Each large and luxurious seat tracks forward, back and side and can lean horizontally in several configurations. Standby boost pumps are activated by FADEC for starting or if a low fuel pressure condition is detected, automatically during fuel transfer and if selected manually to ‘on’ by the pilot.1.7.8LimitationsSee Chapter 2 LIMITATIONSAdditional Limitations:Battery:Lithium battery - min.

There is no separate fuel cut-off other than through the FIRE buttons, which also isolate the hydraulic pump and the generator field circuit on the respective side for emergency engine shutdown.Eachenginehasadualignitionsystemwith2igniterscontrolledbytheFADEC fired either singly or together as required by the FADEC. 1.7.1Engines The CJ4 is fitted with Two Williams FJ44-4A turbofan engines with Full Authority Digital Engine Control (FADEC). Fs2020 Cessna Citation CJ4 auto throttle. The integrated system allows selecting passengers from entertainment media such as CDs, DVDs and MP3s. The Citation CJ4 is powered by two Williams FJ44-4A turbofan engines, each of which produces 16,11 kN of power.
Max Landing Weight: 15.660 lbs 4. I did a short flight and i landed at about 120 KIAS, the plane violently bounced, i had about 30% fuel at the time, was i going too fast? The auxiliary input interface allows installation of an iPod or similar device. The active FGC will take roll, pitch and yaw inputs from the selected PFD and accompanying AHRS, and compute flight guidance commands for the flight director and autopilot. Cessna Citation CJ4 approach speed? Il primo Citation CJ4+ di produzione della Cessna volò nel maggio del 2009, la sua prima consegna avvenne l'anno successivo. Back-up electrical power for the FADEC is the main aircraft electrical system. If a complete loss of aircraft electrical power occurs, each PMA will power its respective FADEC unit to maintain engine operation. It is not reasonable for the pilot to remember all the appropriate actions for each of these and a comprehensive QRH needs to be immediately available in the cockpit for every flight.The systems architecture is such that emergency memory items are few, however the inter- relationship between systems and their automation means that a series of messages may appear at one time, revealing a number of symptoms that may be the result of a single system fault. Useful Fuel Capacity: 5828 lbs1.7.5Flight ControlsThe main (dual) flight controls are all cable operated. Normal, over-wing refuelling caps are also provided on top of the outboard end of each wing tank.

The CJ4 system is continually pressurised to 3000 psi by two engine-driven pumps providing hydraulic power on demand to the four hydraulic aircraft sub-systems. GENERAL DESCRIPTION The Cessna Citation CJ4 is a low-wing aircraft with re-tractable tricycle landing gear and a “T” tail. Only approximately 3⁄4 of the chart is visible, although it is possible to scroll the chart to see the top or bottom.The IFIS system is powered through the aircraft main DC power system. The engines are twin-spool (co-rotational) medium bypass turbofans with mixed exhaust and high-cycle pressure ratio. A secondary power circuit and control system is provided for the elevator trim, there is no manual trim mechanism available. Useful Load: 6.980 lbs 7. Cessna C525C Citation, CJ4. Therefore, the system is not suitable for approval of a ‘paperless’ operation and a suitable backup must be carried on board.Own ship position (FMS position) is presented on many of these charts. Unless a digital Airport Moving Map (AMM) has been used for the taxi chart, the error in the chart can be so large as to present the incorrect taxiway under the aircraft position symbol. Professional Pilot and Technician Training Programs A s the factory-authorized training provider for Cessna (Textron Aviation) for more than four decades, we offer type-specific, simulator-based training on all Cessna Citation models, including the Citation CJ4. Ha ottime performance al decollo e all'atterraggio, fatto che gli permette di avere accesso ad aeroporti con piste brevi, quali Lugano o St. Tropez, che sono spesso richiesti. Does anyone know how to do this. operating altitude with DC GEN OFF L/R: FL350Min. 21 comments. The FGP is equally accessible from either cockpit seat.

The aircraft has a maximum operating altitude of 45,000', a normal cruise speed of 425 KTS/490 MPH, and a 1,625 NM/1,872 SM seats-full range. XM Radio is also available for passengers. The aircraft also has a Venue cabin management system by Rockwell Collins, maintains electronic entertainment and controls the cabin cooler and heating environment. Max Take Off Weight: 17.111 lbs 3. 1.7.4Weight & BalanceRefer to AFM, Weight and Balance Data, Section VI.1. share. Distinctive detents are provided at take-off, climb and maximum cruise power settings for ease of operation. This is unlike all the other C525 aeroplanes, which have an open system that is pressurised on demand by the closing of a single bypass valve. Landing gear actuation, wing flaps, speed brakes and ground spoilers all use this hydraulic pressure for operation. Maximum fuel imbalance for normal operations is 200lbs. Ignition is activated automatically for starting and on approach to land and whenever a loss of combustion, excessively low engine speed or rapid deceleration is detected by the FADEC. I can dial in the preferred speed but I can't figure out how to activate it. Puoi disiscriverti in qualsiasi momento tramite il link fornito in Newsletter Le informazioni che hai fornito saranno elaborate in base all'informativa sulla privacy di LunaJets.Il tuo indirizzo di posta elettronica, Punteggio di soddisfazione media dei clienti basato su. Whenever ignition is active the message IGN appears in the EICAS display beside the N1 tapes.1.7.2Avionics / Cockpit Layout. In July 2011, the first CJ4 Citation was sent for charter operations in Germany. The CESSNA Citation CJ4 has a 3,412' balanced field length and 3,038' landing distance. Il sistema radar meteo all'avanguardia permette di rilevare con un certo anticipo condizioni meteo potenzialmente difficili e quindi di evitare turbolenze, garantendo un volo più tranquillo. A Citation CJ4 production model with the right cabin made its debut at the National Business Aviation Association (NBAA) trade show in October 2008. The distance is 3,708 km and the service ceiling is 13,716m. Ciò è in parte dovuto all'eccellente cabina del CJ4 che, essendo stato allungato a 5,29 m, è più spazioso rispetto a tutti gli altri aerei della gamma CJ, e ospita fino a 7 passeggeri. Engine start, required thrust and shut down are selected by the pilot through the cockpit engine starter control buttons, thrust lever position and run/stop buttons respectively. Cessna Citation type rating, line training. Citation CJ4 is basically a stretch version of CJ3 and tracks its roots back to the Cessna Citation 525 series launched in 1989 to replace Citation and Citation 1 and now include Cess Citation 1 to CJ1. Rockwell Collins Pro Line 21 avionics suite is provided with enhancements, including FMS (flight management system) v4.0 allowing WAAS (wide area augmentation system) capabilities and IFIS (integrated flight information system) v6.0 to provide display improvements, temporary flight restrictions and information higher.
Basic Operating Weight: 10.280 lbs 6. There is no thrust reverse or thrust attenuation system.Engine start sequence, power control, and shutdown are managed by the respective FADEC unit, each of which is independently powered by its own engine driven Permanent Magnet Alternator (PMA). temperature for engine start: -10°CNickel-cadmium & lead-acid battery min temp. A rudder bias system uses engine bleed air to assist in directional control during engine-out operation.A single autopilot is able to follow commands from one of 2 Flight Guidance Computer s (FGC) and is controlled through a single flight guidance panel (FGP) at the top centre of the main instrument panel.