Dynon Avionics SV-INTERCOM-2S Manual do Utilizador descarregar pdf (Página 8)

SPECIFICATION & DESCRIPTION Pag. | 7

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• Design weight and capacities

Standard empty weight

Max Take-off Weight:

Landing Weight:

Maximum Useful Load:

Fuel Capacity:

780lb

1320lb

540lb

22,4

US Gal

355

600kg

245

90lt

• Performance (600kg

\1320lbs-912 ULS-Sensenich propeller)

Service

Ceiling:

Takeoff

Distance

S.L. (Ground Roll):

Tak eoff

Distance

S.L.

(

Clear 50ft.

Obstacle):

Max Climb Rate

S.L:

Max

Speed S.L:

Max

Range:

Cruise

Speed

(75% pwr at

6.500ft):

(never exceed this speed)

Landing

Distance

(Ground Roll):

Landing

Distance

(

Clear 50 ft

Obstacle):

Stall

Speed,

flap UP

Stall

Speed,

flap DW

15.000ft

590ft

1180ft

1100

ft/min

120kt

493nm

116kt

141kt

394ft

915ft

44kt

39kt

4572mt

0mt

60mt

mt/sec

km/h

20mt

280

81km/h

72km/h

1 2 3 4 5 6 7 8 9 10 11 12 13 ... 19 20

TECNAM P92 EAGLET 2
Table of Contents 3
General description 4
Construction 4
Interiors & Exteriors 5
Powerplant and propeller 5
(*)If required 8,33 MH 13
Engine Upgrade 16
Packages 16
OPTIONALS 17
TECNAM COLORS 19

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