Dassault Falcon 50 DA-50 Flight Training & Type Rating Courses
The Dassault Falcon 50 is a French-built super mid-sized, long-range corporate jet, featuring a three jet engine layout with an S-duct central engine. It has the same fuselage cross section and similar capacity as the earlier Falcon 20 twinjet but is a completely new design that is Area ruled and includes a more advanced wing design.
The first prototype flew on 7 November 1976, with French airworthiness certification on 27 February 1979, followed by U.S. Federal Aviation Administration certification on 7 March 1979. Dassault developed a maritime surveillance and environmental protection version as the Gardian 50.
The Falcon 50 was later replaced by the Falcon 50EX, the first of which flew in 1996, and the last of which was delivered in 2008.The Falcon 50EX features improved engines and other enhancements to give further range improvements to an already long-legged jet. It remains a very popular corporate jet for its long-range, luxury, and for the recognition of status for owning a fast three-engined jet.
The last Falcon 50EX was built in late 2007 and delivered in early 2008.
Successors of the Falcon 50 are the Falcon 7X and the Falcon 900 featuring a larger fuselage and the same three-engine arrangement. Dassault announced in January 2008 what is essentially a replacement aircraft for the Falcon 50, codenamed the “SMS” (Super Mid Size). The basic design process, including engine select was supposed to be completed by the early 2009. However, in a June 2009 press conference, CEO Charles Edelstenne said that all design choices had been reopened and the goal was intended to the end of the year.
Dassault and Aviation Partners Inc. have announced that High Mach blended winglets were being developed for the Falcon 50 as a retrofit kit.
Dassault Falcon 50 DA-50 Specifications
Data from Jane’s All the World’s Aircraft 1988-89
- Crew: Two
- Capacity: 8 to 9 passengers
- Length: 18.52 m (60 ft 9¼ in)
- Wingspan: 18.86 m (61 ft 10½ in)
- Height: 6.98 m (22 ft 10½ in)
- Wing area: 46.83 m² (504.1 ft²)
- Empty weight: 9,163 kg (20,200 lb)
- Max. takeoff weight: 17,600 kg (37,478 lb)
- Powerplant: 3 × Garrett TFE731-3-1C turbofan engines, 16.5 kN (3,700 lbf) each
- Maximum speed: Mach 0.86 (915 km/h, 494 knots, 568 mph)
- Cruise speed: Mach 0.82 (888 km/h, 479 knots, 551 mph)
- Range: 6,480 km (3,500 NM, 4,025 sm)
- Service ceiling: 14,935 m (49,000 ft)
Azma Flt Inc Offers the Following Type Rating Courses for Falcon 50 DA-50 Which Qualifies You To Perform Duties Of Pilot In Command and Second in Command in Falcon 50 DA-50, DA-50EX, DA-900, DA-900EX
- Initial Pilot in Command Type Rating Course for Falcon 50 DA-50
- Initial Second in Command Type Rating Course for Falcon 50 DA-50
- Recurrent Training FAR 61.58 for Falcon 50 DA-50
For details regarding customized courses to meet your needs, please contact us
Falcon 50 DA-50 Type Rating Course
Azma FLT Inc. Will Provide you with an accelerated Pilot in Command type rating flight-training course specifically designed for you, based on your previous education and flight experience in a Falcon 50 DA-50.
Your Falcon 50 DA-50 will be added to your Private Pilot, Commercial Pilot and or Airline Transport Pilot Certificate.
Your Pilot in Command Falcon 50 DA-50 Type Rating and or Falcon 50 DA-50 Second in command Type Rating practical test will be administered by current and qualified FAA Designated Pilot Examiner, John S. Azma founder of Azma FLT Inc or FAA qualified pilot examiner of your choice according to our current Airline Transport Pilot Practical Test Standard (PTS).
Duration and Location of your Flight Training
Depending on your previous flight experience, education Azma Flt Inc will be able to provide you with an accelerated course designed based on your skills in between 3 to 5 days in duration, which will require your full time participation. Our dedicated instructors are able to travel to your location and provide you with your flight training in Falcon 50 DA-50 at your location and or in our office located at Orlando International Airport
Falcon 50 DA-50 INITIAL TYPE RATING COURSE and Falcon 50 DA-50 SECOND IN COMMAND TYPE RATING COURSE Will Include:
A- AIRCRAFT SYSTEM PERFORMANCE AND LIMITATIONS
- Landing gear—extension/retraction system(s); indicators, float devices, brakes, antiskid, tires, nose-wheel steering, and shock absorbers.
- Power plant—controls and indications, induction system, carburetor and fuel injection, turbocharging, cooling, fire detection/protection, mounting points, turbine wheels, compressors, deicing, anti-icing, and other related components.
- Fuel system—capacity; drains; pumps; controls; indicators; cross feeding; transferring; jettison; fuel grade, color and additives; fueling and defueling procedures; and fuel substitutions, if applicable.
- Oil system—capacity, grade, quantities, and indicators.
- Hydraulic system—capacity, pumps, pressure, reservoirs, grade, and regulators.
- Electrical system—alternators, generators, battery, circuit breakers and protection devices, controls, indicators, and external and auxiliary power sources and ratings.
- Environmental systems—heating, cooling, ventilation, oxygen and pressurization, controls, indicators, and regulating devices.
- Avionics and communications—autopilot; flight director; Electronic Flight Instrument Systems (EFIS); Flight Management System(s) (FMS); Doppler Radar; Inertial Navigation Systems (INS); Global Positioning System/ Wide Area Augmentation System/Local Area Augmentation System (GPS/WAAS/LAAS); VOR, NDB, ILS, GLS, RNAV systems and components; traffic (MLS deleted) awareness/warning/avoidance systems, terrain awareness/warning/alert systems; other avionics or communications equipment, as appropriate; indicating devices; transponder; and emergency locator transmitter.
- Ice protection—anti-ice, deice, pitot-static system protection, propeller, windshield, wing and tail surfaces.
- Crewmember and passenger equipment—oxygen system, survival gear, emergency exits, evacuation procedures and crew duties, and quick donning oxygen mask for crewmembers and passengers.
- Flight controls—ailerons, elevator(s), rudder(s), control tabs, balance tabs, stabilizer, flaps, spoilers, leading edge flaps/slats and trim systems.
- Pitot-static system with associated instruments and the power source for the flight instruments.
B. TASK: PERFORMANCE AND LIMITATIONS
- Performance and limitations, including a thorough knowledge of the adverse effects of exceeding any limitation.
- Demonstrates proficient use of Falcon 50 DA-50 performance charts, tables, graphs, or other data relating to items, such as:
- Accelerate-stop distance.
- Accelerate-go distance.
- Takeoff performance—all engines and with engine(s) inoperative.
- Climb performance including segmented climb performance with all engines operating—with one or more engine(s) inoperative, and with other engine malfunctions as may be appropriate.
- Service ceiling—all engines, with engines(s) inoperative, including drift down, if appropriate.
- Cruise performance.
- Fuel consumption, range, and endurance.
- Descent performance.
- Landing distance.
- Land and hold short operations (LAHSO).
- Go-around from rejected landings (landing climb).
- Other performance data (appropriate to the airplane).
- Describes Falcon 50 DA-50 the airspeeds used during specific phases of flight.
- Describes the effects of meteorological conditions upon performance characteristics and correctly applies these factors to a specific chart, table, graph, or other performance data.
- Computes the center-of-gravity location for a specific load condition including adding, removing, or shifting weight.
- Determines if the computed center-of-gravity is within the forward and aft center-of-gravity limits, and that lateral fuel balance is within limits for takeoff and landing.
- Adverse effects of airframe icing during pre-takeoff, takeoff, cruise and landing phases of flight and corrective actions.
- Procedures for wing contamination recognition and adverse effects of airframe icing during pre-takeoff, takeoff, cruise, and landing phases of flight.
- Procedures in applying operational factors affecting airplane performance. Stabilized approach procedures and the decision criteria for go-around or rejected landings.
C- FLIGHT TRAINING PREFLIGHT PROCEDURES, INFLIGHT MANEUVERS AND POSTFLIGHT PROCEDURE
- PREFLIGHT INSPECTION
- PRE-TAKEOFF CHECKS
- TAKEOFF AND DEPARTURE PHASE
- NORMAL AND CROSSWIND TAKEOFF
- CONFINED-AREA TAKEOFF AND CLIMB
- INSTRUMENT TAKEOFF
- POWERPLANT FAILURE DURING TAKEOFF
- REJECTED TAKEOFF
- DEPARTURE PROCEDURES
- APPROACHES TO STALLS
- POWERPLANT FAILURE
- SPECIFIC FLIGHT CHARACTERISTICS
- RECOVERY FROM UNUSUAL ATTITUDES
- STANDARD TERMINAL ARRIVAL/FLIGHT MANAGEMENT SYSTEM PROCEDURES
- PRECISION APPROACHES (PA)
- NON PRECISION APPROACHES (NPA)
- CIRCLING APPROACH
LANDINGS AND APPROACHES TO LANDINGS
- NORMAL AND CROSSWIND APPROACHES AND LANDINGS
- LANDING FROM A PRECISION APPROACH
- APPROACH AND LANDING WITH (SIMULATED) POWERPLANT FAILURE
- LANDING FROM A CIRCLING APPROACH
- CONFINED-AREA APPROACH AND LANDING
- REJECTED LANDING
- LANDING FROM A NO FLAP OR A NONSTANDARD
- FLAP APPROACH
- NORMAL AND ABNORMAL PROCEDURE
Your course of training will include aircraft flight training manual current ATP practical test standards.
FOR ADDITIONAL INFORMATION PLEASE CONTACT JOHN AZMA