AIRBUS EC135 P2i / P2+ SP/DP IFR and SP NVIS certified. Aerolite EMS interior. Always hangared, and operated by the Norwegian Air Ambulance. Rotables, dynamics, airframe and engines covered by Airbus PbH and P&W ECP AIRCRAFT TYPE MODEL SERIAL NUMBER REGISTRATION AC TOTAL TIME EC135 P2+ 2005 0399 LN-OOH 7700 FH MTOW ENGINE LOCATION AVAILABLE ASKING PRICE 2910 kg PW206B2 Norway January 2018 TBD CONTACT Cathrine Dekko VP Sales Østnes Helicopters Cathrine@ostnes.no +47 9096 6562 Page 1
INTERIOR Aerolite EMS Interior EASA STC 10043032 EMS P/N 135520-502 Further description upon request EXTERIOR EMS yellow with red stripes Standard Landing Gear Reinforced rear landing gear cross tube OPTIONAL EQUIPMENT Bleed Air Heating 7 copilot instrument panel with glare shield AC system 50 VA Starter-Generator 2x200A instead of standard generator Single Pilot Night Vision Imaging System (NVIS) certified with NVG curtains Standard Cockpit Layout & Illumination (NVG) External Lightning kit - NVG Height adjustable pilot & copilot seat instead of standard seat Cabin Sliding Doors, LH and RH Sliding Door fastener, max position RH One-Hand latching system for clam-shell doors Cockpit Jettisoning doors Dual Controls Dual External Cargo Hook Engine Fire Extinguisher Fuel Management System Accelerometers for track& balance system VMSII (Chadwick Helmuth) Fixed Landing Light on the Cross Tube P&R SAS Rotor Brake System Search and Landing Light (Retractable) Engine Compressor wash kit Multifunction handle om main gearbox cowling LH & RH Multipurpose attachment hard points (5ea) integrated in the cabin Window in clam-shell door L/H Page 2
OPTIONAL EQUIPMENT, CONTINUED Tinted sun shades for cockpit windshields roof section White Strobe lights Windshield Wipers Wire Strike Protection, Basic kit AVIONICS Airborne Collision Avoidance System (ACAS) RYAN 9900 Interface to Garmin GNS 430 3-Axis Digital Automatic Flight Control System (DAFCS) Digital Moving Map System EURONAV IV+ (RN6) - Interface to Garmin GNS 430 Distance Measuring Equipment (DME) Honeywell (Bendix/King) DM 441B ELT Artex C406-N Flight Control Display System (3-screen version (2x SMD 45 1 X SMG 68) Software version V650 GPS/NAV/COM Garmin GNS430, Dual installation VOR/ILS interfaced to FCDS/MEGHAS 2 stand-by horizon NVG Avionics Package DP / IFR Marker Receiver Honeywell (Bendix/King) KR21 Mode-S Transponder System Garmin GTX330 Radio Altimeter Honeywell (Bendix/King) KRA 405B. With Audio voice Weather Radar System, RDR 1600 (Telephonics) Copilot pitot static system Free steering mode for Attitude and Heading Reference Systems (AHRS) PROVISIONS (REMOVABLE PARTS WILL NOT FOLLOW) IFR training screens fixed provisions Provision Analog Tactical Radio (NAT NTX-138 System) Provisions for 2 nd Landing & Search Light Page 3
EASA APPROVED MINOR MODIFICATIONS Wireless Polycon (Loose equipment to be defined) Heli-One Mod. AHSE- 61712 Provisions for IPAD holder EASA 10053714 Provision Mobile Phone EASA Approved Installation for Nokia handheld mobile phone is included. Use during flight by non-flying crew member and operation is depending on local approval EASA.R.C.02659 Provision for Dual Cobham TETRA radio (Removable Parts; Transceiver Cobham 7-450-14-52, Controller CH250-13-00 & Remote Controller RH150-13 (Incl in NVIS Certification) will be removed) Scandinavian Avionics 2082433-STC Intercom System Digital Becker 6100 Retrofitted EASA Certified Scandinavian Avionics 2090308-STC DART Bear Paws EASA 10038103 COMPONENT STATUS Part Number TSO / TSN TBO / SLL Main Transmission 4649020010 2150 4000 Tail Rotor Gearbox L652A0101052 1849 3600 Main Rotor Blades L621M1010056 /Yellow 3224 12400 L621M1010056 /Green 6941 12400 L621M1010056 /Blue 5437 12400 L621M1010056 /Red 6942 12400 Tail Rotor Blades L642A2002101 /1 1408 12000 L642A2002101 /2 1408 12000 L642A2002101 /3 7071 12000 L642A2002101 /4 7071 12000 L642A2002101 /5 7071 12000 L642A2002101 /6 7071 12000 L642A2002101 /7 7071 12000 L642A2002101 /8 7071 12000 L642A2002101 /9 7071 12000 Page 4
COMPONENT STATUS, CONTINUED Tail Rotor Blades L642A2002101 /10 7071 12000 Pratt &Whitney, PW206 B2 PW206B2 /Left 788 4500 Pratt &Whitney, PW206 B2 PW206B2 /Right 3004 4500 Fuel Management Module 3055982-01 /Left 3616 4500 Fuel Management Module 3055982-01 /Right 3004 4500 Page 5
PICTURES The following pictures are illustration photos taken from a representative EC135P2i / P2+: Page 6
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KeyDwg No: Title Note 1 135461-501 EMS SERVICE PNL 2 135301-502 EMS FLOOR 4 135380-502 MED SEAT RH AFT 5 135356-501 MED SEAT LH FWD 6 135550-501 CTR STOWAGE CAB HH (HALF HEIGHT) 7 135049-502 STOW CONTAINER 8 135469-502 SHELF RH 9 135457-501 EQUIP RAIL AFT LH 10 135457-502 EQUIP RAIL AFT RH 11 135473-501 EQUIP RAIL CEILING 12 135023-501 EQUIP RAIL WINDOW LH 13 135023-502 EQUIP RAIL WINDOW RH 14 135552-502 MED EQUIP WINDOW RH INSTL 15 135552-501 MED EQUIP WINDOW LH INSTL 18 007031-501 TIE DOWN WEB 20 135471-501 ATMOPORT RETAINER INSTL 23 135321-507 PROPAQ SYSTEM INSTL No retainers included 24 135508-501 MODUL OXYGEN INTERFACE RET. 26 135058-501 OXYLOG RETAINER INSTL 27 135292-503 STRETCHER 29 135554-502 SPINE BOARD RETAINER 30 135-0020969-502 CYLINDER RACK GAS SYSTEM 32 135-0000823-501 CARGO PLATFORM INSTL No Cargo Platform included REMARKS The helicopter is operating actively today, hence the condition and component status will be subject to changes. Verification of the condition of the helicopter and its components shall be the responsibility of the purchaser. Page 20