Cessna citation operating manual

The Cessna Citation CJ4 is a low-wing aircraft with re-tractable tricycle landing gear and a “T” tail. A pressur- All performance data is based on a standard aircraft configuration, operating in International Standard Atmosphere (ISA) con - ditions with zero wind. Takeoff and landing field lengths are based on a level, hard surface, dry. 18 Heavy CE Weights – in pounds Ramp 14, Takeoff 14, Landing 12, Zero Fuel 9, Opt. ZFW 11,  · The Cessna Citation X (Model ) is an American business jet with 3, nmi (6, km) of range produced by Cessna and part of the Citation www.doorway.ruced at the October NBAA convention, it made its maiden flight on Decem, received its type certification on June 3, and was first delivered in July

The main landing gear of the CJ4 Gen2 jet is located inboard, reducing the track and making all aspects of ground handling smoother. The same long-stroke, trailing-link landing gear common to all Citation jets allows the softest landings and smooth taxiing. Special Missions. The Cessna Citation X [a] (Model ) is an American business jet with 3, nmi (6, km) of range produced by Cessna and part of the Citation www.doorway.ruced at the October NBAA convention, it made its maiden flight on Decem, received its type certification on June 3, and was first delivered in July The updated Citation X+ was offered from with a 14 in ( Page 1 This manual provides a description of the major airframe and engine systems in the Cessna Citation Mustang (Figure ). This material does not supersede, nor is it meant to sub- stitute for, any of the manufacturer's maintenance or flight manuals. The material pre- sented has been prepared from current design data.

Refer to Weight and Balance Data Sheets and Model Citation X Airplanes and On FAA Approved Weight and Balance Manual. BALLAST FUEL Ballast fuel is fuel that remains within the wing fuel tanks which cannot be used without causing the aft center-of-gravity limit to be exceeded. Ballast fuel is nonusable fuel. 20 Eaglesoft Development Group: Citation II SP/2 C Operating Manual SPECIFICATIONS Dimensions Length 47’, 3” Height 14’, ” Wingspan 51’, ” Horizontal Stabilizer Span 18’, 10” Wheelbase (Main to Nose Gear) 18’, 2” Stance (Distance between Main Gear) 17’, 7” Cabin Length (Pressure Vessel) 20’, 11” Height 4’, 9” Width 4’, 11” Capacities Oil Tank Gallons Per Engine Fuel (Maximum Usable) ~ Lbs. Per tank ( gallons) Oxygen (Full Bottle) Page 1 This manual provides a description of the major airframe and engine systems in the Cessna Citation Mustang (Figure ). This material does not supersede, nor is it meant to sub- stitute for, any of the manufacturer’s maintenance or flight manuals. The material pre- sented has been prepared from current design data.