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| Specification
& Weight
In a CJ1+, you’ll be a mover, not a shaker. That’s
because the CJ1+ flies at cruise speeds of up to 389 knots (448
mph) – 150 mph faster, two miles higher, and unquestionably
smoother than comparable turboprops. You’ll avoid weather
and traffic, while traveling in silky-smooth quiet.
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Maximum Cruise Speed (mid-cruise weight) |
 389 ktas (720
km/hr), at 31,000 ft (9,449 m)
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Airspeed Limits |
VMO from sea level to 30,500 ft (9,296 m) 260 kcas (481 km/hr)
MMO at 30,500 ft (9,296 m) and above M 0.71 (Indicated)
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Ceiling |
41,000 ft (12,497 m) maximum certified
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Rates of Climb |
All engines 3,290 fpm (1,003 m/min)
Single engine 957 fpm (292 m/min)
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Stall Speed |
86 kcas (159 km/hr) MLW, landing configuration
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Pressurization |
Nominal pressure differential 8.5 psi (59 kP)
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NBAA IFR Range
(100 nm alternate) |
1,285 nm (2,380 km) with full fuel and maximum takeoff weight
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Airport Performance
(dry, level, hard-surfaced runway with zero wind) |
Takeoff distance (SL, ISA, MTOW) 3,200 ft (975 m)
Landing distance (SL, ISA, MLW) 2,840 ft (866 m)
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Engines |
Two Williams FJ44-1AP
Takeoff thrust 1,941 lb (8.63 kN)
Bypass ratio 2.65:1
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Baggage Capacity |
Volume 45 ft3 (1.27 m3)
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Outside Dimensions |
Wingspan 46 ft 11 in (14.30 m)
Overall height 13 ft 9 in (4.19 m)
Overall length 42 ft 7 in (12.98 m)
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Cabin Dimensions
(with typical interior installed) |
Height 57 in (1.45 m)
Width 58 in (1.47 m)
Length (excluding cockpit) 132 in (3.35 m)
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Design Weights & Fuel Capacity
| Design
Weights & Fuel Capacity |
| Maximum
ramp weight |
10,800
lb (4,898 kg) |
| Maximum
takeoff weight |
10,700
lb (4,853 kg) |
| Maximum
landing weight |
9,900
lb (4,490 kg) |
| Maximum
zero fuel weight |
8,400
lb (3,810 kg) |
| Maximum
fuel capacity (6.7 lb/gal) |
3,220
lb (1,461 kg) |
| Typical
empty weight* |
6,690
lb (3,035 kg) |
| One
pilot plus furnishings |
200
lb (91 kg) |
| Typical
basic operating weight (BOW) |
6,890
lb (3,125 kg) |
| Useful
load** |
3,910
lb (1,774 kg) |
| Payload
with full fuel |
690
lb (313 kg) |
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).
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