Cessna Citation II

Jet • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
385
KTAS
Cruise Speed
10
Occupants
1520
nm
Max Range
1479
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna Citation II

Cessna Citation II (Model 550)

The Citation II is the definitive light jet that established Cessna’s dominance in the segment. Stretched significantly over the original Citation I, the Model 550 offers a true 8-passenger cabin while maintaining the docile, ‘straight-wing’ flight characteristics that make it a favorite for flight departments transitioning from turboprops.

Key Features for GA Buyers

  • Mission Versatility: Unlike the single-pilot II/SP, the standard Model 550 has a much higher MTOW (up to 15,100 lbs in later serials), allowing for a respectable payload even with significant fuel on board.
  • Runway Performance: Famous for its ‘short-field’ capabilities, it can operate out of 3,500-foot runways at gross weight, providing access to smaller regional airports.
  • Proven Platform: With over 600 airframes built, parts availability and maintenance expertise are widespread throughout the global GA network.

Trade-offs

  • Two-Pilot Requirement: This model requires a crew of two, which increases operational costs compared to the 551 variant.
  • Block Speeds: While it is faster than the Citation I, it still cruises below 400 knots, meaning it will be outpaced by swept-wing competitors on longer legs.
  • Engine Maintenance: The JT15D-4 engines are reliable but represent a significant portion of the operating budget during overhaul cycles.

Technical Specifications

Dimensions

Wingspan
52.2 ft
Length
47.3 ft
Height
15.0 ft
Parking area (ft2)
3253.06 ft2

Weights

Max Takeoff Weight
15,100 lbs
Max Landing Weight
13,500 lbs
Useful Load
6,450 lbs
Fuel Capacity
742 gal

Performance

Cruise Speed
385 KTAS
Never-Exceed (Vne)
403 KIAS
Max Structural Cruise (Vno)
262 KIAS
Approach Speed
99 KIAS
Stall, Clean (Vs1)
82 KIAS
Range
1520 NM
Service Ceiling
43,000 ft
Rate of Climb
3040 fpm
Takeoff over 50 ft obstacle
2,990 ft
Landing ground roll
2,270 ft

Engines

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