Specifications & Weights
Cessna Citation CJ1+ · Specifications
Overview
This document provides detailed specifications and performance data for the Cessna Citation CJ1+. It is intended for pilots and aviation enthusiasts seeking to understand the aircraft's capabilities, dimensions, and operational limits. Key information includes maximum speeds, climb rates, weight limits, and engine specifications. The document serves as a reference for operational planning and performance assessment, ensuring that users have the necessary data to operate the CJ1+ safely and efficiently.
- Maximum cruise speed: 389 knots (720 km/h) at 31,000 ft (9,449 m)
- Maximum certified ceiling: 41,000 ft (12,497 m)
- Rate of climb: 3,290 fpm (1,003 m/min) with all engines
- Takeoff distance (MTOW): 3,250 ft (994 m)
- Maximum ramp weight: 10,800 lb (4,898 kg)
Document
Source
Originally published by www.aviation-broker.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 2006
- Pages
- 2
- File size
- 24 KB
- Publisher
- www.aviation-broker.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 1,300
- Height (ft)
- 13
- Length (ft)
- 42
- Wingspan (ft)
- 46
- Engine model
- Williams FJ44-1AP
- Max speed (kt)
- 389
- Cruise speed (kt)
- 389
- Empty weight (lb)
- 6,765
- Fuel capacity (gal)
- 482
- Rate of climb (fpm)
- 3,290
- Service ceiling (ft)
- 41,000
- Max takeoff weight (lb)
- 10,700
Performance
- Landing over 50ft
- 2,590
- Takeoff over 50ft
- 3,250
- Landing distance (ft)
- 2,590
- Takeoff distance (ft)
- 3,250
- Stall speed clean (kt)
- 83
V-speeds
- VNE
- 263
- VS1
- 83
Weight & balance
- Useful load (lb)
- 3,835
- Max ramp weight (lb)
- 10,800
- Basic empty weight (lb)
- 6,765
- Max landing weight (lb)
- 9,900
- Max takeoff weight (lb)
- 10,700
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation CJ1+.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Maximum Cruise Speed
The CJ1+ achieves a maximum cruise speed of 389 knots (720 km/h) at a mid-cruise weight of 31,000 feet (9,449 m). This speed allows for efficient travel, significantly faster than comparable turboprop aircraft.
Ceiling and Climb Rates
The maximum certified ceiling for the CJ1+ is 41,000 feet (12,497 m). The aircraft has a rate of climb of 3,290 feet per minute (1,003 m/min) with all engines operational and 906 feet per minute (276 m/min) on a single engine.
Takeoff and Landing Performance
For takeoff from sea level under standard conditions at maximum takeoff weight (MTOW), the CJ1+ requires a distance of 3,250 feet (994 m). The landing distance at maximum landing weight (MLW) is 2,590 feet (789 m).
Engine Specifications
The CJ1+ is powered by two Williams FJ44-1AP engines, each providing a takeoff thrust of 1,965 pounds (8.74 kN) with a bypass ratio of 2.58:1.
Weight and Capacity
The maximum ramp weight of the CJ1+ is 10,800 pounds (4,898 kg), with a maximum takeoff weight of 10,700 pounds (4,853 kg) and a maximum landing weight of 9,900 pounds (4,490 kg). The aircraft has a useful load of 3,835 pounds (1,740 kg).
Full document text
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. Specifications & Weights ENGLISH (METRIC) Maximum Cruise Speed (mid-cruise weight) 389 ktas (720 km/hr), at 31,000 ft (9,449 m) Airspeed Limits VMO from sea level to 30,500 ft (9,296 m) 263 KIAS (487 km/hr) MMO at 30,500 ft (9,296 m) and above M 0.71 (Indicated) Ceiling 41,000 ft (12,497 m) maximum certified Rates of Climb All engines 3,290 fpm (1,003 m/min) Single engine 906 fpm (276 m/min) Stall Speed 83 kcas (153 km/hr) MLW, landing configuration Pressurization Nominal pressure differential 8.5 psi (59 kP) NBAA IFR Range (100 nm alternate) 1,300 nm (2,408 km) with full fuel and maximum takeoff weight Airport Performance (dry, level, hard-surfaced runway with zero wind) Takeoff distance (SL, ISA, MTOW) 3,250 ft (994 m) Landing distance (SL, ISA, MLW) 2,590 ft (789 m) Engines Two Williams FJ44-1AP Takeoff thrust 1,965 lbs (8.74 kN) takeoff thrust Bypass ratio 2.58:1 Baggage Capacity Volume 45 ft3 (1.27 m3) 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) 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) Design Weights & Fuel Capacity ENGLISH (METRIC) TOP 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* 6,765 lb (3,069 kg) One pilot plus furnishings 200 lb (91 kg) Typical basic operating weight (BOW) 6,965 lb (3,164 kg) Useful load** 3,835 lb (1,740 kg) Payload with full fuel 615 lb (279 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). 08/08/2006
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