M-NBLA: Airbus H135T3

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Description

HIGHLIGHTS

VIP ACH Interior
Engines Enrolled in SBH
Helionix step 3.1
Concorde Lead Acid Battery Installation
Fixed Parts for Aux Fuel
  

Avionics

INSTRUMENTS
Flight Display Subsystem (FDS) composed of 3 smart multifunction displays (6 x 8 inch) providing the following functions
- Flight & 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    
- 3 Attitude and Heading Reference System   
- Air Data sensor pilot side (electrically heated pitot tube and static port)    
- 2 Magnetometers 
Standby instruments    
- Integrated Electronic Standby Instrument (IESI)   
- Standby compass
AVIONICS
Radar altimeter KRA 4058 (Honeywell)
Helicopter Terrain Awareness and Warning System (H-TAWS) - Helionix
Synthetic Vision System (SVS) - Helionix
Additional Attitude and Heading Reference System (AHRS)
Copilot pilot static system
4-axis Automatic Flight Control System (AFCS)
Lightweight Aircraft Recording System (LARS) Alerts
Vision 1000
  

Airframe

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 engines 
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 Stage, Multi Color)
POWER PLANT
Two Safran Helicopter Engines ARRIUS 2B2plus turbine engines. These two engines are equipped with:
- Fire detectors
- Full Authority Digital Engine Control (FADEC)
- Chip detectors with quick-disconnect plugs
- Overspeed protection system
- Cycle Indication On MFD 
Twin-engine OEl-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)
ELECTRICAL INSTALLATION
Two starter I generators (2x200 A, 28 VDC) 
Lead Acid Battery, (24 VDC, 27 Ah)   
- External power connector (STANAG 3302, LN9064, SAE AS 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 A)   
- Battery bus 
One utility receptacle in LH side of cargo compartment (28 VDC, 1O A)
ROTOR & FLIGHT CONTROLS
Bearingless 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-erosion strips, control cuff, elastomeric lead-lag dampers 
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 tail 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 4-axis SAS (Stability Augmentation System) 
Mast moment system
  

Engines / Mods

Turbomeca 2B2+ with fire detectors, FADEC, chip detectors/fuzz burn & training mode
Engine #1
S/N:  33123
TSN:  667:58
Cycles: N1-427   N2-967
Engine #2
S/N:  33125
TSN:  667:58
Cycles:  N1-416   N2-963
  

Interior / Exterior

COCKPIT, CABIN & 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 rest 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 
Engine controls with manual engine back-up system at pilot’s collective pitch lever 
Instrument panel with extension and glare shield on pilot's side and slant console 
Ram-air and electrical ventilating system for cockpit and cabin 
Headset 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
  

Remarks

MANDATORY ITEMS
General Equipment:    
- First aid kit    
- Engine fire extinguishing system    
- Fuzz burners for engines    
- Engine cowling heat protection    
- Engine compressor wash kit    
- Flashlight for copilot side    
- Tinted sun shades for cockpit windshield roof section   
- Windshield wiper system    
- Center console    
- Avionics compartment    
- Copilot flight controls, detachable parts    
- Instrument panel extension on copilot side    
- Map case in copilot door    
- Map cases on instrument panel glare shield    
- Bleed air heating system    
- Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery    
- Rotor brake system
Specific Mission Equipment:   
- Search & landing light, fixed provisions    
- Search & landing light, detachable parts    
- Emergency Locator Transmitter (ELT) 
Interior Layout:   
- Special interior painting
Avionics (Solution):    
- Avionics Package DP IFR GC GTN 750    
- Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot    
- Transponder GTX 335R (Garmin) incl. ADS-B out    
- Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins)    
- Marker beacon receiver MKR3300-1 (Becker)   
- GPS/NAV/COM GTN 750 (Garmin), pilot    
- GPS/NAV/COM GTN 750 (Garmin), copilot    
- Approach charts (IFR) georeferericed for GTN 750    
- Flight Display Subsystem (FDS), copilot    
- Avionics Package DP IFR GTN Series interconnection/ wiring
OPTIONAL ITEMS
General Equipment:   
- Full cover set     
- Complex exterior painting instead of standard painting    
- Surface protective coating (Airglaze)    
- Main rotor blade erosion protection paint    
- Boarding grips for cockpit    - Inlet Barrier Filter (IBF) system    
- Corrosion protection for high corrosive environment    
- Tinted front windshields    
- Tinted windows in cockpit doors    
- Tinted windows in cabin incl. sliding windows in sliding doors    
- Air Conditioning System (ACS)    
- Internal long range fuel tank system, fixed provisions    
- Fuel management system (fuel flow meters)    
- Lashing points for wind speeds up to 40 kts, fixed provisions   
- Lashing points for wind speeds up to 40 kts, detachable parts   
- Lashing points for ship landings, fixed provisions    
- Lashing points for ship landings, detachable parts 
Specific Mission Equipment:    
- External multi-purpose camera on tail boom, fixed provisions   
- External multi-purpose camera on tail boom, detachable parts    
- 2 white strobe lights   
- Second search and landing Light    
- Emergency floats incl.     
- Emergency floats skids 
Interior layout (Solution):    
- Stylence®, 5 passengers, 1 cabinet, package (AAT - STC), 2018    
- Stylence height adjustable copilot seat instead of standard copilot    
- Stylence height adjustable pilot seat instead of standard pilot seat    
- Stylence front middle passenger seat    
- Stylence front passenger seats (2 seats)    
- Stylence rear passenger seats (2 seats)    
- 5 Stylence passenger seat protective cover    
- 2 Stylence pilot seat protective cover    
- Stylence armrest in rear window niches    
- Stylence entrance rails    
- Stylence carpet for cargo compartment     
- Stylence carpet for cabin    
- Stylence carpet for cockpit    
- Stylence leather cuffs for flight controls    
- Stylence rear cabinet with USS power socket    
- Stylence Passenger Service Units (PSU)    
- Stylence metal placards 
Interior layout:   
- Enhanced sound proofing kit    
- Separation wall for cabin / cargo compartment    
- One-hand latching system for clam-shell doors    
- Jettisonable cockpit doors    
- Map cases in sliding doors    
- Variable tie-down net    
- Retractable coat hooks in rear cabin (2 hooks) 
Avionics:    
- Garmin Flight Stream 510    
- Iridium satellite transceiver GSR 56 (Garmin)    
- Color weather radar RDR 2000 (Honeywell), fixed provisions    
- Traffic Advisory System TAS620A (Avidyne), fixed provisions    
- Traffic Advisory System TAS620A (Avidyne), detachable parts   
- Moving map - Helionix    
- iPad Air Holder Copilot    
- iPad Air Holder Pilot    
- Headset electrical power supply (28VDC),  fixed provisions    
- 7 Headset adapter cable crew GLENAIR/LEMO ANR    
- Electrical fixed provisions, 5 VDC, copilot    
- Electrical fixed provisions, 5 VDC, pilot
  

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