# N808MH: 2005 Eurocopter EC 130 B4

- Status: Valid registration
- Airframe: [Eurocopter EC 130 B4](https://openairdocs.org/model/eurocopter-ec-130-b4) (registry code 8680989, 6 seats)
- Engine: [Turbomeca ARRIEL-2B1](https://openairdocs.org/engine/turbomeca-arriel-2b1) (registry code 60056)
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU) (Airbus Helicopters), [TCDS E00054EN](https://openairdocs.org/tcds/E00054EN) (Safran Helicopter Engines S.A.) (OpenAirDocs)
- Serial number: 3914
- Year built: 2005
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Standard, normal
- Airworthiness date: May 27, 2005
- Certificate issued: February 17, 2015
- Expires: February 29, 2028
- Mode S code: AB00B0
- Registered owner: [Airstar Leasing LLC](https://openairdocs.org/faa-owner/AIRSTAR%20LEASING%20LLC)
- Location: [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson)
- Owner type: LLC
- Owner's area on the map: 35.9799° N, 115.1079° W: Placed by OpenAirDocs at the center of ZIP code 89052, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808MH
- Page: https://openairdocs.org/aircraft/N808MH

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 64 in force

### Matched by airframe (Eurocopter EC 130 B4)

- [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
- [AD 2002-03-52](https://openairdocs.org/ad/2002-03-52): Adhesive Bead and the Metal Bushing Bonded on Each STARFLEX Star Arm End · Airbus Helicopters AS355E, AS355F, AS355F1 and 11 more. Effective Apr 4, 2002

### Matched by engine (Turbomeca ARRIEL-2B1)

- [AD 2021-13-03](https://openairdocs.org/ad/2021-13-03): Fuel Control/Turbine Engines · Safran Helicopter Engines Arriel 2B, Arriel 2B1, Arriel 2C and 4 more. Effective Aug 13, 2021
- [AD 2018-12-01](https://openairdocs.org/ad/2018-12-01): Engine Fuel and Control · Safran Helicopter Engines Arriel 2B and Arriel 2B1. Effective Sep 12, 2018
- [AD 2016-25-13](https://openairdocs.org/ad/2016-25-13): Engine accessory gearbox (AGB) · Safran Helicopter Engines Arriel 2B, Arriel 2B1, Arriel 2C and 6 more. Effective Feb 3, 2017
- [AD 2015-13-04](https://openairdocs.org/ad/2015-13-04): Engine accessory gearbox (AGB) · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 16 more. Effective Sep 1, 2015
- [AD 2014-12-05](https://openairdocs.org/ad/2014-12-05): HMU drive gear shaft · Turbomeca Arriel 2B, Arriel 2B1, Arriel 2C and 4 more. Effective Aug 4, 2014
- [AD 2014-07-06](https://openairdocs.org/ad/2014-07-06): Hydromechanical metering unit · Turbomeca Arriel 2B1. Effective May 15, 2014
- [AD 2012-18-18](https://openairdocs.org/ad/2012-18-18): Gas generator (GG) turbine blade · Turbomeca Arriel 2B, Arriel 2B1, Arriel 2C2 and 1 more. Effective Oct 24, 2012
- [AD 2012-08-18](https://openairdocs.org/ad/2012-08-18): PT Blade Rupture · Turbomeca Arriel 2B and Arriel 2B1. Effective May 30, 2012
- [AD 2009-09-03 R1](https://openairdocs.org/ad/2009-09-03-R1): Uncommanded in-flight engine shutdown · Turbomeca Arriel 2B and Arriel 2B1. Effective Nov 1, 2010
- [AD 2009-08-08 R1](https://openairdocs.org/ad/2009-08-08-R1): PT Blades · Turbomeca Arriel 1B, Arriel 1D, Arriel 1D1 and 2 more. Effective May 7, 2010
- [AD 2009-01-11](https://openairdocs.org/ad/2009-01-11): Hydro Mechanical Unit (HMU) low fuel pressure switch · Turbomeca Arriel 2B and Arriel 2B1. Effective Feb 27, 2009
- [AD 2007-10-06](https://openairdocs.org/ad/2007-10-06): Cases of flameout · Turbomeca Arriel 2B1. Effective May 29, 2007
- [AD 2005-25-13](https://openairdocs.org/ad/2005-25-13): Tree turbine shield · Turbomeca Arriel 2B and Arriel 2B1. Effective Dec 28, 2005
- [AD 2003-03-12](https://openairdocs.org/ad/2003-03-12): Bleed Valve · Turbomeca Arriel 1A2, Arriel 1C, Arriel 1C1 and 12 more. Effective Mar 7, 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
- [AD 2016-04-12](https://openairdocs.org/ad/2016-04-12) (historical): Engine accessory gearbox (AGB) · Turbomeca Arriel 2B, Arriel 2B1, Arriel 2C and 6 more. Effective Apr 14, 2016
- [AD 2014-19-05](https://openairdocs.org/ad/2014-19-05) (historical): Engine accessory gearbox (AGB) · Turbomeca Arriel 1A1, Arriel 1A2, Arriel 1B and 16 more. Effective Nov 5, 2014
- [AD 2012-03-11](https://openairdocs.org/ad/2012-03-11) (historical): High-pressure/low-pressure (HP/LP) pump hydro-mechanical metering units  
 (HMUs) · Turbomeca Arriel 2B and Arriel 2B1. Effective Mar 20, 2012
- [AD 2011-13-05](https://openairdocs.org/ad/2011-13-05) (historical): Gas Generator (GG) Turbine Blade · Turbomeca Arriel 2B and Arriel 2B1. Effective Aug 12, 2011
- [AD 2007-19-09 R1](https://openairdocs.org/ad/2007-19-09-R1) (historical): Pressure relief valve · Turbomeca Arriel 2B1. Effective Jul 7, 2010
- [AD 2010-03-06](https://openairdocs.org/ad/2010-03-06) (historical): Fuel pump · Turbomeca Arriel 2B and Arriel 2B1. Effective Mar 11, 2010
- [AD 2009-09-03](https://openairdocs.org/ad/2009-09-03) (historical): Turbine blade · Turbomeca Arriel 2B and Arriel 2B1. Effective Jun 1, 2009
- [AD 2007-19-09](https://openairdocs.org/ad/2007-19-09) (historical): Constant delta pressure valve · Turbomeca Arriel 2B1. Effective Oct 3, 2007
- [AD 2007-10-07](https://openairdocs.org/ad/2007-10-07) (historical): HP/LP pump assembly drive shaft · Turbomeca Arriel 2B and Arriel 2B1. Effective May 29, 2007
- [AD 2007-03-14](https://openairdocs.org/ad/2007-03-14) (historical): Hydro-mechanical metering unit (HMU) · Turbomeca Arriel 2B1. Effective Feb 20, 2007
- [AD 2006-21-10](https://openairdocs.org/ad/2006-21-10) (historical): Splines of high-pressure (HP) pump drive gear shaft · Turbomeca Arriel 2B and Arriel 2B1. Effective Nov 24, 2006

## Information bulletins (advisory) (5 in force)

- [SAIB SW-17-23R2](https://openairdocs.org/saib/SW-17-23R2): Fuel System. Issued Jul 15, 2019
- [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
- [SAIB SW-17-23R1](https://openairdocs.org/saib/SW-17-23R1) (historical): Fuel System. Issued Mar 2, 2018

## 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 LAX07LA281](https://openairdocs.org/ntsb/LAX07LA281), Sep 27, 2007: Eurocopter France EC 130 B4 (N808MH), Meadview, AZ, substantial damage. Probable cause: Collision with a bird during cruise flight.

## 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 20070927023409A](https://openairdocs.org/incident/20070927023409A), Sep 27, 2007: Urocop EC130B4 (N808MH), Meadview, AR, Substantial damage. (-23) Helicopter struck a large bird which came through the wind screen striking occupants. Helicopter landed on a dirt strip, pearce ferry airstrip (L25)…

## Service difficulty reports (16)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR M7K2008F00032](https://openairdocs.org/sdr/M7K2008F00032), May 23, 2008: FITTING. CRACKED. DURING ROUTINE INSPECTION, THE FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO FLANGE EDGE. NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FO
- [SDR M7K2008F00031](https://openairdocs.org/sdr/M7K2008F00031), May 23, 2008: FITTING. CRACKED. DURING ROUTINE INSP THE FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO THE FLANGE EDGE. A NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR
- [SDR M7K2008F00008](https://openairdocs.org/sdr/M7K2008F00008), May 12, 2008: POTENTIOMETER. DEFECTIVE. (REF 0423083914) A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF THE YAW POTENTIOMETER. A NEW PART WAS INSTALLED AND NO FURTHER FAULT WAS DETECTED
- [SDR M7K2008F00107](https://openairdocs.org/sdr/M7K2008F00107), Apr 14, 2008: POTENTIOMETER. DEFECTIVE. UPON AC SHUTDOWN A FAILURE CODE WAS GENERATED INDICATING THE COLLECTIVE POTENTIOMETER WAS DEFECTIVE. A NEW PART WAS INSTALLED WITH NOT FURTHER DEFECT REPORTED. 
- [SDR M7K2008F00104](https://openairdocs.org/sdr/M7K2008F00104), Apr 14, 2008: FITTING. CRACKED. DURING ROUTINE INSPECTION, A CRACK WAS DISCOVERED RADIATING TO THE EDGE OF THE MOUNTING FLANGE AND INWARD TOWARD THE CENTER OF THE FLANGE FROM THE EDGE OF THE S
- [SDR M7K2008F00103](https://openairdocs.org/sdr/M7K2008F00103), Apr 14, 2008: MOUNT. CRACKED. DURING ROUTINE INSP, A CRACK WAS DISCOVERED RADIATING FROM A MOUNTING BORE HOLE TO THE EDGE OF THE MOUNTING FLANGE AND INWARD TOWARD THE CENTER OF THE FLANGE FR
- [SDR M7K2008F00099](https://openairdocs.org/sdr/M7K2008F00099), Apr 14, 2008: BRACKET. CRACKED. BRACKET FOUND CRACKED DURING 100 HOUR INSPECTION. (K)
- [SDR M7K2008F00098](https://openairdocs.org/sdr/M7K2008F00098), Apr 14, 2008: PRESSURE SWITCH. FAILED. HYDRAULIC PRESSURE LIGHT FAILED TO EXTINGUISH ALTHOUGH SYS WAS PRODUCING NORMAL PRESSURE AND OPERATING NORMALLY IN ALL OTHER RESPECTS. A NEW SWITCH WAS INSTALLE
- [SDR M7K2008F00081](https://openairdocs.org/sdr/M7K2008F00081), Apr 14, 2008: FITTING. CRACKED. FOUND CRACKED INTO 2 PIECES DURING ROUTINE INSP ON THE MOUNTING FLANGE SURFACE RADIATING FROM A MOUNTING BORE AND TO BOTH EDGES OF THE FLANGE. A NEW FITTING WAS
- [SDR M7K2008F00074](https://openairdocs.org/sdr/M7K2008F00074), Mar 3, 2008: POTENTIOMETER. DEFECTIVE. PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER AS THE LIKELY DEFECTIVE UNIT. A NEW PART W
- [SDR M7K2008F00065](https://openairdocs.org/sdr/M7K2008F00065), Jan 8, 2008: POTENTIOMETER. FAILED. PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO TH
- [SDR M7K2008F00146](https://openairdocs.org/sdr/M7K2008F00146), Nov 5, 2007: WINDSCREEN. DAMAGED. ACFT STRUCK BIRD WITH LOSS OF PILOTS AND CENTER WINDSCREENS. ACFT LANDED AT FIRST PRACTICAL LANDING SPOT. A MAJOR REPAIR OF LT CANOPY FRAME AND LT CENTER FRAME 
- [SDR M7K2008F00057](https://openairdocs.org/sdr/M7K2008F00057), Oct 30, 2007: FITTING. FAILED. PART FOUND CRACKED DURING ROUTINE INSPECTION IAW AD2004-01-14, REQUIREMENTS AT THE 110 HOUR INTERVAL INSPECTION. A NEW PART OF THE OLD PN WAS INSTALLED. SUGGEST
- [SDR M7K2008F00056](https://openairdocs.org/sdr/M7K2008F00056), Oct 30, 2007: LIGHT. INOPERATIVE. STROBE FLASH BECAME WEAKER AS THE DAYS PASSED UNTIL UNIT WOULD NO LONGER PASS STROBE INTENSITY REQUIREMENTS AND WAS REPLACED IAW A FIELD APPROVED 337BY THE INST
- [SDR M7K2007F00003](https://openairdocs.org/sdr/M7K2007F00003), Aug 6, 2007: FREQ ADAPTER. CRACKED. DURING ROUTINE POSTFLIGHT INSPECTION THE CRACK WAS FOUND VISUALLY ON THE YELLOW BLADES FREQUENCY ADAPTER ELASTOMER SURFACE TRAILING EDGE SIDE JUST BEGINNING TO 
- [SDR M7K2007F00001](https://openairdocs.org/sdr/M7K2007F00001), Aug 6, 2007: SUPPORT FITTING. DAMAGED. DURING ROUTINE POSTFLIGHT INSPECTION THE CRACK WAS FOUND VISUALLY ON THE RT LOWER SUPPORT FITTING POSITION ON THE PARTS TRAILING EDGE FACE AND FOUND TO EXTEND A

## STCs that may be installed (OpenAirDocs) (134, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Eurocopter EC 130 B4)

- [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/aircraft/N808MH/stcs.md

## Related

- Other Eurocopter EC 130 B4 aircraft: https://openairdocs.org/model/eurocopter-ec-130-b4/aircraft.md
- The Turbomeca ARRIEL-2B1 engine: https://openairdocs.org/engine/turbomeca-arriel-2b1.md

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