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Grob G-115 vs Tecnam P2002

Grob G-115 vs Tecnam P2002 at a glance — top speed 270 vs 250 km/h, range 1,150 vs 1,092 km, max takeoff weight 990 vs 598 kg.

Grob G-115 military training aircraft side profile drawing
🇩🇪 Grob G-115
Tecnam P2002 military training aircraft side profile drawing
🇮🇹 Tecnam P2002
Specifications
Grob G-115 Tecnam P2002
Origin country 🇩🇪 Germany 🇮🇹 Italy
Category Military Training Aircraft Military Training Aircraft
Manufacturer Grob Tecnam
First flight 1 November 1985 --
Year introduced 1999 2002
Number produced 204 units N/A
Average unit price -- --
Wing area 12.2 m² 11.5 m²
Wingspan 10.0 m 8.6 m
Height 2.4 m 2.4 m
Length 7.5 m 6.6 m
Maximum speed 270 km/h 250 km/h
Operational range 1,150 km 1,092 km
Service ceiling 3,048 m 3,995 m
Max. takeoff weight 990 kg 598 kg
Empty weight 690 kg 331 kg
Total thrust 1 x 134 kW 1 x 74 kW
Performance Radar Chart

Detailed Comparison

The Grob G 115 and Tecnam P2002 occupy the entry-level tier of military aviation, serving as ab-initio screening and elementary flying training (EFT) platforms. Both filter pilot candidates before transitioning them to advanced turboprop trainers, but they originate from separate procurement models. The German-built Grob G 115 is a purpose-built composite trainer that secured large institutional contracts in the late 1990s, while the Italian Tecnam P2002 is an all-metal Light Sport Aircraft (LSA) adapted for military screening.

Development and Design

The G 115 utilizes a carbon composite airframe, integrating the fuselage and wing spars into a single piece to yield the high fatigue resistance required for repetitive training cycles. Powered by a 180-horsepower Lycoming AEIO-360 piston engine, it requires an inverted oil system to sustain its +6G/-3G aerobatic envelope. Tecnam took an austere route with the P2002, utilizing an all-metal low-wing monoplane design derived from the civilian LSA market. The P2002 relies on a 98-horsepower (73.5 kW) Rotax 912 S2 engine. Despite its civilian origins, the P2002 airframe is stressed to the same +6G/-3G limits as the Grob.

Specifications and Performances

Mass dictates the performance delta between the two airframes. The G 115 operates with a Maximum Takeoff Weight (MTOW) of 990 kg, 392 kg heavier than the P2002’s 598 kg limit. The Grob requires 134 kW of thrust to reach a 270 km/h maximum speed. The Tecnam reaches 250 km/h using barely half that power. The lighter footprint of the P2002 yields a higher climb rate (6.2 m/s versus the Grob’s 5.3 m/s) and a higher service ceiling (3995 m compared to 3048 m). The Grob offsets this with a heavier payload capacity and a 1150 km range.

Deployment and usage

Procurement strategies for these aircraft diverge based on institutional budgets and training doctrine:

  • The UK Ministry of Defence integrated the G 115E (Tutor T1) via a Private Finance Initiative with Babcock International, operating it across the Royal Air Force, Royal Navy, and Army Air Corps until partial replacement in 2018.
  • The Egyptian Air Force procured 74 G 115 airframes to serve as the backbone of their basic training pipeline.
  • The Hellenic Air Force operates the P2002-JF at Tatoi strictly for initial pilot selection.

Air forces procure the Rotax-powered Tecnam explicitly to minimize fuel and maintenance overhead during the high-attrition screening phase, accepting a lighter, less complex airframe in exchange for lower costs per flight hour.

Conclusion

The Grob G 115 holds the advantage as a comprehensive elementary trainer. Its heavier mass, higher wing loading, and constant-speed propeller force student pilots to manage energy states in a manner closer to heavier military aircraft, providing a superior transition platform to military turboprops. The Tecnam P2002 succeeds exclusively as a grading tool. Militaries utilizing the P2002 are purchasing a low-cost screening mechanism to wash out underperforming candidates before investing military training budgets into their progression.

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Frequently Asked Questions

Which is faster, the Grob G-115 or Tecnam P2002?
The Grob G-115 is faster with a maximum speed of 270 km/h compared to the Tecnam P2002's 250 km/h, a difference of 20 km/h.
Which has longer range, the Grob G-115 or Tecnam P2002?
The Grob G-115 has a longer range at 1,150 km compared to the Tecnam P2002's 1,092 km.
Which can fly higher, the Grob G-115 or Tecnam P2002?
The Tecnam P2002 has a higher service ceiling at 3,995 meters (13,106 ft) compared to the Grob G-115's 3,048 meters (10,000 ft).
Which is heavier, the Grob G-115 or Tecnam P2002?
The Grob G-115 has a higher maximum takeoff weight at 990 kg compared to the Tecnam P2002's 598 kg.
Which is larger, the Grob G-115 or Tecnam P2002?
The Grob G-115 is longer at 7.5 meters compared to the Tecnam P2002's 6.6 meters.
Which entered service first, the Grob G-115 or Tecnam P2002?
The Grob G-115 entered service first in 1999, 3 years before the Tecnam P2002 which entered service in 2002.