2015 Boeing 787-9 for sale, Switzerland

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)

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

Warranty: Airframe & Systems 90 months or 5,000 hours Engines 4,000 hours or 10 years
• 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.