N109RX1993 Agusta S P A A109K2
This N-number isn't registered right now. Below is its last known registration, canceled Mar 11, 2019.
Safety record in brief:No NTSB accidents or incidents since 198226 ADs may apply17 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Ihc Health Services INC
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Nov 10, 2009
- Canceled
- Mar 11, 2019
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 29, 2011
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 dataAirframe
- Manufacturer
- Agusta S P A
- Model
- A109K2
- Year
- 1993
- Serial number
- 10016
- 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
- A027B0
Engine
- Make and model
- Turbomeca Arriel 1k1
- Type
- Turbo-shaft
- Power
- 738 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2009 – 2019Ihc Health Services INCSalt 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, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (26)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-13-14 | Engine (Turbine/Turboprop) | Jul 25, 2023 | Engine (ARRIEL 1K1) |
| 2021-07-05 | Leonardo S.p.a. (Type Certificate Previously Held by Agusta S.p.A.) (Leonardo) Helicopters | Apr 8, 2021 | Airframe (A109K2)Only with: Main rotor blade P/N 709-0103-01 (all dash numbers) installed. |
| 2020-15-16 | Tail Rotor Drive System | Aug 27, 2020 | Airframe (A109K2)Only with: Tail rotor blade retention bolt P/N 709-0160-57-101 installed. |
| 2018-06-51 | Agusta S.p.A. Helicopters | Jun 7, 2018 | Airframe (A109K2)Only with: Swashplate support P/N 109-0110-05-101 installed. |
| 2016-22-10 | Turbomeca S.A. Turboshaft Engines | Dec 6, 2016 | Engine (ARRIEL 1K1)Only with: Engines with modification TU376 installed. |
Show all 26 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2016-18-18 | Agusta S.p.A. Helicopters | Oct 20, 2016 | Airframe (A109K2)Only with: Tail rotor drive shaft assembly P/N 109-8412-02-1 or 109-8412-02-3 installed. |
| 2015-13-04 | Turbomeca S.A. Turboshaft Engines | Sep 1, 2015 | Engine (ARRIEL 1K1) |
| 2015-11-08 | Agusta S.p.A. (Agusta) Helicopters | Jun 24, 2015 | Airframe (A109K2) |
| 2015-05-52 | Agusta S.p.A. Helicopters | Apr 29, 2015 | Airframe (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. |
| 2014-23-02 | Agusta S.p.A. Helicopters (Type Certificate Currently Held by AgustaWestland S.p.A.)… | Dec 26, 2014 | Airframe (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. |
| 2014-11-07 | Agusta S.p.A Helicopters (Type Certificate Currently Held by AgustaWestland S.p.A)… | Jun 18, 2014 | Airframe (A109K2)Only with: Nut P/N MS21042-4 connecting the main rotor swashplate support to the upper case of the main transmission installed. |
| 2014-09-01 | AgustaWestland S.p.A. (Type Certificate Previously Held by Agusta S.p.A.) (Agusta)… | Jun 5, 2014 | Airframe (A109K2)Only with: Tail rotor blade retaining bolt P/N 109-8131-09-1 installed. |
| 2013-24-05 | Turbomeca S.A. Turboshaft Engines | Jan 28, 2014 | Engine (ARRIEL 1K1)Serial numbers per Figure 2 of Turbomeca S.A. Alert MSB No. A292 72 0838, Version A, dated May 24, 2013. Only with: Equipped with free turbine (FT) module (M04) with part and serial numbers listed in Figure 2 of Turbomeca Alert MSB No. A292 72 0838. |
| 2013-20-51 | AgustaWestland S.p.A. (Agusta) Helicopters | Oct 25, 2013 | Airframe (A109K2)Only with: With a tail rotor drive shaft flexible disc coupling (Thomas coupling) nut P/N MS21042L4 installed. |
| 2012-27-02 | Turbomeca S.A. Turboshaft Engines | Feb 14, 2013 | Engine (ARRIEL 1K1) |
| 2012-24-03 | Turbomeca S.A. Turboshaft Engines | Jan 7, 2013 | Engine (ARRIEL 1K1)Only with: Engines that have not incorporated Turbomeca S.A. Modification TU360. |
| 2011-17-01 | Agusta S.p.A. Model A109A, A109A II, A109C, and A109K2 Helicopters | Sep 12, 2011 | Airframe (A109K2) |
| 2009-26-07 | Turbomeca Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K1, 1S, and 1S1 Turboshaft… | Jan 12, 2010 | Engine (ARRIEL 1K1)Serial numbers per Figure 1 of Turbomeca Mandatory Service Bulletin No. A292 72 0825, Version B. Only with: Engines modified by Turbomeca Modification TU332 and fitted with a reduction gearbox (module M05) listed by serial number in the MSB. |
| 2004-15-21 | Agusta S.p.A. Model A109K2 Helicopters | Aug 17, 2004 | Airframe (A109K2)Only with: Tail rotor trunnion assembly P/N 109-0131-05 (all dash numbers) installed. |
| 2003-16-03 | Turbomeca Arriel 1 Series Turboshaft Engines | Sep 12, 2003 | Engine (ARRIEL 1K1)Only with: Engines that have not incorporated modification TU 202. |
| 2003-12-13 | Agusta S.p.A. Model A109K2 Helicopters | Jul 11, 2003 | Airframe (A109K2)Only with: Tail rotor blades P/N 109-8132-01-107 with 1,500 or more hours TIS installed. |
| 2001-24-07 | Agusta S.p.A. Model A109C, A109E, and A109K2 Helicopters | Jan 7, 2002 | Airframe (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. |
| 2000-20-01 | Turbomeca Arriel 1 Series Turboshaft Engines | Oct 17, 2000 | Engine (ARRIEL 1K1) |
| 99-04-20 | Agusta S.p.A. Model A109K2 Helicopters | Mar 4, 1999 | Airframe (A109K2)Only with: Breeze-Eastern rescue hoist P/N BL29700 (all dash numbers) installed. |
| 99-02-09 | Agusta S.p.A. Model A109C and A109K2 Helicopters | Jan 15, 1999 | Airframe (A109K2) |
| 98-13-28 | Agusta S.p.A. Model A109C and A109K2 Helicopters | Jul 13, 1998 | Airframe (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 (17)
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.
- Landing gear · pitch control · separatedMar 20, 2010
DURING CRUISE FLIGHT, PILOT NOTED A SLIGHT VIBRATION IN THE MAIN ROTOR SYS. THE FLIGHT WAS COMPLETED. UPON POST FLIGHT 1 OF THE 4 UPPER PITCH CHANGE LINK ROD ENDS WERE FOUND TO BE SIGNIFICANTLY WORN. A DETAILED INSP BY MX REVEALED THE PITCH CHANGE LINK ROD END PN 709-0101-18-111 HAD WORN TO THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Tail rotor · nut · looseMay 20, 2008
DURING PREFLIGHT INSPECTION, PILOT NOTED THE TAIL ROTOR BALANCE WHEEL HAD SLIGHT ROTATIONAL MOVEMENT. MAINTENANCE WAS DISPATCHED TO INSPECT THE TAIL ROTOR ATTACHMENT. TAIL ROTOR RETENTION NUT 109-0130-85-1 WAS LOOSE CAUSING SLIGHT WEAR TO THE TAIL ROTOR GEARBOX OUTPUT SHAFT(SPLINES) AND TRUNNION…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · crackedApr 7, 2008
DURING A 3,000-HOUR INSPECTION THE UPPER LT TAILBOOM ATTACH FITTING WAS FOUND TO HAVE A 2-INCH CRACK. THIS EXACT LONGERON/ATTACH FITTING WAS REPLACED JUNE 2004 AT AIRCRAFT TOTAL TIME 5626.7 THE ORIGINAL REPAIR WAS COMPLETED AND APPROVED ON FAA FORM 337 DATED JUNE 17,2004 - DWG 109-0951-60.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Tail rotor · trunnion · overheatedAug 5, 2004
UPON 25 HOUR INSPECTION, TRUNION SHOWS SIGNS OF EXCESSIVE HEAT, DISCOLORED (BROWN) COATING. ENAMEL PAINT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · rod ends · wornOct 26, 1999
UPPER ROD END WORN BEYOND LIMITS. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · coupling · wornOct 25, 1999
SPLINES WORN BEYOND LIMITS. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · starter · malafunctionedOct 10, 1999
STARTER INTERMITTENTLY WILL NOT TURN OVER. WHEN ENGINE IS HOT, STARTER WILL NOT TURN. WHEN AIRCRAFT COOLS FOR 30 MINUTES, ENGINE WILL START. SUBMITTER SUSPECTED BEARINGS IN STARTER/GENERATOR TO BE THE PROBLEM. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Navigation · faceplate · damagedSep 13, 1999
FACEPLATE DAMAGED AND UNREADABLE. P/N 58410A2B2C2D2F4L92. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Navigation · sensor · malfunctionedAug 4, 1999
GPS SLOW TO COME ON LINE. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · transducer · failedApr 13, 1999
PRESSURE TRANSDUCER FAILED; WENT BELOW ZERO PSI DURING FIRST FLIGHT. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 17 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