- Registered owner
- Mustang Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 4125
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- November 29, 2006
- Expires
- October 31, 2028
- Mode S code
- AB2478
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 N817MHMatched 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 N817MHMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7KA201301301125Bearing · failedON SHORT FINAL TO LANDING, ACFT CAUTION WARNING PANEL ENGINE CHIP LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN NORMALLY, INSPECTION OF THE CHIP DETECTORS, METAL WAS FOUND THAT APPEARED TO BE MORE THAN TYPICAL. CLEANED THE CHIP PLUGS, A 10 MINUTE PENALTY GROUND SDR M7KA20090211#4125Spar · crackedDURING REPAIR OF ADJACENT TAILCONE SKIN CRACKS A DETAILED VISUAL INSP OF THE UPPER RT HORIZONTAL STABILIZER SPAR REVEALED A CRACK RADIATING FROM A SINGLE STABILIZER ATTACHMENT FITTING, ATTACHMENT BORE AROUND THE SPAR'S FLANGE RADIUS AND ENDING AT A RIVET BORE SDR M7KA20090212#4125Skin · crackedTAILBOOM CONE SKIN AND SKIN DOUBLER CRACKS WERE DISCOVERED DURING ROUTINE 100 HOUR INTERVAL IMPS LOCATED ADJACENT TO THE RT, AFT, LWR HORIZONTAL STABILIZER'S TAILBOOM THROUGH MOUNT CUTOUT.SDR M7KA0809084125Light · inoperativeNAV LIGHT ASSY, FOUND INOPERATIVE DURING ROUTINE POST FLIGHT INSPECTION, INSTALLED NEW REPLACEMENT, OPERATIONAL CHECK WAS CORRECT. THIS PART HAS HAD VIBRATION RELATED FAILURES IN OUT FLEET ON SEVERAL OCCASIONS. (K)SDR MK7A0811084266Fairing · crackedFOUND CRACKS RADIATING FROM A SINGLE SCREW BORE DURING ROUTINE INSPECTION. INSTALLED NEWLY REPAIRED AND PAINTED ASSY. FOLLOWING DOUBLER INSTALLATION AT SCREW BORE POSITIONS. THIS PART HAS HAD A HISTORY OF SIMILAR CRACK DEVELOPMENT UNTIL DOUBLERS WERE APPLIED. SDR M7K2008F00004Hinge · crackedDURING ROUTINE INSPECTION, HINGE WAS FOUND CRACKED THROUGH A SCREW MOUNTING BORE TO THE METALS EDGE. THIS IS A VERY COMMON FAILURE FOR THIS PART. (K)SDR M7K2008F00054Hinge · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. THIS IS A VERY COMMON FAILURE FOR THIS PART. (K)SDR M7K2008F00002Hinge · crackedDURING ROUTINE 100 HOUR INSP, A CRACK IN THE HINGE OF THE ENGINE FAIRING WAS FOUND RADIATING FROM THE 2ND HOLE FROM ONE END OF THE HINGE WITH THE CORNER HAVING SEPARATED FROM THE HINGE FROM CRACKS EMANATING FROM THE 1ST HOLE. THIS IS A COMMON FAILURE FOR THISSDR M7K2008F00001Freq Adapter · crackedDURING ROUTINE 100 HOUR INSPECTION, A CRACK IN THE BLUE BLADE ELASTOMER WAS FOUND ON THE T/E LWR IB SURFACE RADIATING FROM THE INSPECTION BORE. THIS CRACK HAD REACHED THE MM LIMITATION OF 10MM IN TOTAL LENGTH. THIS IS A VERY COMMON FAILURE FOR A PART WITH A SDR M7K2008F00080Blower Motor · seizedPILOT REPORTED BLOWER VERY NOISY/GROWLS IN OPERATION. CLOSER EXAMINATION REVEALED VERY ROUGH SHAFT BEARING. A NEW REPLACEMENT MOTOR WAS INSTALLED. THIS BLOWER MOTOR IS USUALLY VERY RELIABLE IF A BIT NOISY IN NORMAL OPERATION. LIKELY CAUSE IS POOR QUALITY O
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