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Aircraft record

N822MH2006 Eurocopter EC 130 B4

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:1 NTSB accident (substantial damage, Oct 2010)13 ADs may apply10 service difficulty reports

Registration
Valid
expires Jul 31, 2028
Based in
Henderson, NV
owner city / state
Engine
ARRIEL 2B1 · 747 hp
Turbomeca
Owners
1
since 2008
NTSB events
1
substantial, 2010
ADs may apply
13
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Mustang Leasing LLC
Owner type
LLC
City, state
Henderson, NV
Certificate issued
Oct 2, 2008
Expires
Jul 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Jan 23, 2007

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Eurocopter
Model
EC 130 B4
Year
2006
Serial number
4142
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
H9EU
Mode S code
AB3964

Engine

Make and model
Turbomeca Arriel 2b1
Type
Turbo-shaft
Power
747 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2008 – nowMustang Leasing LLCHenderson, NV · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Oct 1, 2010 · Meadview, AZ

The pilot's distraction with another departing helicopter while maneuvering in a hover for departure, which resulted in his failure to maintain clearance between the tail rotor and an umbrella.

Damage
Substantial
Injuries
None
Report
WPR10LA481

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR10LA481)

Accident history for this model

ADs published since 1998 that may apply (13)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2016-25-13Safran Helicopter Engines, S.A. (Formerly Turbomeca S.A.) Turboshaft EnginesFeb 3, 2017Engine (ARRIEL 2B1)Only with: Engine accessory gearbox (AGB) P/N 0292120650 with a machined front casing installed.
2015-13-04Turbomeca S.A. Turboshaft EnginesSep 1, 2015Engine (ARRIEL 2B1)
2014-12-05Turbomeca S.A. Turboshaft EnginesAug 4, 2014Engine (ARRIEL 2B1)
2014-07-06Turbomeca S.A. Turboshaft EnginesMay 15, 2014Engine (ARRIEL 2B1)Only with: Engines that do not have modification TU157 incorporated.
2012-18-18Turbomeca S.A. Turboshaft EnginesOct 24, 2012Engine (ARRIEL 2B1)Only with: Engines not modified by TU166 modification.
Show all 13 ADs
ADSubjectEffectiveApplies to
2012-03-11Turbomeca S.A. Turboshaft EnginesMar 20, 2012Engine (ARRIEL 2B1)
2011-06-07Eurocopter France (Eurocopter) Model EC130 B4 HelicoptersApr 6, 2011Airframe (EC 130 B4)Only with: Flotation gear unit "1G" (1G unit), P/N 350A63256300, installed.
2009-09-03Turbomeca S.A. Arriel 2B and 2B1 Turboshaft EnginesJun 1, 2009Engine (ARRIEL 2B1)
2009-08-08Turbomeca Arriel 1B, 1D, 1D1, 2B, and 2B1 Turboshaft EnginesApr 29, 2009Engine (ARRIEL 2B1)Serial numbers per Figure 1 of Turbomeca Alert MSB No. A292 72 0827, Version A (Arriel 1B/1D/1D1) and Figure 1 of Turbomeca Alert MSB No. A292 72 2833, Version A (Arriel 2B/2B1), both dated March 20, 2009. Only with: Engines with power turbine modules M04 installed, as listed by SN in the referenced service bulletins.
2009-01-11Turbomeca Arriel 2B and 2B1 Turboshaft EnginesFeb 27, 2009Engine (ARRIEL 2B1)
2007-19-09Turbomeca Arriel 2B1 Turboshaft EnginesOct 3, 2007Engine (ARRIEL 2B1)
2007-10-06Turbomeca Arriel 2B1 Turboshaft EnginesMay 29, 2007Engine (ARRIEL 2B1)
2005-25-13Turbomeca Arriel 2B and 2B1 Turboshaft EnginesDec 28, 2005Engine (ARRIEL 2B1)Only with: Engines without modification TU22 incorporated.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (10)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Fuselage · doubler · undersizeMar 11, 2009

    TAILBOOM SKIN CRACK WAS DISCOVERED DURING ROUTINE PERIODIC CLEANING AND INSPECTION FOLLOWING REMOVAL OF THE HORIZONTAL STABILIZER DURING UNRELATED DEFECTIVE PART REPLACEMENT. THIS CRACK WAS CONCEALED BENEATH A TAIL CONE DOUBLER WHEN EXTERNALLY VIEWED BUT EASILY SEEN WITH THE STABILIZER REMOVED AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · actuator · intermittentNov 17, 2008

    GOVENOR LIGHT ILLUMINATES INTERMITTENTLY WITH THIS EMERGENCY BACKUP CONTROL. ACTUATOR INSTALLED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · labyrinth seal · leakingSep 1, 2008

    ENGINE SMOKING FOLLOWING SHUTDOWN WAS THE OBSERVED SYMPTOM. CLOSER INSPECTION REVEALED TRACES OF OIL STREAKING FROM POWER TURBINE BLADE ROOTS. A SERVICEABLE LABYRINTH RING ASSEMBLY HAS BEEN INSTALLED. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Main rotor drive · seal · leakingSep 1, 2008

    FOUND LEAKING EXCESSIVELY BOTH STATICALLY AND IN OPERATION DURING ROUTINE INSPECTION. INSTALLED NEWLY OVERHAULED FREE WHEEL SHAFT ASSY WITH NO FURTHER LEAKAGE NOTED. TEAR DOWN OF REMOVED ASSY REVEALED SEAL LIP HAD BEEN DAMAGED DURING ASSY. AS THE SHAFT WAS REPORTED TO BE INSTALLED FOR TEST CELL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · pressure sensor · intermittentAug 4, 2008

    OIL PRESSURE LIGHT ILLUMINATES AT GROUND IDLE. NEW SWITCH INSTALLED. NO FURTHER DEFECT NOTED. THIS 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.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Indicating and recording systems · warning system · failedJun 12, 2008

    WHEN AC POWER WAS TURNED ON ALL WARNING LIGHTS OF CENTRAL WARNING PANEL ILLUMINATED AS IF WARNING LIGHT TEST SWITCH WAS ACTIVATED. A NEW ASSY WAS INSTALLED AND NO FURTHER DEFECT NOTED. PREVIOUS EXPERIENCE AN INTERNAL SHORT WAS FOUND THAT CAUSED THIS PROBLEM, THIS IS A RARE FAILURE OF THIS PART. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedApr 14, 2008

    DURING ROUTINE INSP, A CRACK WAS DISCOVERED STARTING AT ATTACHMENT BORE HOLE AND RADIATING OFF THE EDGE OF THE ATTACHMENT FLANGE. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · chip detector · contaminatedApr 10, 2008

    ENGINE CHIP WARNING LIGHT ILLUMINATED. AN UNEVENTFUL PRECAUTIONARY LANDING TO FIRST SUITABLE SPOT PERFORMED. ALL ENGINE CHIP DETECTORS WERE INSPECTED FOR ABNORMAL METAL. ONE, NOT RECOVERABLE, HAIRLIKE SLIVER, FOUND ON THE ELECTRICITY WIRED DETECTOR WAS REMOVED. GROUND PENALTY RUN COMPLETED. NO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · hinge · crackedMar 24, 2008

    DURING 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. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · seal · leakingSep 17, 2007

    SEAL FOUND LEAKING FUEL OVERBOARD WITH FUEL BOOST PUMP PRESSURE APPLIED. FOLLOWING STARTUP AND SHUTDOWN OF THE FUEL BOOST PUMP FUEL LEAK SLOWED BUT CONTINUED AND WAS BEYOND ALLOWABLE LIMITS OF THE MM. THIS IS A VERY COMMON PROBLEM WITH ALMOST ALL CONTROLS REQUIRING SEAL REPLACEMENT TYPICALLY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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