# Eurocopter EC 130 T2

- Type: Aircraft model (FAA registry)
- Registry code: 868099A
- Manufacturer (registry): EUROCOPTER
- Model: EC 130 T2
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 8
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 22
- Page: https://openairdocs.org/model/eurocopter-ec-130-t2

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 2026-19-02](https://openairdocs.org/ad/2026-19-02): Main rotor blades · Airbus Helicopters EC130T2. Effective Nov 2, 2026
- [AD 2026-16-10](https://openairdocs.org/ad/2026-16-10): Tail rotor drive shaft · Airbus Helicopters EC130T2. Effective Sep 18, 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 2026-12-08](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 2025-18-13](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 2023-23-01](https://openairdocs.org/ad/2023-23-01): Fuselage Structure · Airbus Helicopters EC130T2. Effective Nov 29, 2023
- [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 2022-06-17](https://openairdocs.org/ad/2022-06-17): Main Rotor Drive System · Airbus Helicopters EC130T2. Effective May 9, 2022
- [AD 2022-05-02](https://openairdocs.org/ad/2022-05-02): Engine Fuel Control/Turbine Engines · Airbus Helicopters AS350B3 and EC130T2. Effective Mar 30, 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 2020-22-20](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 2018-02-02](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 2014-22-51](https://openairdocs.org/ad/2014-22-51): Main Rotor Drive Rotorcraft Cooling Fan System · Airbus Helicopters EC130T2. Effective Feb 25, 2015

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 2023-25-14](https://openairdocs.org/ad/2023-25-14) (historical): Tail Rotor Drive Shaft · Airbus Helicopters EC130T2. Effective Jan 12, 2024
- [AD 2022-27-09](https://openairdocs.org/ad/2022-27-09) (historical): Tail Rotor Drive Shaft · Airbus Helicopters EC130T2. Effective Jan 30, 2023
- [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 2022-01-05](https://openairdocs.org/ad/2022-01-05) (historical): Fuselage Structure · Airbus Helicopters EC130T2. Effective Jan 14, 2022
- [AD 2021-24-06](https://openairdocs.org/ad/2021-24-06) (historical): Fuselage Structure · Airbus Helicopters EC130T2. Effective Dec 9, 2021
- [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 2021-11-25](https://openairdocs.org/ad/2021-11-25) (historical): Engine Fuel Control/Turbine Engines · Airbus Helicopters AS350B3 and EC130T2. Effective Jul 29, 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 2016-08-20](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

## Information bulletins (advisory) (1)

- [SAIB SW-15-20](https://openairdocs.org/saib/SW-15-20): Air Conditioning System Wiring. Issued Aug 13, 2015

## Registered aircraft (22)

- [N11EQ](https://openairdocs.org/aircraft/N11EQ): [Nevada Helicopter Leasing LLC](https://openairdocs.org/faa-owner/NEVADA%20HELICOPTER%20LEASING%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2012, S/N 7485
- [N11FQ](https://openairdocs.org/aircraft/N11FQ): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2013, S/N 7571
- [N11KQ](https://openairdocs.org/aircraft/N11KQ): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2013, S/N 7723
- [N130CS](https://openairdocs.org/aircraft/N130CS): [Indiana Helicopters LLC](https://openairdocs.org/faa-owner/INDIANA%20HELICOPTERS%20LLC), [Fort Wayne, IN](https://openairdocs.org/faa-place/IN/Fort%20Wayne), built 2013, S/N 7660
- [N208SH](https://openairdocs.org/aircraft/N208SH): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2013, S/N 7644
- [N213SH](https://openairdocs.org/aircraft/N213SH): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2013, S/N 7651
- [N216SH](https://openairdocs.org/aircraft/N216SH): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), S/N 7674
- [N247KD](https://openairdocs.org/aircraft/N247KD): [130h LLC](https://openairdocs.org/faa-owner/130H%20LLC), [Springville, UT](https://openairdocs.org/faa-place/UT/Springville), built 2013, S/N 7758
- [N703AC](https://openairdocs.org/aircraft/N703AC): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2013, S/N 7710
- [N741AC](https://openairdocs.org/aircraft/N741AC): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2014, S/N 7845
- [N813AM](https://openairdocs.org/aircraft/N813AM): [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village), built 2013, S/N 7735
- [N832GC](https://openairdocs.org/aircraft/N832GC): [Zuni LLC](https://openairdocs.org/faa-owner/ZUNI%20LLC), [Kirkland, WA](https://openairdocs.org/faa-place/WA/Kirkland), built 2013, S/N 7667
- [N833GC](https://openairdocs.org/aircraft/N833GC): [Xebec LLC](https://openairdocs.org/faa-owner/XEBEC%20LLC), [Kirkland, WA](https://openairdocs.org/faa-place/WA/Kirkland), built 2013, S/N 7747
- [N834GC](https://openairdocs.org/aircraft/N834GC): [American Helicopters LLC](https://openairdocs.org/faa-owner/AMERICAN%20HELICOPTERS%20LLC), [Kirkland, WA](https://openairdocs.org/faa-place/WA/Kirkland), built 2014, S/N 7829
- [N872MH](https://openairdocs.org/aircraft/N872MH): [Mustang Leasing LLC](https://openairdocs.org/faa-owner/MUSTANG%20LEASING%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2012, S/N 7355
- [N873MH](https://openairdocs.org/aircraft/N873MH): [Mustang Leasing LLC](https://openairdocs.org/faa-owner/MUSTANG%20LEASING%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2013, S/N 7532
- [N875MH](https://openairdocs.org/aircraft/N875MH): [Mustang Leasing LLC](https://openairdocs.org/faa-owner/MUSTANG%20LEASING%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2013, S/N 7592
- [N876MH](https://openairdocs.org/aircraft/N876MH): [Mustang Leasing LLC](https://openairdocs.org/faa-owner/MUSTANG%20LEASING%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2013, S/N 7621
- [N877MH](https://openairdocs.org/aircraft/N877MH): [Mustang Leasing LLC](https://openairdocs.org/faa-owner/MUSTANG%20LEASING%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2013, S/N 7637
- [N878MH](https://openairdocs.org/aircraft/N878MH): [Mustang Leasing LLC](https://openairdocs.org/faa-owner/MUSTANG%20LEASING%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2013, S/N 7779
- [N922RJ](https://openairdocs.org/aircraft/N922RJ): [Enloe Medical Center DBA](https://openairdocs.org/faa-owner/ENLOE%20MEDICAL%20CENTER%20DBA), [Chico, CA](https://openairdocs.org/faa-place/CA/Chico), built 2013, S/N 7628
- [N94AS](https://openairdocs.org/aircraft/N94AS): [Amara Sky LLC](https://openairdocs.org/faa-owner/AMARA%20SKY%20LLC), [Newark, DE](https://openairdocs.org/faa-place/DE/Newark), built 2012, S/N 7507

## NTSB investigations

None matched to aircraft with this model.

## 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.

- [Incident 20141125023549I](https://openairdocs.org/incident/20141125023549I), Nov 25, 2014: Eurocopter EC 130 T2 (N876MH), Peach Springs, AZ, Minor damage. 11/25/2014 ? Received phone call from poi maverick helicopters, reference helicopter, N876MH an EC-130-T2 model helicopter, operated by maverick helicopters…

## Service difficulty reports (130, newest 50)

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

- [SDR QMLA2026102720082](https://openairdocs.org/sdr/QMLA2026102720082), Oct 25, 2026: GENERATOR. FAULTED. GENERATOR LIGHT CAME ON IN FLIGHT, AMPS DROPPED TO 0, VOLTAGE DROPPED TO 24.8V. GENERATOR WAS TURNED OFF FOR A MINUTE, THEN RESET AND TURNED BACK ON. GENERATOR 
- [SDR QMLA 202608272006](https://openairdocs.org/sdr/QMLA%20202608272006), Aug 27, 2026: MAIN ROTOR. FOD. JUST PRIOR TO LANDING, A SMALL PLASTIC BAG FLOATED UP AND INTO THE MAIN ROTOR SYSTEM. IT BLEW OUT ALMOST IMMEDIATELY AFTER THE FACT. A NORMAL LANDING AND SHUTDO
- [SDR 2A6D20260814](https://openairdocs.org/sdr/2A6D20260814), Aug 14, 2026: FRAME. CORRODED. CORROSION ON THE COLLECTIVE SPLIT FRAME ON FWD AND AFT SIDE OF OPENING.
- [SDR 2A6D20260813002](https://openairdocs.org/sdr/2A6D20260813002), Aug 13, 2026: RIB. CHAFED. CHAFE DAMAGE ON BL 1263 RIB ON RH SIDE OF HORIZONTAL STABILIZER.
- [SDR 2A6D20260813001](https://openairdocs.org/sdr/2A6D20260813001), Aug 13, 2026: CROSSBEAM. CHAFED. GOUGE/CHAFE DAMAGE TO THE AFT LANDING GEAR ATTACHMENT FWD CROSSBEAM AND SUPPORT ANGLE.
- [SDR QMLA2026071820047](https://openairdocs.org/sdr/QMLA2026071820047), Jul 15, 2026: BEARING. FAULTED. PILOTS REPORT "AFTER ILLUMINATION OF THE HYD2 AND SERVO LIGHTS, NURSE AND MEDIC SAW WHITISH GRAY SMOKE FROM VICINITY IN FRONT OF THE CABIN TDFM RADIO CONTROL HE
- [SDR PG9A2026070600568](https://openairdocs.org/sdr/PG9A2026070600568), Jul 4, 2026: HYDRAULIC SYSTEM. FAULTED. AIRCRAFT WAS DOING LEFT 180 AT QUARTERMASTER CANYON FOR BURNT SPRINGS PILOT STARTED TO NOTICE A STRANGE ODOR IN THE AIRCRAFT. ABOUT 5 SECONDS LATER, A TON OF WH
- [SDR 2A6R2026031675205](https://openairdocs.org/sdr/2A6R2026031675205), Mar 16, 2026: LANDING GEAR. CRACKED. DURING INSPECTION SEVERAL COMPONENTS OF THE LANDING GEAR WERE FOUND DAMAGED BEYOND LIMITS. THE LEFT SKID (350A41-6002-0201) HAD A CRACK MEASURING 1.14''. THE RI
- [SDR 2A6R2026040675204](https://openairdocs.org/sdr/2A6R2026040675204), Mar 16, 2026: SKIN. CRACKED. DURING AN INSPECTION A CRACK WAS FOUND ON THE TOP OF THE HORIZONAL STABILIZER MEASURING 4.25 IN LONG. THE HORIZONTAL WAS REMOVED AND REPLACED. FOR MORE INFORMAT
- [SDR 2A6R2026031675203](https://openairdocs.org/sdr/2A6R2026031675203), Mar 16, 2026: STATOR. CORRODED. DURING A 12-YEAR INSPECTION, THE STATOR WAS REMOVED AND FOUND TO HAVE MULTIPLE LEGS WITH CORRODED BASES. THE DEPTH OF CORROSION VARIED FROM .020 TO .030 DEEP. P
- [SDR 2A6R2026031675202](https://openairdocs.org/sdr/2A6R2026031675202), Mar 16, 2026: XMSN DECK. CHAFED. DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK FWD DOUBLER AND THE AFT DOUBLER IN THE FORM OF SEVERAL CHAFE DAMAGE AREAS. THE CHAFE DAMAGE AREAS ARE ALL LOCATED
- [SDR 2A6R2026031675201](https://openairdocs.org/sdr/2A6R2026031675201), Mar 16, 2026: SUPPORT FRAME. DAMAGED. DAMAGE TO THE LEFT EDGE FRAME AND RT EDGE FRAME, IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAME
- [SDR 2A6D20260305001](https://openairdocs.org/sdr/2A6D20260305001), Mar 3, 2026: FUEL LINE. BENT. WHILE HOVER TAXIING THE AIRCRAFT DURING CHECK FLIGHTS, THE PILOT REPORTED A FUEL P LIGHT AND TURNED THE AIRCRAFT AROUND TO RETURN TO THE RAMP. DURING THE FLIGHT
- [SDR QMLA2025101420105](https://openairdocs.org/sdr/QMLA2025101420105), Oct 14, 2025: UNKNOWN. ODOR. STRONG BURNING SMELL IN COCKPIT.
- [SDR QMLA2025100620099](https://openairdocs.org/sdr/QMLA2025100620099), Oct 5, 2025: ICS BOX. FAULTED. HEAVY STATIC IN ICS SYSTEM. PROBLEM OCCURRED APPROXIMATELY 10-12 MINUTES IN FLIGHT AND THEN DISAPPEARED. INSPECTED AUDIO CONTROLLER/INTERCOM HARNESS AND PINS, C
- [SDR 2A6R 09222025743](https://openairdocs.org/sdr/2A6R%2009222025743), Sep 22, 2025: SKIN. CRACKED. DURING THE 600 HOUR / 24 MONTH AIRFRAME INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM SKIN (TAILBOOM P/N: 350A2307150002 S/N: TB7538) ON THE UPPER R/H CORNER OF
- [SDR QMLA2025092220097](https://openairdocs.org/sdr/QMLA2025092220097), Sep 22, 2025: SKIN. CRACKED. DURING THE 600 HOUR / 24 MONTH AIRFRAME INSPECTION, A CRACK WAS FOUND ON THE TAILBOOM SKIN (TAILBOOM P/N: 350A2307150002 S/N: TB7538) ON THE UPPER R/H CORNER OF
- [SDR QMLA2025081320087](https://openairdocs.org/sdr/QMLA2025081320087), Aug 13, 2025: MOTOR. FAILED. ENROUTE BACK TO BASE AFTER A TRANSPORT, THE CREW SMELLED A BURNING ELECTRICAL SMELL. SMOKE IN THE COCKPIT EP WAS FOLLOWED AND IT WAS DETERMINED THAT THE SMELL W
- [SDR QMLA2025072520078](https://openairdocs.org/sdr/QMLA2025072520078), Jul 25, 2025: WIRE. BROKEN. GENERATOR LIGHT ILLUMINATED IN FLIGHT AND WOULD NOT RESET. LANDED AT A NEARBY AIRPORT. FOUND WIRE BROKEN AT TERMINAL ON THE GENERATOR.
- [SDR JBZA20250710001](https://openairdocs.org/sdr/JBZA20250710001), Jul 2, 2025: ELEC CONNECTOR. ARCED. DURING FINAL APPROACH TO BASE AN ELECTRICAL SMELL WAS DETECTED COMING FROM THE CENTER CONSOLE TDFM / SKY TRAC PANELS. DURING EVALUATION OF THE SYSTEMS IT WAS DI
- [SDR 2A6D20250502001](https://openairdocs.org/sdr/2A6D20250502001), Jun 2, 2025: XMSN DECK. CHAFED. GOUGING- TOOL DAMAGE WAS DISCOVERED ON THE LH SIDE OF THE TRANSMISSION DECK. THE DEPTH IS APPROXIMATELY 0.026". THE MAXIMUM APPROXIMATE LENGTH IS .6 AND WIDTH I
- [SDR EVCA20250502001](https://openairdocs.org/sdr/EVCA20250502001), May 1, 2025: STRUCTURE. CRACKED. CRACK EXCEEDING THE MANUFACTURES LIMITS IN THE HORIZONTAL STABILIZER
- [SDR QMLA2025040920046](https://openairdocs.org/sdr/QMLA2025040920046), Apr 7, 2025: WIRE. SHORTED. ARCING OM ENGINE DECK, FOUND STARTER WIRE ELECTRICAL SHORT TO ENGINE COWLING AND FUSELAGE.
- [SDR QMLA2025022520026](https://openairdocs.org/sdr/QMLA2025022520026), Feb 25, 2025: FAN. DAMAGED. AFTER LIFTING GENESIS EAST MED CENTER AND HEADING TO IOWA CITY. THE AV FAN CAME ON FOLLOWED BY A STRONG BURNING SMELL. FOUND INOP AVIONICS FAN RIGHT SIDE UNDER 
- [SDR QMLA2024110420142](https://openairdocs.org/sdr/QMLA2024110420142), Oct 31, 2024: CONNECTOR. CONTAMINATED. FAULT PRESENTED IN FLIGHT FL1 FAIL OVERLIMIT DETECTED, FAILURE DETECTED MSG, THIS OCCURRED ON THE WAY TO PICK UP PATIENT FROM NEARBY HOSPITAL AND PILOT RETURNED
- [SDR QMLA2024090620108](https://openairdocs.org/sdr/QMLA2024090620108), Sep 5, 2024: ENGINE. POWER LOSS. ON PICKUP I NOTICED THE FLI WAS HIGHER THAN NORMAL, I CAN USUALLY LIFTOFF AT 7/7.5 ON THE FLI AT MGW BUT THIS TIME I WAS 100LBS UNDER MGW AND IT DIDNT LIFT OFF 
- [SDR 2A6D20240614001](https://openairdocs.org/sdr/2A6D20240614001), Jun 14, 2024: ATTACH ANGLE. CRACKED. DAMAGE TO THE BAGGAGE COMPARTMENT LH FWD LOWER ANGLE (P/N: 350A210053.28) IN THE FORM OF GOUGE/CRACK. THE GOUGE/CRACK DAMAGE MEASURED TO BE APPROXIMATELY 0.13” 
- [SDR QMLA2024060520058](https://openairdocs.org/sdr/QMLA2024060520058), Jun 5, 2024: ELECTRICAL SYS. BURNED. DURING NORMAL STARTUP AFTER N1 REACHED 67% AND THE GENERATOR SWITCH WAS TURNED ON. THERE WAS A BURNING SMELL OF BURNED RUBBER, AND THEN SMOKE STARTED COMING OUT
- [SDR 2A6D20240528001](https://openairdocs.org/sdr/2A6D20240528001), May 28, 2024: FRAME. CORRODED. DAMAGE TO THE AFT UPPER FRAME (P/N: 350A21-1242.35) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS ON THE UPPER FLANGE OF FRAME AT LH AND RH BOTTOM SIDE NEAR
- [SDR QMLA2024051720053](https://openairdocs.org/sdr/QMLA2024051720053), May 14, 2024: INDICATOR. FAILED. AIRSPEED INDICATOR FAILED IN FLIGHT (BOTH G500 AND BACKUP INDICATOR). UPON LANDING AT BASE MECHANIC FOUND MUD DOBBER IN PITOT TUBE, BUG/DEBRIS WAS REMOVED AND S
- [SDR 2A6D20240509003](https://openairdocs.org/sdr/2A6D20240509003), May 9, 2024: FLOORBEAM. CORRODED. DAMAGE IS ON THE LH CABIN FLOOR EDGE FITTING (P/N: 350A214753.20) IN THE FORM OF CORROSION AND CRACKS. THE LH FITTING PLATE IS EXCESSIVELY CORRODED AND THE CRAC
- [SDR 2A6D20240509002](https://openairdocs.org/sdr/2A6D20240509002), May 9, 2024: BONDING PLATE. CORRODED. DAMAGE IS ON THE TAIL BOOM VHF ANTENNA BASE PLATE (P/N: 350A65-1707.00) IN THE FORM OF CORROSION. THE BASE PLATE IS EXCESSIVELY CORRODED AND DEPTH OF THE DAMAGE
- [SDR 2A6D20240509001](https://openairdocs.org/sdr/2A6D20240509001), May 9, 2024: BULKHEAD. CORRODED. THE UPPER 7° BULKHEAD DOUBLER (PN: 350A21-0849.20) IS CORRODED AT THE LOCATION OF A PASS-THRU HOLE. THE DAMAGE AREA WAS REPORTED TO BE 0.80” X 0.50” AND 0.030” 
- [SDR 2A6D20240508003](https://openairdocs.org/sdr/2A6D20240508003), May 8, 2024: CROSSTUBE. CORRODED. THE AFT LANDING GEAR CROSSTUBE FITTING (PN: 350A21-0960.20) IS CORRODED IN MULTIPLE AREAS ON THE LOWER SURFACE. THE DEEPEST DAMAGE AREA WAS REPORTED TO BE 0.022
- [SDR 2A6D20240508002](https://openairdocs.org/sdr/2A6D20240508002), May 8, 2024: CROSSBEAM. CORRODED. THE RH X2244 CROSSBEAM (PN: 350A21-0861.20) IS CORRODED IN AN AREA ON THE LOWER OUTBOARD CORNER OF THE CROSSBEAM. THE DAMAGE WAS REPORTED TO BE 0.572” X 0.179” 
- [SDR 2A6D20240508001](https://openairdocs.org/sdr/2A6D20240508001), May 8, 2024: CROSSBEAM. CORRODED. THE RH X1790 CROSSBEAM (PN: 350A21-0572.20) IS CORRODED IN AN AREA WHERE IT CONTACTS THE RH Y400 BEAM (PN: 350A21-0587.20)
- [SDR QMLA2024043020045](https://openairdocs.org/sdr/QMLA2024043020045), Apr 25, 2024: SKIN. CRACKED. CRACK FOUND ON TOP OF THE HORIZONTAL STABILIZER, CURRENTLY WORKING WITH SERVICE ENGINEERING DEPT. TO DETERMINE THE REPAIRABLE LIMITS.
- [SDR 2A6D20240425009](https://openairdocs.org/sdr/2A6D20240425009), Apr 25, 2024: SKIN PANEL. CORRODED. CORROSION DAMAGE ON THE FWD UPPER SKIN MEASURED TO BE APPROXIMATELY 0.80” X 0.60” X 0.003”
- [SDR 2A6D20240425008](https://openairdocs.org/sdr/2A6D20240425008), Apr 25, 2024: STIFFENER. CORRODED. DAMAGE TO THE TAIL BOOM LH FWD STIFFENER MEASURED TO BE APPROXIMATELY 0.85” X 0.85” X 0.0125” IN THE FORM OF CORROSION.
- [SDR 2A6D20240425007](https://openairdocs.org/sdr/2A6D20240425007), Apr 25, 2024: ATTACH ANGLE. CORRODED. REAR LANDING GEAR ATTACHMENT LOWER ANGLE HAS DAMAGE IN THE FORM OF CORROSION. THE DAMAGE NEAR THE ANGLE OVERLAPS WITH MACHINED FRAME AND AFT LOWER BELLY FAIRING
- [SDR 2A6D20240425006](https://openairdocs.org/sdr/2A6D20240425006), Apr 25, 2024: CRADLE. CORRODED. RH AFT FUEL CRADLE REINFORCEMENTS HAS DAMAGE IN THE FORM OF CORROSION. THE RH AFT CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 2.1” X 0.80” X 0.009”.
- [SDR 2A6D20240425005](https://openairdocs.org/sdr/2A6D20240425005), Apr 25, 2024: CRADLE. CORRODED. THE LH FWD FUEL CRADLE REINFORCEMENTS HAD DAMAGE IN THE FORM OF CORROSION. THE LH FWD CORROSION DAMAGE MEASURED TO BE APPROXIMATELY 1.0” X 0.80” X 0.008”.
- [SDR 2A6D20240425004](https://openairdocs.org/sdr/2A6D20240425004), Apr 25, 2024: SKIN PANEL. CORRODED. DAMAGE IS ON THE AFT FUSELAGE RH SIDE SKIN PANEL (P/N: 350A210046-21 IN THE FORM OF CORROSION. THE RH SIDE SKIN DAMAGE IS NEAR TOP EDGE WHERE ENGINE DECK OVERLA
- [SDR 2A6D20240425003](https://openairdocs.org/sdr/2A6D20240425003), Apr 25, 2024: SKIN PANEL. CORRODED. FIRST DAMAGE IS ON THE AFT FUSELAGE LH SIDE SKIN PANEL IN THE FORM OF CORROSION. THE LH SIDE SKIN DAMAGE IS NEAR TOP EDGE WHERE ENGINE DECK OVERLAPS AND MEASURE
- [SDR 2A6D20240425002](https://openairdocs.org/sdr/2A6D20240425002), Apr 25, 2024: BRACE. CORRODED. DAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CORRODED AREA IS LOCATED AT THE BOTTOM END
- [SDR 2A6D20240425001](https://openairdocs.org/sdr/2A6D20240425001), Apr 25, 2024: WEB. CORRODED. DAMAGE TO THE LOWER CENTER WEB IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LIGHTENING HOLES AND MEASURED TO BE THROUG
- [SDR 2A6D20240320001](https://openairdocs.org/sdr/2A6D20240320001), Mar 20, 2024: SUPPORT ANGLE. CORRODED. EXFOLIATION CORROSION LOCATED ON FWD. L/H SIDE STIFFENER OF MASTER ELECTRICAL BOX.
- [SDR M3XA2024012219001](https://openairdocs.org/sdr/M3XA2024012219001), Jan 19, 2024: B-NUT. LOOSE. PILOT REPORTED ON POST FLIGHT INSPECTION, DISCOVERED OIL ON OUTSIDE OF ENGINE COWLING, DRAINING FROM ENGINE DECK DRAIN LINES AND SMOKE COMING OFF OUTSIDE OF EXH
- [SDR QMLA202312231222](https://openairdocs.org/sdr/QMLA202312231222), Dec 23, 2023: UNKNOWN. UNKNOWN. DURING CLIMB OUT THE AIRCRAFT HAD SIGNIFICANT INCREASED RIGHT CYCLIC PRESSURE THAT SUDDENLY RELEASED CAUSING THE AIRCRAFT TO SLIGHTLY JOLT TO THE RIGHT. THE FLI
- [SDR QMLA2023111420103](https://openairdocs.org/sdr/QMLA2023111420103), Nov 13, 2023: MOTOR. ODOR. DURING SHUT DOWN AT JACKSON GENERAL HOSPITAL AFTER DROPPING OFF PATIENT, SMELLED AN ELECTRICAL BURNING SMELL COMING FROM COCKPIT. REPLACED BLOWER MOTOR.

All 130: https://openairdocs.org/model/eurocopter-ec-130-t2/reports.md

## STCs that may be installed (OpenAirDocs) (78, 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 SR09502RC](https://openairdocs.org/stc/SR09502RC): Installation of Air Methods Corporation Emergency Medical System and Avionics Package. Air Methods LLC
- [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 SR11944WI](https://openairdocs.org/stc/SR11944WI): Installation of a Garmin GFC 600H Helicopter Flight Control System. Garmin International 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 SR11839IB](https://openairdocs.org/stc/SR11839IB): Manufacture and Installation of Seat Refurbishment. Icarus Aero Inc
- [STC SR00216IB](https://openairdocs.org/stc/SR00216IB): Installation and Configuration of the Standard Interior Modification. Airbus Helicopters Canada Limited
- [STC SR04610NY](https://openairdocs.org/stc/SR04610NY): Installation of Outerlink IRIS SATCOM, Flight Data Monitoring and Tracking System. Outerlink Corporation
- [STC SR09909AC](https://openairdocs.org/stc/SR09909AC): Installation of Emergency Medical Service (EMS) Interior. Kilroy Aviation LLC
- [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 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 SR03640AT](https://openairdocs.org/stc/SR03640AT): Installation of miscellaneous windows. Tech-Tool Plastics Inc
- [STC SR04644NY](https://openairdocs.org/stc/SR04644NY): Installation of Airframe-Mounted Fuel Filter. Airbus Helicopters Canada Limited
- [STC SR04590NY](https://openairdocs.org/stc/SR04590NY): Heavy-Duty Battery Installation must be in accordance with Airbus Helicopters Master Drawing List MDL-17-002, Revision A, Transport Canada Civil Aviation (TCCA) approved December 16, 2019, or later TCCA approved revision. Airbus Helicopters Canada Limited
- [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 SR11198DS](https://openairdocs.org/stc/SR11198DS): Installation of Garmin Optional Features. Airbus Helicopters Inc
- [STC SR09511DS](https://openairdocs.org/stc/SR09511DS): Installation of LED Taxi and Landing Lights with Optional Pulse. Airbus Helicopters Inc
- [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 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 SR04169CH](https://openairdocs.org/stc/SR04169CH): Installation of a Medical Interior. LifePort LLC
- [STC SR00871DE](https://openairdocs.org/stc/SR00871DE): Installation of Garmin GTS 800 Traffic Avoidance System (TAS). 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 SR04297NY](https://openairdocs.org/stc/SR04297NY): Installation of the Alternate Standby Altimeter. Airbus Helicopters Canada Limited
- [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
- [STC SR00828DE](https://openairdocs.org/stc/SR00828DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the Garmin G330ES or G33H ES Transponder and qualified position sensor. Peregrine
- [STC SR02609SE](https://openairdocs.org/stc/SR02609SE): Installation of Cable Cutters. Dart Aerospace USA Inc
- [STC SR03077NY](https://openairdocs.org/stc/SR03077NY): Installation of a HELICOM V2 NUM System or HELICOM V2+ NUM System for tracking a set of flight and system parameters during operation of the rotorcraft. International Services Electronique Informatique

All 78: https://openairdocs.org/model/eurocopter-ec-130-t2/stcs.md

## PMA parts (OpenAirDocs) (387, 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
- [46870-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169946283120260610102754.0001): CCP, SWITCH CTRL BOX, EURO. Korry Electronics Co · PMA PQ0134NM · Replaces 46870-001 · Feb 3, 2026
- [EC120-1006-34](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190298803120251209183244.0001): Window Assy,Fwd Door RH. Tech Tool Plastics Inc · PMA PQ0504SW · Modification part · Dec 8, 2025
- [EC120-1006-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166216685320251209183243.0001): Window Assy,Fwd Door RH. Tech Tool Plastics Inc · PMA PQ0504SW · Modification part · Dec 8, 2025
- [EC120-1005-31](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147732571720251209183243.0001): Window Assy,Aft Door LH. Tech Tool Plastics Inc · PMA PQ0504SW · Modification part · Dec 8, 2025
- [EC120-1004-31](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143467397320251209183242.0001): Window Assy,Fwd Door LH. Tech Tool Plastics Inc · PMA PQ0504SW · Modification part · Dec 8, 2025
- [EC120-1004-33](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139086992320251209183243.0001): Window Assy,Fwd Door LH. Tech Tool Plastics Inc · PMA PQ0504SW · Modification part · Dec 8, 2025
- [EC120-1007-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136023562320251209183244.0001): Window Assy,Aft Door RH. Tech Tool Plastics Inc · PMA PQ0504SW · Modification part · Dec 8, 2025
- [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
- [117-02189-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194586209020250725112820.0001): ROD ASSEMBLY, GFC 600H, PITCH CONTROL, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [340-00305-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192183780120250725112821.0001): SWITCH, PUSHBUTTON, BLUE, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [117-02189-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184846737920250725112820.0001): ROD ASSEMBLY, GFC 600H, YAW CONTROL, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [117-02189-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183685391520250725112820.0001): ROD ASSEMBLY, GFC 600H, ROLL CONTROL, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04601-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175128227020250725112819.0001): COVER 2 ASSEMBLY RH, PEDAL, AIRBUS EC130, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [117-02312-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168489325020250725112821.0001): CONNECTOR, ROLL CONTROL ROD, GFC 600H, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04435-20](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163968900520250725112818.0001): BRACKET, CONNECTOR, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04601-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163292666520250725112819.0001): COVER 2 ASSEMBLY LH, PEDAL, AIRBUS EC130, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04430-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160119196320250725112817.0001): BRACE, LRU RACK, STEP 2, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [117-01222-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159213254720250725112820.0001): MOUNT, SENSOR, COLLECTIVE POSITION, AIRBUS H125. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04368-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155160817420250725112817.0001): BRACKET ASSEMBLY, ROLL SERVO, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [161-06452-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154325765520250725112821.0001): PLACARD SET, GFC 600H, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04435-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149093591120250725112818.0001): BRACKET, POSITION SENSOR, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04601-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142413281420250725112819.0001): COVER 1 ASSEMBLY RH, PEDAL, AIRBUS EC130, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04367-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136816308320250725112816.0001): BRACKET ASSEMBLY, PITCH SERVO, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04601-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132022399420250725112818.0001): CONTACT, WIRED, PEDAL, AIRBUS EC130, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [117-02190-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128404687220250725112821.0001): CONNECTOR, YAW CONTROL ROD, GFC 600H, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04435-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125322138920250725112817.0001): BRACKET, RELAY, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [011-05126-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125105670520250725112816.0001): Conn Kit, String Pot, Sub-Assy (FAA-PMA). Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04430-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125026810820250725112817.0001): BRACE, LRU RACK, STEP 3, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04435-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121779264320250725112818.0001): SUPPORT, WIRING HARNESS, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04601-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117679786620250725112818.0001): COVER 1 ASSEMBLY LH, PEDAL, AIRBUS EC130, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04367-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115551784420250725112816.0001): SUPPORT ASSEMBLY, PITCH SERVO, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [340-00304-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109912967720250725112821.0001): SWITCH, LED, HFCS ON-OFF, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04369-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109515393120250725112817.0001): BRACKET ASSEMBLY, YAW SERVO, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [115-04601-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105360801020250725112819.0001): WIRE GUIDE, PEDAL, AIRBUS EC130, PMA. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 2025
- [117-02188-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103630550820250725112820.0001): LEVER, PITCH CONTROL, GFC 600H, PMA, AIRBUS EC130. Garmin International Inc · PMA PQ3742CE · Modification part · Jun 27, 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
- [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

All of them: https://openairdocs.org/model/eurocopter-ec-130-t2/pma.md

## The same model under other registry codes

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

- [Airbus Helicopters EC 130 T2](https://openairdocs.org/model/airbus-helicopters-ec-130-t2): 124 registered aircraft, registry code 1145302

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