This stunning Falcon 100 is the fastest light jet ever produced and its pilot-owner has spared no expense in completely modernizing its flight deck with new universal avionics featuring Nav Display with Synthetic Vision, TAWS, TCAS II and Electronic Charts and a Super Flight Management System with WAAS and LPV. The new completion interior and exterior provide this efficient Falcon 100 a pedigree with the highest levels of technology, performance and tastefully appointed refinement.
Airframe: 4675 hours / 4355 landings
- New Universal Flight Deck
- AVTRACK Enrolled
- Thrust Reverse
- Aft Baggage Mod
- JSSI Platinum
Honeywell TFE731-2 Engines: 4555 hours / 4325 cycles
C & 2C complied with 15 June 2013 next due 30 April 2019 & 15 June 2025
3C complied with 30 April 2007 – next due 01 March 2025
B complied with 15 June 2013 – next due 01 July 2023
3B complied with 2004 – next due 13 August 2035
|Engines MPI||remaining engine #1: 840.7 Hrs||engine #2: 412.4 Hrs|
|Engines CZI||remaining engine #1: 3640.7 Hrs||engine #2: 3212.4 Hrs|
Flight Deck Modernization
Flight deck modernization with the Universal EFI-890R features integrated Flat Panel Displays offering significant improvement in situational awareness and reduces pilot workload which adds to the overall safety of your flight. The EFI-890R Advanced Flight Display offers flexibility as a stand-alone Primary Flight Display (PFD) or Multi-Function Display (MFD), as well as a fully integrated PFD/Navigation Display (ND) cockpit system. The EFI-890R replaces ADI, HSI, Radar Indicator, Altimeter, VSI, RMI and Air-speed Indicators with PFD and ND large multi- format displays.
EFI-890R 3-DISPLAY Universal Avionics EFI-890R 3-Display Flat Panel Electronic Flight Information System certified in accordance with Elliot Aviation STC (ST02194CH)
UNS-1Lw FMS WAAS/LPV Universal Avionics UNS-1Lw Super Flight Management System with WAAS and LPV
TAWS CLASS A Class A Universal Avionics Terrain Awareness Warning System
UNS VISION-1 Universal Avionics Vision-1 System
UNS EFI-890 Universal Avionics dual Application Server
UNS RCU / RTU Universal Avionics Radio Control Unit
VHF & HF RADIO MODS ICAO Annex 10 VHF FM Immunity and 8.33Khz Comm Radio Frequency Spacing requirements for European operation
TCAS-4000 Collins TCAS-4000 TCAS II Collision Avoidance and Traffic Alert System certified in accordance with Duncan Aviation STC ST01367CH-D
F100 w/COLLINS ADC-87 Collins ADC-87 Air Data Computers to replace existing ADC-80’s to meet requirements for Reduced Vertical Separation Minimums (RVSM) certified in accordance with Standard Aero STC 01361CH- D and STC ST01723CH
AIRCELL ALT-55B AirCell ST 3100 Iridium Transceiver
WSI AV-301 (provisions) Provisioned new wiring for a WSI AV-301 InFlight Satellite Weather System
DC COCKPIT OUTLET circuit-protected DC outlet receptacle in the cockpit area
AC & DC CABIN OUTLET circuit-protected AC outlet receptacle and a new circuit-protected DC outlet receptacle in the forward right hand cabin by the #2 seat using acceptable practices and guidelines of Section 2 of FAA approved document DUN-A1 Rev. 11, GDMR101 Rev. Orig., EPS-0020 Rev. E, and EPS-0090 Rev. B
Overall Snow White featuring light beige accent striping.
Luxurious Tahitian Beige eight passenger fireblocked interior featuring three fully-articulating seats with a three place divan and certified forward two place side facing seat with a belted
The Preceding Preliminary Aircraft Presentation by Premier Jet Aviation, Inc. Is For Discussion Purposes Only, Is Subject To Verification By Purchaser, Is Subject To Change Without Notice, And Is Not To Be Considered A Representation Of This Aircraft. Interested Parties Should Rely Upon Their Own Inspection Of The Aircraft And Its Records. Aircraft Is Offered Subject To Prior Sale Or Withdrawal From Market.