The Tecnam P-Mentor
A modern 2-seat aircraft built for efficiency, safety, and travel
The Tecnam P-Mentor
A modern 2-seat aircraft built for efficiency, safety, and travel
Why Pilots Love the P-Mentor
The Tecnam P-Mentor has earned a fast following because it blends something rare in training aircraft—a sweet spot of efficiency, modern avionics, and reassuring handling that serves brand-new students and time-building pilots alike. With fuel burns as low as ~4 gallons per hour from its Rotax powerplant, a contemporary Garmin glass cockpit, and excellent visibility under a spacious canopy, the P-Mentor makes every flight feel current and confidence-building.
Add in stable manners, low operating costs, and full IFR training capability, and it’s easy to see why so many schools and owners call it their favorite two-seat trainer.
Tecnam P-Mentor Specs
Performance numbers and key features that set the P-Mentor apart from other four-seat aircraft.
3.7 gal/hr fuel burn
Consumption at 60% (14 I/h)
1 × Rotax 912iSc3, four-stroke, fuel-injected, 100 HP
117 kts max speed
(13,000 ft, MCP)
104 kts cruise speed at 85 %
95 kts cruise speed at 75 %
13,000 ft service ceiling
Max operating altitude
650 ft/min max rate of climb (MSL)
950 nm max range
Includes auxiliary tanks which are standard in the USA
14 US gal/hr fuel consumption at 60 %
2 seat capacity
Comfortable access for all on board is assured through the sliding canopy and ergonomically designed cabin for comfort and visibility
628 lbs useful load
Baggage is stowed in the generous nose compartments and cabin, offering maximum loading flexibility for any mission
Tecnam P-Mentor Specs
Performance numbers and key features that set the P-Mentor apart from other four-seat aircraft.
3.7 gal/h
Consumption at 60% (14 L/H)
1 × Rotax 912iSc3, four-stroke, fuel-injected, 100 HP
117 kts
Max. speed (13,000 ft, MCP)
104 kts cruise speed at 85 %
95 kts cruise speed at 75 %
13,000 ft
Max. operating altitude (6,096 m)
650 ft/min max. rate of climb (MSL)
2 seats
Comfortable access for all on board is assured through the sliding canopy and ergonomically designed cabin for comfort and visibility.
950 nm
Max. range (incl. auxiliary tank)
14 US gal/h fuel consumption at 60 %
628 lbs
Useful load (285 kg)
Baggage is stowed in the generous nose compartments and cabin, offering maximum loading flexibility for any mission.
The Ideal Single-Engine Aircraft
The Tecnam P-Mentor offers excellent versatility, efficiency, and performance in a light twin-engine aircraft design. It is ideal for flight training, leisure flying, and commercial applications, offering advanced avionics, strong fuel efficiency, and stable flight characteristics.
P-Mentor Market: Curious about pricing?
See our live P-Mentor for sale listings for real-time market prices.
Training Excellence
The Tecnam P-Mentor redefines flight training by offering the perfect platform for pilots to unlock their full potential. P-Mentor is designed to be the ultimate two-seat trainer, combining exceptional performance with a focus on training excellence. It is the first choice for PPL (Private Pilot License), IR (Instrument Rating), and UPRT (Upset Prevention and Recovery Training), making it a versatile option for flight schools.
Whether you're a flight school looking for the smartest training platform or a private owner wanting an efficient, high-performance aircraft, the P-Mentor is designed to bring training to the next level.
Design and Comfort
The Tecnam P-Mentor features a modern, comfortable cabin with ergonomic seats, shaped control sticks, and large windows that provide excellent visibility.
Its wide sliding canopy allows easy access, while corrosion-protected structures and refined finishes highlight Tecnam’s signature craftsmanship.
Propulsion and Avionics
The P-Mentor is powered by the Rotax 912iSc engine, a 100 HP four-stroke, fuel-injected engine known for its efficiency and reliability.
The two-blade MT fixed-pitch or constant-speed propeller features advanced blade geometry for optimized performance, fuel efficiency, and smooth operation.
The fully integrated Garmin G3X Touch avionics suite is complemented by a range of options to suit various training missions, including a backup Garmin GI 275 and an optional Garmin GFC 500 autopilot with RNAV capability.
Explore the Entire Tecnam Family
Learn about the history of Tecnam Aircraft, the unique qualities of each model, and what makes Tecnam among the most advanced and trusted general aviation manufacturers in the world today.
Frequently Asked Questions
It uses a 100 hp Rotax 912iSc / 912iSc3 four-stroke engine.
Average fuel consumption is just 14 L/hr (3.7 US gal/hr), keeping hourly costs impressively low.
Yes — it’s fully IFR-approved under EASA CS-23 for PPL, CPL, IR, and UPRT training.
It features the Garmin G3X Touch glass cockpit with a GI 275 backup and optional GFC 500 autopilot.
Take-off ground roll is approximately 1,017 ft under standard conditions.
Useful load is about 628 lb, enough for two people, fuel, and gear.
The Rotax 912iSc engine can run on both avgas and unleaded mogas, depending on certification and region.
It’s the only CS-23-certified piston trainer offering full IFR and UPRT capability in a two-seat configuration.
Yes — it’s praised for light, balanced handling, excellent visibility, and predictable flight behavior.
It’s built with a steel safety cage, crash-resistant seats, and modern composite structures for enhanced occupant protection.
Powerplant
|
Engine |
Rotax 912iSc3, four-stroke, fuel-injected, 100 HP |
|---|---|
|
Propeller |
MTV-21 A/180-51, 2-blade constant speed propeller |
|
Fuel grades |
Mogas and Avgas |
Performance (max. mass)
|
Max. speed |
217 km/h TAS |
117 kts TAS |
||
|---|---|---|---|---|
|
Stall speed, landing configuration |
82 km/h | 44 kts | ||
|
Rate of climb (ISA SL) |
3.3 m/s |
650 ft/min |
||
|
Max. range (incl. auxiliary tank) |
1,760 km |
950 nm |
||
|
Fuel consumption |
14 l/h (@60%) |
3.7 US gal/h (@60%) |
||
|
Take-off ground roll (ISA SL) |
520 m |
1,706 ft |
||
|
Landing ground roll (ISA SL) |
198 m |
650 ft |
||
|
Max. operating altitude |
3,962 m |
13,000 ft |
Dimensions
Mass and Loading
| Seats | 2 | - | ||
|---|---|---|---|---|
|
Empty weight |
435 kg | 919 lbs | ||
|
Useful load |
285 kg | 628 lbs | ||
|
Max. take off mass |
720 kg | 1,587 lbs | ||
|
Fuel capacity total |
147 l / 101 kg | 37 US gal / 222 lbs |
Interested in the P-Mentor?
Reach out to us to see if this plane is a good fit for your mission.
