Installation and certification of Night Vision Imaging Systems. The modification comprehends of the installation of cockpit, cabin, external lighting system for use with Night Vision Goggles NVG.. The certification of each helicopter includes extensive ground and flight testing carried out with Airlift's qualified flight test crews. The AS Dauphin full-flight simulator at Airbus Helicopters Southeast Asia began operation in April , and to date has been used for the training of more than pilots from over 20 countries.
Rejoindre Breizhbook. Bienvenue dans Breizhbook Connectez-vous Or sign in with:. Fibreglass-roving spar Moltoprene filler Integrated weight Balancing weight support Bonding strip. Technical Data FENESTRON Tail Rotor: safety and discretion The FENESTRON tail rotor provides outstanding characteristics compared to classical tail rotors: safety on ground: with nearly 30 years in operation, no injury to ground personnel was reported; discretion: the 10 blades are unevenly distributed around the rotor hub to reduce noise safety in flight: tail fin asymmetrical profile design provides anti-torque thrust.
Tail Rotor Blades: The 10 rotor carbon fibre composite blades take advantage from Resin Transfer Molding advanced technology. Individually-interchangeable, they have the following characteristics: Length Chord length Profile Built-in twist. Instrument-panel equipment: 2 Collins MFD Primary Flight Displays PFD 2 Collins MFD Navigation Displays ND 1 stand-by gyro-horizon 1 stand-by altimeter 1 stand-by airspeed indicator 1 dual torquemeter 2 engine T4 indicators 2 engine oil temperature indicators 2 engine oil pressure indicators 2 fuel pressure indicators 2 hydraulic circuit 1 and 2 pressure indicators 1 MGB oil pressure indicator 1 MGB oil temperature indicator 1 voltmeter 1 ammeter 1 dual fuel gauge 2 stopwatches 1 triple tachometer rotor and engine 1 and 2 free wheel r.
Luggage hold with floor, tie-down net and access door RH. Tail boom with stabilizer fitted with 2 lateral fins and terminated by a shrouded tail rotor built into the vertical main fin. Anti-corrosion protection Fixed parts for the main blade-folding system. Structural reinforcements for 1, kg 3, lb cargo-sling. Structural reinforcements for hoist. Jacking, hoisting, mooring and gripping points. Interior colour: beige.
CABIN 1 cabin floor capable of the various optional types of arrangements. Each engine is equipped with an anti-icing fuel system efficient down to O. F 1 fuzz burner system on engine lubrication system 2 fire detection and extinguishing systems 2 anti-icing air-intake grids 2 phase angle torquemeter sensors built into the engines 2 engines exhaust pipes Engine flushing device without cowlings removing.
Note: weight breakdown values are given for information and shall not be considered as contractual. The mode S identification must be communicated by the customer two months at the latest before the delivery. The customer must take out a subscription to the data base in order to use the GPS after having taken delivery of the helicopter. Removable Parts. Includes the supply of the standard cowlings. NVG compatibility. Deliverable with standard upholstery. This equipment is submitted to Export Licence Allowance.
The references of most equipment fitted with a control box must be changed to switch to NVG compatible version. The corresponding stretchers are not certified. Not certified equipment.
Mandatory for seats facing backwards. Quantity to be defined. Includes Digital Jeppesen Map. The operational geographic zone of the helicopter must be communicated by the customer two months at the latest before the delivery.
Includes an underwater beacon. The vendor is responsible for the conformity, performance and certification of this installation regarding the final customer. Any request from a customer should be subject of a specific quotation from A.
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