- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 9091
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- December 5, 2011
- Expires
- December 31, 2027
- Mode S code
- A0B6DC
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 58
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2007 | 1 |
|---|---|
| 2008 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 4 |
| 2013 | 8 |
| 2014 | 5 |
| 2015 | 1 |
| 2016 | 5 |
| 2017 | 5 |
| 2018 | 1 |
| 2019 | 6 |
| 2020 | 1 |
| 2021 | 7 |
| 2022 | 9 |
| 2023 | 2 |
| 2024 | 2 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland MBB-BK 117 C-2
AD 2026-17-05Cabin Equipment/FurnishingsAD 2026-09-08Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Eurocopter Deutschland MBB-BK 117 C-2
SAIB SW-18-04Engine Oil Drainage SystemSAIB SW-12-22MBB BK117 C-2 Auto Flight SystemSAIB SW-08-04Night Vision Imaging System installation on BK -117C-2 HelicopterNTSB investigations
No NTSB investigations matched to N145SJMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter Deutschland MBB-BK 117 C-2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N145SJMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter Deutschland MBB-BK 117 C-2 aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2024123072102Floor Panel · dentedDURING 800-HOUR INSPECTION, FOUND DAMAGE TO THE COCKPIT FLOOR (P/N: B531M8002101) IN THE FORM OF DENTS TO THE UPPER SKIN PANEL BETWEEN THE PILOT SEAT TRACK NEAR THE AFT SIDE OF THE CYCLIC OPENING. THE INBD DENT DAMAGE MEASURED TO BE APPROXIMATELY 1.90” IN DIAMSDR 2A6R2024123072101Frame · crackedDURING 800 HOUR INSPECTION, DAMAGE TO THE FORWARD BOTTOM FRAME 1 IN THE FORM OF A CRACK WAS DISCOVERED AT LBL 195MM AND IS APPROXIMATELY 1.2” IN LENGTH. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN ASDR QMLA2019011019016Frame · cracked2 CRACKS WERE FOUND IN THE TAILCONE OF AIRCRAFT DURING A 1200 HOUR INSPECTION ON A SECTION OF FRAME AT STATION 6616 AND THE ATTACHED DOUBLER. THESE CRACKS WERE REPAIRED AND DOCUMENTED ON AN FAA FORM 337 DATED 01/29/2019.SDR QMLA2015063015051Frame · crackedDURING AN AIRFRAME ZONE 12 INSPECTION FOUND THE SHELF THAT THE ANTI-COLLISION LIGHT POWER SOURCE IS MOUNTED TO IS BROKEN & UPON FURTHER INSPECTION FOUND A CRACK IN UPPER FRAME 9LA.SDR QMLA2013110913162Gearbox · making metalTAILROTOR CHIP LIGHT CAME ON IN FLIGHT SOON AFTER TAKEOFF. PILOT USED FUZZ BURNER BUT LIGHT STAYED ON. ACFT RETURNED TO AIRPORT. FOUND CHIPS CONSISTENT WITH FIGURE F IN AMM 65-21-00, 6-1.SDR QMLA2012100112160Belt · brokenIN FLIGHT, PILOT AND PASSENGERS DETECTED THE ODOR OF SMOKE. NO SMOKE OR EVIDENCE OF FIRE WAS VISIBLE INSIDE OR OUTSIDE THE ACFT. PILOT SHUTOFF BOTH GENERATORS AND AIR CONDITIONER IAW CHECKLIST. ACFT MADE A PRECAUTIONARY LANDING AND PERFORMED AN EMERGENCY SHUSDR QMLA2012060512090Disk · damagedWHILE PERFORMING TU360 UPGRADE TO ENGINE SN 18789 FOUND THE SECOND STAGE TURBINE DISK BLADE LOCKS DISPLACED LEADING TO BLADE SHIFT. R & R MODULE 3.SDR QMLA2011081111084Line · disconnectedPILOT REPORTED AFTER TAKEOFF THEY SMELLED FUEL ODOR IN CABIN. INSPECTED ENGINES AND AIRFRAME FUEL EXPANSION BOX FOR EVIDENCE OF FUEL AND LEAKS. NO LEAKS OR FUEL WERE FOUND. DURING INSP OF THE EXPANSION BOX THE OUTER DUCT AROUND THE LOWER FUEL VENT LINE WAS SDR QMLA2011032311036Skin · crackedA RIVET HEAD WAS FOUND MISSING ON THE DOUBLER ON THE RT SIDE OF THE VERTICAL FIN AT THE TAILBOOM/ VERTICAL FIN TRANSITION. FURTHER INSP REVEALED A CRACK IN THE VERTICAL FIN FWD BULKHEAD/ SPAR STRUCTURE, STARTING FROM THE TOP RT AFT RECEPTACLE HOLE FOR THE TRA
STCs that may be installed · 111
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Eurocopter Deutschland MBB-BK 117 C-2
STC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC SR00006RDnstallation of Emergency Medical System (EMS) equipment part number 145121-501 or 145121-502STC SR00601DEInstallation of a cabin air conditioning system.