The K8-E aircraft has a length of 11.6 meters, width of 9.63 meters, and height of 4.21 meters. It has a maximum takeoff weight of 3,846 kg and can fly at a maximum speed of 800 km/h for up to 4.2 hours with a range of 2,140 km. The aircraft has a low wing layout with two tandem seats and a tricycle landing gear. It uses rigid controls for surfaces like the aileron, rudder and elevator.

2. 0-General عام اعداد مجموعة الدعم الفنى للطائرة K8-E اكتوبر 2007

6. The wing is of a thin-spared structure riveted with the front spar, main spar, rear spar, ribs, stringers and skins. The wing is connected with frames 12, 14 and 16 of the fuselage at near rib 4.integral fuel tank ,main landing gear well , flap connections and aileron connections 2-Wing Assy. Structure الجناح

7. Flap structure are front and rear spar, two more stringers , ribs 2-1 Flap

8. The aileron is of a mono-spar thin-spared , ribs structure. 2-2 A ileron

9. Horizontal Tail is double-spar thin-spared , ribs structure The elevator is of a mono-spar thin-spared , ribs structure 3- Horizontal Tail الذيل الافقى ( الموازن الافقى )

12. The control system consists of the controls of aileron, elevator and rudder, which are all the rigid control mechanisms being composed of pull-rods, rocker arms and support. 6-Control System نظام التحكم

14. 8- Ejection Seat الكرسى المنقذ ف

16. هذه المحاضرات للتدريب فقط و لا تستخدم فى التجميع بل يتم استخدام المواصفات المعتمدة شكرا