AW  169         Commercial  in  Confidence        

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  
 
 
 
 

CONFIGURATION  
 
 ■  Airframe   ■  Transmission  Drive  System  and  Hydraulic  System    
• Airframe  structure  including  nose  radome,  cockpit,  manin  cabin   • Main  transmission  gearbox  with  two  direct  drive  engine  inputs,  
with  flat  floor  and  baggage  compartment,  tail  boom,  vertical  fin,   lubrication  system  with  oil  ducts  integrated  in  the  casing  and  oul  cooling  
horizontal  stabilizers,  fuel  tank  housing   system.  
• Attachments  for  main  gearbox  and  engines   • Three  main  transmission  chip  detectors/debris  collectors  with  burning  
• Upper  deck  cowlings   capability    
• Landing  gear  attachments   • Intermediate  gearbox  with  sight  gauge  and  magnetic  drain  plug/chip  
• Heated  pilot  tubes  (2)   detector  with  burning  capability  
• Forced  fan  ventilation     • Tail  gearbox  with  sight  gauge  and  magnetic  drain  plug/chip  detector  
• Bleed  air  heater  and  defroster  with  air  noise  supression     with  burning  capability  
• Cockpit  air  adjustable  outlets     • Dual  independent,  redundant  hydraulic  system    
• Cockpit  instrument  panel,  overhead  panel  and  interseat  console     • Two  main  transmission  driven  hydraulic  mechanical  pumps  for  controls  
• Cockpit  Windshields   and  wheel  brake  actuation  
• Pilot  and  co-­‐pilot  windshield  wipers     • Two  hydraulic  power  control  modules  (PCMs)  
• Overhead  cockpit  windows     • Three  main  rotor  dual  servo  actuator    
• Lower  cockpit  windows     • One  T/R  actuator  shut  off  valve  
• Pilot  doors  with  emergency  exit  windows  and  “storm  window”   ■  Electrical  Systems    
onpilot  side.   • DC  primary  power  generation  system:  28  V  DC  provided  by  two  
• Lower  pilot/Co-­‐pilot  doors  windows     independent  300  A  stater  generators  
• Plug  in  sliding  doors  (2)  for  passengers  cabin  access  with  four   • One  heavy  duty  battery  (33AH)  
emergency  exit  windows     • One  auxiliary  battery  (13AH)  
• Baggage  compartment  (one  door-­‐access  from  left  hand  side)   • 28  V  DC  external  power  receptacle    
• Baggage  compartment  cargo  tie-­‐down  fitting     • DC  power  distribution  system  (including  bus  bars,  circuit  breaker  panels  
• Lockable  baggage  compartment  doors   and  controls).    
■ Landing Gear ■  Lighting  System  
• Wheeled  fixed  tricyle  landing  gear  with  two  wheels  on  nose  gear,   • Internal  lighting    
one  wheel  with  brakes  on  main  landing  gears  and  mooring  rinhgs.   -­‐ Instrument  cockpity  panel  lighting    
■ Rotor and Controls -­‐ Inter  sear  cockpit  console  lighting    
• Main rotor system with composite blades -­‐ Overhead  cockpit  console  lighting    
• Tail rotor system with composite blades -­‐ Cockpit  dome  light  (1),(2),(3)  
• Rotating M/R and T/R flight controls -­‐ Baggage  compartment  light    
• Pilot fixed flight controls • External  Lighting    
• Copilot fixed flight controls -­‐ Anti  collision  light  (1)  
• Force trim system -­‐ Navigation  lights  (red,white,green)  
• Four parallel actuators (4-axis autopilot) -­‐ Retractable  swivelling  landing/taxiing  lights  (2)  
■ Power plant and fuel system -­‐ External  emergency  lights  (2)  
• Two pratt & whitney Canada 210A turboshaft engines -­‐ External  lights  night  vision  goggles  friendly.  
• APU mode on left hand side engine ■  Standard  Avionics  Package    
• Two anti-icing fuel systems and two magnetic chip detectors • Cockpit  display  system  (CDS)  
• Engines control panel • One  integrated  standby  instrument  system  (ISIS)  
• Engine bay group • Two  display  control  panels    
• Fire detection system • Two  cursor  control  devices  
• Fire extinguisher system • One  reversionary  contorl  panel  
• Fire detection and extinguisher control panel • One  display  dimming  panel  
• Crashworthy fuel cells • Two  master  caution  lights    
• Filler port for gravity refuelling (on left hand side) • Two  master  warning  lights    
• Fuel quantity gauging system • Two  avionics  full  duplex  ethernet  switches  
• Aircraft  monitioring  &  management  system  
    • Four  axis  automatic  flight  control  system  
• Radio  comm  and  navigation  system  

This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
1   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        

  • Interphone  Communication  system  

• Primary  flight  instruments    
 
■  Interior    
• Cockpit  compartment  utility  finishing  interior  
Proposed  Configuration  
• Cockpit  panel  sun0glare  shields     ■  Interior  equipment  -­‐  cabin  
• Pilot/Co-­‐pilot  crashworthy  adjustable  seats     • Enviromental  control  system  dual  zone  –  air  conditioning    
• 28V  DC/10A  cockpit/cabin  utility  power  socket     • Corporate  interior  
• Baggage  compartment  utility  finishing  interior  rear  tail  separation   • Corporate  layout  “silver  4+2+2”  
■  Interior  equipment  -­‐  cockpit  
• Baggage  smoke  sensor    
• Approach  plates  chart  holders  with  lights  for  pilot  and  co-­‐pilot    
• Pilot/Co-­‐pilot  headsets    
■  Painting     • Co-­‐pilot  hinged  window    
• Standard  colour  scheme  from  company  paint  selection,  solid   • Tablet  cradle  for  chart  holders    
colours.   • Windshield  washing  system    
• Cockpitcabinet    
Optional  Equipment   • Pen,  Pencil,  torch  holder    
• Steps  for  cockpit/  cabin  access     • Carpet  for  cockpit  &  cabin  
• Rotor  brake  system     • Second  fire  extinguisher  in  cockpit  
• Second  radar  altimeter     • Leather  boots  on  cyclic  and  collective    
• One  solid  state  cockpit  and  voice  flight  data  recorder  with  ULB   • Carpet  on  cockpit  floor  with  metal  scuff  plates  under  pilot  feet  
• One  emegency  locator  transmitter  (ELT-­‐3  Frequencies)  (fixed)  
• Overhead  cockpit  windows  sun  shadesFirst  aid  kit    
Avionics  Equipment    
• One  cockpit  and  one  one  cabin  fire  extinguisher     • TCAS  II  rockwell  collins  TCAS-­‐4100  provision  
• USB  interseat  console  socket   • TCAS  II  rockwell  collins  TCAS-­‐4100  removable    
■  Additional  Navigation  and  Fleet  Management  System   • Moving  map    
• ADS-­‐B  out   • Weather  radar  rockwell  collins  RTA-­‐4112  multiscan  provision    
• Health  usage  monitoring  system   • Weather  radar  roclwell  collins  RTA-­‐4112  multiscan  removable      
• Flight  data  monitoring  system   Utility  Equipment    
• Helicopter  terrain  avoidance  and  warning  system   • Camera  on  the  tail  fin    
• Synthetic  vision  system   • Emergency  floats  provision    
Miscellaneous  /  Ground  equipment   • Engine  air  particle  separators  provision    
• Extension  headset     • Engine  air  particle  seprators  –  romovable  Hinged  fuel  cap    
• Covers  and  flags  for  engines,  pilot  and  connectors     • Grab  handles  in  cabin  both  sides    
• Manuals  and  parts  catalogue     Mission  Equipment    
• Tie  down  assemblies  for  main  rotor  blades     •  Increased  gross  weight  (4800  KG  MTOW)  
• Tail  rotor  blades  flapping  block  (1)   •  Enhanced  vision  system  –  maxviz  EVS-­‐1500  
Main  rotor  blades  sock  pole  (1)  
•
• Main  landing  gear  wheel  chocks  (2)  
Finishing  –  Painting      
• Customized  painting  scheme  
• Landing  gear  handle  locking  pin(1)  
• Main  and  tail  rotor  high  visibility  painting    
• Tow  bar(1)  
• All  engine  cowls  inside  painted  heat  resistant  white  “polyurethane”  
• Losse  equipment  bag(1)  
• Baggage  compartment  cargo  net   Loose  Equipment    
 
 
 
 
   
 
 

 
 
 
 
 
 
 
 
 
 
 
 
This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
2   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        

 
 
Pilot  Training    
 
Seller  should  provide  the  following  pilot  training:  
 
• Glass  cockpit  and  automation  management  (Glam)  
-­‐ Number  of  students:  5  
• AW169  VFR/IFR  type  rating    
-­‐ Number  of  students:  5  
• AW169  type  rating  instructor    
-­‐ Number  of  students:  2  
 
Technical  Training    
 
 
• AW169  (PWC  210)  airframe  maintenance  type  training  course  B1.3  (Theoretical  Elements)  
-­‐ Number  of  students:  3  
• AW169  (PWC  210)  airframe  maintenance  type  training  course  B1.3  (Practical  Elements)  
-­‐ Number  of  students:  3  
• AW169  (PWC  210)  avionic  maintenance  type  training  course  B1.3  (Theoretical  Elements)  
-­‐ Number  of  students:  3  
• AW169  (PWC  210)  avionic  maintenance  type  training  course  B1.3  (Practical  Elements)  
-­‐ Number  of  students:  3  
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
3   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        

CARPET  AND  CEILING    

 

 
 

This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
4   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        

 
 

 
This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
5   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        

   
This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
6   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        

 
 
 
   
   
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
7   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        

PAINTING  SCHEME  AND  FINAL  DRAWING  

 
 
   
 

This  specification  has  been  prepared  from  information  supplied  by  vendor.  All  details  are  subject  to  verification  during  
8   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.