 |
 |
 |
|
|
 |
|
|
|
|
| |
A new moderately swept wing design borrowed from the successful Citation Sovereign coupled with new Williams FJ44-4A engines produce exceptional performance benefits. The CJ4 is an outstanding combination of power, size and speed that will comfortably put you in the 500-mph club and deliver 1,825 nm of range with NBAA IFR 100 nm reserves.
|
|
| |
|
|
| |
 |
Specifications
& Weights
|
ENGLISH
(METRIC)
|
|
|
|
Maximum Cruise Speed |
435 KTAS (806 km/hr) at 35,000 ft (10,668 m)
|
|
Ceiling |
45,000 ft (13,716 m) maximum certified
|
|
Engines |
Two Williams FJ44-4A
Takeoff thrust 3,400 lbs ea. (15.12 kN)
|
Airport Performance
(dry, level, hard-surfaced runway with zero wind) |
Takeoff distance (SL, ISA, MTOW) 3,300 ft (1,006 m)
Landing distance (SL, ISA, MLW) 2,665 ft (812 m)
|
|
Outside Dimensions |
Overall width 50' 10" (15.49 m)
Overall height 15' 4" (4.67 m)
Overall length 53' 4" (16.26 m)
|
|
Cabin Dimensions |
Height 57" (1.45 m)
Width 58" (1.47 m)
Length (excluding cockpit) 208" (5.29 m)
|
|
Exterior Baggage Capacity |
Volume 65 ft3 (1.84 m3)
|
|
Range NBAA IFR Range |
1,825 nm (3,380 km) full fuel, maximum takeoff weight
|
|
|
| |
|
|
| |
|
Design
Weights & Fuel Capacity
|
ENGLISH
(METRIC)
|
TOP
|
|
| Full Fuel Payload |
With two pilots (400 lbs) 1,000 lbs (454 kg) |
| Maximum takeoff weight |
N/A |
Note: Performance
conditions are based on the International Standard Atmosphere.
Takeoff and landing field lengths are based on level, hard-surface,
dry runways with no wind.
*Reflects standard aircraft with typical options, typical interior
and unusable fuel and oil.
**Amount of payload and fuel that can be carried, over and above crew
(based on ramp weight). |
|
| |
10/16/06 |
|
| |
|
|
|
|
|
|
|
|
|
|
|
