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
Agusta Spa
Model
A119
Year
2000
Serial number
14006
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
8
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H7EU
Mode S code
A1AC3C
Engine
Make and model
P&W Pt6 Series
Type
Turbo-shaft
Power
500 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2006 – 2022Tri State Care Flight LLCGreenwood Village, CO
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Incident · minor damage
Oct 20, 2012 · Dolan Springs, AZ
Insufficient clearance between a truck and the main rotor blades of a helicopter on the ground with the engine running because of the lack of on-scene coordination between the agencies that responded to and were tasked with managing the vehicle accident site.
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (7)
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.
DURING FLIGHT APPROX 20 MINUTES INTO IT ENGINE OIL PRESSURE LIGHT CAME ON. PILOT MADE PRECAUTIONARY LANDING IN CLEAR AREA. THE OIL PRESSURE GAUGE WAS STILL SHOWING GOOD PRESSURE, BUT THE LIGHT WAS ILLUMANTED ON MASTER CAUTION PANEL. REMOVED AND REPLACED OIL PRESSURE SWITCH WITH NEW ONE, CLEARED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · bulkhead · crackedApr 18, 2018
WHILE PERFORMING REPAIR OF RT FORWARD PILOT OVERHEAD BULKHEAD FRAME IAW SRM 04-01-19, MULTIPLE CRACKS WERE DISCOVERED WHEN SEALANT WAS REMOVED AND OLD FRAME WAS REMOVED. ON FUSELAGE STATION 2049.5, WL 1550, LBL 520 LT AND RT SIDES UPPER BULKHEADS HAVE 1-2 INCH CRACKS IN SKIN ABOVE PILOT AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Electrical power · wire · brokenFeb 19, 2017
DURING CRUISE, SMELLED A STONG ACRID ODOR WHICH APPEARED TO BE THAT OF AN ELECTRICAL PROBLEM. MONITORED THE GAUGES AND SAW NO INDICATION OF ANY MALFUNCTION. CHECKED THE COCKPIT FOR ANY SMOKE AND NONE NOTED. CONTINUE TO THE CLOSEST AIRPORT, ON LANDING AND SHUTDOWN, DID NOT FIND ANY INDICATIONS OF…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
Electrical power · circuit breaker · failedNov 28, 2016
WHILE AIRCRAFT WAS RETURNING TO BASE, SMOKE AND A BURNING SMELL WAS COMING FROM THE UPPER CIRCUIT BREAKER PANEL CLOSE TO THE GOVERNOR CONTROL BREAKER. AFTER FURTHER TROUBLESHOOTING, IT WAS DETERMINED THAT A WIRE FOR THE GOV CONTROL BREAKER HAD CHAFED NEXT TO A STANDOFF AND METAL SUPPORT. THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Fuselage · retainer · crackedSep 12, 2016
ON THE EVENING OF 9/21/2016, A CRACK WAS DISCOVERED VERTICALLY ADJACENT OF THE LT A/F DOOR PILLAR LATCH DURING A PREFLIGHT BY THE PILOT. A REPAIR SCHEME HAS BEEN REQUESTED FROM MFG FOR A/F PILLAR AND A/F SLIDING DOOR POST OUTER SHEET METAL COVER IS ON ORDER.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Main rotor drive · gear · crackedApr 12, 2012
DURING 4800 HR O/H INSPECTION, SUBJECT GLEASON CROWN GEAR WAS FOUND TO HAVE A CRACK.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Engine fuel and control · fuel control · malfunctionedJun 7, 2009
THIS DISCREPANCY WAS TROUBLESHOT FOR SEVERAL DAYS, THE INITIAL DISCREPANCY WAS NR DROP TO 96 PERCENT WITH A COLLECTIVE CHANGE THAN IT WENT TO 94 PERCENT WITH AN COLLECTIVE CHANGE AND FINALLY TO 94 PERCENT WITH NOT COLLECTIVE INPUT AT ALL. BOTH THE MECHANIC AND THE SUPERVISOR VERIFIED THAT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.