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Aircraft record

N123RXAgusta S P A A109K2

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 28, 2009.

Safety record in brief:1 NTSB accident (destroyed damage, Jun 2003)17 ADs may apply23 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Engine
ARRIEL 1SER · 681 hp
Turbomeca
Owners
1
since 1994
NTSB events
1
destroyed, 2003
ADs may apply
17
confirm with A&P
Service reports
23
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
I H C Hospitals INC DBA
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Apr 20, 1994
Canceled
May 28, 2009
Airworthiness
Standard · Normal
Airworthiness date
Dec 14, 1993

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 S P A
Model
A109K2
Serial number
10018
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
8
Engines
2
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H7EU
Mode S code
A06064

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. 1994 – 2009I H C Hospitals INC DBASalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · destroyed

Jun 8, 2003 · Salt Lake City, UT

Fatigue of the tail rotor trunnion resulting in complete trunnion failure and subsequent tail rotor separation from the helicopter. Factors contributing to the accident were the low altitude, low airspeed, excessive tail rotor loading, and the worn tail-rotor blade grip bushings.

Damage
Destroyed
Injuries
Fatal
Report
DEN03FA099

From NTSB records; matched by N-number.Read NTSB report (search CAROL for DEN03FA099)

ADs published since 1998 that may apply (17)

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
2021-07-05Leonardo S.p.a. (Type Certificate Previously Held by Agusta S.p.A.) (Leonardo) HelicoptersApr 8, 2021Airframe (A109K2)Only with: Main rotor blade P/N 709-0103-01 (all dash numbers) installed.
2020-15-16Tail Rotor Drive SystemAug 27, 2020Airframe (A109K2)Only with: Tail rotor blade retention bolt P/N 709-0160-57-101 installed.
2018-06-51Agusta S.p.A. HelicoptersJun 7, 2018Airframe (A109K2)Only with: Swashplate support P/N 109-0110-05-101 installed.
2016-18-18Agusta S.p.A. HelicoptersOct 20, 2016Airframe (A109K2)Only with: Tail rotor drive shaft assembly P/N 109-8412-02-1 or 109-8412-02-3 installed.
2015-11-08Agusta S.p.A. (Agusta) HelicoptersJun 24, 2015Airframe (A109K2)
Show all 17 ADs
ADSubjectEffectiveApplies to
2015-05-52Agusta S.p.A. HelicoptersApr 29, 2015Airframe (A109K2)Only with: Tail rotor pitch control link P/N 109-0130-05-117 installed with 100 hours or less time-in-service since overhaul.
2014-23-02Agusta S.p.A. Helicopters (Type Certificate Currently Held by AgustaWestland S.p.A.)…Dec 26, 2014Airframe (A109K2)Only with: Main transmission P/N 109-0400-03-103, 109-0400-05-103, or 109-0400-03-109 with Gleason crown P/N 109-0403-07-103 installed.
2014-11-07Agusta S.p.A Helicopters (Type Certificate Currently Held by AgustaWestland S.p.A)…Jun 18, 2014Airframe (A109K2)Only with: Nut P/N MS21042-4 connecting the main rotor swashplate support to the upper case of the main transmission installed.
2014-09-01AgustaWestland S.p.A. (Type Certificate Previously Held by Agusta S.p.A.) (Agusta)…Jun 5, 2014Airframe (A109K2)Only with: Tail rotor blade retaining bolt P/N 109-8131-09-1 installed.
2013-20-51AgustaWestland S.p.A. (Agusta) HelicoptersOct 25, 2013Airframe (A109K2)Only with: With a tail rotor drive shaft flexible disc coupling (Thomas coupling) nut P/N MS21042L4 installed.
2011-17-01Agusta S.p.A. Model A109A, A109A II, A109C, and A109K2 HelicoptersSep 12, 2011Airframe (A109K2)
2004-15-21Agusta S.p.A. Model A109K2 HelicoptersAug 17, 2004Airframe (A109K2)Only with: Tail rotor trunnion assembly P/N 109-0131-05 (all dash numbers) installed.
2003-12-13Agusta S.p.A. Model A109K2 HelicoptersJul 11, 2003Airframe (A109K2)Only with: Tail rotor blades P/N 109-8132-01-107 with 1,500 or more hours TIS installed.
2001-24-07Agusta S.p.A. Model A109C, A109E, and A109K2 HelicoptersJan 7, 2002Airframe (A109K2)Only with: Main rotor blade P/N 709-0130-01 (all dash numbers) with blade S/N up to and including 1428 with prefix "EM-" or "A5-" installed.
99-04-20Agusta S.p.A. Model A109K2 HelicoptersMar 4, 1999Airframe (A109K2)Only with: Breeze-Eastern rescue hoist P/N BL29700 (all dash numbers) installed.
99-02-09Agusta S.p.A. Model A109C and A109K2 HelicoptersJan 15, 1999Airframe (A109K2)
98-13-28Agusta S.p.A. Model A109C and A109K2 HelicoptersJul 13, 1998Airframe (A109K2)Only with: Tail rotor blades P/N 109-8132-01-107, serial number A5-all dash numbers, 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 (23)

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.

  • Main rotor · trunnion · scoredOct 26, 1999

    DURING A PRE-FLGIHT INSPECTION, PILOT NOTED FLAPPING OF TAIL ROTOR BLADES TO BE TIGHTER THAN NORMAL AND FELT TO BE ROUGH. MAINTENANCE NOTIFIED, TAIL ROTOR ASSY REMOVED AND INSPECTED. TAIL ROTOR TRUNNION WAS FOUND SCORED WITH TWO AREAS THAT APPEARED TO BE PITS. THE FIRST AREA WAS .75 INCH LONG AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · switch · intermittentOct 15, 1999

    SWITCH INTERMITTENTLY INOPERATIVE. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · hub assy · damagedOct 13, 1999

    DURING PRE-FLIGHT INSPECTION, PILOT NOTED THE FLAPPING OF THE TAIL ROTOR BLADES TO BE TIGHTER THA NORMAL AND FELT TO BE ROUGH. MAINTENANCE REMOVED AND INSPECTED TAIL ROTOR ASSEMBLY. THE TAIL ROTOR TRUNNION WAS FOUND SCORED WITH TWO AREAS THAT APPEARED TO BE PITS IN THE FIRST AREA WAS .75 INCHES…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Navigation · faceplate · damagedSep 13, 1999

    FACEPLATE DAMAGED AND UNREADABLE. P/N 58410A2B2C2D2F4L9N2. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · window · crackedAug 1, 1999

    WINDOW CRACKED IN SEVERAL PLACES. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · drive coupling · wornApr 27, 1999

    SPLINES WORN BEYOND TOLERANCE. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · rod ends · wornApr 23, 1999

    ROD ENDS WORN. REPLACED FOUR EACH. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · bushing · wornApr 23, 1999

    MRH SWASHPLATE FIXED SCISSORS. REPLACED BEARINGS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · damper · wornApr 23, 1999

    BUSHINGS WORN. PAC WOULD NOT SUPPLY BUSHING. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · rod end · wornApr 22, 1999

    ROD END WORN. (X)

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

Showing the 10 most recent of 23 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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