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**Macchi c. 207 **powered by DB. 603 HP 1510 power at an altitude of 5700 m and 2500 RPM.

Equipped with Wing 21 m ˛. Armament-4 wing-mounted 20 mm cannon.

Dimension

Weight ; The total weight of the load kg :

**4340**, Empty aircraft weight kg :

**3292**

Lifting capacity kg :

**1048**, The composition of the payload Parachute pilot kg :

**85**, 4 guns CAL. 20 mm kg :

**169**,

250 rounds per barrel (total 1000) kg :

**218**, Radio system kg :

**56**, Collimator, oxygen inhaler kg :

**13**, Gasoline (total) kg :

** 470**, Oil kg :

**37**, Total kg :

**1048**, Fuel tanks capacity : Front fűzelâžnyj l :

**405** 2 wing tank only l :

**160**, Tail fűzelâžnyj l :

**80**

, Total l :

**645**,

Expected characteristics.

Maximum speed at altitude-700 km/h.

Characteristics of the engine DB. 603

Length mm : 2610, Width mm : 1167, Height mm : 830, Motor shaft rotational speed RPM : 2500

Rotational speed of screw RPM : 1295

Power emergency at an altitude of 2750 m 5700 rpm and inlet pressure 1.40 kg/cm ˛ makes 1620 HP

Nominal power at an altitude of 5700 m, 2500 rpm and inlet pressure 1.30 kg/cm ˛ is 1510 HP

Power take-off, 2700 rpm and inlet pressure 1.30 kg/cm ˛ is 1750 HP

C. 205V C. 205V C. 205N C. 205N C. 206 C. 207 C. 202

1 ' serie 3 ' serie M.m. 499 M.m. 500

Wingspan m 10.58 10.58 11.25 11.25 12.142 12.142 10.58

Length m 8.85 8.85 9.549 9.549 9.335 9.735 8.85

Height in the parking lot m 3.036 3,075 3.25 3.25 3.095 3.25 3,075

Average wing chord m 1.59 1.59 1.69 1.69 1.795 1.795 1.59

Wing area m ˛ 16.8 16.8 19 19 21 21 16.8

Screw diameter m 3.050 3.050 3.050 3.050 3.050 3.150 3.050

Empty aircraft weight kg 2.568 2,518 2,699 2.759 2.578 3.292 2,284

The total weight of the kg 3.268 3.408 3.621 3.794 3.650 4.340 2.937

Wing loading kg/m ˛ 194.5 202.8 190.6 199.7 173.8 206.6 174.8

Engine power (the standards.) HP 1250 1250 1250 1250 1250 1510 1000

Specific load on the power kg/HP 2.61 2.73 2.89 3.03 2.92 2.87 2.94

Power per unit area PS/m ˛ 74.4 74.4 65.79 65.79 59.52 71.9 59.52"