- Registered owner
- Mustang Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 4134
- Year built
- 2006
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 24, 2006
- Certificate issued
- January 30, 2007
- Expires
- April 30, 2029
- Mode S code
- AB35AD
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 N821MHMatched 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 N821MHMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7KA201610111134Pump · leakingDURING ROUTINE INSPECTION, A HYDRAULIC FLUID LEAK WAS NOTED ON THE BELT DRIVEN HYDRAULIC PUMP DRIVE AND A PREVIOUSLY REPAIRED YELLOW TAGGED PUMP ASSEMBLY INSTALLED. THE REPLACEMENT PUMP DRIVE SHAFT LIP SEAL HAD BEEN REPLACED AS PART OF THE REPAIR. A NORMAL GROSDR M7KA20110501#4134Skin · misrepairedDURING PREFLIGHT INSP, A CRACK WAS DISCOVERED RADIATING FROM THE INSIDE LOWER AFT RT CORNER OF THE TAIL BOOM TAIL CONE CUTOUT FOR THE HORIZ STABILIZER. AN OVER LYING DOUBLER WAS NOT CRACKED AND OBSCURED THE CRACK FROM EASY VIEWING. WITH THE HORIZ STABILIZER SDR M7KA1030084134Freq Adapter · crackedDURING ROUTINE MX INSPECTION 1 OF THE 3 FRQUENCY ADAPTERS FOUND TO HAVE A CRACK IN THE ELASTOMER NEARING ITS MAXIMUM ALLOWABLE LIMITATION OF 10MM. A NEW KIT OF 3 MATCHED ADAPTERS WERE INSTALLED.SDR M7KA0628084134Wire Harness · damagedFAILURE CODE AT SHUTDOWN INDICATED FAULT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED AND NO FURTHER DEFECT REPORTED. IT WAS RECENTLY DISCOVERED THAT THE ROUTING OF AIR CONDITIONING SYSTEM WIRING IN CONTACT WITH THE UNSHIELDED ELECTRICASDR M7K2008F00046Control Panel · failedPOSITION LIGHTS FAILED TO ILLUMINATE WITH CB NOT POPPED AND NO APPARENT SHORTS FOUND. INVESTIGATION REVEALED CIRCUIT TRACE ON THE PCB SUPPLYING POWER TO THE POSITION LIGHT SWITCH HAD MELTED/BLOWN LIKE A FUSE. THIS A COMMON PROBLEM FOR THIS PART. SUGGEST MORESDR M7K2008F00045Spacer · wornDURING ROUTINE INSP, SPACER WAS FOUND WITH EXCESSIVE WEAR AT ENDS WHERE IT MAKES SCISSOR LINK BUSHING CONTACT. POSSIBLE DIRT ACCUMULATION IN THE GREASE WAS A FACTOR IN THE WEAR. THIS IS A COMMON FAILURE FOR THIS PART. SUGGEST THIS PART BE KEPT CLEAN IN SANDSDR M7K2008F00020Fitting · crackedDURING ROUTINE INSP FITTING WAS FOUND CRACKED IN (2) PIECES. NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THIS PART. PART MAY HAVE BEEN SHIMMED INCORRECTLY OR BORE HOLE NOT ALIGNED PERFECTLY. SUGGEST A MORE DURABLE MATERIAL BE USED IN THIS PARTS MFSDR M7K2008F00010Freq Adapter · cracked(REF 0429084134) DURING ROUTINE INSPECTION, THE ELASTOMER ON (1) FREQUENCY ADAPTER WAS FOUND CRACKED. A NEW SET OF (3) ADAPTERS WAS INSTALLED. THIS IS A VERY COMMON DEFECT FOR THIS PART. SUGGEST A DIFFERENT ELASTOMER FORMULATION BE UTILIZED. AN OLDER PN FREQSDR M7K2008F00005Hinge · cracked(REF 0429084134) DURING ROUTINE INSPECTION, HINGE WAS FOUND CRACKED THROUGH TO SCREW MOUNTING BORES TO THE METALS EDGE. THIS IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST PART BE MFG OF MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL. (K)SDR M7K2008F00090Hinge · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. THIS IS A VERY COMMON FAILURE FORSDR M7K2008F00000Latch · failedTHIS PART CALLED A SHOCK ABSORBER DEVICE BY THE MFG IS USED TO SEQUENCE THE DOOR LATCHING MECHANISM TO PREVENT DOOR CLOSURE WITH LATCH PINS EXTENDED AND IMPACTS WITH THE DOOR FRAME. IT IS MFG OF A VERY BRITTLE BRONZE TYPE MATERIAL THAT WILL CRACK WITH JUST TH
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