- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0339
- Year built
- 2004
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- January 8, 2016
- Certificate issued
- January 10, 2014
- Expires
- January 31, 2030
- Mode S code
- ADF067
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PW206B model are included below.
On this page
Airworthiness directives that may apply · 51
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2000 | 1 |
|---|---|
| 2004 | 1 |
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC 135 P2+
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N998AMMatched 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 EC 135 P2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N998AMMatched 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 EC 135 P2+ aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025110374707Support Frame · corrodedDURING A 1000 HOUR INSPECTION CORROSION DAMAGE WAS DISCOVERED ON THE SUPPORT FRAME ANGLE (L533M1039209) ON THE AFT LOWER ANGLE. MAXIMUM DEPTH OF THE MAIN DAMAGE IS 0.035" WITH AN AREA OF 1.50”"X 0.60". A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPASDR 2A6R2025112574706Keelbeam · corrodedTHE LH & RH KEEL BEAM CAPS ARE DAMAGED IN THE FORM OF MULTIPLE AREAS OF CORROSION. THE LH KEEL BEAM CAP HAS TWO (2EA) AREAS OF CORROSION WITH ONE AREA REPORTED TO BE 0.4 X 0.4” IN SIZE AND 0.027 DEEP AT THE DEEPEST POINT, AND THE OTHER AREA REPORTED TO BE 0.5”SDR 2A6R2025112574705Frame · crackedDURING A 1000 HR. INSPECTION, THE RH SIDE OF FRAME 7 IN THE TAIL CONE IS DAMAGED IN THE FORM OF A CRACK. THE CRACK IS LOCATED IN THE BEND RADIUS OF THE FLANGE NEAR THE LOWER RH OMEGA STRINGER AND IS REPORTED TO BE APPROXIMATELY 0.35 LONG. A DETAILED DESCRIPTISDR 2A6R2025110374704Frame · chafedTHE RH SIDE FRAME 4 INNER SKIN PANEL IS DAMAGED IN THE FORM OF TWO (2EA) CHAFE DAMAGE AREAS. THE FIRST CHAFE DAMAGE AREA IS REPORTED TO BE 1.75” X 0.6” IN SIZE AND 0.026” DEEP AT THE DEEPEST POINT. THE SECOND CHAFE DAMAGE AREA IS REPORTED TO BE 1.25” X 1.0” INSDR 2A6R2025112574703Floor Skin · dentedDURING A 1000 HR. INSPECTION, THE COCKPIT FLOOR UPPER SKIN PANEL WAS FOUND DAMAGED IN THE FORM OF MULTIPLE DENTS AND AREAS OF CORROSION. THE LARGEST DENT DAMAGE AREA IS REPORTED TO BE APPROXIMATELY 3.25” X 3.0” IN SIZE AND 0.025” DEEP AT THE DEEPEST POINT. THESDR 2A6R2025110374702Attach Angle · corrodedCORROSION DAMAGE WAS DISCOVERED ON THE LOWER LH, RH & AFT BROOM CLOSET ATTACHMENT ANGLES (L533M1052317 (X2) & L533M1052318). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED FABRICATED PROCEDURE IS PROVIDED IN EA 23-5300-EA-5341; INITIAL REVISION DATED 13 SDR 2A6R2025112174701Frame · crackedDURING 1000-HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE RT FRAME 5 SIDE WALL ATTACHMENT FOR THE UPPER MOUNT OF THE AFT MEDICAL WALL AT APPROXIMATELY FUSELAGE STATION 4,709MM WATER LINE 2,375MM. THE CRACK IS APPROXIMATELY 1.4” IN LENGTH. THE CRACK WAS
STCs that may be installed · 74
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 EC 135 P2+
Earlier aircraft with this N-number · 1
This aircraft carried N998AM before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.