N135NP

Cancelled 2026

Deregistered aircraft · 1998 Eurocopter Deutschland EC135T1 · Turbomeca ARRIUS-2F

Cancelled
October 14, 2026
Status when cancelled
Valid registration
Serial number
0068
Year built
1998
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
March 23, 1999
Certificate issued
January 25, 2012
Last registry action
December 9, 2024
Mode S code
A08EFE
Owner when cancelled
Air Methods LLC
Owner type
LLC

From the FAA registry file of November 4, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 8

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2A6R2023101366804Unknown · unknownDURING A 1000 HOUR INSPECTION, FOUND CRACK ON THE RIGHT SIDE OF THE TAIL CONE SKIN P/N L533M102216. PERFORMING A REPAIR I.A.W. AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2023-2976Oct 13, 2023 · N135NP · Urocop EC135P1 · Rotorcraft Tail BoomSDR 2A6R2023101166802Unknown · unknownDURING A 1000 HOUR AIRFRAME INSPECTION FOUND MULTIPLE CRACKS IN THE LEFT AND RIGHT SIDE OF FRAME 5 P/NL533M1088104. PERFORMING A REPAIR I.A.W AIRBUS HELICOPTERS RDAS NO. AHI 135-53-048-19Oct 11, 2023 · N135NP · Urocop EC135P1 · Fuselage Structure (General)SDR 2A6R2023100566802Unknown · unknownDURING A 1000 HOUR AIRFRAME INSPECTION FOUND L/H KEEL BEAM CAP P/N L533M1009203 AND R/H KEEL BEAM CAP P/N L533M1010203 CORRODED AT THE END OF THE CAP ON BOTH SIDES. THE CORROSION IS THROUGH THE FULL THICKNESS OF THE CAP. PERFORMING A REPAIR AS PER AIRBUS REPAIOct 5, 2023 · N135NP · Urocop EC135P1 · Fuselage Structure (General)SDR 2A6R2023092166801Fitting · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND THE LEFT FORWARD LANDING GEAR FITTING CORRODED. REPAIRED IAW AIRBUS RDAS-EC135-53-2023-2753 ISSUE A DATED: 09/20/2023Sep 21, 2023 · N135NP · Urocop EC135P1 · Fuselage, Landing Gear Attach FittingsSDR QMLA2020100520051Gps · shortedHTAWS FAILED FOLLOWED BY THE GNS 530 FOLLOWED BY THE TECHNOSONIC HEAD IN MEDICAL COMPARTMENT WITH SMOKE. INSPECTED WIRING AND CONNECTORS, NO VISIBLE DAMAGE. DETERMINED INTERNAL SHORT IN GARMIN 530 WHICH CAUSED SMOKE AND SMELL IN CABIN. REMOVED AND REPLACED Oct 3, 2020 · N135NP · Urocop EC135T1 · Global Positioning SystemSDR QMLA2017060917059Frame · crackedCRACK FOUND IN THE 5A FRAME DURING HEAVY MAINTENANCE. THIS CRACK WAS REPAIRED PER THE MANUFACTURERS STRUCTURAL REPAIR MANUAL.Jun 9, 2017 · N135NP · Urocop EC135T1 · Fuselage Main, FrameSDR QMLA2013052713071Control Unit · failedNR 1 ENGINE DEGRADE & FADEC FAILURE CAUTION. ENGINE FAILURE, ATTEMPTING MANUAL THROTTLE BY PILOT DURING FLIGHT, TROUBLESHOT SYSTEM FOUND DECU/FADEC HARD FAILED.May 27, 2013 · N135NP · Urocop EC135T1 · Fuel Controlling SystemSDR RMXA11092007Skin · crackedLADDER FELL OVER AND HIT AGAINST THE RT TAILBOOM SHROUD AND CAUSED A 0.5 INCH LONG CRACK IN THE COMPOSITE STRUCTURE.Nov 9, 2007 · N135NP · Urocop EC135T1 · Rotorcraft Tail Boom