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Textron Aviation Citation latitude

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VeritasJet™ Score
VeritasJet™ Score
Payload Simulation
Textron Aviation Citation latitude Payload-Range Diagram
Fuel / Payload Tradeoff
Passengers 12
Estimated Range 3200 nm
Aircraft Specifications
Aircraft
Manufacturer Textron Aviation
Model Citation latitude
Seating 9
External Dimensions
Length 62 ft (19 m)
Height 21 ft (6.4 m)
Wingspan 72 ft (22 m)
Cabin
Length 16 ft (4.8 m)
Height 6 ft (1.8 m)
Width 4 ft (1.2 m)
Volume 391 ft³ (11 m³)
Per Seat 43 ft³/seat (1.23 m³/seat)
Characteristics
Wing Loading 56.8
Power Loading 2.61
Noise 87.7 / 73.5 / 87.7
Cabin Diff (Psi) 9.7
Engine / Power
Engines 2 P&WC PW306D1
Power Output 5,907 lb
Inspection 6,000t
Airport Performance
TOFL (SL/ISA) 0
TOFL (5000ft/25C) 5070
Weight (Mission) 30,675 lb (13,914 kg)
Range 2,700 nm (5,000 km)
V2 115 kt (213 km/h)
Vref 95 kt (176 km/h)
Landing Distance 2085 ft (635.5 m)
Weights
Max Ramp 31,050 lb (14,084 kg)
Max Takeoff 30,800 lb (13,971 kg)
Max Landing 27,575 lb (12,508 kg)
Zero Fuel 21,430 lb (9,720 kg)
BOW 18,656 lb (8,462 kg)
Max Payload 2,774 lb (1,258 kg)
Useful Load 12,394 lb (5,622 kg)
Max Fuel 11,394 lb (5,168 kg)
Payload (Max Fuel) 1,000 lb (454 kg)
Fuel (Max Payload) 9,620 lb (4,364 kg)
Address-to-Address Mission Time
Compare real-world travel time from address to address, including airport transfer, security delays, and overnight hotel impact.
  • Address-to-Address Mission Time
  • Private vs airline total journey time
  • Overnight stay probability included

This module is in development. Early version will launch soon.
VeritasJet™ Methodology

Disclaimer

All aircraft specifications, performance data, and computed scores are provided for general informational purposes only. Values are based on publicly available data and standardized modeling assumptions, and may vary depending on aircraft configuration, payload, weather conditions, and operational procedures.

VeritasJet™ and related metrics are analytical indicators and do not represent manufacturer-certified performance. This information should not be used as the sole basis for purchasing, operational, or financial decisions. Always consult aircraft manufacturers or authorized operators for official performance data.

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