SN-BOEING-37109: Boeing BBJ 787-9

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Description

FERRY TIME ONLY
GREEN BOEING COMPLETION
AVAILABLE FOR VIEWINGS IN EUROPE
AVAILABLE FOR IMMEDIATE DELIVERY
  

Avionics

The Boeing 787-9 is equipped with an integrated avionics suite. A general summary of this aircraft’s avionics suite is as follows (Unit Descriptions in bold indicate optional/added equipment):
Type of Unit	                                                                           Quantity	Unit Description
EFIS (Electronic Flight Instrument System)	 	
ESIS (Electronic Standby Instrument System)	 	 
FMS (Flight Management System)	 	 
GPS (Global Positioning System)	                                           Single	        Honeywell
DCMF (Data Communication Management Function)	           Single	
CDU (Control Display Unit)	 	
ADC (Air Data Computer)	 	
NAV (Navigation Radio)	 	
RMI (Radio Magnetic Indicator)	 	
DME (Distance Measuring Equipment)	                                     Dual	         Honeywell
HUD (Head Up Display)	Single	
ADF (Automatic Direction Finder)		
AFCS (Auto Flight Control System)		
A/P (Autopilot)		
SELCAL (Selective Calling System)	                                     Single	
VHF COM (Very High Freq. Communication)	                             Triple	         Collins
HF COM (High Freq. Communications)		
SATCOM (Satellite Communications)	                                     Single	         Dual Channel Aero H+
RADAR	Single	Collins ISSPU
RADAR ALT (Radar Altimeter)		
XPNDR (Transponder)		
GPWS (Ground Proximity Warning System)	                             Single	         Collins TAWS
TCAS (Traffic Collision Avoidance System)	                             Single	
ELT (Emergency Locator Transmitter)	                                     Single	
CVR (Cockpit Voice Recorder)		
FDR (Flight Data Recorder)

NAVIGATION & COMPLIANCE
Data link message exchanges with ground ACARS stations, using VHF (including VDL Mode 2 when suitable ground stations are available), HF, or SATCOM.
Air traffic services (ATS) data link using the future air navigation system-1 (FANS-1) standards for controller-pilot data link communications (CPDLC), automatic dependent surveillance (ADS), and ATS facilities notification (AFN), with these functions integrated with the flight management system (FMS). The 787 ATS data link functionality is fully compatible with the global air traffic management (ATM) environment. The FANS-1 functionality is interoperable with oceanic data link systems.
ATS data link using VDL Mode 2 and the ICAO aeronautical telecommunications network (ATN) baseline-1 standards for CPDLC, and context management, with these functions integrated with the FMS (allowing, for example, automatic loading of uplinked route clearances) and the FANS-1 function. This provides a single unified crew interface, allowing operators to have both FANS-1 and a standard and recommended practices (SARP) compliant ATN application on the same airplane with a single set of crew procedures. ATN coupled with the FANS-1 function, provides what is commonly termed FANS-2 capability.
Flight information services (FIS) data link message exchanges, including departure clearances, oceanic clearances, and digital automatic terminal information service (D-ATIS)
Data link message exchanges with ground ACARS stations, using VHF (including VDL Mode 2 when suitable ground stations are available), HF, or SATCOM.
  

Engines / Mods

Left Engine	                                Right Engine
Description	                General Electric GEnx-1B74/75/B2
Serial Number(s)	        956518	                                        956520
Total Cycles Since New	6 Cycles	                                         6 Cycles
  

Interior / Exterior

Crew Rest - Forward location with Two (2) Beds
Jumpseat - Yes
Cargo Hold - Total volume 5,452 ft3/154.4 m3
Class C forward, aft, and bulk lower hold cargo compartments are provided. Cargo can be loaded into the forward and aft compartments in certified and non-certified airplane unit load devices (ULD), or containers and pallets). Loose baggage and other parcels can be loaded into the bulk compartment.

The cargo handling system provides hardware for ULD guidance, restraint, conveyance and powered movement. The system accepts LD-3 (side-by-side), A-size (88- by 125-inch) and M-size (96- by 125-inch) pallets. It also accepts LD-1, LD-2, LD-3-46W/-46, LD-4, LD-5, LD-6, LD-7, LD-8, LD-9, LD-10 and LD-11 containers, and K-, L-, and N-size pallets. All containers and pallets are individually restrained.

Base Paint Color(s)	 - Matterhorn White
Last Painted Date - Original
  

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