Cessna Citation II/SP

Jet • twin engine • Low Wing • Retractable gear

Range Visualization

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

Payload vs. Range

Customize assumptions

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
374
KTAS
Cruise Speed
10
Occupants
1520
nm
Max Range
-530
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna Citation II/SP

Cessna Citation II/SP (Model 551)

The Citation II/SP is the single-pilot version of the popular Model 550 Citation II. By certifying the aircraft under FAR Part 23 standards (restricting the MTOW to 12,500 lbs), Cessna enabled owner-operators to fly a high-performance jet without the requirement for a second-in-command, revolutionized the light jet market.

Key Features for GA Buyers

  • Single-Pilot Operation: The primary draw for owner-operators, significantly reducing crew costs and increasing scheduling flexibility.
  • Docile Handling: Its straight-wing design provides excellent low-speed handling and stability, making it a relatively easy transition for pilots moving up from high-performance turboprops.
  • Airport Access: With a landing distance of well under 3,000 feet, the II/SP can utilize thousands of smaller community airports that larger swept-wing jets must bypass.
  • Spacious Cabin: Despite its ‘light jet’ classification, it often features a 7-8 passenger club seating arrangement and a private aft lavatory.

Trade-offs

  • Weight Limitations: To stay within the 12,500 lb single-pilot limit, the II/SP has a lower MTOW than the standard Citation II. Carrying a full load of passengers often necessitates a significant reduction in fuel, limiting range.
  • Speed: The straight wing that provides great short-field performance also limits top-end cruise speed to around 370-380 knots, slower than contemporary swept-wing competitors.
  • Avionics Upgrades: Many older 551s still have legacy cockpit tech; buyers should look for units with Garmin G600/G700 or GTN upgrades to meet modern ADS-B and navigation requirements.

Technical Specifications

Dimensions

Wingspan
51.7 ft
Length
47.2 ft
Height
15.0 ft
Parking area (ft2)
3220.74 ft2

Weights

Max Takeoff Weight
12,500 lbs
Max Landing Weight
12,000 lbs
Useful Load
4,441 lbs
Fuel Capacity
742 gal

Performance

Cruise Speed
374 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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