> For the complete documentation index, see [llms.txt](https://docs.flightsim-studio.com/llms.txt). Markdown versions of documentation pages are available by appending `.md` to page URLs; this page is available as [Markdown](https://docs.flightsim-studio.com/tecnam-p2012/aircraft-flight-manual/section-1-general.md).

# Section 1 - General

### THREE-VIEW

<figure><img src="/files/EBFIAmc1jW200TC7ASqU" alt=""><figcaption></figcaption></figure>

***

### DIMENSIONS

#### Overall dimensions

* **Wingspan:** 14 m / 46 ft
* **Length:** 11.9 m / 39.1 ft
* **Overall height:** 4.4 m /14.4 ft

#### Wing

* **Wing surface:** 25.4 m2 / 273 ft2
* **Mean Geometric Chord:** 1.814 m / 5.95 ft
* **Aspect ratio:** 7.7

#### Main Landing Gear

* **Track:** 2.5 m / 8.2 ft
* **Wheelbase:** 4.8 m / 15.7 ft
* **Tire:** 6.00-10

#### Nose Landing Gear

* **Tire:** 6.00-6

***

### POWERPLANT

#### Engine

* **Manufacturer:** Lycoming
* **Model:** TEO-540-C1A
* **Certification basis:** FAR 33
* **Type Certificate:** EASA TCDS no. IM.E.119
* **Engine type:** Direct - drive six - cylinder, horizontally opposed, turbocharged, air-cooled engine, equipped with electronic fuel injection, electronic ignition, down exhaust.
* **Maximum power:** 375hp @ 2575rpm
* **Maximum continuous power:** 375hp @ 2575rpm

#### Propeller

* **Manufacturer:** MT Propeller
* **Model:** MTV-14-B-C-F/CF195-30
* **Blades:** 4 blades
* **Diameter:** 1950 mm / 6 ft 4.77 in
* **Type:** Variable pitch - hydraulically controlled

#### Governor

* **Manufacturer:** MT Propeller
* **Model:** P-881-71
* **Type:** Hydraulic

***

### MAXIMUM WEIGHTS AND SPECIFIC LOADINGS

#### Maximum Weights

* **Maximum Ramp Weight:** 3618 kg (7976 lb)
* **Maximum Take-Off Weight:** 3600 kg (7937 lb)
* **Maximum Landing Weight:** 3600 kg (7937 lb)

#### Specific Loadings

* **Wing Loading:** 142 kg/m2 (29 lb/ft2)
* **Power Loading:** 4.8 kg/hp (10.6 lb/hp)