Airbus H225 VIP (2007)

Specifications

INTERIOR

VVIP Configured

Front lounge: 4 VIP Seats & 2 tables

Rear lounge: 4 VIP, 2 tables, 1 Steward seat

AVIONICS

TCAS TRC899 L-3 Communications

Weather Radar 1400C Amphenol

ATC Transponder TDR-94D Collins

Flight Management System

AVIONICS

VHF AM 422D Collins x2

Marine VHF/FM NPX138 Collins

UHF AM/FM 805-1 Chelton

Fixed ADELT ELF ELF-500 HR Smith

Portable ELT ELT-500 HR Smith x2

DME 442 Collins

ADF 462 Collins

GPS CMA3012 CMC

Radio Altimeter AHV16 Thales

EGPWS MKXXII Honeywell

Airbus H225 VIP (2015)

Specifications

Dassault Falcon 7X (2013)

Specifications

Overview

Airframe: 1,672 TSN – 617 CSN

Engines: Pratt & Whitney 307A

• On ESP Gold Plan

APU: Honeywell GTCP36-150(FN)

• 1,329 Hours
• On Honeywell MSP

Equipment

Electronic Jeppesen Charts Honeywell EASy
Electronic flight bag (EFB)
Autothrottle Honeywell EASy
Air Data Goodrich Smartprobes
Central Maintenance Computer Honeywell EASy
230 VAC 50HZ 2000VA Inverter KGS Electronics SB200
3 Each Telex Airman 850 Headsets (Supplied as Loose Equipment)
Communication Management Function w/ ARINC Honeywell EASy
Electronic Display & Management Honeywell EASy
Honeywell Standby Instrument Display
Attitude Heading Reference System Honeywell
Uplink weather capability Honeywell Easy

EASy II Avionics Suite

COM Triple VHF Communication Honeywell TR-866B
NAV Dual Honeywell NV-877A
ADF Dual Honeywell DF-855
DME Dual Honeywell DM-855
RADALT Dual Honeywell KRA-405B
RADAR Honeywell WU880
FMS Triple Each Honeywell FMS Functions
TXPDR Dual Honeywell XS-858B
HF Dual Honeywell KHF-1050
EGPWS Honeywell EGPWM-100
TCAS II ACSS TCAS 3000
FDA Triple Honeywell AV-900
FDR Dual Honeywell AR-Combi Recorders
CVR Dual Honeywell AR-combi
SELCAL Honeywell
LSS Honeywell LSS-860
ELT Honeywell RESCU 406AF
MIRU Triple Honeywell LASEREF V
FRS Dual Honeywell AR-Combi

Interior

14 Pax. LH 13” Convertible Crew Closet, located behind the Pilot Seat
Third Crewmember seat
RH 30” Forward Lavatory
RH 50” Main Galley
Cabin Sliding door
Forward Cabin consists of four 20” Single Seats, and two Console Tables
Mid Cabin consists of one LH Electrical Hi/Low dining table, two LH 20” Dual Seats
Aft Cabin consists of dual 80” three-place Electrical Divan with armrests
Aft Lavatory consists of a 47” Toilet-Vanity, and a 47” Closet
Aft Baggage Compartment

Gulfstream G650ER (2018)

Specifications

Leonardo AW139 (2007)

Specifications

Leonardo AW169 (2016)

Specifications

Airframe

Year of Manufacture: 2016
Entry Into Service: 2017
Total Time Since New: 255 Hours
Total Landings Since New: 606

Engines

Model: PW210A
ENGINE 1 ENGINE 2
Serial Number: PCE-BP0039 PCE-BP0012
Total Time Since New: 255 Hours 255 Hours
Total Cycles Since New: 606 606

Highlights

One owner from New
VIP ‘’Pearl’’ Interior 3+2+2
Conversion kit for 4+2+2 interior
Soundproofing
Removable Emergency Floats
Removable External Life Raft on Sponson
Tail Fin Camera
ADS-B
SVS
JAR Ops 3 / EASA IFR Equipped
Increased Gross Weight (4800 kg MTOW)

Cockpit Equipment

Three Rockwell Collins Display Units 10” X 8” colour AMLCD
with LED backlight and NVIS compatibility:
2 Primary Flight Displays and 1 Multi-Function Display
Integrated Standby Instrument System (ISIS)
Two Display / cursor Control Panels/Devices (DCP/CCD)
Reversionary Control Panel (RCP)
Two Master Caution / Warning Lights (MCL/MWL)
Two Avionics Full Duplex Ethernet (AFDX) switches
Two Aircraft Monitoring & Management Computers (AMMC)
Data Transfer Device (DTD)
Two touch screen control panels
Four Axis Automatic Flight Control System (AFCS)
Two Flight Control Computer (FCC)
Flight Control System (FCS) Control Panel
Two VHF-AM radios
Two NAV (VOR/ILS/MB) receivers
One ADF / DME
Transponder with Enhanced Surveillance Mode (Mode S)
First SBAS GNSS (GPS)
Second SBAS GNSS (GPS)
Two Audio Control Panels (Pilot and Co-pilot stations)

Other Equipment

Anti-icing fuel systems and two magnetic chip detectors (one per engine)
Independent dual-channel FADEC systems (one per engine)
Fire detection/ extinguisher system
Crashworthy fuel cells (1140 litres of usable fuel)
Filler port for gravity refuelling (on left hand side)
Dual independent, redundant hydraulic system
Retractable swivelling Landing / taxiing lights (2)

Interior

VIP “Pearl” 3+2+2 Interior Layout
Conversion Kit to achieve Pearl 4+2+2
VIP Composite Liners leather/leatherette covered with enhanced
soundproofing extended for rear seats
Rear Cabin windows (left and right)
Cabin ambient Mood Multicolor – LED lights, white LED reading light
Environmental Control system (ECS) – Air Conditioning
Inter-Communication System for all passengers inc. Headsets ANR type (Qty. 7)
Handmade customised passenger carpet
Comfortable VIP seat leather covered sliding and with reclinable backrest x 3
Extra wide armchairs leather covered sliding and with reclinable backrest x 2
VIP Seats in the rear cabin bay x 2
Basic Entertainment and Cabin Management System inc. 4.3” Touch screen
panel and one iPad mini for lighting system and ECS control
Window and roll up curtain on pilots’ side
Cabin Active Comfort Enhancer VIP
Hinged passenger doors in lieu of sliding doors with dedicated liners
28V DC cabin power outlet
Electrical ‘limo’ window for the separation wall

Audio Management Unit interfacing external transceivers
Passenger Intercom Amplifier
Two flux valves
Two Air Data and Altitude Heading Reference Systems (ADAHRS)
One Radar Altimeter
Pilot Clock/Co-Pilot Clock
TCAS II Rockwell Collins TCAS-4100 –
Moving map
Weather Radar Rockwell Collins RTA-4112 MultiScan
SATCOM Iridium Skytrack ISAT 200 A integrated
ADS-B Out
Health and Usage Monitoring System (HUMS)
Flight Data Monitoring system (FDM)
Helicopter Terrain Avoidance and Warning System (HTAWS)
Synthetic Vision System (SVS)
Second radar altimeter
Rotor brake system
One solid state Cockpit and Voice Flight Data Recorder with ULB
One Emergency Locator Transmitter (ELT – 3 frequencies) (fixed)
Approach plates chart holders with lights for pilot and co-pilot
Co-pilot hinged window (storm window)

Cockpit – Interior

Pilot/ Co-pilot crashworthy adjustable seats (with inertial reels
and separate 5 points safety belts)
28V DC cockpit power outlet
First aid kit (as per JAR OPS 3)
One cockpit and one cabin fire extinguisher (as per JAR OPS 3)

Exterior

Upper areas painted in white and lower areas in mid blue
Silver accent stripes
Retractable Landing Gear
Electrically operated cabin dual step
Baggage Compartment extension Baggage smoke sensor
Emergency Floats – Removable
External Life Raft on Sponson – Removable
Tail Fin Camera
Strobe lighting

Mil Mi-8AMT (2011)

Specifications

Exterior

Overall White with Yellow, Orange and Black stripes

Interior

13 passenger VVIP interior.
Forward – 3-place divan opposite a 2-place club with a fixed executive table.
Aft – 8-place club layout with stowaway executive tables.
Glass partition between forward and aft compartments.
All seats in Cream leather with Gold plate accessories. High gloss wood veneer cabinetry.
Burgundy patterned carpet. Aft toilet and baggage storage.
Entertainment system with forward bulkhead monitor and four monitors in overhead locations.

Engines

Klimov TV3-117VM

Time since new: 1,183hrs (Left); 1,183 (Right)

Time between overhauls: 2,000 (Left); 2,000 (Right)

APU

Ivchenko AI-9B

Time since new: 44

Time between overhauls: 150

Avionics

Autopilot: AP-34

Rad Alt: A-037

GPS/NAV/com: Garmin GNS 530

ELT: 406

CVR: P-503B

Com: ORLAN-85ST

ADF: APK-15M

DME: King KN63

Radar: King RDR 2000

MFD: King KMD 850

Features

Dual controls

Anti-icing system

Long range fuel system with internal aux fuel tank & external fuel tank

Standby horizon