EasyManua.ls Logo

Tecnam P2006T User Manual

Tecnam P2006T
300 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
Page #1 background imageLoading...
Page #1 background image
Page 0 - 1
Aircraft Flight Manual
Doc. No. 2006/044
4
th
Edition – Rev. 5
2018, January 12
th
TECNAM P2006T
MANUFACTURER: COSTRUZIONI AERONAUTICHE TECNAM S.r.l.
AIRCRAFT MODEL: P2006T
EASA TYPE CERTIFICATE NO: A .185 (DATED 2009, JUNE 5
TH
)
SERIAL NUMBER: …………….................
BUILD YEAR: ……….………...................
REGISTRATION MARKINGS: ……………...
This Aircraft Flight Manual is approved by European Aviation Safety Agency
(EASA).
This Manual contains information required by the FAA to be furnished to the pilot
for operation in the U.S.A. plus information supplied by the manufacturer. It is
approved by EASA on behalf of the FAA per FAR 21.29.
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 srl
Via Maiorise
CAPUA (CE) – Italy
Tel. +39 (0) 823.62.01.34
WEB: www.tecnam.com
Question and Answer IconNeed help?

Do you have a question about the Tecnam P2006T and is the answer not in the manual?

Tecnam P2006T Specifications

General IconGeneral
ManufacturerTecnam
ModelP2006T
TypeLight Twin-Engine Aircraft
Engines2 × Rotax 912S3
Seating Capacity4
Service Ceiling13, 000 ft (3, 962 m)
Maximum Takeoff Weight2, 712 lb (1, 230 kg)
Wingspan11.4 m (37 ft 5 in)
Length8.7 m (28 ft 7 in)
Fuel Capacity52 US gallons (200 liters)

Summary

Section 1 - General

4. Engine

Details about the aircraft's engine, including manufacturer, model, type, and maximum power.

7. Fuel

Information on approved fuel types, fuel tank capacity, and usable/unusable fuel quantities.

8. Lubrication

Details on the lubrication system, recommended oil, and oil capacity.

13. Acronyms and Terminology

Defines various acronyms and terms used in aircraft operations and performance.

Section 2 – Limitations

2. Speed Limitations

Table detailing airspeed limitations (VNE, VNO, VA, VO, VLE, VLO, VFE, VMC) with their operational significance.

4. Powerplant Limitations

Operating limitations for both installed engines, including maximum power, temperatures, and oil pressure.

14. Weights

Specifies maximum takeoff weight, maximum landing weight, and maximum zero wing fuel weight.

15. Center of Gravity Range

Defines the datum, levelling procedure, forward and aft CG limits, and the pilot's responsibility for loading.

20. Fuel

Provides information on fuel tanks, capacity, usable fuel, and approved fuel types, with a caution on Avgas 100LL.

21. Limitations Placards

Lists and describes various placards related to operating limitations installed on the aircraft.

SECTION 3 – Emergency Procedures

2. Airplane Alerts

Describes the annunciator panel lights (green, amber, red) for warnings, cautions, and advisories.

4. Powerplant Emergencies

Covers emergencies related to the powerplant, such as propeller overspeeding and temperature/pressure limit exceedances.

6. One Engine Inoperative Procedures

General procedures for one engine inoperative conditions, emphasizing control and airspeed management.

7. Landing Gear Failures

Details procedures for various landing gear failures, including emergency extension and gear-up landings.

8. Smoke and Fire Occurrence

Procedures for handling smoke and fire incidents, including engine fires and electrical smoke.

10. Landing Emergencies

Covers emergency landing procedures such as landing without engine power or with tire failures.

SECTION 4 – Normal Procedures

2. Airspeeds

Lists significant airspeeds for normal operations at different MTOWs and flap settings.

3. Normal Procedures Checklist

A comprehensive checklist for normal flight operations.

4. Ground Towing, Parking and Mooring

Guidance on ground handling, parking, and mooring the aircraft.

SECTION 5 - Performances

6. Stall Speed

Table showing stall speeds in KIAS and KCAS for different weights, bank angles, and flap configurations.

8. Take-off Performances

Table of takeoff distances for a weight of 1180 kg under various pressure altitudes and temperatures, with corrections.

9. Take-off Rate of Climb

Table showing takeoff rate of climb (Vy) in ft/min for different weights, pressure altitudes, and temperatures.

13. One-Engine Rate of Climb

Table showing one-engine rate of climb (VySE) in ft/min for different weights, pressure altitudes, and temperatures.

16. Landing Performances

Table of landing distances for a weight of 1180 kg under various pressure altitudes and temperatures, with corrections.

SECTION 6 – Weight and Balance

2. Weighing Procedures

Details procedures for weighing, including preparation, levelling, weighing process, and C.G. determination.

3. Weights and C.G.

Chart for defining C.G. position and pilot's responsibility for ensuring correct loading.

5. Equipment List

List of equipment that may be installed in the P2006T, indicating items installed and included in the Basic Empty Weight.

SEZIONE 7 – Airframe and Systems Description

2. Airframe

Description of the aircraft's airframe structure.

3. Powerplant

Details the aircraft's two Rotax 912S engines, their cooling systems, and related instruments.

8. Fuel System

Describes the fuel system, including integrated wing tanks, fuel pump, gascolator, and fuel selectors.

9. Landing Gear System

Explains the electro-hydraulic landing gear retraction system, operating modes, and indication components.

10. Brakes

Describes the hydraulically actuated brake system for each main wheel, including master cylinders and parking brake.

17. Instruments Panel

Illustrates the typical layout of the aircraft's instruments panel, including LH and central panels.

18. Electrical System

Describes the electrical system, including power sources, generators, battery, and bus distribution.

SECTION 8 – Aircraft Care and Maintenance

2. Inspection Intervals

Details scheduled and unscheduled inspection requirements and intervals.

4. Maintenance

Covers general maintenance procedures.

5. Ground Towing, Parking and Mooring

Guidance on ground handling, parking, and mooring the aircraft.

6. Cleaning

Guidelines for cleaning aircraft surfaces, propeller, and engine.

7. Ice Removal

Procedure for ice removal, prohibiting anti-icing products and recommending towing to a hangar.

SECTION 9 – Supplements

2. Supplements Lists

Lists supplements for airplanes with analogue instruments and Garmin G950/G1000 NXi.

Supplement no. G1 – Garmin G950 IFDS

Record of Revisions for Supplement G1, detailing changes made to procedures and recommendations.

Related product manuals