Cessna 1SP

Turbofan • 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

345
KTAS
Cruise Speed
7
Occupants
910
nm
Max Range
818
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna 1SP

The Cessna 501 Citation I/SP is the single-pilot certified version of the original Citation I. It was specifically engineered to allow owner-operators to step up from high-performance twins and turboprops into the jet world without the requirement of a second-in-command. While it shares the ‘Slowtation’ reputation, it offers unparalleled simplicity and safety for solo jet operations.

Key Features for GA Buyers

  • Single-Pilot Certification: Unlike the standard Model 500, the 501 is factory-certified for single-pilot flight, significantly reducing operational costs and scheduling complexity for owner-operators.
  • Simplified Systems: Features straight wings and simple mechanical systems that are more reminiscent of a King Air than a complex swept-wing jet, leading to very docile stall characteristics.
  • Runway Flexibility: The 501 includes the wing extensions and thrust reversers that became standard on later Citation Is, allowing for operation on runways as short as 3,000–3,500 ft.
  • No Structural Life Limit: Like its sibling, the 501 airframe has no fatigue life limit, making it a sustainable long-term asset if corrosion is kept at bay.

Trade-offs

  • Legacy Avionics: Many 501s still carry legacy ‘steam gauges’ and early autopilot systems; modernizing the panel (e.g., Garmin G600/G700) is a common but significant six-figure investment.
  • Fuel Efficiency: The JT15D-1A engines are thirsty by modern standards, particularly at lower altitudes where the aircraft is often forced to fly due to RVSM constraints on non-upgraded airframes.
  • Range with Full Seats: With a maximum payload of 2,100 lbs, carrying 5–6 passengers and their bags will significantly trade off fuel, often limiting range to roughly 500–600 nm.

Technical Specifications

Dimensions

Wingspan
47.1 ft
Length
43.5 ft
Height
14.3 ft

Weights

Max Takeoff Weight
11,850 lbs
Max Landing Weight
11,350 lbs
Useful Load
4,597 lbs
Fuel Capacity
564 gal

Performance

Cruise Speed
345 KTAS
Range
910 NM
Service Ceiling
41,000 ft
Rate of Climb
2719 fpm

Engines

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