AW  169         Commercial  in  Confidence          

1   This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  prepurchase  inspection.  This  helicopter  is  offered  subject  to  prior  sale  or  withdrawal.  The  pictures  are  not  of  the  actual  helicopter.  Pictures  are  for  showing  purposes  only.  

 

         

CONFIGURATION      ■  Airframe  • Airframe  structure  including  nose  radome,  cockpit,  manin  cabin  with  flat  floor  and  baggage  compartment,  tail  boom,  vertical  fin,  horizontal  stabilizers,  fuel  tank  housing  

• Attachments  for  main  gearbox  and  engines  • Upper  deck  cowlings  • Landing  gear  attachments  • Heated  pilot  tubes  (2)  • Forced  fan  ventilation    • Bleed  air  heater  and  defroster  with  air  noise  supression    • Cockpit  air  adjustable  outlets    • Cockpit  instrument  panel,  overhead  panel  and  interseat  console    • Cockpit  Windshields  • Pilot  and  co-‐pilot  windshield  wipers    • Overhead  cockpit  windows    • Lower  cockpit  windows    • Pilot  doors  with  emergency  exit  windows  and  “storm  window”  onpilot  side.  

• Lower  pilot/Co-‐pilot  doors  windows    • Plug  in  sliding  doors  (2)  for  passengers  cabin  access  with  four  emergency  exit  windows    

• Baggage  compartment  (one  door-‐access  from  left  hand  side)  • Baggage  compartment  cargo  tie-‐down  fitting    • Lockable  baggage  compartment  doors  

■ Landing Gear • Wheeled  fixed  tricyle  landing  gear  with  two  wheels  on  nose  gear,  one  wheel  with  brakes  on  main  landing  gears  and  mooring  rinhgs.  

■ Rotor and Controls • Main rotor system with composite blades • Tail rotor system with composite blades • Rotating M/R and T/R flight controls • Pilot fixed flight controls • Copilot fixed flight controls • Force trim system • Four parallel actuators (4-axis autopilot)

■ Power plant and fuel system • Two pratt & whitney Canada 210A turboshaft engines • APU mode on left hand side engine • Two anti-icing fuel systems and two magnetic chip detectors • Engines control panel • Engine bay group • Fire detection system • Fire extinguisher system • Fire detection and extinguisher control panel • Crashworthy fuel cells • Filler port for gravity refuelling (on left hand side) • Fuel quantity gauging system

   

■  Transmission  Drive  System  and  Hydraulic  System    • Main  transmission  gearbox  with  two  direct  drive  engine  inputs,  

lubrication  system  with  oil  ducts  integrated  in  the  casing  and  oul  cooling  system.  

• Three  main  transmission  chip  detectors/debris  collectors  with  burning  capability    

• Intermediate  gearbox  with  sight  gauge  and  magnetic  drain  plug/chip  detector  with  burning  capability  

• Tail  gearbox  with  sight  gauge  and  magnetic  drain  plug/chip  detector  with  burning  capability  

• Dual  independent,  redundant  hydraulic  system    • Two  main  transmission  driven  hydraulic  mechanical  pumps  for  controls  

and  wheel  brake  actuation  • Two  hydraulic  power  control  modules  (PCMs)  • Three  main  rotor  dual  servo  actuator    • One  T/R  actuator  shut  off  valve  ■  Electrical  Systems    • DC  primary  power  generation  system:  28  V  DC  provided  by  two  

independent  300  A  stater  generators  • One  heavy  duty  battery  (33AH)  • One  auxiliary  battery  (13AH)  • 28  V  DC  external  power  receptacle    • DC  power  distribution  system  (including  bus  bars,  circuit  breaker  panels  

and  controls).    ■  Lighting  System  • Internal  lighting    

-‐ Instrument  cockpity  panel  lighting    -‐ Inter  sear  cockpit  console  lighting    -‐ Overhead  cockpit  console  lighting    -‐ Cockpit  dome  light  (1),(2),(3)  -‐ Baggage  compartment  light    

• External  Lighting    -‐ Anti  collision  light  (1)  -‐ Navigation  lights  (red,white,green)  -‐ Retractable  swivelling  landing/taxiing  lights  (2)  -‐ External  emergency  lights  (2)  -‐ External  lights  night  vision  goggles  friendly.  

■  Standard  Avionics  Package    • Cockpit  display  system  (CDS)  • One  integrated  standby  instrument  system  (ISIS)  • Two  display  control  panels    • Two  cursor  control  devices  • One  reversionary  contorl  panel  • One  display  dimming  panel  • Two  master  caution  lights    • Two  master  warning  lights    • Two  avionics  full  duplex  ethernet  switches  • Aircraft  monitioring  &  management  system  • Four  axis  automatic  flight  control  system  • Radio  comm  and  navigation  system  

AW  169  –  VIP      Year  of  Manufacture   2017  Airframe  Total  Time   Brand  new  Configuration   VIP  Engines   PW210A  Availability   July  2017  LHD  Warranty   3  years  /  2000  hours  

 

 

AW  169         Commercial  in  Confidence          

2   This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  prepurchase  inspection.  This  helicopter  is  offered  subject  to  prior  sale  or  withdrawal.  The  pictures  are  not  of  the  actual  helicopter.  Pictures  are  for  showing  purposes  only.  

 

  ■  Interior    • Cockpit  compartment  utility  finishing  interior  • Cockpit  panel  sun0glare  shields    • Pilot/Co-‐pilot  crashworthy  adjustable  seats    • 28V  DC/10A  cockpit/cabin  utility  power  socket    • Baggage  compartment  utility  finishing  interior  rear  tail  separation  • Baggage  smoke  sensor    • Pilot/Co-‐pilot  headsets    ■  Painting    • Standard  colour  scheme  from  company  paint  selection,  solid  

colours.  

Optional  Equipment  • Steps  for  cockpit/  cabin  access    • Rotor  brake  system    • Second  radar  altimeter    • One  solid  state  cockpit  and  voice  flight  data  recorder  with  ULB  • One  emegency  locator  transmitter  (ELT-‐3  Frequencies)  (fixed)  • Overhead  cockpit  windows  sun  shadesFirst  aid  kit    • One  cockpit  and  one  one  cabin  fire  extinguisher    • USB  interseat  console  socket  ■  Additional  Navigation  and  Fleet  Management  System  • ADS-‐B  out  • Health  usage  monitoring  system  • Flight  data  monitoring  system  • Helicopter  terrain  avoidance  and  warning  system  • Synthetic  vision  system  

Miscellaneous  /  Ground  equipment  • Extension  headset    • Covers  and  flags  for  engines,  pilot  and  connectors    • Manuals  and  parts  catalogue    • Tie  down  assemblies  for  main  rotor  blades    • Tail  rotor  blades  flapping  block  (1)  • Main  rotor  blades  sock  pole  (1)  • Main  landing  gear  wheel  chocks  (2)  • Landing  gear  handle  locking  pin(1)  • Tow  bar(1)  • Losse  equipment  bag(1)  • Baggage  compartment  cargo  net  

   

   

• Interphone  Communication  system  • Primary  flight  instruments    

 

Proposed  Configuration  ■  Interior  equipment  -‐  cabin  • Enviromental  control  system  dual  zone  –  air  conditioning    • Corporate  interior  • Corporate  layout  “silver  4+2+2”  ■  Interior  equipment  -‐  cockpit  • Approach  plates  chart  holders  with  lights  for  pilot  and  co-‐pilot    • Co-‐pilot  hinged  window    • Tablet  cradle  for  chart  holders    • Windshield  washing  system    • Cockpitcabinet    • Pen,  Pencil,  torch  holder    • Carpet  for  cockpit  &  cabin  • Second  fire  extinguisher  in  cockpit  • Leather  boots  on  cyclic  and  collective    • Carpet  on  cockpit  floor  with  metal  scuff  plates  under  pilot  feet  

Avionics  Equipment    • TCAS  II  rockwell  collins  TCAS-‐4100  provision  • TCAS  II  rockwell  collins  TCAS-‐4100  removable    • Moving  map    • Weather  radar  rockwell  collins  RTA-‐4112  multiscan  provision    • Weather  radar  roclwell  collins  RTA-‐4112  multiscan  removable      

Utility  Equipment    • Camera  on  the  tail  fin    • Emergency  floats  provision    • Engine  air  particle  separators  provision    • Engine  air  particle  seprators  –  romovable  Hinged  fuel  cap    • Grab  handles  in  cabin  both  sides    

Mission  Equipment    •  Increased  gross  weight  (4800  KG  MTOW)  •  Enhanced  vision  system  –  maxviz  EVS-‐1500  

Finishing  –  Painting      • Customized  painting  scheme  • Main  and  tail  rotor  high  visibility  painting    • All  engine  cowls  inside  painted  heat  resistant  white  “polyurethane”  

Loose  Equipment        

   

     

                 

 

 

AW  169         Commercial  in  Confidence          

3   This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  prepurchase  inspection.  This  helicopter  is  offered  subject  to  prior  sale  or  withdrawal.  The  pictures  are  not  of  the  actual  helicopter.  Pictures  are  for  showing  purposes  only.  

 

CARPET  AND  CEILING      

   

   

 

 

AW  169         Commercial  in  Confidence          

4   This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  prepurchase  inspection.  This  helicopter  is  offered  subject  to  prior  sale  or  withdrawal.  The  pictures  are  not  of  the  actual  helicopter.  Pictures  are  for  showing  purposes  only.  

 

 

   

 

 

 

AW  169         Commercial  in  Confidence          

5   This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  prepurchase  inspection.  This  helicopter  is  offered  subject  to  prior  sale  or  withdrawal.  The  pictures  are  not  of  the  actual  helicopter.  Pictures  are  for  showing  purposes  only.  

 

 PAINTING  SCHEME  AND  FINAL  DRAWING