- Registered owner
- Airstar Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 3956
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- February 17, 2015
- Expires
- February 29, 2028
- Mode S code
- AB11E5
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 N812MHMatched 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 N812MHMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7K2008F00147Engine · making metalPRIOR TO OPS CHECK, FLIGHT TAKEOFF ENGINE CHIP LIGHT ILLUMINATED. FLIGHT WAS ABORTED. ALL DEFECTIVE INSPECTED AND METAL RECEIVED. RUNS COMPLETED. NO LIGHT . EVEN THOUGH FOLLOWING SUCCESSFUL PENALTY RUNS AND NO LIGHT AFTER 1.5 HOURS OF FLIGHT CHECK IT WAS APPSDR M7K2008F00007Magnetic Seal · leakingSHORTLY AFTER ENGINE OVERHAUL WAS COMPLETED AND ENGINE RETURNED TO FLIGHT STATUS THE POWERSHAFT SEAL BEGAN TO WEEP AND PROGRESSIVELY THE WEEP BECAME A LEAK. A NEW SEAL WAS INSTALLED AND NO FURTHER LEAKAGE WAS NOTED. SUGGEST IMPROVED QUALITY CONTROL FOR THESESDR M7K2008F00003Fitting · crackedCRACK DISCOVERED DURING ROUTINE INSPECTION ON FITTING FLANGE AND GOING THROUGH AN ATTACHMENT BORE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. THIS IS A VERY COMMON PROBLEM FOR THIS PART. SUGGEST THIS PART BE MANUFACTURED FROM A MORE DURABLE MATERIAL SUCSDR M7K2008F00101Potentiometer · defectivePILOT REPORTS HAVING AN AMBER GOVERNOR LIGHT IN FLIGHT. UPON AC SHUTDOWN, A FAILURE CODE WAS GENERATED INDICATING THE COLLECTIVE POTENTIOMETER WAS DEFECTIVE. A NEW PART WAS INSTALLED WITH NO FURTHER DEFECT REPORTED. THIS IS A RECURRING PROBLEM FOR THIS PARTSDR M7K2008F00095Bracket · crackedFOUND CRACKED DURING ROUTINE 100 HOUR INSPECTION. THIS IS A VERY COMMON PROBLEM FOR THIS PART. SUGGEST A MORE ROBUST MATERIAL SUCH AS SS BE UTILIZED TO REDUCE THE CRACKING OR PERHAPS A MACHINED PART. (K)SDR M7K2008F00078Fitting · crackedCRACK FOUND DURING ROUTINE INSPECTION RADIATING FROM A SCREW HOLE TO THE EDGE OF THE MACHINED FLANGE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K)SDR M7K2008F00066Potentiometer · failedPILOT 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 M7K2008F00048Fitting · crackedCRACK FOUND DURING ROUTINE INSP RADIATING FROM A SCREW HOLE ON MOUNTING FLANGE SURFACE AND ONTO REINFORCEMENT RIB SURFACE. A NEW FITTING HAS BEEN MATCH DRILLED AND INSTALLED. (K)SDR M7K2008F00138Cover · crackedTHIS PART WAS FOUND CRACKED DURING ROUTINE INSPECTION. THE CRACK ALWAYS OCCURS IN THE RADIUS OF THE LOWER IB CORNER FLANGE ALMOST ALL OF THESE SPRING COVERS WILL REQUIRE REPLACEMENT MULTIPLE TIMES WITHIN THE FIRST FEW THOUSAND FLIGHT HOURS OF THE AIRCRAFT. SDR M7K2008F00125Support · looseDURING ROUTINE INSPECTION IT WAS NOTED THAT THE TOP OF THE FLAP DOOR WAS EXCESSIVELY LOOSE. CLOSER INSPECTION REVEALED THAT THE DOOR’S ATTACHMENT HARDWARE HAD LOOSENED ALLOWING THE FITTING TO WEAR AROUND THE SCREW AND ULTIMATELY BREAK THROUGH THE METAL FLANGESDR M7K2008F00086Freq Adapter · crackedDURING SCHEDULED MAINT ONE ADAPTER OF SET OF 3 FOUND TO HAVE INTERNAL/EXTERNAL ELASTOMER CRACK EXCEEDING MM LIMITATIONS OF 10MM. THIS IS A VERY COMMON FAILURE THAT OCCURS AT HALF OR LESS OF THIS PARTS SERVICE LIFE LIMIT OF 3000 HOURS. THE OLDER PN ADAPTERS USDR M7K2005F00002Vent Line · crackedENGINE OIL VENT TUBE, AIRFRAME PART, MOUNTED ON ENG WITH VENTING ORIFICE PLACED IN EXHAUST PATH HAS ANTI-ROTATION CLAMP WELDED TO STAINLESS TUBE BODY, CRACKS INITIATE IN SPOT WELDS CAUSING CLAMP FLANGE TO CRACK. REPAIR, DRESSING OFF FLANGE REMNANTS, INSTALLIN
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