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T-41 Mescalero vs Tecnam P2002

T-41 Mescalero vs Tecnam P2002 at a glance — top speed 232 vs 250 km/h, range 1,159 vs 1,092 km, max takeoff weight 1,134 vs 598 kg.

Cessna T-41 Mescalero military training aircraft side profile drawing
Tecnam P2002 military training aircraft side profile drawing
🇮🇹 Tecnam P2002
Specifications
T-41 Mescalero Tecnam P2002
Origin country 🇺🇸 United States 🇮🇹 Italy
Category Military Training Aircraft Military Training Aircraft
Manufacturer Cessna Tecnam
First flight 1 January 1964 --
Year introduced 1965 2002
Number produced 838 units N/A
Average unit price -- --
Wing area 14.8 m² 11.5 m²
Wingspan 10.9 m 8.6 m
Height 2.7 m 2.4 m
Length 8.2 m 6.6 m
Maximum speed 232 km/h 250 km/h
Operational range 1,159 km 1,092 km
Service ceiling 5,200 m 3,995 m
Max. takeoff weight 1,134 kg 598 kg
Empty weight 618 kg 331 kg
Total thrust 1 x 160 kW 1 x 74 kW
Performance Radar Chart

Detailed Comparison

The USAF procured the Cessna T-41 Mescalero during the 1960s Cold War expansion to rapidly push student pilots through basic flight familiarization. Four decades later, European air arms adopted the Tecnam P2002 to execute the same flight screening mission under strict cost-containment parameters. The comparison centers on a heavy, high-wing utility aircraft adapted for the military versus a modern, lightweight low-wing trainer engineered specifically for basic flying instruction.

Development and Design

Cessna developed the T-41 by militarizing the commercial Model 172F, subsequently utilizing the heavier 175 Skylark type certificate to accommodate 210 hp Continental IO-360 engines in the B, C, and D variants. Its high-wing, strut-braced design prioritized stability over agility. Tecnam engineered the P2002 as a light sport aircraft and certified trainer (P2002-JF). Its low-wing monoplane configuration and bubble canopy closely mimic the visual references of advanced tactical aircraft. The P2002 airframe is stressed to +6g and -3g, allowing for upset recovery and basic aerobatic screening that the structurally restricted T-41 cannot perform.

Specifications and Performances

The P2002 extracts higher performance metrics from less than half the engine power. A direct comparison of the primary metrics isolates the aerodynamic differences:

  • The P2002 (73.5 kW) achieves a 6.2 m/s climb rate and a 250 km/h maximum speed.
  • The T-41 (160 kW) manages a 4.5 m/s climb rate and a 232 km/h maximum speed.

This kinetic discrepancy stems entirely from airframe mass. The T-41’s maximum takeoff weight is 1134 kg, nearly double the P2002’s 598 kg. The heavier Cessna burns more fuel and incurs higher maintenance overhead, whereas the Tecnam's lighter airframe translates the low-torque Rotax output into superior climb and speed figures.

Deployment and usage

The USAF acquired 237 T-41As in 1964 for primary flight screening, using its docile handling to introduce candidates to basic airmanship. The US Army and foreign militaries, including Greece and Turkey, procured the up-engined variants for similar roles. However, the T-41's inherent stability masked poor pilot aptitude, a negative screening trait that led the USAF to replace it in 1993 with the fully aerobatic Slingsby T-3A Firefly to increase candidate washout rates early in the pipeline. The P2002 currently serves air arms like the Hellenic Air Force for initial selection. Operating at a fraction of a turboprop's cost, the P2002 functions strictly as a financial filter to weed out failing students before they transition to heavier trainers like the T-6 Texan II.

Conclusion

The Tecnam P2002 is definitively the superior ab-initio military screening platform. The T-41’s commercial high-wing origins and extreme aerodynamic stability make it too forgiving to evaluate military pilot aptitude accurately—a limitation that drove its removal from USAF screening programs. The P2002’s low-wing configuration, fighter-style bubble canopy, and +6/-3g structural limits provide instructors with a demanding, maneuverable platform to identify candidate flight deficiencies before militaries invest budget in the turboprop and jet training phases.

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Frequently Asked Questions

Which is faster, the T-41 Mescalero or Tecnam P2002?
The Tecnam P2002 is faster with a maximum speed of 250 km/h compared to the T-41 Mescalero's 232 km/h, a difference of 18 km/h.
Which has longer range, the T-41 Mescalero or Tecnam P2002?
The T-41 Mescalero has a longer range at 1,159 km compared to the Tecnam P2002's 1,092 km.
Which can fly higher, the T-41 Mescalero or Tecnam P2002?
The T-41 Mescalero has a higher service ceiling at 5,200 meters (17,060 ft) compared to the Tecnam P2002's 3,995 meters (13,106 ft).
Which is heavier, the T-41 Mescalero or Tecnam P2002?
The T-41 Mescalero has a higher maximum takeoff weight at 1,134 kg compared to the Tecnam P2002's 598 kg.
Which is larger, the T-41 Mescalero or Tecnam P2002?
The T-41 Mescalero is longer at 8.2 meters compared to the Tecnam P2002's 6.6 meters.
Which entered service first, the T-41 Mescalero or Tecnam P2002?
The T-41 Mescalero entered service first in 1965, 37 years before the Tecnam P2002 which entered service in 2002.