EC135 P2+

Production Year: 2001
TSN: 4,486 hours
Availability: Immediate
Mission: Pax transport / EMS


Please feel free to download the datasheet of the pre-owned/used EC135 Helicopter mentioned above.






















Actual product(s) may differ from photographs.

PRODUCTION YEAR:
TSN:
MISSION:
AVAILABILITY:

  • 2001
  • 4,486 HOURS
  • PAX TRANSPORT / EMS
  • IMMEDIATE


LIST OF EQUIPMENTS:

ACC Air Conditioning System

Windshield wiper

Wire Strike Kit 400/200W

Aerolite Clamshell Door Locking System

High Skid gear

Settling protectors (not fitted)

Cargo hook (FP)

NVG compatible Cockpit w/cabin separation curtain

Concord Lead Acid Battery

Tinted Sunshades, Pilot & Co-pilot side

Engine Compressor Washing Device

Search and Landing Light 3 x 200W

Strobe Lights

Cabin arrangement:
-Aerolite EMS Kit
-5 Pax seats

 



LIST OF AVIONICS:

NVG compatible lighting AHRS

3 axis Autopilot with FCDS

VHF/AM – KTR 908 / KFS 598A NVG (*2)

VOR ILS NAV – KNR634A / KFS 564A NVG (*2)

Colour Weather Radar – RDR 2000 KTR908/KFS598A

ICS station AS3100-12

TAC COM – NAT NTX 138 (FP)

VEMD & CAD

SMD 45 (*2)

SMD 68

Air Data System

Transponder Mode S – MST 67A / KFGS 578A

ELT - Artex 110-406

Radar Altimeter KRA 405B

DME – DMS 44A

ADF – DFS43A / CD432B

 



COMPONENTS
REMAINING TIMES vs TBO:
As of May 2012

Main gear box:

Tail gear box:

Main rotor blades (4):
 

Tail rotor blades (*10)

 

Engines PWC 206B2

1,445 / 4,000 hrs

1,545 hrs / 3,000 hrs

11,163 - 11,301 - 10,799 - 11,212 / 12,400 hrs (SLL)

9,084 / 12,000 hrs (SLL)

 

2,602 - 2,732 / 3,500hrs (OH)

 



Inspection status:
As of May 2012

Engines 800 hrs inspection due in 649 hrs Engine-1 and 32 hrs Engine-2

 



NOTES:

  • Engines maintained under PWC Eagle Service Plan
  • Conversion of P2 to P2+ occurred on 03/06/2008 by Eurocopter Donauworth
  • No incident History. Aircraft is in good condition
  • Offered with Valid C of A
  • We offer the Aircraft: “As is” Ex-Works Oceania

 

Aircraft availability subject to prior sale. Components remaining times, configuration and equipment subject to buyer's verfication prior to purchase.


Multi-Mission Flexibility
The EC135 is a powerful, lightweight, twin-engine multi-mission helicopter that showcases top-notch technology while offering low operating costs. The EC135’s high endurance and extended range enables this helicopter to perform a full range of mission requirements, while carrying more payload over longer distances than any aircraft in its class. Incorporating a modern cockpit and avionics – as well as Eurocopter’s Fenestron® tail rotor and bearingless main rotor –the EC135 is recognized for its high performance and outstanding maneuverability.




Please feel free to download the Eurocopter Technical Data of the EC135 Helicopter


EC135
 


MTOW:
MAX RANGE WITH STANDARD FUEL TANK:
STANDARD CONFIGURATION:

  • 2,910 kg
  • 630 km
  • 1+7 pax


©Copyright all Helicopter photos courtesy of Eurocopter.





The data set forth in this document are general in nature and for information purpose only. They may vary with conditions. For performance data and operating limitations, reference must be made to the approval flight manual and all appropriate documents.


Subject EC135 P2+, 2001, 4,486 hours

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