7/25/2019 1968 - 2786

1/1

902 903

LIGHTnternational 28November

,'J4

Lead ins Data

Span,

34ft

6in

(over

ti p

tanks, 38ft 1.5m),length, 33ft

I lin ;

height overal l,

I

Oft lOin:

wing area, gross, 209.14

sq ft;

weight empty, 5,4851b; fully loaded, 7,7001b; wing

loading,

35.4lb/sq

ft; max

speed,

s.l.,

420kt;

max

rate

of

climb,

s.l.,

4,S00ft/min;

take-off

to

50ft, 2,100ft;

max

range,

770

miles;

max

endurance,

2 hr 30 min.

Structure

1 Access to forward equipment

compartment

2 Cockpit front bulkhead

3 Windscreen frame

4 Manually opera ted front canopy

5 Manually operate d rear canopy

6

Operat ing handle

7 Canopy latches

8 Canopy open side support

9 Inflatable canopy seal

10 Blind-fly ing hood, rear cockpit

only

11 Folland Type

I-B

lightweight

ejector seat

12 Cockpit rear bulkhead

13 Fuselage main longerons

14 Fuselage frames

15 L-section stringers

It Intake trunking

17 Boundary-layer

air

bleed

18 Engine-removal fuselage break

point

19 Centre equipment-bay access

hatches

20 Rear fuselage tie-bol ts (four)

21

Fin

front spar

22

Fin

rear spar

23 Top-heat-section stringers

24

Fin

front attachment

SOKO G LEB

25

Fin and

tailplane rear attachment

24 Tailplane front spar

27 Tailplane rear spar

28

.

Removable tailcone

29 Underfinandtai l bumper

30 Wing fron t spar

31 Win g rear spar

32 L-section spar booms

;

33 Wing ribs

34 Main gear leg-support beam

35 Wing spar root fittings

36 Steel-bushed attachments boles,

topandbottom

37 Wing spar carry-through struc-

ture

38 Wing-support fuselage frames

39 Removable

t ip

tanks

40 Root section NACA-64 A2I3

41

Tip

section NACA-64 A2I2.0

Air System

A l Compressor bleed

air

supply

A2 De-icingandde-mistingair

A3 Footwarmer

and

cabin distiwJ-

tion duct

,

A4 Cabin fresh-airramintake (op^n)

ontrols

Cl Control column

C2 Aileron