Cessna 500/Citation I

Turbofan • twin engine • Low Wing • Retractable gear

Range Visualization

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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
357
KTAS
Cruise Speed
7
Occupants
1325
nm
Max Range
818
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna 500/Citation I

Overview

The Cessna Citation I (Model 500) is the foundational light jet that brought turbofan-powered business flying within reach of operators stepping up from cabin-class twins and pressurised turboprops. Affectionately (and mockingly) called the Slowtation for its straight-wing design and modest cruise speeds, the Citation I rewards owners with forgiving handling, short-field access, and an airframe with no published life limit. Three principal variants share the type: the original 500 (1971 to 1976, JT15D-1), the upgraded Citation I (1976+, JT15D-1A), and the 501 Citation I/SP (1977+), a single-pilot-certified variant that opened jet ownership to owner-operators who could not justify a two-pilot crew. 689 airframes were built across all variants from 1971 through 1985.

For the GA buyer, the Citation I is the most accessible turbofan path into cabin-class jet ownership. Acquisition prices remain among the lowest of any twin-jet on the market, the Pratt & Whitney JT15D family is parts-supported and well understood, and the airframe’s docile manners make it a viable first-jet transition for pilots stepping up from high-performance turboprops. The economic trap is engine overhaul: JT15D hot-section and full-overhaul cycles can approach the cost of acquisition, so a clean engine status at pre-buy carries outsized weight in the value calculus.

Key Features for GA Buyers

  • Short field capability. The straight-wing design allows access to regional airports with runways under 3,500 ft, often unreachable by faster swept-wing jets.
  • Docile handling. Approach speeds in the 90 to 100 KIAS band and straightforward flight characteristics make the Citation I one of the most owner-friendly first-jet options on the market.
  • No airframe life limit. Unlike many modern jets, the Citation I carries no structural life limit. A well-maintained airframe can remain in service indefinitely.
  • Single-pilot certification on the I/SP. The 501 Citation I/SP variant is type-certificated for single-pilot operations, the most accessible Citation airframe for owner-flown turbojet operations.

Trade-offs

  • Speed. A max cruise near 357 KTAS at FL350 is meaningfully slower than contemporaries like the Learjet 35. The Slowtation nickname is earned.
  • Engine overhaul economics. The JT15D-1A turbofans are reliable and parts-supported, but a hot-section or full-overhaul cycle can approach the acquisition cost of the airframe itself.
  • Payload and range. Range is limited to roughly 1,300 nm with reserves, and a full cabin significantly restricts fuel and trip range.

See Also

Technical Specifications

Dimensions

Wingspan
47.1 ft
Length
43.5 ft
Height
14.3 ft
Parking area (ft2)
2769.35 ft2

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
357 KTAS
Never-Exceed (Vne)
398 KIAS
Max Structural Cruise (Vno)
355 KIAS
Approach Speed
91 KIAS
Stall, Clean (Vs1)
85 KIAS
Range
1325 NM
Service Ceiling
41,000 ft
Rate of Climb
800 - 2719 fpm
Takeoff over 50 ft obstacle
2,930 ft
Landing ground roll
2,300 ft

Engines

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