# Airbus Helicopters EC120B

- Type: Aircraft model (FAA registry)
- Registry code: 868099C
- Manufacturer (registry): AIRBUS HELICOPTERS
- Model: EC120B
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 5
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS R0001RD](https://openairdocs.org/tcds/R0001RD) (OpenAirDocs)
- Holder: Airbus Helicopters
- Registered aircraft: 1
- Page: https://openairdocs.org/model/airbus-helicopters-ec120b

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 2026-20-03](https://openairdocs.org/ad/2026-20-03): Placards and Markings · Airbus Helicopters AS350B, AS350BA, AS350B1 and 11 more. Effective Nov 5, 2026
- [AD 2026-14-02](https://openairdocs.org/ad/2026-14-02): Indication/Recording System · Airbus Helicopters AS350B2, AS350B3, EC120B and 1 more. Effective Aug 14, 2026
- [AD 2026-04-07](https://openairdocs.org/ad/2026-04-07): Rotorcraft Flight Control · Airbus Helicopters EC120B. Effective Apr 7, 2026
- [AD 2025-20-10](https://openairdocs.org/ad/2025-20-10): Tail Rotor System · Airbus Helicopters EC120B. Effective Dec 30, 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 2025-05-12](https://openairdocs.org/ad/2025-05-12): Main Rotor Head · Airbus Helicopters EC120B. Effective May 8, 2025
- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024
- [AD 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 2022-02-13](https://openairdocs.org/ad/2022-02-13): Rotorcraft Tail Boom · Airbus Helicopters EC120B. Effective Mar 17, 2022
- [AD 2022-02-06](https://openairdocs.org/ad/2022-02-06): Tail Rotor Blades · Airbus Helicopters EC120B. Effective Mar 17, 2022
- [AD 2021-24-08](https://openairdocs.org/ad/2021-24-08): Main Rotor System · Airbus Helicopters EC120B. Effective Jan 14, 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 2020-25-11](https://openairdocs.org/ad/2020-25-11): Doors · Airbus Helicopters EC120B and EC130B4. Effective Jan 21, 2021
- [AD 2020-12-02](https://openairdocs.org/ad/2020-12-02): Tail rotor blades · Airbus Helicopters EC120B. Effective Jul 13, 2020
- [AD 2017-26-04](https://openairdocs.org/ad/2017-26-04): Emergency Equipment · Airbus Helicopters EC120B. Effective Jan 24, 2018
- [AD 2017-06-11](https://openairdocs.org/ad/2017-06-11): failure of an air conditioner compressor drive pulley (pulley) or tail rotor output wheel (wheel) · Airbus Helicopters EC120B with STC SR00491DE. Effective May 8, 2017
- [AD 2016-12-13](https://openairdocs.org/ad/2016-12-13): Engine/Transmission Coupling--Coupling Tube, Engine Mount, and Engine Mount Base · Airbus Helicopters EC120B. Effective Jul 27, 2016
- [AD 2015-26-04](https://openairdocs.org/ad/2015-26-04): Cabin Equipment/Furnishings · Airbus Helicopters EC120B. Effective Feb 4, 2016
- [AD 2013-16-19](https://openairdocs.org/ad/2013-16-19): Emergency Flotation Section · Airbus Helicopters EC120B and EC130B4. Effective Sep 27, 2013
- [AD 2011-21-18](https://openairdocs.org/ad/2011-21-18): Cyclic Control Stick · Airbus Helicopters EC120B. Effective Dec 20, 2011
- [AD 2011-11-04](https://openairdocs.org/ad/2011-11-04): Contaminated Gas · Airbus Helicopters AS355E, AS355F, AS355F1 and 12 more. Effective Jun 17, 2011
- [AD 2005-09-05](https://openairdocs.org/ad/2005-09-05): Tail rotor drive shaft (drive shaft) · Airbus Helicopters EC120B. Effective Jun 13, 2005
- [AD 2003-22-10](https://openairdocs.org/ad/2003-22-10): Electrical bonding braid (bonding braid) that is installed on the left cyclic pitch control stick base · Airbus Helicopters EC120B. Effective Dec 10, 2003
- [AD 2003-08-04](https://openairdocs.org/ad/2003-08-04): Cyclic pitch flight control torque tube · Airbus Helicopters EC120B. Effective May 22, 2003
- [AD 2002-15-08](https://openairdocs.org/ad/2002-15-08): Cargo Hooks · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 21 more. Effective Sep 6, 2002
- [AD 2001-24-08](https://openairdocs.org/ad/2001-24-08): Cabin Sliding Door Rail · Airbus Helicopters EC120B. Effective Jan 7, 2002

Historical (superseded or no longer in force):

- [AD 2021-26-07](https://openairdocs.org/ad/2021-26-07) (historical): Tail rotor system · Airbus Helicopters EC120B. Effective Jan 27, 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 2021-04-21](https://openairdocs.org/ad/2021-04-21) (historical): Main Rotor System · Airbus Helicopters EC120B. Effective May 7, 2021
- [AD 2020-11-05](https://openairdocs.org/ad/2020-11-05) (historical): Tail rotor system · Airbus Helicopters EC120B. Effective Jun 8, 2020
- [AD 2015-24-51](https://openairdocs.org/ad/2015-24-51) (historical): Air Comm Corporation (Air Comm) air conditioning kit · Airbus Helicopters EC120B with STC SR00491DE
- [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 2010-05-51](https://openairdocs.org/ad/2010-05-51) (historical): Main rotor hub · Airbus Helicopters EC120B. Effective May 14, 2010
- [AD 2009-25-07](https://openairdocs.org/ad/2009-25-07) (historical): Emergency Floatation Gear Lighting and Ancillary Control Unit (LACU) · Airbus Helicopters EC120B. Effective Dec 28, 2009
- [AD 2008-10-01](https://openairdocs.org/ad/2008-10-01) (historical): Spherical thrust bearings · Airbus Helicopters EC120B. Effective May 21, 2008
- [AD 2002-13-11](https://openairdocs.org/ad/2002-13-11) (historical): Yaw control · Airbus Helicopters EC120B. Effective Aug 13, 2002
- [AD 2001-04-12](https://openairdocs.org/ad/2001-04-12) (historical): Main Gearbox Coupling Tube Assembly · Airbus Helicopters EC120B. Effective Mar 20, 2001
- [AD 2000-17-07](https://openairdocs.org/ad/2000-17-07) (historical): Cabin Sliding Door · Eurocopter France EC120B. Effective Sep 12, 2000
- [AD 2000-05-17](https://openairdocs.org/ad/2000-05-17) (historical): Engine Coupling Tube · Airbus Helicopters EC120B. Effective Mar 27, 2000
- [AD 99-19-23](https://openairdocs.org/ad/99-19-23) (historical): Engine Coupling Tube Inspection · Eurocopter France EC120B. Effective Oct 19, 1999

## Information bulletins (advisory) (5)

- [SAIB AIR-21-09](https://openairdocs.org/saib/AIR-21-09): LANDING GEAR SYSTEM, Landing gear skid tube. Issued Jun 10, 2021
- [SAIB SW-15-20](https://openairdocs.org/saib/SW-15-20): Air Conditioning System Wiring. Issued Aug 13, 2015
- [SAIB SW-12-17](https://openairdocs.org/saib/SW-12-17): Autopilot System. Issued Feb 3, 2012
- [SAIB SW-04-71](https://openairdocs.org/saib/SW-04-71): . Issued Jul 14, 2004
- [SAIB SW-04-35](https://openairdocs.org/saib/SW-04-35): . Issued Dec 19, 2003

## Registered aircraft (1)

- [N520DT](https://openairdocs.org/aircraft/N520DT): [City Of San Antonio Texas](https://openairdocs.org/faa-owner/CITY%20OF%20SAN%20ANTONIO%20TEXAS), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), built 2015, S/N 1688

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (222, newest 50)

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

- [SDR CA190604025](https://openairdocs.org/sdr/CA190604025), May 30, 2019: SWASHPLATE. DAMAGED. (CAN) DURING A 500FH INSPECTION OF THE SWASHPLATE ASSEMBLY, IT WAS NOTED THAT INJECTION OF GREASE INTO THE BALL BEARING WAS NOT POSSIBLE. UPON DISASSEMBLY FOR F
- [SDR CA190509010](https://openairdocs.org/sdr/CA190509010), May 8, 2019: BEARING. ROUGH. (CAN) EXCESSIVE HEAT WAS NOTED DURING THE POST MAINTENANCE CHECK FOR HEATING IN THE FORWARD TAIL ROTOR SHAFT BEARING. DURING DISASSEMBLY OF THE BEARING UNIT IT 
- [SDR CA190423019](https://openairdocs.org/sdr/CA190423019), Mar 29, 2019: BEARING. SEIZED. (CAN) FOLLOWING A REPORT OF THE COLLECTIVE JAMMING DURING TAKEOFF, THE AIRCRAFT FLIGHT AND ENGINE CONTROLS WERE INSPECTED. THERE WAS NO FAULT FOUND AT FIRST. TH
- [SDR 2018FA0000077](https://openairdocs.org/sdr/2018FA0000077), Mar 5, 2018: DISPLAY. MALFUNCTIONED. RECEIVED A MODIFIED VEMD. AFTER INSTALLATION, AND INITIAL POWER UP, BOTH SCREENS DISPLAYED LANE FAILURE.
- [SDR 2017FA0000324](https://openairdocs.org/sdr/2017FA0000324), Jun 27, 2017: WIRE. CHAFED. THE MAIN GEAR BOX OIL PRESSURE SWITCH WAS CAUSING MG8 PRESSURE LIGHT TO ILLUMINATE ON CAUTION PANEL. THIS OIL PRESSURE SWITCH ONLY LASTED 21 DAYS WITH 101.6 HRS
- [SDR 2017FA0000323](https://openairdocs.org/sdr/2017FA0000323), Jun 26, 2017: PRESSURE SWITCH. CHAFED. THIS MAIN GEAR BOX OIL PRESSURE SWITCH WAS CAUSING MGB PRESSURE LIGHT TO ILLUMINATE ON CAUTION PANEL. FURTHER RESEARCH INTO THIS PARTICULAR PART SHOWED INTERNAL
- [SDR KW1R20161215005](https://openairdocs.org/sdr/KW1R20161215005), Dec 18, 2016: FIRE DETECTOR. CONTAMINATED. SEVERAL MINUTES AFTER TAKE-OFF "ENG FIRE" WARNING LIGHT ILLUMINATED AND A PRECAUTIONARY LANDING WAS EXECUTED. WARNING LIGHT EXTINGUISHED PRIOR TO LANDING, LIGHT
- [SDR CA160222001](https://openairdocs.org/sdr/CA160222001), Feb 16, 2016: ANGLE. DETACHED. (CAN) REFERENCE SB 53-10 REINFORCEMENT OF XL710 FRAME FOR LATERAL Y VIBRATION DAMPER SUPPORT. SHEARED RIVETS IN ANGLE P/N C533A2103301. DAMAGE APPEARS TO BE FRO
- [SDR 1HTR2016011300001](https://openairdocs.org/sdr/1HTR2016011300001), Dec 29, 2015: PRESSURE SWITCH. MALFUNCTIONED. IN FLIGHT ILLUMINATION OF MAIN GEAR BOX PRESSURE CAUTION LIGHT, RED, PILOT MADE AN UNSCHEDULED PRECAUTIONARY LANDING. PRESSURE SWITCH WAS STICKING.
- [SDR KW1R20151228004](https://openairdocs.org/sdr/KW1R20151228004), Dec 24, 2015: VALVE. BINDING. P2 HEAT VALVE WOULD NOT TURNOFF WHILE ENGINE WAS RUNNING. P2 VALVE WAS ABLE TO BE TURNED OFF AFTER ENGINE SHUTDOWN.
- [SDR KW1R20151222003](https://openairdocs.org/sdr/KW1R20151222003), Dec 22, 2015: VALVE. BINDING. UPON RETURNING FROM A FLIGHT PILOT WAS UNABLE TO SHUTOFF THE P2 HEAT VALVE, CABIN HEAT ON, AIRCRAFT SHUTDOWN.
- [SDR CA151123007](https://openairdocs.org/sdr/CA151123007), Nov 20, 2015: SCISSOR LINK. SCORED. (CAN) ON VISUAL DAILY INSPECTION THE COTTER PIN SAFETY DEVICE ON THE FASTENING BOLT/NUT FOR THE SCISSOR ASSEMBLY TO THE MAIN ROTOR MAST WAS FOUND SHEARED OFF ON
- [SDR 2015FA0000294](https://openairdocs.org/sdr/2015FA0000294), Jun 29, 2015: PRESSURE SWITCH. CHAFED. MAIN GEAR BOX PRESSURE SWITCH CAUSING FALSE READING, LIGHT TO ILLUMINATE. FURTHER RESEARCH SHOWS THAT CAUSE WAS INTERNAL WIRE CHAFING.
- [SDR CA150601007](https://openairdocs.org/sdr/CA150601007), May 14, 2015: DRIVE ASSY. BROKEN. (CAN) HELICOPTER OPERATOR DETECTED ENGINE VIBRATION. TROUBLESHOOTING DETERMINED THE STARTER WAS THE CAUSE. ST/GEN RECEIVED BY O/H AMO FOR INSPECTION/REPAIRS. FO
- [SDR KW1R20150129002](https://openairdocs.org/sdr/KW1R20150129002), Jan 28, 2015: VALVE. BINDING. DUCT TEMPERATURE WARNING LIGHT ILLUMINATED AND PILOT ATTEMPTED TO TURN OFF CABIN HEAT. VALVE WAS BINDING AND WAS DIFFICULT TO SHUTOFF. VALVE WAS JUST INSTALLED 
- [SDR CA141030006](https://openairdocs.org/sdr/CA141030006), Oct 29, 2014: SCISSOR LINK. SEIZED. (CAN) MALE BUSHING, SEIZED INTO THE FEMALE BUSHING ON THE SCISSOR LINK BLOCK. THE PARTS IN QUESTION HAVE BEEN REMOVED FROM SERVICE AND QUARANTINED AND THE SCISS
- [SDR 2014FA0000627](https://openairdocs.org/sdr/2014FA0000627), Oct 13, 2014: INJECTOR. CLOGGED. IN CONJUNCTION WITH LT & RT FUEL INJECTOR MANIFOLDS, ARE CAUSING EXCESSIVE EXHAUST FUMES IN THE COCKPIT. PART TIME ONLY REACHED 215.6 HOURS BEFORE BECOMING CLOG
- [SDR CA140923008](https://openairdocs.org/sdr/CA140923008), Aug 29, 2014: DISPLAY. FAILED. (CAN) ENGINE FAILED POWER CHECK PLUS 4 TO BAD, PILOT DID 3 POWER CHECK ALL FAIL BY A FEW DEGREES C. CHANGED THE FDC FILTER AS IT WAS DIRTY AND ALSO DID A COMPRE
- [SDR CA140702013](https://openairdocs.org/sdr/CA140702013), Jun 27, 2014: BUSHING. SEIZED. (CAN) THE ROTATING SCISSOR ASSLY HAS 2 MAIN PARTS, THE SCISSOR LINK BLOCK PN C623A2005103 AND THE BUSHINGS, PN MM2599973, 4 EA. ON A DAILY CHECK IT WAS DISCOVER
- [SDR CA140219001](https://openairdocs.org/sdr/CA140219001), Feb 18, 2014: SUPPORT BRACKET. BROKEN. (CAN) DURING HIS DI THE PILOT NOTICED THAT THE T4.5 SUPPORT BRACKET ASSY WAS FOUND TO BE BROKEN AT BOTH MOUNTING HOLES THAT ATTACH IT TO THE ENGINE FLANGE.
- [SDR CA140120002](https://openairdocs.org/sdr/CA140120002), Dec 25, 2013: ENGINE. MALFUNCTIONED. (CAN) THE PILOT NOTICED A SUDDEN OIL PRESSURE LOSS AND HE ELECTED TO SHUTDOWN THE ENGINE. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGHT EXAMINATION 
- [SDR 2013FA0000760](https://openairdocs.org/sdr/2013FA0000760), Dec 19, 2013: BUSHING. SEIZED. OUTER BUSHING SEIZED ON INNER BUSHING.
- [SDR CA131210002](https://openairdocs.org/sdr/CA131210002), Dec 6, 2013: ENGINE. FAILED. (CAN) AIRFRAME AND ENGINE TOTAL TIME 23.2. DURING AUTOROTATION TRAINING WITH POWER RECOVERY, IN A 3 FOOT HOVER, AN ENGINE CHIP LIGHT INDICATOR ILLUMINATED. AS T
- [SDR 2013FA0000762](https://openairdocs.org/sdr/2013FA0000762), Nov 4, 2013: BUSHING. SCORED. ROTATING SCISSOR "H" LINK, HAS SCORING ON BUSHINGS.
- [SDR 2013FA0000744](https://openairdocs.org/sdr/2013FA0000744), Oct 28, 2013: SCISSOR LINK. DEBONDED. SCISSOR LINK FIXED BUSHING DISBONDED FROM SCISSOR LINK, INNER ROTATING, SLIP BUSHING SEIZED IN OUTER STATIONARY BUSHING.
- [SDR 2013FA0000759](https://openairdocs.org/sdr/2013FA0000759), Oct 22, 2013: BUSHING. DEBONDED. FIXED BUSHING FROM SCISSOR LINK DISBONDED & SEIZED ON REMOVABLE CARBIDE BUSHING.
- [SDR 2013FA0000761](https://openairdocs.org/sdr/2013FA0000761), Sep 27, 2013: SCISSOR LINK. MISOVERHAULED. SCISSOR LINK FAILED CLEARANCE CHECK.
- [SDR CA130823009](https://openairdocs.org/sdr/CA130823009), Aug 21, 2013: BONDING STRAP. BROKEN. (CAN) DURING THE MORNING DAILY PREFLIGHT INSPECTION, THE AME DISCOVERED THE ELECTRICAL BONDING BRAID ON THE RED BLADE HAD BROKEN AT THE BLADE-END LUG. BONDING S
- [SDR CA130531013](https://openairdocs.org/sdr/CA130531013), May 31, 2013: STATOR VANE. DAMAGED. (CAN) DURING AN INSPECTION, THE PAINT ON TWO FENESTRON STATOR VANES HAS BEEN FOUND CRACKED, AND THE SHAPE OF THE VANES "SWOLLEN", ABOUT 1" OF THE L/E.
- [SDR 2013FA0000285](https://openairdocs.org/sdr/2013FA0000285), May 3, 2013: STRUCTURE. CORRODED. 30 DAY CORROSION INSPECTION NOTED A SLIGHT BUBBLE ON THE EDGE OF THE RADAR ALTIMETER MOUNT AND TAIL BOOM JUNCTION. FURTHER INSPECTION REVEALED INTER-GRANULAR AN
- [SDR CA130215006](https://openairdocs.org/sdr/CA130215006), Feb 13, 2013: BUSHING. SCORED. (CAN) ROTATING SCISSOR ASSY. DURING INSPECTION BUSHING FOUND SCORED. 20 HRS TOTAL TIME ON BUSHING.
- [SDR CA121227002](https://openairdocs.org/sdr/CA121227002), Dec 21, 2012: ADAPTER. DAMAGED. (CAN) ON A FLIGHT ON DECEMBER 21, 2012, THE FLIGHT CREW NOTED A LATERAL VIBRATION THAT BECAME MORE PRONOUNCED DURING DECENT. THE FLIGHT CREW TERMINATED THE FLIG
- [SDR 2013FA0000017](https://openairdocs.org/sdr/2013FA0000017), Dec 19, 2012: OUTLET. BURNED. DURING SCHEDULED INSPECTION, MECHANIC NOTED BURNING AROUND THE AREA OF THE EXHAUST OUTLET. IT WAS NOTED THAT THE BURNING, CRACKING AND DEBONDING HAD TAKEN PLACE
- [SDR 2012FA0000494](https://openairdocs.org/sdr/2012FA0000494), Jul 12, 2012: TORQUE TUBE. WORN. ACFT UNDERGOING 1500 HR INSPECTION AT A TOTAL AIRFRAME TIME OF 1501.4 HRS. THE MECHANIC FOUND THE THE WEAR ADHESIVE TAPE ON THE ORIGINAL ASSY HAD DEBONDED AND C
- [SDR CA120604007](https://openairdocs.org/sdr/CA120604007), May 30, 2012: RAIL. WORN. (CAN) IT WAS BECOMING DIFFICULT TO OPEN OR CLOSE THE SLIDING DOOR. THE BOTTOM RAIL WAS WORN AND SOME AREAS WERE BROKEN. THE ROLLERS WERE NOT MAINTAINED PROPERLY
- [SDR CA111016001](https://openairdocs.org/sdr/CA111016001), Oct 13, 2011: MAGNETIC PLUG. DAMAGED. (CAN) IN CRUISE FLIGHT, PILOT SEES "GB CHIP" LIGHT FLASHING INTERMITTENTLY. HE LANDS SAFELY AND AFTER SHUTDOWN, DISCOVERS THE TAIL GEARBOX CHIP DETECTOR OUT OF 
- [SDR CA110829001](https://openairdocs.org/sdr/CA110829001), Aug 18, 2011: PANEL. DEPARTED. (CAN) WHILE FLYING WITH ALL DOORS OFF, THE COMMUNICATION PANEL (THE PANEL THAT OPENS THE CABIN TO THE REAR CARGO HOLD) FLEW OUT OF THE CABIN. NO DAMAGE WAS FOUN
- [SDR CA110610009](https://openairdocs.org/sdr/CA110610009), Jun 9, 2011: FREQ ADAPTER. FAILED. DURING A MAJOR INSPECTION, DISCOVERED THE FREQUENCY ADAPTER WAS INCORRECT (TOO LONG). PILOT HAD JUST REPORTED A SERIOUS VIBRATION ON THE GROUND. REMOVED THE FRE
- [SDR 2011FA0000311](https://openairdocs.org/sdr/2011FA0000311), May 3, 2011: SKIN. CHAFED. DURING THE INSTALLATION OF A TAIL BOOM ON THE SAME MODEL ACFT THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALO
- [SDR 2011FA0000310](https://openairdocs.org/sdr/2011FA0000310), May 3, 2011: SKIN. CHAFED. DURING THE INSTALLATION OF A TAIL BOOM ON THE SAME MODEL ACFT THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALO
- [SDR 2011FA0000309](https://openairdocs.org/sdr/2011FA0000309), May 3, 2011: STRUCTURE. CRACKED. DURING THE VALVE CHECK A MECHANIC NOTED A CRACK EXTENDING LONGITUDINALLY FROM THE LT FWD NAV/VOR ANTENNA MOUNT. MFG HAS PREVIOUS KNOWLEDGE OF THIS DEFECT AND HA
- [SDR 2011FA0000308](https://openairdocs.org/sdr/2011FA0000308), May 3, 2011: SKIN. CHAFED. DURING THE INSTALLATION OF A TAILBOOM ON THE SAME MODEL ACFT THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALON
- [SDR 2011FA0000307](https://openairdocs.org/sdr/2011FA0000307), May 3, 2011: SKIN. CHAFED. DURING THE INSTALLATION OF THE TAILBOOM THAT HAD BEEN REPAIRED FOR CRACKING IN THE LT FWD VOR ANTENNA MOUNT THE MECHANIC NOTED CHAFING ALONG THE BOTTOM OF THE I
- [SDR 2011FA0000201](https://openairdocs.org/sdr/2011FA0000201), Mar 14, 2011: SKIN. CRACKED. DURING THE QC FINAL INSP PHASE OF A 100 HR INSP THE INSPECTOR NOTED A CRACK EXTENDING LONGITUDINALLY FWD AND AFT FROM THE LT FWD NAV/VOR ANTENNA MOUNT. PHOTO`S 
- [SDR CA110402001](https://openairdocs.org/sdr/CA110402001), Mar 10, 2011: PROBE. FAILED. (CAN) PILOT LOST FUEL QTY INDICATION IN FLIGHT. TROUBLESHOOTING C/O AFTER LANDING. LOWER FUEL PROBE REPLACED, FAILURE CLEARED. ACFT RELEASED.
- [SDR CA110203009](https://openairdocs.org/sdr/CA110203009), Feb 3, 2011: BLOCK. DISLODGED. LIP SEAL OF BEARING BLOCK ASSY DISLOGED.
- [SDR 2011FA0000042](https://openairdocs.org/sdr/2011FA0000042), Jan 25, 2011: CONTROL UNIT. MISALIGNED. FOUND MIXER UNIT MISALIGNED CAUSING THE CYCLIC STICK TO RISE UNCOMMANDED DURING GROUND CHECKS AND ALSO CAUSED THE STRESS OF OTHER FLIGHT CONTROL COMPONENTS IN T
- [SDR CA101116012](https://openairdocs.org/sdr/CA101116012), Nov 16, 2010: SEAL. FAILED. (CAN) SEALS AND SPHERICAL JOINTS REPLACED DUE TO SEAL POPPED OUT OF JOINT ON BEARING P/N 593278 ON BOX EQUIPPED P/N C651A1107101 BUT WHEN GREASE IS APPLIED TO N
- [SDR CA101019003](https://openairdocs.org/sdr/CA101019003), Oct 17, 2010: ENGINE. MAKING METAL. (CAN) DURING FLIGHT ENG CHIP LIGHT WENT ON. KNOWING THE CASE HISTORY OF THIS TYPE OF WARNING ON ENGINES, THE COLLECTIVE WAS LOWERED TO MINIMUM, AUTO ROTATION SP
- [SDR CA101024001](https://openairdocs.org/sdr/CA101024001), Oct 15, 2010: SERVO CONTROL. FAILED. HYD SERVO WHICH CONTROLS FORE/AFT CYCLIC MOVEMENT WOULD NOT SHUTOFF WHEN COLLECTIVE "HYD SHUTOFF" SWITCH IS ACTIVATED. THE SERVO CONTINUED TO OPERATE ON ACCUMUL

All 222: https://openairdocs.org/model/airbus-helicopters-ec120b/reports.md

## STCs that may be installed (OpenAirDocs) (64, 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 SR12074IB](https://openairdocs.org/stc/SR12074IB): Installation of halon free Umlaut fire extinguisher P/N P3APP003010D with extinguishing agent 2-BTP (Halotron® BrX). SABENA TECHNICS BGC
- [STC SR03641AT](https://openairdocs.org/stc/SR03641AT): Replace the existing Eurocopter EC120-B windows with Tech-Tool Plastics, Inc. replacement windows. Tech-Tool Plastics Inc
- [STC SR00217IB](https://openairdocs.org/stc/SR00217IB): Installation of Skid Shoes. Airbus Helicopters Canada Limited
- [STC SR09450RC](https://openairdocs.org/stc/SR09450RC): Installation of SAGEM ICDS-8 Integrated Cockpit Display System that includes a display for the pilot position and a second optional display for the copilot position. Safran Electronics & Defense Avionics USA, LLC
- [STC SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd
- [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 SR02120SE](https://openairdocs.org/stc/SR02120SE): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International 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 SR02028SE](https://openairdocs.org/stc/SR02028SE): Fabrication of Onboard Systems International Model 200-351-00, Cargo Hook Kit,. Onboard Systems International LLC
- [STC SR01673SE](https://openairdocs.org/stc/SR01673SE): Installation of Chelton Flight Systems Electronic Flight Instrument System (EFIS) and associated equipment. Genesys Aerosystems Inc
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings 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 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 SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC
- [STC SR02478AK](https://openairdocs.org/stc/SR02478AK): Installation of the L-3 Aviation Products Lynx multilink surveillance system model NGT-9000() part number 9029000-20000 or Garmin GTX-345 ADS-B transponder part number 011-03302-40. Vector Aerospace Helicopter Services USA Inc
- [STC SR09263RC-D](https://openairdocs.org/stc/SR09263RC-D): Installation of a SFIM VFR Autopilot System. Safran Electronics & Defense Avionics USA, LLC
- [STC SR11230SC](https://openairdocs.org/stc/SR11230SC): Installation of HeliSAS Stability Augmentation System and Autopilot (SAS/AP). S-TEC Corporation
- [STC SR02475AK](https://openairdocs.org/stc/SR02475AK): Installation of the Lexavia Integrated Systems LFS3500 Enhanced Vision System (EVS) on Part 27 Airbus Helicopters equipped with a panel-mounted Multi-Function Display (MFD), primary navigational display or dedicated display with the ability to display video imagery. Lexavia Integrated Systems
- [STC SR02470AK](https://openairdocs.org/stc/SR02470AK): Installation of the L-3 Communications NGT -1000/2000/2500 ADS-B System. ADS-B Technologies, LLC
- [STC SR02471AK](https://openairdocs.org/stc/SR02471AK): Installation of the L-3 Communications NGT -9000/9000R ADS-B System. ADS-B Technologies, LLC
- [STC SR03676NY](https://openairdocs.org/stc/SR03676NY): Installation of Aspen EFD 1000H Pro Primary Flight Display and associated components. Motorflug Baden-Baden GmbH
- [STC SR03539NY](https://openairdocs.org/stc/SR03539NY): Installation of Garmin G500H Flight Display System. Maxcraft Avionics Ltd
- [STC SR03524NY](https://openairdocs.org/stc/SR03524NY): Installation of a MD302 Standby Attitude Module. Maxcraft Avionics Ltd
- [STC SR01130NY-D](https://openairdocs.org/stc/SR01130NY-D): Installation of NS Microwave Antenna Installation. Sikorsky Aircraft Corporation
- [STC SR00491DE](https://openairdocs.org/stc/SR00491DE): Installation of cabin air conditioning system. Air Comm Corporation
- [STC SR00549DE](https://openairdocs.org/stc/SR00549DE): Installation of Bleed Air Cabin Heater/Defroster System. Air Comm Corporation
- [STC SR09427RC](https://openairdocs.org/stc/SR09427RC): Installation of Night Vision Goggle (NVG) Compatible Interior Lighting System. REB Technologies Inc
- [STC SR00780LA](https://openairdocs.org/stc/SR00780LA): Installation of Apical Emergency Float Kit, P/N 20498. Apical Industries Inc. dba Dart Aerospace
- [STC SR01191SE](https://openairdocs.org/stc/SR01191SE): Installation of an engine air filter. Aerometals
- [STC SR03383NY](https://openairdocs.org/stc/SR03383NY): Installation of a Latitude Technologies IONODE Flight Data Monitoring (FDM). Latitude Technologies Corporation
- [STC SR03364NY](https://openairdocs.org/stc/SR03364NY): Installation of a Garmin G500H Flight Display System. Kitchener Aero Avionics Ltd
- [STC SR03243NY](https://openairdocs.org/stc/SR03243NY): Installation of Right-Hand Door Handle. Eurocopter Canada Limited
- [STC SR03152NY](https://openairdocs.org/stc/SR03152NY): The installation of the Brite Saver 2 Data Monitoring System. ECT Industries
- [STC SR02232LA](https://openairdocs.org/stc/SR02232LA): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc
- [STC SR02939NY](https://openairdocs.org/stc/SR02939NY): Installation of a SkyTrac ISAT-200 Airborne Position/Data Communicator in accordance with Avionics Design Services Ltd. Master Drawing List MDL10033, Revision C, dated February 02, 2011, Transport Canada approved February 02, 2011, or later Transport Canada approved revision. SkyTrac Systems Ltd
- [STC SR09371RC-D](https://openairdocs.org/stc/SR09371RC-D): Cabin Floor Protector Kits in accordance with Aeronautical Accessories, Inc. Drawing List, Report No. AA-03084, Revision A, dated February 16, 2004, or later DAS approved revisions; and installation per Report No. AA-03082, No Revision, dated November 12, 2003, and/or AA-03083, Revision A, dated February 16, 2004, or later DAS approved revisions. Bell Helicopter Textron Inc
- [STC SR01609SE](https://openairdocs.org/stc/SR01609SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SR02189NY](https://openairdocs.org/stc/SR02189NY): Iinstallation of SkyTrac ISAT-100 Airborne Position/Data Communicator System. SkyTrac Systems Ltd
- [STC SR01892NY](https://openairdocs.org/stc/SR01892NY): Installation of an Improved Heating System. Eurocopter Canada Limited
- [STC SR09466RC](https://openairdocs.org/stc/SR09466RC): Installation of Night Vision Goggle Compatible Interior Lighting System and Red Position Light. Aero Dynamix Inc
- [STC SR01701NY](https://openairdocs.org/stc/SR01701NY): Installation of SX-16 Nightsun Searchlight System. Exterior mount must be installed per STC SR01302LA. Eurocopter Canada Limited
- [STC SR02244NY](https://openairdocs.org/stc/SR02244NY): Installation of FLIR 8000 series System. Eurocopter Canada Limited
- [STC SR01245NY](https://openairdocs.org/stc/SR01245NY): Installation of Settling Protectors. Eurocopter Canada Limited
- [STC SR01302LA](https://openairdocs.org/stc/SR01302LA): Installation of side utility mount. Airfilm Camera Systems
- [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models. Technisonic Industries Limited
- [STC SR01842NY](https://openairdocs.org/stc/SR01842NY): Installation of Air Cruisers emergency flotation system. Air Cruisers Company
- [STC SR09136RC-D](https://openairdocs.org/stc/SR09136RC-D): Installation of a Forward L/H External Mount. American Eurocopter Corporation
- [STC SR09108RC-D](https://openairdocs.org/stc/SR09108RC-D): Installation of a left or right pilot instrument panel. American Eurocopter Corporation

All 64: https://openairdocs.org/model/airbus-helicopters-ec120b/stcs.md

## PMA parts (OpenAirDocs) (714, 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.

- [120-0350-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196860534720260923124204.0001): Condenser Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219002 · Aug 31, 2026
- [120-0252-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154471258620260923124204.0001): Evaporator Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219008 · Aug 31, 2026
- [ES43030-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133438376520260923124210.0001): Receiver /Drier Bottle. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219004 · Aug 31, 2026
- [120-0850-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131997049020260923124205.0001): Plumbing Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219005 · Aug 31, 2026
- [120-0261-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125881580220260923124204.0001): Blower Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A4219011 · Aug 31, 2026
- [120-0450-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101017034320260923124204.0001): Compressor Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A4219000 · Aug 31, 2026
- [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
- [ES43030-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190774262120250213205408.0001): Receiver /Drier Bottle. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219004 · Feb 10, 2025
- [120-0252-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147408688120250213205400.0001): Evaporator Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219008 · Feb 10, 2025
- [120-0450-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126407892720250213205401.0001): Compressor Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A4219000 · Feb 10, 2025
- [120-0850-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115024751220250213205401.0001): Plumbing Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219005 · Feb 10, 2025
- [120-0261-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111434906020250213205400.0001): Blower Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A4219011 · Feb 10, 2025
- [120-0350-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102933320120250213205400.0001): Condenser Assembly. Air Comm Corporation · PMA PQ0072NM · Replaces 7052A3219002 · Feb 10, 2025
- [M2001-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100776285420240802183931.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 150SG1009-5 · Jun 20, 2024
- [TA2407-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137249120120240531131429.0001): Heli- Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Apr 24, 2024
- [TA2407-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107344472620240531131429.0001): Heli- Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Apr 24, 2024
- [98020120-1009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156740552420240408225724.0001): Airbus Helicopters EC120 NVG Modification Kit. REB Technologies Inc · PMA PQ1018SW · Modification part · Mar 7, 2024
- [AAI- 150SG1070](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117245936520240320173347.0001): Friction Disc. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 150SG1070 · Jan 31, 2024
- [BCN150SG-K1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127350601720221024173133.0001): Overhaul Hardware Kit 150SG, 160SG Series Starter Generators. BCN Aerospace, Inc. · PMA PQ2149NE · Replaces NJ150SG-K1 · Oct 14, 2022
- [WM150SG-K1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198054363320220816120605.0001): Overhaul Hardware Kit 150SG, 160SG Series Starter Generators. Wesco Manufacturing, Inc. · PMA PQ00011EB · Replaces Aircraft Parts Corporation… · Aug 9, 2022
- [200-351-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159291607720220811112146.0001): Cargo HookKit EC120B. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [200-308-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133331688120220811112127.0001): EC120B Cargo HookSuspension Kit. Onboard Systems International · PMA PQ0055NM · Modification part · Jul 28, 2022
- [M150SG1379-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113110641320220808142311.0001): Washer, Lock. Miraj Corporation · PMA PQ0870NE · Replaces 150SG1379-8 · Jul 19, 2022
- [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176126973820220610124251.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 6, 2022
- [AG627000-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184635456520220809130824.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · May 10, 2022
- [AG844000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117227094120220809102500.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · Apr 18, 2022
- [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158989887620220408135719.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022
- [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174170167320220408135654.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022
- [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177857739220220408135616.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021
- [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105964510220220408140206.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104198365520220408135730.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID808531119720211110110425.0001): Gasket-UHD/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 9, 2021
- [ETR 25-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID268900254920210909204053.0001): Starter-Generator Mod Kit. NAASCO Northeast Corp · PMA PQ0961NE · Replaces Skurka Aerospace Inc.(Aircraft Parts… · Jul 22, 2021
- [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID375660849202107271951120.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 2020
- [AG786000-01](https://drs.faa.gov/browse/excelExternalWindow/F240EB736CAF9B6F86258639004F7BE3.0001): Gasket - StormScope Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 8, 2020
- [SA350A41107620](https://drs.faa.gov/browse/excelExternalWindow/7D6927FCA8C45C598625864100419443.0001): Pad Leaf. Seginus Aerospace LLC · PMA PQ4083CE · Replaces Airbus Helicopter 350A41107620 · Dec 6, 2020
- [AG477000-35](https://drs.faa.gov/browse/excelExternalWindow/CAA7A03C831CF5A78625861F004520E1.0001): Gasket - GPS ANTENNA. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 11, 2020
- [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174396567820240320173402.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 06-201020 · Oct 6, 2020
- [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163395973720240320173409.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 150SG1139 · Oct 6, 2020
- [98020120-1008](https://drs.faa.gov/browse/excelExternalWindow/66CAC626C50C3212862585E5005BCE9A.0001): Airbus Helicopters EC120 NVG Modification Kit. REB Technologies Inc · PMA PQ1018SW · Modification part · Sep 2, 2020
- [AG822000-03](https://drs.faa.gov/browse/excelExternalWindow/25D416C8B528F4988625859F003C440E.0001): Gasket - TCAS Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · May 31, 2020
- [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/44F91AF19B0D8D4586258591003A1785.0001): Gasket - UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 1, 2020

All of them: https://openairdocs.org/model/airbus-helicopters-ec120b/pma.md

## The same model under other registry codes

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

- [Eurocopter EC120B](https://openairdocs.org/model/eurocopter-ec120b): 68 registered aircraft, registry code 8680987
- [Eurocopter France EC120B](https://openairdocs.org/model/eurocopter-france-ec120b): 1 registered aircraft, registry code 8680995

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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.