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Aircraft record

N609CF2001 Agusta Spa A119

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 1, 2022.

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply5 service difficulty reports

Registration
Deregistered
Last based in
Greenwood Village, CO
owner city / state
Engine
PT6B-37A · 900 hp
P&W Canada
Owners
1
since 2013
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Tristate Careflight LLC
Owner type
LLC
City, state
Greenwood Village, CO
Certificate issued
Aug 21, 2013
Canceled
Nov 1, 2022
Airworthiness
Standard · Normal
Airworthiness date
Sep 3, 2013

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
2001
Serial number
14018
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
A7E8E6

Engine

Make and model
P&W Canada Pt6b-37a
Type
Turbo-shaft
Power
900 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. 2013 – 2022Tristate Careflight 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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (2)

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
2020-18-05Fuel Control/ Turbine EnginesOct 7, 2020Engine (PT6B-37A)Certain serial numbers: PT6B-37A …–PCE-PU0289. Only with: Engines without an installed FCU incorporating a stainless steel air adapter per P&WC SB No. PT6B-72-39107, Revision No. 1.
2019-22-03Turbine Engine Reduction GearDec 24, 2019Engine (PT6B-37A)Certain serial numbers: PT6B-37A …–PCE-PU0275; PT6B-37A PCE-PU0278

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

Service Difficulty Reports (5)

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 · not reported · crackedApr 27, 2018

    ONE CRACK FOUND AT B.L. 510, STATION 3627 W.L. 1349 MEASURING 30MM IN LENGTH. / TWO CRACKS FOUND AT STATION 4010, BUTT LINE 6, WATER LINE 1020 MEASURING 30MM & 50MM. / TWO CRACKS FOUND AT STATION 4010, BUTT LINE 0 & 1, WATER LINE 1020 MEASURING 8MM & 10MM. / ONE CRACK FOUND AT B.L. 250, STATION…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · blade · crackedApr 9, 2018

    1.5 INCH CRACK FOUND ON TRAILING EDGE OF BLADE FAIRING. CRACK STARTS AT 60MM FROM TOP OF BLADE FAIRING AND RUNS DOWN AND UNDERNEATH BLADE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedDec 19, 2017

    AFTER PILOT WASHED AIRCRAFT, BS 8081, WL 1300 ON PILOTS SIDE OF TAIL BOOM THERE WAS A 2.5 INCH CRACK SEEN BETWEEN THE MOUNTED STRINGER RIVET LINES. A SECOND CRACK WAS LOCATED AT BS 8085, WL 1400 ON PILOTS SIDE OF TAILBOOM THERE WAS A 2.25 INCH CRACK NOTED AFTER A DYE PEN INSPECTION ON THE UPPER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Fuselage · doubler · crackedJan 11, 2017

    DURING DAILY AIRWORTHINESS CHECK, AN APPROXIMATELY 1/2" CRACK WAS FOUND ON THE RIGHT HAND TAILROTOR GEARBOX MOUNT BULKHEAD DOUBLER PN 109-0373-21-104. CRACK IS LOCATED IN THE RADIUS BEND OF DOUBLER TOWARDS UPPER RIGHT HAND EDGE BEHIND NUTPLATE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor drive · transmission · making metalMay 16, 2016

    AIRCRAFT WAS PREPARING TO TAKEOFF AFTER START UP, WHEN THE MAIN TRANSMISSION CHIP LIGHT ILLUMINATED. PILOT SHUTDOWN THE ACFT. REMOVED MAIN TRANSMISSION CHIP DETECTOR & FOUND IT SATURATED WITH METAL PARTICLES. IAW THE MM, DRAINED & FLUSHED THE MAIN TRANSMISSION OIL SYS, CHANGED THE OIL FILTER, &…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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