# Airbus Helicopters EC 130B4

- Type: Aircraft model (FAA registry)
- Registry code: 8680150
- Manufacturer (registry): AIRBUS HELICOPTERS
- Model: EC 130B4
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 8
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 2
- Page: https://openairdocs.org/model/airbus-helicopters-ec-130b4

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 2026-22-01](https://openairdocs.org/ad/2026-22-01): Cabin equipment/furnishings · Airbus Helicopters AS350B2, AS350B3, AS355N and 2 more. Effective Nov 12, 2026
- [AD 2026-20-03](https://openairdocs.org/ad/2026-20-03): Placards and Markings · Airbus Helicopters AS350B, AS350BA, AS350B1 and 11 more. Effective Nov 5, 2026
- [AD 2026-16-01](https://openairdocs.org/ad/2026-16-01): Main rotor drive · Airbus Helicopters AS350B, AS350BA, AS350B1 and 5 more. Effective Sep 10, 2026
- [AD 2026-14-02](https://openairdocs.org/ad/2026-14-02): Indication/Recording System · Airbus Helicopters AS350B2, AS350B3, EC120B and 1 more. Effective Aug 14, 2026
- [AD 2026-12-08](https://openairdocs.org/ad/2026-12-08): Time Limits/Maintenance Checks · Airbus Helicopters AS350B2, AS350B3, EC130B4 and 1 more. Effective Jul 21, 2026
- [AD 2026-12-03](https://openairdocs.org/ad/2026-12-03): Main rotor gearbox · Airbus Helicopters AS350B, AS350B1, AS350B2 and 11 more. Effective Jul 14, 2026
- [AD 2026-01-08](https://openairdocs.org/ad/2026-01-08): Tail Rotor Drive · Airbus Helicopters EC130B4 and EC130T2. Effective Feb 2, 2026
- [AD 2025-24-06](https://openairdocs.org/ad/2025-24-06): Cabin Equipment/Furnishings · Airbus Helicopters AS350B2, AS350B3, AS355N and 2 more. Effective Jan 12, 2026
- [AD 2025-18-13](https://openairdocs.org/ad/2025-18-13): Engine Controls · Airbus Helicopters AS350B3, EC130B4 and EC130T2. Effective Oct 23, 2025
- [AD 2025-17-14](https://openairdocs.org/ad/2025-17-14): Tail Rotor Drive System · Airbus Helicopters EC130B4 and EC130T2. Effective Oct 7, 2025
- [AD 2025-17-02](https://openairdocs.org/ad/2025-17-02): Emergency Flotation Section · Airbus Helicopters EC120B, EC130B4 and EC130T2. Effective Sep 26, 2025
- [AD 2025-16-08](https://openairdocs.org/ad/2025-16-08): Tail Rotor Blades · Airbus Helicopters EC130B4 and EC130T2. Effective Sep 22, 2025
- [AD 2025-10-01](https://openairdocs.org/ad/2025-10-01): Cabin Equipment/Furnishings · Airbus Helicopters AS350B2, AS350B3 and EC130B4. Effective Jul 11, 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 2023-14-06](https://openairdocs.org/ad/2023-14-06): Main Landing Gear Strut, Axle, Truck · Airbus Helicopters EC120B, EC130B4 and EC130T2. Effective Sep 8, 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 2022-10-51](https://openairdocs.org/ad/2022-10-51): Flight Control System · Airbus Helicopters AS350B, AS350B1, AS350B2 and 22 more. Effective Jun 7, 2022
- [AD 2022-01-01](https://openairdocs.org/ad/2022-01-01): Main Rotor System · Airbus Helicopters AS350B, AS350BA, AS350B1 and 17 more. Effective Mar 7, 2022
- [AD 2021-17-17](https://openairdocs.org/ad/2021-17-17): Cabin Equipment/Furnishings · Airbus Helicopters EC135P3, EC135T3, MBB-BK 117 C-2 and 32 more. Effective Nov 22, 2021
- [AD 2021-19-02](https://openairdocs.org/ad/2021-19-02): Rotorcraft flight control · Airbus Helicopters EC130B4 and EC130T2. Effective Nov 1, 2021
- [AD 2021-10-25](https://openairdocs.org/ad/2021-10-25): Tail rotor blades · Airbus Helicopters EC130B4 and EC130T2. Effective Jul 6, 2021
- [AD 2021-09-05](https://openairdocs.org/ad/2021-09-05): Rotorcraft Tail Boom · Airbus Helicopters EC130B4 and EC130T2. Effective Jun 2, 2021
- [AD 2021-04-13](https://openairdocs.org/ad/2021-04-13): Main Rotor Mast Inner Race Rings · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Apr 14, 2021
- [AD 2020-25-11](https://openairdocs.org/ad/2020-25-11): Doors · Airbus Helicopters EC120B and EC130B4. Effective Jan 21, 2021
- [AD 2020-23-09](https://openairdocs.org/ad/2020-23-09): Doors · Airbus Helicopters EC130B4. Effective Dec 24, 2020
- [AD 2020-22-20](https://openairdocs.org/ad/2020-22-20): Main Rotor Gearbox · Airbus Helicopters AS355E, AS355F, AS355F1 and 12 more. Effective Dec 14, 2020
- [AD 2020-20-14](https://openairdocs.org/ad/2020-20-14): Rotorcraft Servo System · Airbus Helicopters AS-365N2, AS-365N3, AS355F and 11 more. Effective Oct 23, 2020
- [AD 2020-12-09](https://openairdocs.org/ad/2020-12-09): Tail rotor blade · Airbus Helicopters EC130B4 and EC130T2. Effective Jul 28, 2020
- [AD 2020-09-02](https://openairdocs.org/ad/2020-09-02): Cabin Equipment/Furnishings · Airbus Helicopters AS355NP, Model 358 Torso Restraint System, AS350B2 and 3 more. Effective May 29, 2020
- [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 2018-02-02](https://openairdocs.org/ad/2018-02-02): Main Gearbox Mast · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Feb 12, 2018
- [AD 2016-25-20](https://openairdocs.org/ad/2016-25-20): Main Rotor Drive System · Airbus Helicopters AS355E, AS355F, AS355F1 and 13 more. Effective Jan 31, 2017
- [AD 2015-17-11](https://openairdocs.org/ad/2015-17-11): Main Rotor System · Airbus Helicopters AS355E, AS355F, AS355F1 and 13 more. Effective Sep 29, 2015
- [AD 2014-20-15](https://openairdocs.org/ad/2014-20-15): Rotorcraft Tail Boom · Airbus Helicopters EC130B4. Effective Oct 22, 2014
- [AD 2013-16-19](https://openairdocs.org/ad/2013-16-19): Emergency Flotation Section · Airbus Helicopters EC120B and EC130B4. Effective Sep 27, 2013
- [AD 2013-07-05](https://openairdocs.org/ad/2013-07-05): Window/Windshield System · Airbus Helicopters EC130B4. Effective May 15, 2013
- [AD 2013-05-21](https://openairdocs.org/ad/2013-05-21): Cabin vibration damper · Airbus Helicopters EC130B4. Effective Apr 30, 2013
- [AD 2013-01-05](https://openairdocs.org/ad/2013-01-05): Starter-Generator · Airbus Helicopters AS350B3 and EC130B4. Effective Mar 11, 2013
- [AD 2011-10-12](https://openairdocs.org/ad/2011-10-12): Pinion · Airbus Helicopters AS350B, AS350B1, AS350B2 and 3 more. Effective Jun 22, 2011
- [AD 2011-06-07](https://openairdocs.org/ad/2011-06-07): Emergency Flotation Gear · Airbus Helicopters EC130B4. Effective Apr 6, 2011
- [AD 2010-15-03](https://openairdocs.org/ad/2010-15-03): Landing Gear System Wiring · Airbus Helicopters EC130B4. Effective Aug 20, 2010
- [AD 2010-06-07](https://openairdocs.org/ad/2010-06-07): Rotorcraft Flight Control · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 14 more. Effective Apr 21, 2010
- [AD 2008-06-22](https://openairdocs.org/ad/2008-06-22): Twist grip drive · Airbus Helicopters EC130B4. Effective Apr 28, 2008
- [AD 2008-05-16](https://openairdocs.org/ad/2008-05-16): Battery overheat sensing circuit · Airbus Helicopters EC130B4. Effective Apr 16, 2008
- [AD 2008-05-15](https://openairdocs.org/ad/2008-05-15): Tube-to-flange · Airbus Helicopters EC130B4. Effective Apr 16, 2008
- [AD 2006-10-19](https://openairdocs.org/ad/2006-10-19): Throttle twist grip (twist grip) assembly · Airbus Helicopters EC130B4. Effective Jul 27, 2006
- [AD 2005-03-08](https://openairdocs.org/ad/2005-03-08): Fuel bleed lever · Airbus Helicopters AS350B, AS350B1, AS350B2 and 6 more. Effective Mar 21, 2005
- [AD 2004-11-05](https://openairdocs.org/ad/2004-11-05): Fuel Transfer Line and Air Exhaust Duct · Airbus Helicopters AS350B3 and EC130B4. Effective Jul 9, 2004
- [AD 2004-01-14](https://openairdocs.org/ad/2004-01-14): Forward fittings · Airbus Helicopters EC130B4. Effective Jan 26, 2004
- [AD 2003-14-19](https://openairdocs.org/ad/2003-14-19): Main servocontrols · Airbus Helicopters AS-365N2, AS-365N3, AS355F and 7 more. Effective Aug 21, 2003

Historical (superseded or no longer in force):

- [AD 2025-23-52](https://openairdocs.org/ad/2025-23-52) (historical): Tail Rotor Drive Shaft · Airbus Helicopters EC130B4 and EC130T2. Effective Dec 8, 2025
- [AD 2025-06-04](https://openairdocs.org/ad/2025-06-04) (historical): Main Rotor Gearbox · Airbus Helicopters AS350B, AS350B1, AS350B2 and 11 more. Effective May 9, 2025
- [AD 2022-11-08](https://openairdocs.org/ad/2022-11-08) (historical): Electrical Power System, Aircraft Fuel System, Hydraulic Power System, Doors, Fuselage Structure, Main Rotor System, Main Rotor Drive System, Tail Rotor System, Tail Rotor Drive System, Rotorcraft Flight Control · Airbus Helicopters AS350B, AS350BA, AS350B1 and 5 more. Effective Jul 8, 2022
- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021
- [AD 2021-05-02](https://openairdocs.org/ad/2021-05-02) (historical): Main Rotor System · Airbus Helicopters AS350B, AS350BA, AS350B1 and 12 more. Effective Apr 16, 2021
- [AD 2020-24-07](https://openairdocs.org/ad/2020-24-07) (historical): Engine Control System Wiring · Airbus Helicopters AS350B3, EC130B4 and EC130T2. Effective Jan 12, 2021
- [AD 2018-26-02](https://openairdocs.org/ad/2018-26-02) (historical): Engine Control System Wiring · Airbus Helicopters AS-350B3, EC 130 B4 and EC 130 T2. Effective Jan 30, 2019
- [AD 2017-16-04](https://openairdocs.org/ad/2017-16-04) (historical): Cabin Equipment/Furnishings · Airbus Helicopters AS-350B2, AS-350B3, AS355NP and 3 more. Effective Sep 22, 2017
- [AD 2016-25-19](https://openairdocs.org/ad/2016-25-19) (historical): Engine controls · Airbus Helicopters AS-350B3 and EC 130 B4. Effective Feb 2, 2017
- [AD 2016-08-20](https://openairdocs.org/ad/2016-08-20) (historical): Rotorcraft Tailboom · Airbus Helicopters EC 130 B4 and EC 130 T2. Effective Jun 6, 2016
- [AD 2014-12-51](https://openairdocs.org/ad/2014-12-51) (historical): Rotorcraft Tailboom · Airbus Helicopters EC 130 B4 and EC 130 T2. Effective Aug 20, 2014
- [AD 2014-12-12](https://openairdocs.org/ad/2014-12-12) (historical): Emergency Exits · Airbus Helicopters EC 130 B4 and EC120B. Effective Aug 4, 2014
- [AD 2012-02-13](https://openairdocs.org/ad/2012-02-13) (historical): Rotorcraft Tail Boom · Airbus Helicopters EC 130 B4. Effective Feb 22, 2012
- [AD 2010-21-07](https://openairdocs.org/ad/2010-21-07) (historical): Engine Control System Wiring · Airbus Helicopters AS-350B3 and EC 130 B4. Effective Nov 18, 2010
- [AD 2002-02-51](https://openairdocs.org/ad/2002-02-51) (historical): Metal bushing and the STARFLEX star arm end (arm end) · Eurocopter France AS-350B, AS-350B1, AS-350B2 and 11 more

All 66: https://openairdocs.org/model/airbus-helicopters-ec-130b4/ads.md

## Information bulletins (advisory) (6)

- [SAIB SW-17-23R2](https://openairdocs.org/saib/SW-17-23R2): Fuel System. Issued Jul 15, 2019
- [SAIB SW-17-23R1](https://openairdocs.org/saib/SW-17-23R1) (historical): Fuel System. Issued Mar 2, 2018
- [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-12-17](https://openairdocs.org/saib/SW-12-17): Autopilot System. Issued Feb 3, 2012
- [SAIB SW-11-07](https://openairdocs.org/saib/SW-11-07): Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 Helicopters. Issued Dec 20, 2010

## Registered aircraft (2)

- [N130CZ](https://openairdocs.org/aircraft/N130CZ): [Orbic Air LLC](https://openairdocs.org/faa-owner/ORBIC%20AIR%20LLC), [Burbank, CA](https://openairdocs.org/faa-place/CA/Burbank), built 2006, S/N 4060
- [N30EZ](https://openairdocs.org/aircraft/N30EZ): [Hover Air LLC](https://openairdocs.org/faa-owner/HOVER%20AIR%20LLC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 2011, S/N 7285

## NTSB investigations (1)

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 CEN24MA111](https://openairdocs.org/ntsb/CEN24MA111), Feb 10, 2024: Airbus Helicopters EC 130 (N130CZ), Halloran Springs, CA, destroyed, 6 fatal. Probable cause: The pilot’s decision to continue the visual flight rules flight into instrument meteorological conditions, which resulted in the pilot’s spatial disorientation and loss of control. Contributing to…

## 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 20240210020049A](https://openairdocs.org/incident/20240210020049A), Feb 10, 2024: Airbus Helicopters EC-130B4 (N130CZ), Halloran Spring, CA, Destroyed, 6 fatal. On February 9, 2024, about 2208 pacific standard time, an Airbus Helicopters ec 130B4 helicopter,[privacy data omitted], was destroyed when it was involved in…

## Service difficulty reports (724, newest 50)

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

- [SDR 2A6R2026101275802](https://openairdocs.org/sdr/2A6R2026101275802), Oct 12, 2026: FRAME. CORRODED. DAMAGE TO THE LT EDGE FRAME, IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OTBD FACES OF THE FRAME.
- [SDR 2A6R2026101275801](https://openairdocs.org/sdr/2A6R2026101275801), Oct 12, 2026: FRAME. CORRODED. DAMAGE TO THE RT EDGE FRAME IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACES OF THE FRAME.
- [SDR QMLA2026100820077](https://openairdocs.org/sdr/QMLA2026100820077), Oct 8, 2026: UNKNOWN. ODOR. POTENT FUEL ODOR, AFTER TAKEOFF IN COCKPIT WITH PATIENT ON BOARD.
- [SDR QMLA2026092820074](https://openairdocs.org/sdr/QMLA2026092820074), Sep 18, 2026: BLOWER MOTOR. FAILED. ELECTRICAL BURN SMELL 5 TO 10 MINUTES INTO FLIGHT IN CABIN. THE SMELL WAS VERY POTENT BUT ONLY LASTED ABOUT 5 TO 10 SECONDS WITH NOW LINGERING EFFECTS.
- [SDR 2A6R2026310875801](https://openairdocs.org/sdr/2A6R2026310875801), Aug 31, 2026: DOUBLER. CORRODED. CORROSION DAMAGE WAS DISCOVERED ON THE FORWARD FUEL TANK SADDLE DOUBLER. REPLACEMENT PART WAS UNAVAILABLE WITHIN THE REQUIRED RETURN-TO-SERVICE SCHEDULE. A REPL
- [SDR QMLA2026082420059](https://openairdocs.org/sdr/QMLA2026082420059), Aug 23, 2026: RELAY. FAILED. GENERATOR LIGHT ILLUMINATED, VERIFIED ZERO AMPS ON THE VEMD., REPLACED RELAYS
- [SDR QMLA2026081320055](https://openairdocs.org/sdr/QMLA2026081320055), Aug 13, 2026: BLOWER MOTOR. BURNED OUT. ODOR OF BURNT ELECTRICAL WIRING. FOUND SMELL COMING FROM AFT AC VENTS. FOUND CONDENSATION/WATER IN ELECTRICAL MOTOR. REPLACED AFT BLOWER MOTOR
- [SDR QMLA2026080920052](https://openairdocs.org/sdr/QMLA2026080920052), Aug 8, 2026: ELEC CONNECTOR. BURNED. ON APPROACH PILOT AND CREW DETECTED FAINT ELECTRICAL SMELL NO SMOKE PRESENT. AMT DISCOVERED 1 EACH MOLEX CONNECTER WITH DISCOLORATION REPLAIRED DAMAGED WIRING.
- [SDR 2026FA0000304](https://openairdocs.org/sdr/2026FA0000304), Apr 28, 2026: CHIP DETECTOR. FALSE INDICATION. ENGINE CHIP EVENT - INTERMITTENT ILLUMINATION OF ENGINE CHIP INDICATION DURING CRUISE FLIGHT AFTER MAKING A TURN. DURING DESCENT AND LANDING AT A LOCAL BALL FIE
- [SDR 2A6R2026042175104](https://openairdocs.org/sdr/2A6R2026042175104), Apr 21, 2026: FRAME. DENTED. A LARGE DENT WAS DISCOVERED ON THE TRANSMISSION DECK SKIN AND CENTER BEAM PN: 355A21-2109-21. THE DAMAGE TO THE DECK SKIN IS APPROXIMATELY 0.060” DEEP AND 3.5” 
- [SDR 2026FA0000273](https://openairdocs.org/sdr/2026FA0000273), Apr 16, 2026: SEARCH LIGHT. OVERHEATED. ELECTRICAL FUMES SMELT DURING CRUISE FLIGHT. AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. AFTER TROUBLESHOOTING WAS COMPLETED IT WAS DISCOVERED THAT THE SEARCHLI
- [SDR 2A6R2026110375103](https://openairdocs.org/sdr/2A6R2026110375103), Mar 11, 2026: FRAME. DENTED. A DENT WAS DISCOVERED ON THE TRANSMISSION DECK SKIN ON THE LH SIDE. THE DAMAGE IS APPROXIMATELY 0.038” DEEP AND 0.5” IN DIAMETER. AN APPROXIMATE LOCATION OF THE
- [SDR 2A6R2026110375102](https://openairdocs.org/sdr/2A6R2026110375102), Mar 11, 2026: FRAME. CORRODED. DAMAGE TO THE RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACE OF THE FRAME. THE RH EDGE FRAME WAS PARTIALLY RE
- [SDR 2A6R2026110375101](https://openairdocs.org/sdr/2A6R2026110375101), Mar 11, 2026: FRAME. CORRODED. DAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22), IN THE FORM OF CORROSION, WAS IDENTIFIED ACROSS THE ENTIRE LENGTH OF THE OUTBOARD FACE OF THE FRAME. THE LH ED
- [SDR QMLA2026012120003](https://openairdocs.org/sdr/QMLA2026012120003), Jan 21, 2026: UNKNOWN. ODOR. WHILE REPOSITIONING ACFT FROM GRIFFIN MX FACILITY BACK TO JASPER, NOTICED A BURNING ODOR IN THE COCKPIT. MADE TURNS TO BOTH SIDE FOR CREWMEMBERS TO SEE IF THERE
- [SDR QMLA012120003](https://openairdocs.org/sdr/QMLA012120003), Jan 21, 2026: UNKNOWN. ODOR. WHILE REPOSITIONING N325AM FROM MX FACILITY BACK TO JASPER, THE CREW NOTICED A BURNING ODOR IN THE COCKPIT. DISCUSSED PLACES TO LAND. MADE TURNS TO BOTH SIDE FO
- [SDR 2A6R2025121774403](https://openairdocs.org/sdr/2A6R2025121774403), Dec 17, 2025: FRAME. CHAFED. DURING 600-HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED AT THE CENTER OF THE LH AND RH X-FRAME. THE MAX DEPTH OF DAMAGE ON THE LH SIDE IS 0.018” WITH AN AREA OF
- [SDR 2A6R2025121074402](https://openairdocs.org/sdr/2A6R2025121074402), Dec 10, 2025: FRAME. CORRODED. DAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22) AND RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LE
- [SDR 2A6R2025121074401](https://openairdocs.org/sdr/2A6R2025121074401), Dec 10, 2025: STRINGER. CRACKED. DURING 600 HOUR INSPECTION, A CRACK APPROXIMATELY 0.9” LONG WAS DISCOVERED DURING ROUTINE INSPECTION ON THE TAIL BOOM STRINGER JUST BELOW THE BATTERY DOOR FRAME
- [SDR QMLA2025120420122](https://openairdocs.org/sdr/QMLA2025120420122), Dec 4, 2025: WINDSHIELD. CRACKED. UPON LANDING, A CRACK WAS FORMED AND WAS DISCOVERED LATERALLY ON THE RT WINDSCREEN THAT WENT FROM THE LT EDGE ALMOST TO THE RT EDGE.
- [SDR 2A6D20251125001](https://openairdocs.org/sdr/2A6D20251125001), Nov 25, 2025: CROSSBEAM. CHAFED. VARIOUS DAMAGES AT THE AFT LANDING GEAR LOCATION, THE FIRST DAMAGE (#1) IS AT THE AFT LANDING GEAR CROSS BEAM SHIM (P/N: 350A214344.20) IN THE FORM OF CHAFING. 
- [SDR 2A6R1124202574604](https://openairdocs.org/sdr/2A6R1124202574604), Nov 24, 2025: SKIN. DAMAGED. OVERSIZED FASTENER HOLE DAMAGE WAS FOUND ON THE L/H FUSELAGE SKIN (P/N: 350A210053.BW), FWD FRAME ANGLE (P/N: 350A211036.28), AFT FRAME (P/N: 350A211240.00), LO
- [SDR 2A6R2025111804604](https://openairdocs.org/sdr/2A6R2025111804604), Nov 18, 2025: ANGLE. DAMAGED. DAMAGE WAS IDENTIFIED ON THE ATTACHMENT ANGLE (PN 350A21-4064-21), AS ILLUSTRATED IN FIGURE 1 OF DOCUMENT 17-5300-EA-5339, REV. –. THE DAMAGED COMPONENT, LOCATE
- [SDR 2A6R1118202574602](https://openairdocs.org/sdr/2A6R1118202574602), Nov 14, 2025: XMSN DECK. CHAFED. CHAFING DAMAGE WAS FOUND ON THE L/H TRANSMISSION DECK BESIDE THE 7° BULKHEAD BRACE STRUT MOUNT. THIS DAMAGE MEASURED 0.5” IN WIDTH, 0.5” IN LENGTH, AND 0.048” I
- [SDR 2A6R1024202574601](https://openairdocs.org/sdr/2A6R1024202574601), Oct 24, 2025: RAIL. CHAFED. CHAFING DAMAGE WAS FOUND ON THE TAIL BOOM L/H TRDS SUPPORT RAIL/STIFFENER SHEET (P/N: 350A231028.66) JUST FORWARD OF THE #3 TRDS BEARING SUPPORT. THIS DAMAGE IS
- [SDR QMLA2025102720109](https://openairdocs.org/sdr/QMLA2025102720109), Oct 20, 2025: MOUNT. CRACKED. HORIZONTAL STAB RH LOWER MOUNT CRACKED, FELL OFF WHEN REMOVING HORIZONTAL STABILIZER FOR 300 HR INSPECTION. LEVEL 4 REPAIR. AIRBUS REPLACED FITTING AND APPLIED 
- [SDR 2A6R2025100673904](https://openairdocs.org/sdr/2A6R2025100673904), Oct 6, 2025: RAIL. CHAFED. DAMAGE TO THE RH TRDS SUPPORT RAIL (PN 350A23-1053-59) WAS FOUND IN THE FORM OF SEVERAL CHAFES AT THE #3 BEARING SUPPORT (PN 350A23-1053-42). THE #3 BEARING SUP
- [SDR 2A6R2025100673903](https://openairdocs.org/sdr/2A6R2025100673903), Oct 6, 2025: CHANNEL. CORRODED. DAMAGE TO THE RH EDGE FRAME Z CHANNEL, IN THE FORM OF CORROSION, WAS FOUND AT SEVERAL LOCATIONS FWD AND AFT OF FUSELAGE STATION 1405 MM. DAMAGE AFT OF FUSELAGE 
- [SDR 2A6R2025100673902](https://openairdocs.org/sdr/2A6R2025100673902), Oct 6, 2025: BEARING. CHAFED. LH DOOR POST BEARING (P/N 350A21-4459-2251) WAS FOUND TO BE CHAFED BY CONTACT WITH LH SLIDING DOOR CENTER ARM. A NEW DOOR POST BEARING WAS FABRICATED FROM .050”
- [SDR 2A6R2025100673901](https://openairdocs.org/sdr/2A6R2025100673901), Oct 6, 2025: CROSSBEAM. CHAFED. DAMAGE TO THE AFT MAIN LANDING GEAR FITTING AREA WAS FOUND IN 2 LOCATIONS. CHAFE DAMAGE WAS FOUND ON A PREVIOUSLY INSTALLED “AFT LANDING GEAR CROSS BEAM REPAIR 
- [SDR QMLA2025100420098](https://openairdocs.org/sdr/QMLA2025100420098), Sep 30, 2025: DISPLAY. FAULTED. JUST LIFTED OFF FROM A PR EVENT & HEADING BACK TO BASE, NOTICED UPPER SCREEN OF VEMD HAD REVERTED TO 3-PARAMETERS ENGINE PAGE & NG INDICATION MISSING & YELLOW. 
- [SDR QMLA2025091820095](https://openairdocs.org/sdr/QMLA2025091820095), Sep 18, 2025: WARNING LIGHT. ILLUMINATED. GEN LIGHT ILLUMINATED 5 TIMES IN FLIGHT. IT RESET EVERY TIME. OPTED NOT TO CONTINUE THE FLIGHT BEYOND SYRACUSE.
- [SDR QMLA2025083020092](https://openairdocs.org/sdr/QMLA2025083020092), Aug 29, 2025: NONE. NONE. STARTER GENERATOR INSPECTION OVERFLOWN
- [SDR QMLA2025082020090](https://openairdocs.org/sdr/QMLA2025082020090), Aug 20, 2025: CHIP DETECTOR. ACTIVATED. ON START UP THE ENGINE CHIP LIGHT ILLUMINATED AND REMAINED ON.
- [SDR QMLA2025080420082](https://openairdocs.org/sdr/QMLA2025080420082), Aug 2, 2025: LATCH. WORN. BATTERY COMPARTMENT LATCH CAME APART FROM DOOR DUE TO EXCESSIVE WEAR ON THE PIN HOLE WEAR AND PIN FALLING OUT. R+R AIRCRAFT BATTERY DOOR. OPS CHECKED GOOD. ALL 
- [SDR QMLA2025070220071](https://openairdocs.org/sdr/QMLA2025070220071), Jul 2, 2025: GEARBOX. WARNING MESSAGE. MAIN ROTOR GEARBOX CHIP LIGHT ILLUMINATED IN FLIGHT: 4TH RECENT EVENT.
- [SDR QMLA2025062920070](https://openairdocs.org/sdr/QMLA2025062920070), Jun 29, 2025: GEARBOX. MAKING METAL. MGB CHIP LIGHT ILLUMINATED DURING STABLE 3-5FT HOVER PRIOR TO TAKEOFF. INSPECTED AND CLEANED MGB CHIP DETECTOR. CLASS F CHIP FOUND. PERFORMED GROUND RUN UP WITH
- [SDR QMLA2025022720081](https://openairdocs.org/sdr/QMLA2025022720081), Jun 23, 2025: DOOR. NO DISCREPANCY. WHILE AT CRUISE ALTITUDE, THE SLIDING DOOR BEHIND THE PILOT CAME OPEN. AFTER SLOWING DOWN THE AIRCRAFT THE CREW WAS ABLE TO CLOSE THE DOOR. THE DOOR THEN OPENED
- [SDR 2A6R2025160673201](https://openairdocs.org/sdr/2A6R2025160673201), Jun 16, 2025: CHANNEL. CRACKED. A CRACK WAS DISCOVERED ON THE TOP FLANGE OF THE RH EDGE FRAME "Z" CHANNEL JUST AFT OF THE STA 845 FRAME. THE CRACK IS APPROXIMATELY 0.75" LONG.
- [SDR QMLA2025061620067](https://openairdocs.org/sdr/QMLA2025061620067), Jun 14, 2025: VENT LINE. LEAKING. MAJOR OIL LEAK. DISCOVERED BY NURSE STOWING EQUIPMENT IN REAR COMPARTMENT. HE ADVISED ME OF OIL ALL OVER THE SIDE OF AIRCRAFT. I SHUT DOWN THE AIRCRAFT AND EXIT
- [SDR QMLA2025052820060](https://openairdocs.org/sdr/QMLA2025052820060), May 27, 2025: HMU. FAULTED. MULTIPLE ENGINE CHIP CAUTIONS OVER A HANDFUL OF FLIGHTS SINCE MID-APRIL. MOST RECENT EVENT (THIS INCIDENT) OCCURRED LESS THAN ONE DAY AND 0+45 FLIGHT HOURS AFTE
- [SDR QMLA2025052420059](https://openairdocs.org/sdr/QMLA2025052420059), May 24, 2025: VENT. SMOKE. PILOT STATED THAT HE SMELLED AND OBSERVED SMOKE FROM THE FORWARD EVAPORATOR AIR VENTS. THE PILOT STATES THAT HE HAD SELECTED THE LOW BLOWER SPEED SETTING.
- [SDR QMLA2025052020058](https://openairdocs.org/sdr/QMLA2025052020058), May 20, 2025: GEARBOX. MAKING METAL. MAIN ROTOR GEARBOX CHIP 'MGB CHIP' LIGHT ILLUMINATED IN FLIGHT. INSPECTED FOUND 1 CLASS F PARTICLE. - GROUND RUN CW - OPS CHECK GOOD.
- [SDR QMLA2025051520056](https://openairdocs.org/sdr/QMLA2025051520056), May 16, 2025: GEARBOX. WARNING LIGHT. MAIN ROTOR GEAR BOX CHIP INDICATOR LIGHT ILLUMINATED IN FLIGHT. FIRST SET OF FLIGHTS FROM CHANGING OF MBG OIL FILTER YESTERDAY.
- [SDR 2A6R2025050272901](https://openairdocs.org/sdr/2A6R2025050272901), May 2, 2025: SKID. CORRODED. DURING 600 HOUR / AAIP INSPECTIONS, FOUND OEM LH SKID TUBE PN 350A41-6002-0001 CORRODED NEAR RIVETS IN ZONE C2 (AMM32-11-00,6-6). REMOVED THE AIRBUS LEFT LANDIN
- [SDR QMLA2025042120051](https://openairdocs.org/sdr/QMLA2025042120051), Apr 20, 2025: O-RING. LEAKING. IN CRUISE FLIGHT, EN ROUTE TO A SCENE. CREW FIRST REPORTED FUEL SMELL, THEN A FEW SECONDS LATER I SMELLED FUEL. MOMENTS LATER CREW REPORTED SMELLING SMOKE, WHIC
- [SDR QMLA2025032420040](https://openairdocs.org/sdr/QMLA2025032420040), Mar 23, 2025: MOTOR. SHORTED. ELECTRICAL SMOKE ODOR IN CABIN. AFT EVAPORATOR MOTOR HAD INTERNAL SHORT CAUSING SMOKE SMELL AND CAUSING AFT PORTION OF A/C TO BE INOP.
- [SDR QMLA2025030720033](https://openairdocs.org/sdr/QMLA2025030720033), Mar 7, 2025: SCANNER. DAMAGED. ELECTRICAL FIRE SMELL FROM THE LOWER CENTER CABIN. AFTER THROTTLE MOVED FROM IDLE TO FLY. TROUBLE SHOT SYSTEM. DURING NEXT RUN UP THEY NOTICED THE SUPER NIGHT S
- [SDR QMLA2025030520033](https://openairdocs.org/sdr/QMLA2025030520033), Mar 5, 2025: MOTOR. FAILED. WHENEVER THE AIR CONDITIONING IS TURNED ON THERE IS A STRONG BURNING ELECTRICAL SMELL/FUMES
- [SDR QMLA2025021820019](https://openairdocs.org/sdr/QMLA2025021820019), Feb 18, 2025: MOUNT BRACKET. CRACKED. FOUND HORIZONTAL STABILIZER UPPER MOUNT BRACKETS CRACKED ON PRE-FLIGHT INSP.

All 724: https://openairdocs.org/model/airbus-helicopters-ec-130b4/reports.md

## STCs that may be installed (OpenAirDocs) (134, 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 SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group 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 SR03029NY](https://openairdocs.org/stc/SR03029NY): The installation of a SkyTrac ISAT-200 Airborne Position/Data Communicator upgrade. SkyTrac Systems Ltd
- [STC SR12092IB](https://openairdocs.org/stc/SR12092IB): Manufacturing and Installation of Cargo Hold Nets. ICARUS AERO INC
- [STC SR00115IB](https://openairdocs.org/stc/SR00115IB): Installation of the Advanced Lithium Ion Battery Replacement of Ni-Cad Battery. Vertical Flight Solutions Inc
- [STC SR04711NY](https://openairdocs.org/stc/SR04711NY): Replacement of Luminator LS400 LED searchlight (steerable landing light). Sterling Helicopter
- [STC SR04641CH](https://openairdocs.org/stc/SR04641CH): Installation of a Helitak FT1400 Liquid Dispensing System. U.S. Technical Consultants Inc
- [STC SR00495DE-D](https://openairdocs.org/stc/SR00495DE-D): Installation of an Emergency Medical Services (EMS) system. Air Methods LLC
- [STC SR00216IB](https://openairdocs.org/stc/SR00216IB): Installation and Configuration of the Standard Interior Modification. Airbus Helicopters Canada Limited
- [STC SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd
- [STC SR02345LA](https://openairdocs.org/stc/SR02345LA): Installation of HeliSAS stability augmentation system and autopilot. S-TEC Corporation
- [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 SR00154IB](https://openairdocs.org/stc/SR00154IB): Installation of Quick Removal System. SAFRAN AEROSYSTEMS
- [STC SR02120SE](https://openairdocs.org/stc/SR02120SE): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc
- [STC SR04535NY](https://openairdocs.org/stc/SR04535NY): Installation of the Astronics (Max-Viz) 1200 or 1400 EVS. Avio Design Group 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
- [STC SR00376BO](https://openairdocs.org/stc/SR00376BO): The STC installs a SATCOM and Flight Data Monitoring System KIT 350-SAT-100. Outerlink Corporation
- [STC SR04557NY](https://openairdocs.org/stc/SR04557NY): Installation of the Fuel Cap Replacement. Avio Design Group Inc
- [STC SR00059IB](https://openairdocs.org/stc/SR00059IB): Installation of Garmin GRA Radar Altimeter System. Maxcraft Avionics Ltd
- [STC SR03512AT](https://openairdocs.org/stc/SR03512AT): Installation of HID Landing and Taxi Lights. Whelen Aerospace Technologies
- [STC SR02073LA](https://openairdocs.org/stc/SR02073LA): Installation of Concorde RG350 Sealed Lead Acid Battery. Rotorcraft Support Inc
- [STC SR09500RC-D](https://openairdocs.org/stc/SR09500RC-D): Installation of L-3 Trilogy ESI-2000 or ESI-500 Electronic Standby Indicator. Airbus Helicopters Inc
- [STC SH3509SW](https://openairdocs.org/stc/SH3509SW): Installation of a Single and Dual Condenser Blower Air Conditioning System. RSG Products Inc
- [STC SR00886SE](https://openairdocs.org/stc/SR00886SE): Installation of Onboard Systems International Cargo Hook Kits. Onboard Systems International
- [STC SR01588SE](https://openairdocs.org/stc/SR01588SE): Fabrication of Onboard Systems Model 200-299-00 Fuel Drain Guard Kit in accordance with Federal Aviation Administration (FAA) approved Onboard Systems Master Drawing List No. 155-111-00, Rev. 6, dated March 11, 2011, or later FAA-approved revision and Installation of the Fuel Drain Guard Kit. Onboard Systems International LLC
- [STC SR01815SE](https://openairdocs.org/stc/SR01815SE): Fabrication of Onboard Systems Model 200-321-00 Cargo Hook Swing Suspension Kit and 200-322-00 Cargo Hook Sling Suspension Kit. Onboard Systems International
- [STC SR03640AT](https://openairdocs.org/stc/SR03640AT): Installation of miscellaneous windows. Tech-Tool Plastics Inc
- [STC SR04583NY](https://openairdocs.org/stc/SR04583NY): Installation of the COVID Barrier. Avio Design Group Inc
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SR01052DE](https://openairdocs.org/stc/SR01052DE): Installation of Non-Aviation Band FM Radio Systems. Cert Works LLC
- [STC SR02622SE](https://openairdocs.org/stc/SR02622SE): Installation of Garmin G500H TXi Display System (Primary Flight Display (PDF), Multi-Function Display (MFD)). Garmin International Inc
- [STC SR02362AK](https://openairdocs.org/stc/SR02362AK): Installation of a fixed mounted Max-Viz® Enhanced Vision System (EVS) Model 1500 to include a sensor with conformal housing and power supply displaying imagery on any FAA-approved monitor with NTSC RS-170 video interface capability. PECO Inc
- [STC SR09511DS](https://openairdocs.org/stc/SR09511DS): Installation of LED Taxi and Landing Lights with Optional Pulse. Airbus Helicopters Inc
- [STC SR03905NY](https://openairdocs.org/stc/SR03905NY): Installation of STC ST.7501 Fuel tank reinforced metal sheet cradles. AIRBUS HELICOPTERS
- [STC SR03931NY](https://openairdocs.org/stc/SR03931NY): Installation of a crash resistant fuel system. AIRBUS HELICOPTERS
- [STC SR04453CH](https://openairdocs.org/stc/SR04453CH): Installation of Appareo Systems LLC Stratus ES & Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc
- [STC SR02295LA](https://openairdocs.org/stc/SR02295LA): Installation of Garmin Model G500H Flight Display System. Garmin International Inc
- [STC SR02432NY](https://openairdocs.org/stc/SR02432NY): Installation of Helitowcart Bear Paw Models BP350, BP44 or BP130. Dart Aerospace Ltd
- [STC SR02560CH](https://openairdocs.org/stc/SR02560CH): Installation of Inlet Barrier Filter system. Donaldson Company Inc
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SR01185SE](https://openairdocs.org/stc/SR01185SE): Installation of emergency medical stretcher installation. LifePort LLC
- [STC SR00814DE](https://openairdocs.org/stc/SR00814DE): Installation of Garmin Helicopter Terrain Awareness and Warning System (HTAWS). Cert Works LLC
- [STC SR04327NY](https://openairdocs.org/stc/SR04327NY): Installation of the Emergency Float System. Dart Aerospace Ltd
- [STC SR04320NY](https://openairdocs.org/stc/SR04320NY): Installation of the Landing Gear kit. Dart Aerospace Ltd
- [STC SR04318NY](https://openairdocs.org/stc/SR04318NY): Installation of the Advance Lithium Ion Battery to replace the Ni-Cad Battery. Vertical Flight Solutions Inc
- [STC SR11192DS](https://openairdocs.org/stc/SR11192DS): Installation of a Baggage Compartment Floor Protector. Airbus Helicopters Inc
- [STC SR00713DE](https://openairdocs.org/stc/SR00713DE): lnstallation of Night Vision Goggle (NVG) Compatible modifications. Air Methods Corporation
- [STC SR00821DE](https://openairdocs.org/stc/SR00821DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and in functionality using the BendixKing KT74 Transponder and qualified position sensor and ADS-B In Receiver. Peregrine

All 134: https://openairdocs.org/model/airbus-helicopters-ec-130b4/stcs.md

## PMA parts (OpenAirDocs) (785, 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.

- [MDLDL-EC130](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134065242920260923124155.0001): Cabin Air Conditioning System. Air Comm Corporation · PMA PQ0072NM · Modification part · Aug 31, 2026
- [FT1400-H125](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114774366620260705232622.0001): AStar Fire Tank. Helitak USA, LLC · PMA PQ00050WB · Modification part · Jun 16, 2026
- [B60-90-0589](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162823379120251120151805.0001): Member, Laminated Lateral (MGB). KRS Aerospace Elastomeric Solutions · PMA PQ2457CE · Replaces 704A33633153 · Nov 3, 2025
- [B60-90-0590](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113041353320251120151806.0001): Member, Laminated Longitudinal (MGB). KRS Aerospace Elastomeric Solutions · PMA PQ2457CE · Replaces 704A33633151 · Nov 3, 2025
- [117-02393-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167932053620250926140541.0001): Bracket, GSU 75, High Stiffness, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Sep 3, 2025
- [350A37-1191-21ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180079576120251117201615.0001): Washer, Anti-Corrosive. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 350A37-1191-21 · Aug 13, 2025
- [106-11085-1( )](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186350446520250701134152.0001): Seat Shroud. Magee Plastics Company · PMA PQ0734NE · Replaces 159600-20-0 · May 27, 2025
- [194-11054-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139437084820250701134153.0001): Spacer. Magee Plastics Company · PMA PQ0734NE · Replaces C321A2217201 · May 27, 2025
- [106-11084-1( )](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122148366620250701134152.0001): Fairing Lower Assembly. Magee Plastics Company · PMA PQ0734NE · Replaces 159600-11 · May 27, 2025
- [103-11138-1( )](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110586439920250701134151.0001): Seat Belt Recoil Cover. Magee Plastics Company · PMA PQ0734NE · Replaces 159600-10 · May 27, 2025
- [M2001-22HL](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193756421120250408205153.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 150SG1009-16 150SG1009-20 XL2150SG1009-5 · Mar 27, 2025
- [103-11138-1( )](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134793303220250516193606.0001): Seat Belt Recoil Cover. Magee Plastics Company · PMA PQ0734NE · Replaces 159600-10 · Mar 27, 2025
- [194-11054-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113292288620250516193607.0001): Spacer. Magee Plastics Company · PMA PQ0734NE · Replaces C321A2217201 · Mar 27, 2025
- [106-11085-1( )](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111771260620250516193607.0001): Seat Shroud. Magee Plastics Company · PMA PQ0734NE · Replaces 159600-20-0 · Mar 27, 2025
- [106-11084-1( )](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100466513220250516193606.0001): Fairing Lower Assembly. Magee Plastics Company · PMA PQ0734NE · Replaces 159600-11 · Mar 27, 2025
- [350A37-1212-20ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185513700520250318135941.0001): Cup, Friction. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 350A37-1212-20 · Mar 18, 2025
- [7050A3642021ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182426434520250318135942.0001): Outer Bearing Ring. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 7050A3642021 · Mar 18, 2025
- [7050A3642020ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130446346220250318135942.0001): Bearing, Internal Fenestron. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 7050A3642020 · Mar 18, 2025
- [MDLDL-EC130](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108716155820250213205344.0001): Cabin Air Conditioning System. Air Comm Corporation · PMA PQ0072NM · Modification part · Feb 10, 2025
- [1123470-PR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161940861020250220121049.0001): O-RING. Hutchinson Aerospace & Industry Inc. · PMA PQ0524NM · Replaces 81810-160-24B7 · Dec 5, 2024
- [HF1901001 N03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197115859920250108214715.0001): Medical Equipment Sled Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901028 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195339187720250108214716.0001): Installation; D-Size Oxygen Bottle Mount Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901046 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193493725520250108214717.0001): Oxygen Overboard Vent Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901004 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183114688020250108214715.0001): Litter Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901017 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180497989720250108214715.0001): Storage Box Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901048 N02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178160578820250108214718.0001): EC 130 EMS Plumbing Routing Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901001 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169957953820250108214714.0001): Medical Equipment Sled Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901047 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169143292420250108214717.0001): EC 130 EMS Wire Routing Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901018 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168369356720250108214716.0001): Narcotics Box Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901001 N02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165898373820250108214714.0001): Medical Equipment Sled Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901043 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157011645320250108214717.0001): Installation; Ac Shore Power Door Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901019 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154199275320250108214716.0001): Equipment Mount Provisions Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901039 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145772774120250108214716.0001): Equipment Mount Provisions Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901059 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140736774620250108214718.0001): Equipment Mount Provision Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901055 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136936446920250108214718.0001): LHS Floor Protector Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901057 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135839837920250108214718.0001): Door Post Bumper Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901024 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134038345420250108214716.0001): IV Mount Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901048 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133634093020250108214718.0001): EC 130 EMS Plumbing Routing Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901001 N04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123865200420250108214715.0001): Medical Equipment Sled Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [HF1901014 N01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110615053620250108214715.0001): Equipment Tower Installation Kit. Helifab, Inc. · PMA PQ1023SW · Modification part · Sep 23, 2024
- [740978-PR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139689664320241023112028.0001): O-RING. Hutchinson Aerospace & Industry Inc. · PMA PQ0524NM · Replaces 81810-090-24B7 · Sep 20, 2024
- [1111197-PR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122975441520241023112028.0001): O-RING. Hutchinson Aerospace & Industry Inc. · PMA PQ0524NM · Replaces DHS621-100.03 · Sep 20, 2024
- [AAI- J101236C](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134611615720241001211726.0001): O-Ring. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces J101236C · Aug 27, 2024
- [365A31-1859-20ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168211602920240910143955.0001): Washer, Aluminum. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 365A31-1859-20 · Aug 6, 2024
- [M2002-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113376475720240802183932.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 200SGL1009 · Jun 20, 2024
- [M2001-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100776285420240802183931.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 150SG1009-5 · Jun 20, 2024
- [SA350A32502620](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198344905820240621175555.0001): Adjustment Shim. Seginus Aerospace LLC · PMA PQ4083CE · Replaces 350A32502620 · Jun 6, 2024
- [SA350A58155401](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192401785620240621175555.0001): Half Plate. Seginus Aerospace LLC · PMA PQ4083CE · Replaces 350A58155401 · Jun 6, 2024
- [B60-90-0106](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192303780720260625134358.0001): Male Rod End Assembly. SKF Aeroengine - Falconer (formerly MRC Bearings) · PMA PQ0289NE · Replaces 704A3411403912/6891P · Feb 15, 2024
- [B60-90-0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155464626220260811140226.0001): Sealed Spherical Bearing. SKF Aeroengine · PMA PQ0289NE · Replaces 704A33633124, 11-7775P, 11/7775P · Feb 15, 2024

All of them: https://openairdocs.org/model/airbus-helicopters-ec-130b4/pma.md

## The same model under other registry codes

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

- [Eurocopter EC 130 B4](https://openairdocs.org/model/eurocopter-ec-130-b4): 154 registered aircraft, registry code 8680989
- [Eurocopter France EC 130 B4](https://openairdocs.org/model/eurocopter-france-ec-130-b4): 6 registered aircraft, registry code 8680996

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