Airframe:
402 Hours Since New; 151 Landings as of 14 June 2011
Entry to Service Date – October 2010
JAR-OPS1 Compliant
Enrolled on FalconCare
Engines:
| Description | Three (3) Pratt & Whitney Canada PW307A | ||
| Total Time Since New | 402 Hrs | 402 Hrs | 402 Hrs |
| Total Cycles Since New | 151 Cycles | 151 Cycles | 151 Cycles |
| Program Coverage | TBD | ||
APU:
| Description | Honeywell GCTP36-150 (FN) |
| Total Time Since New | 443 |
| Program Coverage | TBD |
Avionics:
The Falcon 7X benefits from the intuitive EASy flight-deck technology developed for the Falcon aircraft and incorporated into the Falcon 900 and Falcon 2000 series. The system displays information on four 14.1-inch, flat-panel LCD screens arranged in a T-shape. It allows pilots to make “heads up” data entry using a Cursor Control Device (CCD) and menu-driven selections. The Cursor Control Device developed by Dassault Aviation for EASy gives an unprecedented ease of use for the pilots, in all situations. The Falcon 7X is the first business jet with a Digital Flight Control System; conferring a range of benefits, such as precise flight path control, automatic trim adjustments during configuration changes, and basic autopilot functions through the cockpit’s side-stick controller for setting heading and attitude.
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Additional Equipment:
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Interior Configuration:
Fifteen (15) passenger configuration featuring a forward four (4) place double club, mid cabin four (4) place dining group opposite of a two (2) place club, and aft two (2) place club opposite of a three (3) place divan. This aircraft has a forward crew lavatory and a large aft lavatory. The full service galley is located in the forward cabin.
Weights:
| Max Ramp Weight – 69,200 lbs | Max Zero Fuel Weight – 41,000 lbs |
| Max Takeoff Weight – 69,000 lbs | Basic Empty Weight – 35,559 lbs |
| Max Landing Weight – 62,400 lbs | Fuel Capacity (Usable) – 31,940 lbs |
Warranty:
The Dassault Falcon Jet 10-year airframe warranty is one of the most comprehensive on any certified aircraft in the industry and is generally outlined as follows:
Major Airframe 10 years / 10,000 Hours
Components Manufactured
by Company or Vendors 5 Years / 5,000 Hours
Paint / Interior 2 Years / 2,000 Hours
Labor for Paint / Interior 2 Years / 2,000 Hours
Labor for Components
Removal & Re-Installation 5 Years / 5,000 Hours
Engines 5 Years / 3,000 Hours
APU 5 Years / 3,000 Hours






















