2015 Boeing 787-9 For Sale, Switzerland

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2015 boeing 787-9 on airfield with grass verges communications tower in background grey sky
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Boeing 787-9 5
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Europe, Switzerland
Year
2015
S/N
37109
Reg
-
TT
16:30

Aircraft Description

Green Boeing Completion

Ferry Time Only

Available for Viewings in Europe

Available for Immediate Delivery

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Jetcraft Corporation
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    AIRFRAME

    Total Time Since New 16:30 Hours
    Total Landings Since New 6 Landings
    Manufacturing Date 28 April 2015
    Delivery Date 30 April 2015
    Serial Number 37109
    Line Number 293
    Variable Number ZB299
    Home Base Basel, Switzerland
    Certification Currently FAA (EASA capable)

    ENGINES

    Description General Electric GEnx-1B74/75/B2
    Serial Number(s) 956518 956520
    Total Hours Since New 16:30 Hours 16:30 Hours
    Total Cycles Since New 6 Cycles 6 Cycles

    APU

    DESCRIPTION HAMILTON APS-5000A
    SERIAL NUMBER HSC-E1525347PL
    APU TOTAL TIME SINCE NEW 36 HOURS
    APU TOTAL CYCLES SINCE NEW 63 CYCLES

    TOTAL TIME

    16:30
  • AVIONICS & CONNECTIVITY
    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)
  • Interior & Entertainment
    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.

  • EXTERIOR
    Base Paint Color(s) Matterhorn White
    Last Painted Date Original
  • Additional Equipment & Information
    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.

    WiFi

    No

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