- Registered owner
- Mustang Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 4038
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- October 2, 2008
- Expires
- July 31, 2028
- Mode S code
- AB20C1
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 N816MHMatched 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 N816MHMatched 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 M7KA0804084038Bracket · crackedFOUND CRACKED DURING ROUTINE PERIODIC INSPECTION. INSTALLED NEW BRACKET AS REQUIRED. (K)SDR M7KA0716084038Exciter · inoperativeDURING ROUTINE INSPECTION THE LT POSITION IGNITER WOULD NOT FIRE. SWAP OF BOX OUTPUT FEEDS TO THE IGNITERS VERIFIED THE BOX CIRCUIT WAS DEFECTIVE. THIS BOX GAVE GOOD SERVICE BUT SEVERAL OTHER HAVE HAD PROBLEMS WITH LOW SERVICE HOURS THESE BOXES ARE NON-REPAIRASDR M7K2008F00043Fitting · crackedCRACK DISCOVERED DURING ROUTINE INSP 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 MFG FROM A MORE DURABLE MATERIAL SUCH AS TITANIUM OR SDR M7K2008F00026Potentiometer · 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 M7K2008F00130Wire · shortedDURING PREFLIGHT INSP POSITION LIGHTS FAILED TO ILLUMINATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. A SHORT WAS LOCATED IN THE TAIL POSITION LIGHT WIRING AND A REPAIR EMBODIED. RESETTING THE BREAKER FOR A GROUND TEST REVEALED NO FUNCTION FOLLOWINSDR M7K2008F00083Light · failedDURING PREFLIGHT INSP, ANTI-COLLISION LIGHT FAILED TO ILLUMINATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. RESETTING THE BREAKER FOR A GROUND TEST REVEALED NO FUNCTION. THIS PART HAS BEEN DEEMED NOT REPAIRABLE BY THE AIRFRAME MFG. (K)SDR M7K2008F00079Fitting · crackedCRACK FOUND DURING ROUTINE INSPECTION ON THE MOUNTING FLANGE SURFACE RADIATING FROM A MOUNTING BORE AND TO THE EDGE OF THE FLANGE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K)SDR M7K2008F00077Fitting · crackedCRACK FOUND DURING ROUTINE INSPECTION RADIATING FROM A SCREW HOLE TO THE EDGE OF THE MACHINED FLANGE AND ACROSS THE ENTIRE FLANGE. PART WAS REMOVED IN TWO PIECES. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K)SDR M7K2008F00127B-Nut · leakingHOSE FOUND TO BE LEAKING NOT FROM THE B-NUT BUT A THE FITTING JUNCTION WITH THE HOSE MATERIAL. NEW REPLACEMENT HOSE INSTALLED AND NO FURTHER LEAKAGE NOTED. IN 55,000 FLIGHT HOURS THIS IS THE ONLY PROBLEM WE HAVE HAD WITH THIS HOSE. LEAK WAS CONSIDERED MINORSDR M7K2008F00085Freq Adapter · failedDURING A PREFLIGHT INSPECTION PILOT, DISCOVERED ONE FREQUENCY ADAPTER WITH A 20MM CRACK IN THE ELASTOMER. MM LIMITATION IS 10MM. THIS IS A COMMON FAILURE WHICH OCCURS AT HALF LIFE OR LESS FOR THIS PART WITH A 3000 HOUR SERVICE LIFE LIMIT. THE OLDER PN ELASTSDR M7K2008F00145Combustion Liner · crackedDURING ROUTINE MONITORING OF EXISTING CRACKS WHICH HAD, TO THIS TIME, REMAINED WITHIN MM LIMITATIONS FOR A REDUCED INTERVAL INSP, NO TO EXCEED 150 FLIGHT HOURS. PARALLEL CRACKS HAVE INTERSECTED WITH THE POSSIBILITY FOR A PIECE TO BREAK FREE AND BE INGESTED BYSDR M7K2008F00112Potentiometer · intermittentTHIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOTALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTL
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