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NAFFCO Airbus Rescue Helicopters
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Features
GENERAL:
- Energy absorbing fuselage.
- Tail boom with fixed horizontal stabilizer.
- Vertical fin with faired-in Fenestron.
- Upper deck with fittings for main gearbox, engines, hydraulic and cooling system.
- Cowlings for main transmission and engine.
- Skid-type landing gear with skid protectors, capable of taking ground-handling wheels.
- Long boarding steps, LH and RH.
- Maintenance built-in steps and grips.
- Exterior painting (single color).
COCKPIT, CABIN AND CARGO COMPARTMENT:
- One-level cabin and cargo compartment floor with integrated rails.
- Glazed canopy.
- Two hinged cockpit doors with sliding window.
- Map case in pilot's door.
- Two wide passenger sliding doors.
- Two rear hinged clam-shell doors.
- Longitudinally adjustable energy absorbing pilot and copilot seats with head rests and 4-point safety belts with automatic locking system.
- Cabin boarding grips LH and RH.
- Interior paneling with integrated basic sound insulation.
- Flight controls for pilot side; fixed provisions of flight controls for copilot side.
- Covers for copilot collective lever, cyclic stick and pedals.
- Collective control guard on copilot side.
- Engine controls with manual engine back-up system at pilot's collective pitch lever.
- Single pilot instrument panel with glare shield and slant console.
- Ram-air and electrical ventilating system for cockpit and cabin.
- Helmet holder in the cockpit.
- Headset holder in the cabin.
- Portable fire extinguisher.
- Stowage net for first aid kit at the LH rear clam-shell door
- Flash light (torch) for pilot side.
Specifications
INSTRUMENTS:
Flight Display Subsystem (FDS} composed of 2 smart multifunction displays (6x8 inch) providing the following functions:
- Flight and Navigation Display (FND) format (incl. PFD. FLI, Master List, NAV, RPM, mast moment & fuel indication).
- Vehicle Management System (VMS) format (incl. engine, gearbox, fuel, electrical system, RPM & clock indication).
Vehicle Management System (VMS) including:
- 2 duplex Aircraft Management Computer (AMC)
Reference sensors:
- 1 Attitude and Heading Reference System Air Data sensor pilot side (electrically heated pitot tube and static port)
- 1 Magnetometer
Standby instruments:
- Integrated Electronic Standby Instrument (IESI)
- Standby compass
- Usage Monitoring System (UMS)
- Flight Data Continuous Recorder (FDCR)
- "One hundred feet" alert.
Directional Gyro Free Steering Mode Warning unit:
- Warning unit:
- Engine fire warning with fuel emergency shut-off.
- Warning Lights.
- Fire extinguishing system warning.
- Cockpit Control Panel (CCP) for FDS.
- Data Transfer Device (DTD) Data Transfer.
- Engine switch panel.
POWER PLANT:
- Two Pratt & Whitney Canada PW206B3 turbine engines or two Safran Helicopter Engines ARRIUS 2B2 plus turbine engines.
- These are equipped with:
- Fire detectors.
- Full Authority Digital Engine Control (FADEC).
- Chip detectors with quick-disconnect plugs Overspeed protection system.
- Cycle indication on FDS.
- Twin-engine OEO-training mode.
- Oil cooling and lubricating system with thermostatic valve.
- Crash resistant fuel system with a flexible bladder-type main tank and supply tank (split into two sections).
- Automatically controlled variable rotor speed system.
- Fuel tank filler flap, lockable.
- Drain system.
- Fire walls.
TRANSMISSION SYSTEM:
- Flat-shaped main gearbox with two stages.
- Chip detector system with quick-disconnect plug (main gearbox).
- Redundant oil cooling and lubrication system.
- Main gearbox attachment with Anti-Resonance Isolation System (ARIS).
- Free wheel assemblies in the engine input drives.
- Tail rotor drive shaft.
- Tail rotor gearbox with splash lubrication and oil level sight gauge.
- Chip detector system with quick-disconnect plug (tail rotor gearbox).
ROTOR AND FLIGHT CONTROLS:
- Bearing less Main Rotor system (BMR) with improved dynamic characteristics, consisting of:
- Rotor head /mast in one piece.
- Four fiber-reinforced composite main rotor blades with anti-erosionn strips, strips, control cuff, elastomeric lead-lag dampers and special blade tip painting.
- Main rotor control system with dual hydraulic boost system.
- Electrical trim system.
- Basic provisions for an easy integration of a track and balance system.
- Fenestron-type tall rotor with ten metal blades (asymmetric blade spacing) and stator.
- Tail rotor gearbox cover.
- Tail rotor control system with flexball cable and single hydraulic booster.
- Digital 3-axis SAS (Stability Augmentation System).
- Mast moment system.
ELECTICAL INSTALLATION:
- Two starter generators (2x200 A, 28 VDC).
- Nickel-Cadmium battery (24 VDC, 27 Ah).
- External power connector (STANAG 3302. LN9064, SAE AAS 25018, SAE AS 35061)
- Power distribution system:
- Two primary busbars
- Two shedding busbars
- Two essential busbars
- Two high load busbars (80 A) -for optional equipment only
- Two high power busbars (200 А)
- Battery bus
- One utility receptable in LH side of cargo compartment (28 VDC, 10A)
- Lighting:
- Anti-collision waning light (red flashing), LED
- Fixed, nose-mounted landing light, LED
- Three position lights (red, green, white), LED
- Adjustable instrument lighting
- One utility light in the cockpit
- 5 spot-lights in the cabin
- One light in cargo compartment RH side Radio:
- Two radio master switches
GROUND HANDLING KIT:
- Oil drain kit
- Fuel tank drain device
- Keys for cockpit doors, cabin doors, clam-shell doors and tank flap (one-key system)
- Battery key
- Lifting points
- Operational software for AMC and MFD
- Primary Configuration File (PCF)
- D-Box subscription (device loan) including FlyScan- Corrective Maintenance & Fleet. Monitoring web applications during 3 years
- Standard Maintenance Laptop (Packaged PC) including:
- Maintenance Ground Station (MGS) software
- Airbus Helicopters Data Loader (AHDL) software full license.
- AASP (Digital software signature checker) software
- HFDM converter Flight Data Continuous Recorder (FDCR) converter software
- HReplay (to read cockpit camera) software
- Garmin GTX 335 transponder installation tool software
- Data Transfer Module (to upload Euronav 7 database) software
