- Ferry Time Only
- Green Boeing Completion
- Available for Viewings in Europe
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
| Left Engine | Right Engine | |
| 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 |
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) | |||||
INTERIOR
| Description | |
| 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 |
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. |
WEIGHTS
| Max Landing Weight | 425,000 lbs | 192,777 kg | Max Zero Fuel Weight | 400,000 lbs | 181,436 kg |
| Max Takeoff Weight | 557,000 lbs | 252,650 kg | Min Flight | 244,000 lbs | 110,677 kg |
| Max Taxi Weight | 559,000 lbs | 253,558 kg |
WARRANTY
Boeing and GE offers comprehensive and fully transferable warranty generally outlined as follows:
| Airframe & Systems | 90 months or 5,000 hours | Engines | 4,000 hours or 10 years |
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