- Registered owner
- Airstar Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 4022
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- September 11, 2008
- Expires
- April 30, 2028
- Mode S code
- AB1D0A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
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 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 3 |
| 2010 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2013 | 4 |
| 2014 | 3 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 3 |
| 2018 | 1 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 9 |
| 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 N815MHMatched 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 N815MHMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7KA0817084022Potentiometer · failedAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND SUBSEQUENT TO FAILURE REPORT GENERATION THE COLLECTIVE POTENTIOMETER WAS INDICATED TO BE DEFECTIVE. A NEW PART WAS INSTALLED AND NO FURTHER DEFECT NOTED. (K)SDR M7K2008F00042Tensioner · crackedDURING ROUTINE MAINT (1) OF (2) BELT TENSIONING ARMS FOUND CRACKED IN (2) PIECES. FAILURE ORIGINATED AT WELDMENT. SEVERAL HAVE FAILED IN THIS MANNER. SUGGEST POST WELD, HEAT TREATMENT TO RELIEVE WELD STRESS. (K)SDR M7K2008F00012Starflex · cracked(REF 0213084022) DURING ROUTINE INSP, ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION UTILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING & STAR ARM END. WITH ROTOR HUB SLEEVES REMOVED BUSHING COULDSDR M7K2008F00062Potentiometer · inoperativePILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPISDR M7K2008F00144Fitting · crackedFITTING FOUND CRACKED DURING POST FLIGHT INSP AND A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AIRCRAFT AND NEVER ON OTHER AIRCRAFT FOR REASONS UNKNOWN. SOME SHIMMING CAN BE REQUIRED AND MSDR M7K2008F00109Potentiometer · defectiveAC HAD SOME SUDDEN YAWING WHEN PASSING THROUGH A SPECIFIC COLLECTIVE POWER SETTING THAT WAS REPEATABLE AND INDICATED A SUDDEN CHANGE OF ENGINE TORQUE SUCH AS ONE MAY EXPERIENCE WITH COMPRESSOR STALLS. NO FAULT CODES WERE GENERATED AD THE ENGINE HAD NO OBSERVASDR M7K2008F00123Power Supply · inoperativeTHIS ANTI-COLLISION LIGHT AND POWER SUPPLY ASSY HAS PROVEN TO BE OF LOW QUALITY AS MOST FAIL WITHIN THEIR FIRST 1000 HOURS OF SERVICE AND ARE NOT REPAIRABLE IAW MFG. AS THIS UNIT IS VERY EXPENSIVE TO REPLACE WE RECOMMEND THAT THE WHEN LED FLASHING ANTI COLLIS
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