Cessna 500/Citation I

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

355
KTAS
Cruise Speed
7
Occupants
910
nm
Max Range
818
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna 500/Citation I

The Cessna Citation I (C500) is the foundational light jet that revolutionized general aviation by making jet travel accessible to turboprop pilots. Often affectionately (or mockingly) referred to as the ‘Slowtation’ due to its straight-wing design and modest cruise speeds, it remains a favorite for its forgiving handling and short-field performance.

Key Features for GA Buyers

  • Short Field Capability: Its straight-wing design allows access to smaller regional airports with runways under 3,500 ft, often unreachable by faster swept-wing jets.
  • Docile Handling: Low approach speeds (approx. 90-100 KIAS) and straightforward flight characteristics make it an ideal first jet for owner-operators.
  • No Airframe Life Limit: Unlike many modern jets, the Citation I has no structural life limit, meaning a well-maintained airframe can remain in service indefinitely.
  • Single-Pilot Upgrades: While the C500 typically requires two pilots, many have been modified via STCs (like the Sierra Eagle/Stallion) or replaced by the 501 I/SP for single-pilot operations.

Trade-offs

  • Speed: With a max cruise of 355 knots, it is significantly slower than contemporary competitors like the Learjet 35.
  • High Maintenance Costs: Despite a low acquisition price, overhauling the Pratt & Whitney JT15D-1 engines can cost nearly as much as the aircraft itself.
  • Payload/Range: Range is limited to approximately 900-1,100 nm, and carrying a full passenger load significantly restricts fuel capacity.

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
355 KTAS
Range
910 NM
Service Ceiling
41,000 ft
Rate of Climb
2719 fpm

Engines

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