EC225LP Super Puma For Sale
The Eurocopter EC225 Super Puma, now known as the Airbus Helicopters H225, is a long-range passenger transport helicopter developed by Eurocopter as the next generation of the civilian Super Puma family. It is a twin-engined aircraft and can carry up to 24 passengers along with 2 crew and a cabin attendant, dependent on customer configuration. The helicopter is marketed for offshore support and VIP passenger transport duties, as well as public service missions.
EC225LP Super Puma For Sale
BRIEF SPECIFICATION
YOM: 2009
Engines: 2 x Turbomeca Makila 2A
Fuel Capacity: 626.7 USG (inc Auxiliary tank)
Avionics: IFR dual pilot, includes FMS, CMA3024 GPS, EGPWS, Telephonics 1600C Weather Radar, dual VOR/ILS and VHF; ADF, DME; ADELT, TCAS1, HOMP etc
HUMS Status: M’ARMS with CVFDR
Role Equipment: Norwegian North Sea operations equipped – emergency floatation gear, two liferafts, HEEL, De-Icing etc
Seats & Configuration: 19 with high comfort upholstery and soundproofing, extended baggage compartment; enlarged cabin grey tinted windows.
Additional equipment Includes: Air Conditioning, enlarged cabin windows, pressure refuelling, hoist fixed parts, cargo hook, mirror and searchlight provisions etc
BASIC CONFIGURATION / DESCRIPTION
The aircraft is configured new from TC holder for 19 passenger offshore cabin configuration, meeting NOROG 066 requirements. 4-point harness on all seats. Seats are crash attenuating seats. No storage facilities or possibilities under seats, nor is this allowed.
Cabin interior is original Airbus Helicopter cabin, including sound proofing.
No external baggage pods at time of lease rejection redelivery.
Cockpit checklists and cabin safety pamphlets must be prepared and installed prior to operation.
ROLE CONFIGURATION / INFORMATION
The aircraft is adapted to offshore passenger transport iaw NOROG 066 requirements.
This involves installation of “Belly Mounted Life raft release” as provided by Heli-One Norway (EASA Part 21 DOA).
The helicopter is fully de-iced.
ENGINE 1. ( L/H)
Makila 2A1, installed on Nov. 30, 2015 with 3274 hrs. Total time is 3617:01 hrs.
The engine was new 03.03, 2005.
OH requirement is 4000/hrs or 5478 Days (15yrs)
This engine has consumed 8,575 % of it’s OH interval and 8,3% of it’s OH calendar interval.
ENGINE 2. (R/H)
Makila 2A1, installed on Oct. 25, 2015 with 2176 hrs. Total time is 3276:25 hrs.
The engine was new at May, 2008.
OH requirement is 4000/hrs or 5478 Days (15yrs)
This engine has consumed 81,9 % of it’s OH interval in hrs. and 57,2 % of it’s OH calendar interval.
AVIONICS
DF935 (Chelton)
Flight Management System CMA9000
Cockpit Voice / Flight Data Recorder
EGPWS Cmd box
TCAS ACAS
Marine VHF
Weather Radar RDR1600
ADC ADU (*2)
Radio Altimeter ERT160 (*2)
Skytrack
SATCOM
Public Address with 12 Speakers
HUMS
VHF Comm VHF-422D (x2) + Control unit (x1)
VHF FM Transceiver NPX138
VOR / LOC / GS Nav./ Marker VOR Receiver (x2) 􀂲
VIR432
ADF 462
ATC Transponder TDR94
Automatic Flight Control Systems AFCS (*2)
Attitude Heading Reference Unit AHRU (*2)
DME 442
Deployable ADELT / CPI (ELT) HR503
Radar Doppler Velocity Sensor
DMSEU (Digital Map System Electronic Unit)
FEATURES
19 Passengers
6th Fuel Tank
Sponson Fuel Tank
Fuel Tank Transfer
Pressure Refuelling System
POD Fuel Tank + Baggage (FP)
Formation & Rotor Lights
Anti-collision Light Belly Mounted
Standard Landing Light
Trakka Search light (FP)
HEEL Lighting
Bubble Windows (2 on each side)
Dual Controls
Air conditioning􀂳cabin side
Emergency Floatation System
Life Rafts (*2)
Dual Hoist (FP & RP)
FLIR Nose Mounted FLIR (FP)
External mirror (FP + RP)
Anchor
De-iced Equipped (MRB, TRB, Horizontal Stabilizer)
Heating Windshield
NVG Compatible