Tecnam P2002JF

Question 1

Wing span of the tecnam?

Answer 1

8.6 meters

Question 2

Aircraft length of the tecnam?

Answer 2

6.61 meters

Question 3

Aircraft height of the tech?

Answer 3

2.43 meters

Question 4

Wing taper of tecnam?

Answer 4

0.6 taper ratio

Question 5

Propeller grand clearance of the tecnam ?

Answer 5

320 mm

Question 6

Aspect ratio of tecnam?

Answer 6

6.4

Question 7

Dihedral of tecnam?

Answer 7

5 degrees

Question 8

Wing area of tecnam?

Answer 8

11.5 m2

Question 9

Number of engines?

Answer 9

1

Question 10

Engine manufacturer of tecnam?

Answer 10

Bombardier - rotax GmbH

Question 11

Engine model number of tecnam?

Answer 11

912 -s2

Question 12

State the engine type of the tecnam

Answer 12

4 cylinder horizontally - opposed twins with overall displacement of 1352 c.c, mixed cooling, (water-cooled heads and air-cooled cylinders), twin carburetors,integrated reduction gear with torque damper

Question 13

State the hp rating and engine speed for maximum 5 minutes

Answer 13

73.5 kW (98.5 hp) @5800 rpm (max.5’)

Question 14

State the hp rating and engine speed for cont.

Answer 14

69.0 kW (92.5 hp) @5500 rpm (cont.)

Question 15

Manufacturer of the tecnam’s propeller

Answer 15

Hoffmann propeller

Question 16

Number of the tecnam’s propeller

Answer 16

HO17GHM A 174 177 C

Question 17

Number of blades of the tecnam’s propeller

Answer 17

2

Question 18

Propeller diameter

Answer 18

1740 mm

Question 19

Propeller type

Answer 19

Fixed pitch

Question 20

Propeller material

Answer 20

Wood

Question 21

Total capacity of fuel

Answer 21

100 liters

Question 22

Total capacity (each tanks )

Answer 22

50 liters

Question 23

Total usable fuel

Answer 23

99 liters

Question 24

Total unusable fuel

Answer 24

1 liter

Question 25

State the approved fuel grades

Answer 25

• MOGAS ASTM D4814
• MOGAS EN 228 Super/Super Plus (Min RON 95)
• AVGAS 100LL (ASTM D910)

Question 26

Lubrication system

Answer 26

Forced type with external reservoir

Question 27

Oil capacity

Answer 27

2 Liters (min) - 3 Liters (max)

Question 28

Maximum Oil Temperature

Answer 28

130°C

Question 29

Minimum Oil Pressure

Answer 29

0.8 bar

Question 30

Maximum Oil Pressure

Answer 30

7 bar

Question 31

State the MTOW/ MLW (Takeoff Weight and Landing Weight under Normal category)

Answer 31

580 kg

Question 32

Standard Empty Weight

Answer 32

337 kg

Question 33

Useful Load

Answer 33

243 kg

Question 34

Baggage Allowance

Answer 34

20 kg

Question 35

Service Ceiling

Answer 35

Maximum operating altitude is 14,000 ft (4260m) MSL

Question 36

Fuel Consumption

Answer 36

4.5 gal/hr or 17 l/hr

Question 37

Fuel Endurance

Answer 37

4 Hrs

Question 38

Takeoff Rotation Speed

Answer 38

42 KIAS

Question 39

Enroute Climb, Flaps up:

Best Rate of Climb, Sea Level

Answer 39

66 KIAS

Question 40

Enroute Climb, Flaps up:

Best Angle of Climb, Sea Level

Answer 40

56 KIAS

Question 41

Stall Speeds

Answer 41

Bank Angle at 0°

Question 42

Stall Speed with Flaps 0°

Answer 42

40 KIAS

Question 43

Stall Speed with Flaps T/O (15°)

Answer 43

35 KIAS

Question 44

Stall Speed with Flaps Full (40°)

Answer 44

30 KIAS

Question 45

Approach Speed, Flaps T/O

Answer 45

66 KIAS

Question 46

Final Approach Speed Speed, Flaps FULL (40°)

Answer 46

51 KIAS

Question 47

Balked Landing

Answer 47

keep over 61 KIAS, climb to VY or VX as applicable

Question 48

Maneuvering Speed

Answer 48

96 KIAS

Question 49

Never Exceed Speed

Answer 49

138 KIAS

Question 50

Maximum Demonstrated Crosswind Velocity:

Takeoff and Landing

Answer 50

22 Knots

Question 51

Engine Failure After T/O

Answer 51

51 KIAS minimum

Question 52

Maximum Glide Speed

Answer 52

69 KIAS