- Registered owner
- Airstar Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 3799
- Year built
- 2004
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 8, 2004
- Certificate issued
- February 17, 2015
- Expires
- February 29, 2028
- Mode S code
- AAF58B
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2002 | 1 |
|---|---|
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 2 |
| 2007 | 4 |
| 2008 | 3 |
| 2009 | 2 |
| 2010 | 7 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 4 |
| 2014 | 6 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 4 |
| 2018 | 2 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 10 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 7 |
| 2026 | 7 |
Airframe · Eurocopter EC 130 B4
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N805MHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter EC 130 B4 aircraft
FAA incident reports
No FAA accident or incident reports matched to N805MHMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter EC 130 B4 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7K2008F00035Magnetic Seal · leakingDURING ROUTINE INSP EXCESSIVE OIL LEAKAGE WAS NOTED AT THE MODULE 5 OUTPUT MAGNETIC SEAL. CLOSE INSP OF REMOVED SEAL REVEALED NO OBVIOUS DEFECT. A NEW SEAL WAS INSTALLED WITH NO FURTHER LEAKAGE NOTED. (K)SDR M7K2008F00140Potentiometer · failedA FAULT CODE WAS GENERATED AT ENGINE SHUTDOWN INDICATING A DEFECT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED. THIS HAS BECOME A VERY COMMON PROBLEM WITH THE LATEST REPLACEMENT PART THAT THEY LAST MUCH LESS THAN THE 2000 HOUR SERVICESDR M7K2008F00055Switch · failedAT END OF FLIGHT, PILOT SELECTED IDLE POSITION AND ENGINE REMAINED IN THE FLIGHT POSITION AND WAS SHUTDOWN FROM FLIGHT POSITION. A FAULT CODE WAS GENERATED THA THE START STOP SWITCH WAS DEFECTIVE IN SOME MANNER. A NEW ENGINE START STOP/ON OFF SWITCH WAS INSTSDR M7K2008F00051Fitting · crackedFITTING FOUND CRACKED DURING POST FLIGHT INSP. A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AC AND NEVER ON OTHERS FOR REASONS UNKNOWN. SOME SHIMMING IS SOMETIMES REQUIRED AND IF DONE POOSDR M7K2008F00049Angle · crackedFITTING FOUND CRACKED DURING INSP. A NEW FITTING INSTALLED. (K)
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 134 STCs