- Registered owner
- Airstar Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 3912
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- May 6, 2005
- Certificate issued
- February 17, 2015
- Expires
- February 29, 2028
- Mode S code
- AAFCF9
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 N807MHMatched 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 N807MHMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7KA0524083912Pressure Sensor · malfunctionedOIL PRESSURE LIGHT ILLUMINATES AT GROUND IDLE. NEW SWITCH NORMALLY WORKS WELL BUT ON OCCASION LOSES INTERNAL CALIBRATION OR IS MISCALIBRATED AS NEW SWITCHES SOMETIMES EXHIBIT THE SAME PROBLEM. SUGGEST A MORE MODERN DESIGN BE CONSIDERED FOR THIS PART. (K)SDR M7K2008F00040Potentiometer · failedUPON SHUTDOWN A FAULT CODE WAS GENERATED THAT INDICATED A FAULT WITH COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED AND NO FURTHER DEFECT NOTED. THIS HAS BEEN A VERY COMMON FAULT FOR THIS PART. RECENTLY IT WAS DETERMINED THAT ELECTRICAL HARNESS SDR M7K2008F00037Igniter Box · malfunctionedDURING ROUTINE INSPECTION AN OPERATIONAL CHECK REVEALED VERY SLOW FUNCTION ON (1) OF THE (2) IGNITERS POWER CIRCUITS. A NEW IGNITER BOX WAS INSTALLED AND OPERATIONAL CHECK WAS NORMAL. THIS PARTIAL LOSS OF A CIRCUIT IS TYPICAL FOR THIS ASSEMBLY. USUALLY THIS SDR M7K2008F00017Pressure Sensor · inoperativeLOW MGB OIL PRESSURE WARNING LIGHT FLICKERED IN FLIGHT WITH NO AUDIBLE WARNING. SWITCH WAS REPLACED WITH A SERVICEABLE PAR AND WITH NO FURTHER DISCREPANCY NOTED. THIS IS TO AN UNCOMMON FAULT FOR THIS PART. SUGGEST IMPROVED DESIGN OR BETTER QC FOR INTERNAL PARSDR M7K2008F00028Potentiometer · failedA FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FURTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODEL HELICOPTER. SUGGESDR M7K2008F00141Freq Adapter · crackedDURING ROUTINE INSP A CRACK IN THE YELLOW BLADES FREQUENCY ADAPTER WAS FOUND TO EXCEED THE MM 10MM LIMITATION, CRACK WAS FOUND ON THE T/E SIDE OF THE ADAPTER. (K)SDR M7K2008F00082Fitting · crackedDURING ROUTINE INSPECTION A CRACK WAS DISCOVERED THROUGH THE STRENGTHENING RIB OF THE MOUNTING FLANGE. CRACK DEVELOPMENT IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST A MORE ROBUST MATERIAL SUCH AS SS OR TITANIUM BE UTILIZED. (K)SDR M7K2008F00131Fitting · crackedDURING ROUTINE 100 HOUR INSPECTION, A CRACK WAS FOUND RADIATING ACROSS THE CORNER OF THE FIRST HOLE ON THE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL ON THE FAIRING ATTACHMENT FLANGE. A NEW PART WAS INSTALLED IAW THE REQUIREMENTS OF AD2004-01SDR M7K2008F00121Transmitter · intermittentPILOT REPORTED THAT THE MAIN GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED INTERMITTENTLY AT IDLE. A NEW OIL PRESSURE TRANSMITTER WAS INSTALLED AND NO FURTHER FALSE INDICATIONS NOTED. THIS SWITCH HAS A MODERATE FAILURE RATE USUALLY BY LOSING ITS LOW ENDSDR M7K2008F00097Potentiometer · intermittentAT FULL BRIGHTNESS ADJUSTMENT ALL CONTROLLED LIGHTING FLICKERS ON AND OFF INTERMITTENTLY. REPLACEMENT WITH NEW PART CORRECTED THE DEFECT. (K)SDR M7K2008F00073Potentiometer · defectivePILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER AS THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FOR THIS PART THAT HASSDR M7K2008F00061Potentiometer · 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 M7K2008F00126Handle · brokenUPON LANDING PILOT FOUND HANDLE TO BE LIMP AND FLOPPING IN THE SLIPSTREAM. DOOR HAD TO BE OPENED UTILIZING THE INSIDE HANDLE. BELLCRANK LEVER WHICH CONNECTED OUTSIDE HANDLE TO THE DOOR LATCHING MECHANISM HAD BROKEN. A NEW DOOR HANDLE ASSY WAS INSTALLED. (KSDR M7K2008F00133Switch · intermittentPILOT REPORTED THAT SEVERAL SELECTIONS TO THE ENGINE START POSITION WERE REQUIRED TO GET THE ENGINE TO START. UPON CLOSER INSP IT WAS DETERMINED THAT SELECTING THE ON OR START POSITION GENTLY WITHOUT SNAPPING THE LEVER INTO THE START POSITION COULD CAUSE THE
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