Tecnam P-Mentor User Manual

Thisdocument and the information thereon is the property of Costruzioni Aeronautiche Tecnam S.p.A., and may only be used
for the purpose for which Tecnam products are supplied, and/or use and maintenance of Tecnam Aircraft.
Reproduction or use of the data, information, drawings thereon, in whole or in part, is strictly Prohibited without
the express written permission of Costruzioni Aeronautiche Tecnam S.p.A.
P-Mentor – Aircraft Flight Manual
Aircraft Flight Manual
Doc. No. 2002/1032
Ed.1 Rev.7
2023, January 09
TECNAM P – MENTOR
MANUFACTURER: COSTRUZIONI AERONAUTICHE TECNAM S.p.A.
AIRCRAFT MODEL: P-MENTOR
SERIAL NUMBER:……………………………….
BUILD YEAR: ……….………………...................
REGISTRATION MARKINGS: …………….……..
This manual must be carried in the airplane at all times.
The airplane has to be operated in compliance with procedures and limitations
contained herein.
Costruzioni Aeronautiche TECNAM S.p.A.
Via Maiorise
CAPUA (CE) – Italy
Tel. +39 0823 99.75.38
WEB: www.tecnam.com

Tecnam P-Mentor Specifications

General

Manufacturer	Tecnam
Model	P-Mentor
Engine	Rotax 912iSc
Horsepower	100 hp
Seating Capacity	2
Height	2.60 m
Range	1, 111 km (600 nm)
Fuel Capacity	100 L
Service Ceiling	15, 000 ft (4, 572 m)
Maximum Takeoff Weight	1, 320 lbs (600 kg)

Summary

SECTION 1 GENERAL

7. Maximum Weights and Specific Loadings

Specifies maximum take-off and landing weights, wing and power loading.

SECTION 2 LIMITATIONS

2. Speed

Details airspeed limitations for normal operations, including VNE, VNO, VA, VO, VFE.

3. Powerplant

Details powerplant specifications and operating limitations for engine, propeller, and oil.

9. Weights and Center of Gravity Limits

Defines weight limits and CG limits with a graphical representation.

13. Avionic System Limitations

Covers general avionic system limitations and specific limitations for Garmin systems.

SECTION 3 EMERGENCY PROCEDURES

2. Electrical System

Covers emergency procedures for electrical system issues like Low Volt, Generator Failure, Bus failures.

4. Avionic System

Details procedures for failures in avionic systems like AHRS, ADC, EIS, COM, and NAV/GPS.

7. Powerplant

Covers emergency procedures related to the powerplant: engine failures, propeller overspeed, and temperature limits.

16. Emergency Landing

Provides procedures for forced landings, both without and with engine power.

SECTION 4 NORMAL PROCEDURES

2. Airspeeds for normal operations

Lists significant airspeeds for normal flight phases like rotation, climb, approach, and cruise.

3. Pre-flight Inspection

4. Checklist

SECTION 5 PERFORMANCE

7. Stall Speed

9. Take-Off Performance

13. Landing Performance

SECTION 6 WEIGHT AND BALANCE

2. Weighing Procedures

3. Weight and Balance Determination for Flight

SECTION 7 AIRFRAME AND SYSTEMS DESCRIPTION

2. Airframe

3. Flight Controls

4. Instrument Panel

8. Electrical System

9. Avionic System