING. LOOSE. ON OCTOBER 26, 2012 THE NR 1 ENGINE FUEL NOZZLE WAS REMOVED AND RESHIMMED FOR AN INTERMITTENT STARTING PROBLEM. THE MAINTENANCE ACTION WAS COMPLETED AND SIGNED 
- [SDR QMLA2012050912076](https://openairdocs.org/sdr/QMLA2012050912076), May 9, 2012: ENGINE. MAKING METAL. NR 1 ENGINE SCAVENGE CHIP LIGHT ILLUMINATED DURING START UP. REMOVED SCAVENGE CHIP DETECTOR AND VISUALLY INSPECTED. FOUND MASS QUANTITIES OF METAL ON THE CHIP D
- [SDR QMLA2012021412024](https://openairdocs.org/sdr/QMLA2012021412024), Feb 14, 2012: STATIC PORT. SHORTED. PILOT REPORTED ELECTRICAL FUMES IN COCKPIT. FOUND STATIC PORT SHORTED
- [SDR QMLD201202090961](https://openairdocs.org/sdr/QMLD201202090961), Feb 8, 2012: GEAR. SPALLED. THE FACE OF THE GEAR TOOTH IS WORN BEYOND LIMITS DUE TO SPALLING. NOTE: MFG DOES NOT COUNT CYCLES BUT PUT 1 IN THE TOTAL CYCLES SO THE SDR SYS WOULD TAKE IT.
- [SDR QMLA2012012512015](https://openairdocs.org/sdr/QMLA2012012512015), Jan 25, 2012: YOKE. CRACKED. DURING 5000 HR INSPECTION, FOUND 2 CRACKS ON 1 OF THE YOKES.
- [SDR CA061023003](https://openairdocs.org/sdr/CA061023003), Oct 20, 2011: CONTROL TUBE. SCRATCHED. (CAN) CONTROL TUBE, PN 222-001-021-145 WAS INSTALLED ON WRONG SIDE OF PILOT CYCLIC STICK LOWER LEVER CAUSING A FOULING CONDITION WITH THE ACFT STRUCTURE IN THE 
- [SDR 2011FA0000289](https://openairdocs.org/sdr/2011FA0000289), Apr 27, 2011: SCREEN. FAILED. BROKEN FUEL SCREEN MOUNTING BRACKET, DISCOVERED BY INSP WHEN INSTALLING FUEL CELL, REF ITEM 66 OF FIG 28-1003, BHT 430-MM-4, PN 222-066-624-101. THE MOUNTING BR
- [SDR AC2R0CT03062011](https://openairdocs.org/sdr/AC2R0CT03062011), Mar 6, 2011: SHAFT. CRACKED. OUTER SHAFT FOUND CRACKED AT TT 259.0 AT DISASSEMBLY. ENGINE WAS REMOVED FOR SMOKING ON SHUTDOWN AND VXP INDICATED VIBRATIONS TRENDING UP. RAN ON TEST CELL AND 
- [SDR AC2A0CF02162011](https://openairdocs.org/sdr/AC2A0CF02162011), Feb 16, 2011: SUPPORT. CRACKED. ON FINAL APPROACH TO HELIPORT, A MODERATE VIBRATION WAS FELT THOUGH THE PEDALS AND AIRFRAME. THE HELICOPTER WAS LANDED AND SHUTDOWN. FOUND EAR BROKEN OFF SUPPOR
- [SDR AC2A0CM01312011](https://openairdocs.org/sdr/AC2A0CM01312011), Jan 30, 2011: WINDOW. DAMAGED. BIRD STRIKE ABOVE LT WINDOW.
- [SDR AC2A0CM01242011](https://openairdocs.org/sdr/AC2A0CM01242011), Jan 24, 2011: FADEC. FAILED. NR1 M/ECU LIGHT ILLUMINATED IN FLIGHT ALONG WITH ECU INDICATION ABOVE NR1 ENGINE INDICATOR. FADEC ON NR 1 ENGINE FAILED.
- [SDR CA100812001](https://openairdocs.org/sdr/CA100812001), Aug 4, 2010: ROD END. LEAKING. MFG RECEIVED REPORT OF A 430 COLLECTIVE FLIGHT CONTROL MALFUNCTION DURING PREPARATION FOR TAKEOFF. EVENT OCCURED ON GROUND. AFTER ACFT WAS SHUTDOWN A OIL LEAK W
- [SDR UG8A2010071201](https://openairdocs.org/sdr/UG8A2010071201), Jul 12, 2010: DISPLAY. INTERMITTENT. PILOTS EFIS FAILED (TOP TUVE) INTERMITTENT.
- [SDR QMLA2010051810014](https://openairdocs.org/sdr/QMLA2010051810014), May 18, 2010: HANGER ASSY. SHEARED. DURING ROUTINE INSPECTION DISCOVERED MOUNTING FLANGE BROKE OFF OF THE NR1 TAIL ROTOR DRIVE SHAFT HANGER BRG. PERFORMED INSPECTION OF THE SURROUNDING AREA AND RE
- [SDR 1E9R201001](https://openairdocs.org/sdr/1E9R201001), Feb 19, 2010: BLADE. CRACKED. ACFT WAS FLOWN TO FACILITY, REPORTED DEBONDING OF TAIL ROTOR BLADE L/E AT TIP OF BLADE. UPON FURTHER INVESTIGATION OF BLADE, IT WAS DISCOVERED THAT THE ROOT END
- [SDR CA100122007](https://openairdocs.org/sdr/CA100122007), Jan 20, 2010: STUD. LOOSE. (CAN) QTY (2) STUDS PARTIALLY BACKED OUT OF THE THREADED HOLES OF THE 2-1/2 BRG CAGE MOUNTING BOSS. STUDS BACKED OUT APPROX 1 AND 2 THREADS RESPECTIVELY. NUTS O
- [SDR 2009FA0000978](https://openairdocs.org/sdr/2009FA0000978), Oct 20, 2009: DUPLEX BEARING. SPALLED. DUPLEX BEARING FOUND TO BE HEAVILY SPALLED. 17/125 BALLS DAMAGED (APPROX 14 PERCENT) ONE INNER RACE DAMAGED 4 PLACES; OUTER RACE DAMAGED 2 PLACES.
- [SDR AC2A2009090183074](https://openairdocs.org/sdr/AC2A2009090183074), Sep 1, 2009: UNKNOWN. MALFUNCTIONED. SIX MINUTES OUT OF VENICE, LA, TRANSMISSION
- [SDR QMLR MC708](https://openairdocs.org/sdr/QMLR%20MC708), Aug 27, 2009: BLADE. CRACKED. FOUND TAIL ROTOR BLADE ROOT TO BE CRACKED IN VICINITY OF PITCH HORN.
- [SDR AC2A2009060782115](https://openairdocs.org/sdr/AC2A2009060782115), Jun 7, 2009: BEARING. WORN. DURING AN OVERSPEED INSP ON THE DRIVE TRAIN, WE FOUND THE NR2 HANGER BEARING ON THE TAILROTOR DRIVESHAFT HAD EXCESSIVE RADIAL PLAY. REPLACED THE HANGER BRG.
- [SDR AC2A2009053181959](https://openairdocs.org/sdr/AC2A2009053181959), May 31, 2009: PICKUP. MALFUNCTIONED. ENROUTE, YELLOW M/ECU2 INDICATOR, WHITE ECU INDICATOR ABOVE THE NR 2 ENGINE TQ AND NP INDICATION FLUCTUATED FOR ABOUT FIVE MINUTES BEFORE IT RETURNED TO NORMAL 

All 392: https://openairdocs.org/model/bell-helicopter-textron-canada-430/reports.md

## STCs that may be installed (OpenAirDocs) (54, 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 SR00149DE-D](https://openairdocs.org/stc/SR00149DE-D): Installation of an Air Methods tail stinger attachment modification. Air Methods LLC
- [STC SR00235DE-D](https://openairdocs.org/stc/SR00235DE-D): Installation of an Articulating Patient Loading System (APLS). Air Methods LLC
- [STC SR09433RC](https://openairdocs.org/stc/SR09433RC): Installation of Aero Seats and Systems Inc., seat part number ASI-6430. Bell Textron Inc
- [STC SR00121BO](https://openairdocs.org/stc/SR00121BO): Installation of OuterLink Corporation CP-2 SATCOM System. Outerlink Corporation
- [STC SR01456LA](https://openairdocs.org/stc/SR01456LA): Installation of Concorde RG407 Batteries. Rotorcraft Support Inc
- [STC SR02330AK](https://openairdocs.org/stc/SR02330AK): Installation of the Max-Viz® Enhanced Vision System (EVS) Models 1000/1500 and associated hardware. PECO Inc
- [STC SR00925DE](https://openairdocs.org/stc/SR00925DE): Installation of Garmin GTX 335/335R and GTX345/345R transponders to provide ADS-B Out and In functionality. Peregrine
- [STC SR01957NY-D](https://openairdocs.org/stc/SR01957NY-D): Installation of a Honeywell Chadwick Model 15175 VXP System. Diagnostic Solution International LLC
- [STC SR02794CH](https://openairdocs.org/stc/SR02794CH): Installation of a an Inlet Barrier Filter (IBF). Donaldson Company Inc
- [STC SH5225NM](https://openairdocs.org/stc/SH5225NM): Installation of a freon air conditioning system. Air Comm Corporation
- [STC SH5226NM](https://openairdocs.org/stc/SH5226NM): Installation of a bleed air cabin heating system. Air Comm Corporation
- [STC SR01668AT](https://openairdocs.org/stc/SR01668AT): Manufacture of Crew Emergency Push Out Windows in accordance with Aeronautical Accessories, Inc. Drawing List Report AA-98035, no revision, dated March 23, 1998, and installation per Report AA-98032, no revision, dated February 26, 1998, or AA-98077, Revision A , dated August 12, 1998, or later FAA approved revisions. Bell Helicopter Textron Inc
- [STC SR09320RC-D](https://openairdocs.org/stc/SR09320RC-D): Installation of the Right or Left Passenger Sliding Door Kit in accordance with drawings listed on Aeronautical Accessories, Inc. Drawing List Report AA-01080, Revision H, dated March 8, 2006, or later FAA approved revision and Instillation Instructions Report No. AA-01039, Revision E, dated February 10, 2006 or later FAA approved revision. Bell Helicopter Textron Inc
- [STC SR09329RC](https://openairdocs.org/stc/SR09329RC): Installation of an Enhanced Ground Proximity Warning System (EGPWS) in accordance with Aeronautical Accessories, Inc., Document Number AA-01100, Revision B, dated October 17, 2001, or later Federal Aviation Administration (FAA) approved revision(s). Bell Helicopter Textron Inc
- [STC SR09338RC-D](https://openairdocs.org/stc/SR09338RC-D): Installation of passenger photo window in accordance with Aeronautical Accessories, Inc. Drawing List AA-02013, Revision F, dated October 14, 2005, or later DAS approved revision. Bell Helicopter Textron Inc
- [STC SR09375RC-D](https://openairdocs.org/stc/SR09375RC-D): Flitestep in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-05095, Revision A, dated December 22, 2005, or later DAS approved revision; and Installation Instructions Report No. AA-05099, Revision A, dated December 8, 2005, or later DAS approved revision. Bell Helicopter Textron Inc
- [STC SR09439RC](https://openairdocs.org/stc/SR09439RC): Combined Cockpit Voice Recorder/Flight Data Recorder in accordance with Aeronautical Accessories, Inc. Report No. AA-05035, Revision D, dated July 13, 2005, or later FAA approved revision and installation per Aeronautical Accessories, Inc. Report No. AA-03103, Revision D, dated June 29, 2005, or later FAA approved revision. Bell Helicopter Textron Inc
- [STC SR01545SE](https://openairdocs.org/stc/SR01545SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SR09081RC](https://openairdocs.org/stc/SR09081RC): Installation of a Bendix/King CAS 66A TCAS I system. Texas Aviation Services
- [STC SR09140RC](https://openairdocs.org/stc/SR09140RC): Installation of a Retractable Passenger Step. Texas Aviation Services
- [STC SR09141RC](https://openairdocs.org/stc/SR09141RC): Installation of a Retractable Utility Step. Texas Aviation Services
- [STC SR09147RC](https://openairdocs.org/stc/SR09147RC): Installation of an Adjustable Executive Couch. Texas Aviation Services
- [STC SR09148RC](https://openairdocs.org/stc/SR09148RC): Installation of 2-Place passenger seating. Texas Aviation Services
- [STC SR01638SE](https://openairdocs.org/stc/SR01638SE): Fabricate and Install the emergency medical equipment, Infant Transport Module including incubator, medical oxygen, delivery and monitoring equipment. Fliegen Works Inc
- [STC SR09546RC](https://openairdocs.org/stc/SR09546RC): Installation of Night Vision Goggle compatible Interior Lighting System. Ahlers Aerospace Inc
- [STC SR01940SE](https://openairdocs.org/stc/SR01940SE): Installation of a Supplemental Lighting System; installed in accordance with photos 1 through 11 for N20SP, dated October 28, 2008, and maintained in accordance with Instructions for Continued Airworthiness ICA 43049086, dated October 28, 2008, or later FAA-approved revisions. Aviation Specialties Unlimited Inc
- [STC SR01922SE](https://openairdocs.org/stc/SR01922SE): ONE ONLY STC, SN 49070: Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SR01923SE](https://openairdocs.org/stc/SR01923SE): Installation of a Supplemental Lighting System;. Aviation Specialties Unlimited Inc
- [STC SR01933SE](https://openairdocs.org/stc/SR01933SE): ONE ONLY STC, SN 49069: Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SH2697SO](https://openairdocs.org/stc/SH2697SO): Installation of a Wire Strike Protection System Kit. Bristol Aerospace Ltd
- [STC SR01450SE](https://openairdocs.org/stc/SR01450SE): Installation of two (2) sliding windows (left and right side) in the passenger compartment. Acrohelipro Global Services USA Inc
- [STC SR01451SE](https://openairdocs.org/stc/SR01451SE): Installation of Cineflex HD V 14 gyro stabilized camera in structural provisions for a nose-mounted camera. Acrohelipro Global Services USA Inc
- [STC SR01452SE](https://openairdocs.org/stc/SR01452SE): Installation of structural provisions for four antenna pods, two on the underside of the fuselage and one each on the tips of the rotorcraft wings. Acrohelipro Global Services USA Inc
- [STC SH935GL](https://openairdocs.org/stc/SH935GL): Installation of Shadin Company digital fuel flow indicator system. Shadin Company Inc
- [STC SR00514DE-D](https://openairdocs.org/stc/SR00514DE-D): Installation of an Emergency Medical Services (EMS) interior. Air Methods Corporation
- [STC SR09443RC](https://openairdocs.org/stc/SR09443RC): Installation of Night Vision Goggle Compatible Lighting System. Aero Dynamix Inc
- [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models. Technisonic Industries Limited
- [STC SR00514DE](https://openairdocs.org/stc/SR00514DE): Installation of an Emergency Medical Services (EMS) interior. Air Methods Corporation
- [STC SR09338RC](https://openairdocs.org/stc/SR09338RC): Installation of passenger photo windows. Aeronautical Accessories, Inc
- [STC SR09158RC](https://openairdocs.org/stc/SR09158RC): Installation of a passenger door Horizontal sliding window. Dart Aerospace USA, Inc
- [STC SR09159RC](https://openairdocs.org/stc/SR09159RC): Installation of a nose mounted Gyrocam camera pod, provisions only. Dart Aerospace USA, Inc
- [STC SR09160RC](https://openairdocs.org/stc/SR09160RC): Installation of an antenna pod provisions. Approval is limited to installation made in Bell 430 serial number 49009 with high skid gear and without floats ONLY. Dart Aerospace USA, Inc
- [STC SR01404NY](https://openairdocs.org/stc/SR01404NY): Installation of Dart Aerospace bearpaws according to Dart Aerospace installation instructions. Dart Aerospace Limited
- [STC SR09320RC](https://openairdocs.org/stc/SR09320RC): Installation of passenger sliding door kit. Aeronautical Accessories, Inc
- [STC SH201WE](https://openairdocs.org/stc/SH201WE): Installation of stirrup assemblies to directional control pedals for operation by handicapped pilot. (US ARMY OH-13E 205A). Dallwig Barry C
- [STC SR02100AK](https://openairdocs.org/stc/SR02100AK): Fabrication and installation of Airglas Engineering P/N L8500AUT or P/N L8500AUTR ski kit. Airglas Inc
- [STC SR00406DE](https://openairdocs.org/stc/SR00406DE): Installation of SpectroLab SX-5 searlight. Air Methods Corporation
- [STC SR00407DE](https://openairdocs.org/stc/SR00407DE): Installation of EMS interior. Air Methods Corporation
- [STC SR00386DE](https://openairdocs.org/stc/SR00386DE): Installation of Modular Medical Cabinet. Air Methods Corporation
- [STC SR00235DE](https://openairdocs.org/stc/SR00235DE): Installation of articulating patient loading system. Air Methods Corporation

All 54: https://openairdocs.org/model/bell-helicopter-textron-canada-430/stcs.md

## PMA parts (OpenAirDocs) (269, 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.

- [403AC-202-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158035021820260923124150.0001): Cabin Air Conditioning System. Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [430H-201-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145321510120260923124151.0001): Bleed Air Cabin Heating System. Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [430AC-200-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127662007420260923124150.0001): Cabin Air Conditioning System. Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [14965](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196333756520250312124244.0001): Cable Assy PC/TRKRPanel Mount Pigtail Airframe. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [8866](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196131521120250312124229.0001): Velocimeter, EMI. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [11758](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195856122820250312124233.0001): Bracket,Accelerometer Vibrex (Allison). Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17367](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193507779220250312124309.0001): Doubler,Baggage Comp Cable Feed Thru Bell 430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14316](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188996389120250312124239.0001): Cable Assembly,Pigtail, HighTemp Accelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17368](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188537471920250312124310.0001): Doubler, BaggageComp CannonPlug Bell 430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14319](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186906279520250312124241.0001): Cable Assy, Pigtail, MagP/U, 200Degree C, Airframe. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17360](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186603277720250312124309.0001): Bracket, ConnectorMounting. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17212](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173037214120250312124303.0001): Panel, RemoteDU/Strobex Aux VEL (4). Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17366](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172752526920250312124309.0001): Doubler, AftFuselage. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16239](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170928194020250312124250.0001): Cable Assy, Pigtail Velo Pnl Jack 6SA/F. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [10494](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170903078220250312124232.0001): Accelerometer Hi-Temp. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [12900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169932331420250312124234.0001): Assy, PhotocellBanner. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [13337](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167855702820250312124235.0001): Bracket,Velocimeter, Cockpit Centerline, S-76. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16415](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157427938520250312124256.0001): Bracket, PhotocellMain DriveShaft Bell 430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16274](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156614474220250312124252.0001): CableAssembly, ICPAccelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17285](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154941073520250312124305.0001): Spacer, Mounting .75OD, .265 ID,.50L. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [13673](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154934413120250312124236.0001): Bracket,Photocell, Banner, T/R, BL 206L. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154733917020250312124301.0001): Kit, Accelerometer, ICP. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17362](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154306577020250312124309.0001): Plate, CoverBell 430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [10200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149714220920250312124231.0001): Photocell Assy. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [14320](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149190602020250312124242.0001): Cable Assy, Pigtail, HighTempAccelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17345](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146401958820250312124308.0001): Bracket, Remote DuMount Bell430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16278](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145859635020250312124253.0001): Doubler Plate ICP Connector. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [13880](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141440165420250312124238.0001): Cable Assy PCELL PigtailAirframe. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16279](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137804838020250312124254.0001): BracketMounting ICP Single. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [8902](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137537753920250312124230.0001): Bracket,Accelerometer Mounting. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [5876](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122393646620250312124224.0001): Magnetic Pickup. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [PL915-17154](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119738631820250312124316.0001): Kit, VXP Hardwire Installation, Bell 430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16580](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113925458220250312124257.0001): Doubler Plate. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16240](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111021548520250312124251.0001): Bracket, ICP. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17358](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105252404320250312124308.0001): Bracket, ConnectorDual Lemo. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [17359](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104467245120250312124309.0001): Bracket, VXPMounting Bell 430. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [15175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104371520420250312124246.0001): VXP Onboard Monitor. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [16167](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101116175420250312124248.0001): Cable Assy, PCELL PigtailAirframeB212/412. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [B8422](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100779607820250312124228.0001): Brkt, Accelerometer. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [6752](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100109408120250312124226.0001): High Freq. Accel, Brkt.. Diagnostic Solutions International, LLC · PMA PQ05321NM · Modification part · Mar 3, 2025
- [430AC-200-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133179941220250213194601.0001): General Arrangement 430 Air Conditioner. Air Comm Corporation · PMA PQ0072NM · Modification part · Feb 12, 2025
- [430H-201-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168154787920250213205336.0001): Bleed Air Cabin Heating System. Air Comm Corporation · PMA PQ0072NM · Modification part · Feb 10, 2025
- [430AC-200-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134384839020250213205335.0001): Cabin Air Conditioning System. Air Comm Corporation · PMA PQ0072NM · Modification part · Feb 10, 2025
- [403AC-202-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117336470320250213205335.0001): Cabin Air Conditioning System. Air Comm Corporation · PMA PQ0072NM · Modification part · Feb 10, 2025
- [M2002-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139662881120240802183933.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 200SGL1009 · Jun 20, 2024
- [BCN200SG-K1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151710598220221024201117.0001): Overhaul Hardware Kit 200SGL, 200SG Series Starter Generators. BCN Aerospace, Inc. · PMA PQ2149NE · Replaces NJ200SG-K1 · Oct 14, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103377342420220819173035.0001): Wesco Manufacturing, Inc. · PMA PQ00011EB · Aug 9, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141689660820220809130832.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · May 10, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115826847420220809102508.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022
- [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148868756720220408135726.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022

All of them: https://openairdocs.org/model/bell-helicopter-textron-canada-430/pma.md

## The same model under other registry codes

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

- [Bell 430](https://openairdocs.org/model/bell-430): 27 registered aircraft, registry code 1182150

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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.