First Aircraft

Aircraft Intelligence Card

Dassault Falcon 8x

Large Cabin Competitive

VeritasJet™ Score

Reachability

64/100

Number of airports reachable under real-world mission assumptions (NBAA IFR). This reflects true operational access rather than theoretical range.

Higher scores indicate greater flexibility and more routing options across the global airport network.

Runway Flexibility

75/100

Measures the ability to operate from shorter or constrained runways.

Higher scores indicate better short-field performance and broader airport access.

Payload Robustness

44/100

Indicates how efficiently the aircraft converts payload into usable range across its full envelope.

Higher scores indicate lower sensitivity to payload and stronger real-world mission flexibility.

Cabin Comfort

69/100

Represents overall passenger comfort based on cabin space, layout quality, pressurization, and noise levels.

It captures real in-flight experience including spaciousness, fatigue, and acoustic environment.

Higher scores indicate a more comfortable and refined passenger experience on longer missions.

Fuel Efficiency

53/100

Measures fuel burn per nautical mile based on cruise performance.

Higher scores indicate more efficient long-range operation and lower operating cost per distance.

VeritasJet™ Score

Payload Simulation

Dassault Falcon 8x Payload-Range Diagram

Fuel / Payload Tradeoff

Passengers 12

                Estimated Range
                
                    3200 nm

Aircraft Specifications

Aircraft

Manufacturer Dassault

Model Falcon 8x

Seating 12

External Dimensions

Length 80 ft (24.4 m)

Height 26 ft (8 m)

Wingspan 86 ft (26.3 m)

Cabin

Length 30 ft (9.1 m)

Height 6 ft (1.9 m)

Width 6 ft (1.9 m)

Volume 1,164 ft³ (33 m³)

Per Seat 97 ft³/seat (2.75 m³/seat)

Characteristics

Wing Loading 95.9

Power Loading 3.62

Noise 88.7 / 80.1 / 90.6

Cabin Diff (Psi) 10.2

Engine / Power

Engines 3 P&WC PW307D

Power Output 6,722 lb

Inspection 7,200c

Airport Performance

TOFL (SL/ISA) 0

TOFL (5000ft/25C) 8540

Weight (Mission) 72,591 lb (32,927 kg)

Range 6,415 nm (11,881 km)

V2 138 kt (256 km/h)

Vref 107 kt (198 km/h)

Landing Distance 2245 ft (684.3 m)

Weights

Max Ramp 73,200 lb (33,203 kg)

Max Takeoff 73,000 lb (33,112 kg)

Max Landing 62,400 lb (28,304 kg)

Zero Fuel 41,000 lb (18,597 kg)

BOW 36,800 lb (16,692 kg)

Max Payload 4,200 lb (1,905 kg)

Useful Load 36,400 lb (16,511 kg)

Max Fuel 35,141 lb (15,940 kg)

Payload (Max Fuel) 1,259 lb (571 kg)

Fuel (Max Payload) 32,200 lb (14,606 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

Methodology

VeritasJet™ models aircraft performance as a multi-dimensional, mission-dependent system rather than a single-metric ranking. While traditional comparisons often emphasize range, real-world aircraft performance is defined by a combination of factors including payload, runway capability, fuel efficiency, and cabin characteristics.

All scores are derived from structured performance data and normalized within aircraft categories using percentile ranking (CDF). This allows consistent comparison across different aircraft types while preserving relative strengths and trade-offs.

Scores are computed directly from underlying performance data using a consistent mathematical framework. No manual ranking or subjective adjustment is applied; results reflect the relative position of each aircraft within the dataset.

VeritasJet™ is formulated as a network-based operational utility model, where aircraft performance is evaluated in terms of expected mission accessibility across a standardized global airport graph under realistic operational constraints.

While model design choices exist, all computations are deterministic, reproducible, and derived from physical and operational constraints rather than subjective scoring or manual ranking adjustments.

The objective is not to identify a universally “best” aircraft, but to provide a data-driven framework that reflects how different designs perform under varying operational constraints and mission profiles.

Developed from experience in aircraft advisory and performance evaluation.

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.

Second Aircraft

Aircraft Intelligence Card

Bombardier Global 7500

Ultra Long Range Balanced

VeritasJet™ Score

Reachability

86/100

Number of airports reachable under real-world mission assumptions (NBAA IFR). This reflects true operational access rather than theoretical range.

Higher scores indicate greater flexibility and more routing options across the global airport network.

Runway Flexibility

60/100

Measures the ability to operate from shorter or constrained runways.

Higher scores indicate better short-field performance and broader airport access.

Payload Robustness

25/100

Indicates how efficiently the aircraft converts payload into usable range across its full envelope.

Higher scores indicate lower sensitivity to payload and stronger real-world mission flexibility.

Cabin Comfort

83/100

Represents overall passenger comfort based on cabin space, layout quality, pressurization, and noise levels.

It captures real in-flight experience including spaciousness, fatigue, and acoustic environment.

Higher scores indicate a more comfortable and refined passenger experience on longer missions.

Fuel Efficiency

22/100

Measures fuel burn per nautical mile based on cruise performance.

Higher scores indicate more efficient long-range operation and lower operating cost per distance.

VeritasJet™ Score

Payload Simulation

Bombardier Global 7500 Payload-Range Diagram

Fuel / Payload Tradeoff

Passengers 12

                Estimated Range
                
                    3200 nm

Aircraft Specifications

Aircraft

Manufacturer Bombardier

Model Global 7500

Seating 17

External Dimensions

Length 111 ft (33.8 m)

Height 27 ft (8.2 m)

Wingspan 104 ft (31.7 m)

Cabin

Length 36 ft (11 m)

Height 6 ft (1.9 m)

Width 7 ft (2.1 m)

Volume 1,518 ft³ (43 m³)

Per Seat 89 ft³/seat (2.53 m³/seat)

Characteristics

Wing Loading 91.6

Power Loading 3.04

Noise 91.6 / 80.3 / 88.8

Cabin Diff (Psi) 10.3

Engine / Power

Engines 2 GE Passport 20-19BB1A

Power Output 18,920 lb

Inspection OC

Airport Performance

TOFL (SL/ISA) 0

TOFL (5000ft/25C) 8679

Weight (Mission) 114,850 lb (52,095 kg)

Range 7,800 nm (14,446 km)

V2 137 kt (254 km/h)

Vref 108 kt (200 km/h)

Landing Distance 2240 ft (682.8 m)

Weights

Max Ramp 115,100 lb (52,208 kg)

Max Takeoff 114,850 lb (52,095 kg)

Max Landing 87,600 lb (39,735 kg)

Zero Fuel 67,500 lb (30,617 kg)

BOW 61,700 lb (27,987 kg)

Max Payload 5,800 lb (2,631 kg)

Useful Load 53,400 lb (24,222 kg)

Max Fuel 51,510 lb (23,365 kg)

Payload (Max Fuel) 1,890 lb (857 kg)

Fuel (Max Payload) 47,600 lb (21,591 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

Methodology

While model design choices exist, all computations are deterministic, reproducible, and derived from physical and operational constraints rather than subjective scoring or manual ranking adjustments.

Developed from experience in aircraft advisory and performance evaluation.

Disclaimer

Third Aircraft

Dassault Falcon 8x

Dassault Falcon 8x Payload-Range Diagram

Disclaimer

Bombardier Global 7500

Bombardier Global 7500 Payload-Range Diagram

Disclaimer

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