Cessna Citation Longitude

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

Endorsements & ratings:
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
483
KTAS
Cruise Speed
12
Occupants
3500
nm
Max Range
1802
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna Citation Longitude

The Cessna Citation Longitude (Model 700) is Textron’s flagship super-midsize jet, evolving the Latitude’s successful wide-body cabin into a transcontinental powerhouse. With a new ~28-degree swept wing and a T-tail, it was designed to challenge the Challenger 350 and Embraer Praetor 600. For the GA buyer, it offers a refined “NetJets-standard” experience: a quiet, flat-floor cabin paired with sophisticated Garmin G5000 avionics.

Key Features for GA Buyers

  • Quiet-Cabin Leader: Marketed as having the quietest cabin in the super-midsize class, it uses advanced soundproofing to ensure a serene environment for business or rest.
  • Modern Flight Deck: The Garmin G5000 system includes fully integrated autothrottles and four touchscreen controllers, drastically reducing workload for the two-pilot crew.
  • Superior Maintenance Intervals: Features industry-leading 800-hour or 18-month maintenance intervals, significantly lowering the total cost of ownership compared to older super-midsize jets.
  • Flat-Floor Space: The 6-foot stand-up cabin and completely flat floor create a seamless transition from the cockpit to the aft baggage area, which is accessible in flight.

Trade-offs

  • Fuel Burn at High Speed: While capable of Mach 0.84, flying at maximum speed notably increases fuel consumption compared to long-range cruise settings (Mach 0.79).
  • Runway Requirements: With a takeoff field length of 4,810 ft at MTOW, it is more runway-limited than its smaller sibling, the Latitude, particularly in ‘hot and high’ conditions.
  • Cabin Width vs. Competition: Although spacious, the fuselage diameter is narrower than the Challenger 300/350 series, which some passengers may notice on 7-hour transatlantic legs.

See also

Technical Specifications

Dimensions

Wingspan
68.9 ft
Length
73.2 ft
Height
19.4 ft
Parking area (ft2)
6169.98 ft2

Weights

Max Takeoff Weight
39,500 lbs
Max Landing Weight
33,500 lbs
Useful Load
16,100 lbs
Fuel Capacity
2134 gal

Performance

Cruise Speed
483 KTAS
Never-Exceed (Vne)
483 KIAS
Max Structural Cruise (Vno)
476 KIAS
Approach Speed
115 KIAS
Stall, Clean (Vs1)
105 KIAS
Range
3500 NM
Service Ceiling
45,000 ft
Rate of Climb
1200 - 4892 fpm
Takeoff over 50 ft obstacle
4,810 ft
Landing ground roll
3,170 ft

Engines

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Range
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