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Aircraft record

N197BH1992 Eurocopter AS 350 B2

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:2 NTSB accidents (destroyed damage at worst, latest Sep 2014)4 ADs may apply13 service difficulty reports

Registration
Valid
expires Jan 31, 2029
Based in
Greenwood Village, CO
owner city / state
Engine
ARRIEL 1SER · 681 hp
Turbomeca
Owners
1
since 2001
NTSB events
2
destroyed, 2014
ADs may apply
4
confirm with A&P
Service reports
13
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Nevada Helicopter Leasing LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Dec 14, 2001
Expires
Jan 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Mar 19, 1998

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
AS 350 B2
Year
1992
Serial number
2666
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H9EU
Mode S code
A1824D

Engine

Make and model
Turbomeca Arriel 1ser
Type
Turbo-shaft
Power
681 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. 2001 – nowNevada Helicopter Leasing LLCGreenwood Village, CO · 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 (2)

Accident · substantial damage

Sep 14, 2014 · Kahului, Maui, HI

The pilot's failure to maintain clearance from the cart while hovering. Contributing to the accident was the failure of ground personnel to remove the cart from the helipad.

Damage
Substantial
Injuries
None
Report
WPR14CA375

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR14CA375)

Accident · destroyed

Sep 8, 1994 · Cascade, CO

A POWER LOSS DUE TO CONTAMINATED FUEL FROM AN UNKNOWN SOURCE THAT CLOGGED THE FUEL FILTER AND INTERNALLY DAMAGED THE FUEL CONTROL UNIT. A FACTOR WAS UNSUITABLE TERRAIN FOR A FORCED LANDING.

Damage
Destroyed
Injuries
Minor
Report
FTW94FA293

From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW94FA293)

Accident history for this model

ADs published since 1998 that may apply (4)

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
2013-23-09Eurocopter France HelicoptersDec 27, 2013Airframe (AS 350 B2)Only with: Helicopters with sliding doors installed, except those with modification AL.4262.
2013-21-01Eurocopter France (Eurocopter) HelicoptersOct 25, 2013Airframe (AS 350 B2)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed.
2013-08-19Eurocopter France HelicoptersJun 5, 2013Airframe (AS 350 B2)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed.
2010-11-51Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, C, D, and D1 Helicopters and…Sep 2, 2010Airframe (AS 350 B2)Only with: Tail gearbox control lever P/N 350A33-1058-00, -01, -02, or -03 not marked with an "X" near the P/N installed.

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

Service Difficulty Reports (13)

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.

  • Rotor flight controls · control servo · leakingJul 18, 2014

    DURING CRUISE FLIGHT, THE HYDRAULIC LIGHT ILLUMINATED AND THE HORN CAME ON. THE PILOT SLOWED THE ACFT AIRSPEED AND TURNED THE HYDRAULICS OFF. HE THEN PROCEEDED TO MAKE A RUN ON LANDING AT A PRIVATE AIRPORT. MECHANIC DISCOVERED THERE WAS NO HYDRAULIC FLUID IN THE RESERVOIR AND HYDRAULIC FLUID WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · compressor · failedJun 14, 2012

    TEN MINUTES INTO FLIGHT, PILOT NOTICED THAT THE AIR CONDITIONER STOPPED WORKING AND SHORTLY NOTICED SMOKE IN COCKPIT. TURNED OFF THE A/C AND THE SMOKE WENT AWAY. RETURNED TO BASE. ON EXAMINATION BY THE MX, IT WAS DETERMINED THE AC COMPRESSOR HAD FAILED INTERNALLY. AFTER REPLACING THE COMPRESSOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · brushes · arcedMay 30, 2007

    (10) MINUTES INTO A TOUR FLIGHT, THE PILOT NOTICED LOW VOLTAGE AND LOW FUEL PRESSURE, WITH NO (GEN) LIGHT ILLUMINATED. THE PILOT RETURNED TO THE HELIPORT. UPON INSPECTION, IT WAS FOUND THAT THE STARTER GENERATOR HAD A BURNING SMELL TO IT. THE STARTER GENERATOR WAS CHANGED AND THE AIRCRAFT OPERATED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Landing gear · float · deployedFeb 28, 2007

    WHILE DOING A PHOTO CHARTER, THE PILOT PRESSED THE ARM PUSHBUTTON TO ARM THE FLOAT SYSTEM AND THE FLOATS DEPLOYED. THE PILOT RETURNED TO THE HELIPORT. THE PILOT CLAIMS THE FLOAT FIRING PUSHBUTTON WAS IN THE REST POSITION, (NOT PUSHED IN). UPON INSPECTION OF THE SYSTEM, THERE WERE NO DISCREPANCIES…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · sensor · malfunctionedAug 22, 2006

    DURING A TOUR FLIGHT, THE HIGH RPM HORN CAME ON (INTERMITTENLY) IN FLIGHT WITH THE ROTOR RPM IN THE GREEN. AFTER LANDING BACK AT HOME BASE, MAINTENANCE TROUBLESHOT THE INTERMITTENT PROBLEM. AFTER REPLACING THE ROTOR TACHOMETER TRANSDUCER, THE PROBLEM DID NOT REOCCUR. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · relay · failedJul 18, 2002

    WHILE ON ROUTINE SIGHTSEEING TRIP, THE PILOT EXPERIENCED A FLICKERING GENERATOR FAILURE WARNING LIGHT WHILE TAKING OFF FROM THE AIRPORT. CONTINUED FLIGHT UNTIL RECEIVED A STEADY GENERATOR FAILURE WARNING LIGHT. RETURN TOT AIRPORT. UPON INSPECTION BY MAINTENANCE PERSONNEL IT WAS DETERMINED THAT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · rod · wornJul 6, 2001

    PART IS WORN BEYOND LIMITS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · rod · wornSep 20, 2000

    PART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS UNDER WARRANTY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · rod · wornSep 20, 2000

    PART IS WORN BEYOND LIMITS.PLEASE REPLACE BEARINGS UNDER WARRANTY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor drive · bearing · wornOct 25, 1999

    PITCH CONTROL WORN BEYOND LIMITS. TIME ON PART IS UNKNOWN.

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

Showing the 10 most recent of 13 reports.

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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