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  • 1. المواصفات العامة الطائرة K8-E
    • الطول الكلى = 11.6 متر
    • العرض الكلى =9.63 متر
    • الارتفاع =4.21 متر
    • وزن للاقلاع = 3846 كجم
    • السرعة القصوى =800 كم / ساعة
    • اقصى زمن للطيران = 4.2 ساعة
    • المدى = 2140 كم
    • اقصر ارتفاع للطيران =13600 متر
    • طول ممر الاقلاع =440 متر
    • طول ممر الهبوط = 530 متر
  • 2. 0-General عام اعداد مجموعة الدعم الفنى للطائرة K8-E اكتوبر 2007
  • 3. K8E Aircraft structure هيكل الطائرة
    • low- wing layout جناح اسفل الجسم
    • tandem seat 2 كرسى
    • step cockpit arrangement, single-piece curved windshield الكابينة
    • a tricycle landing gear layout مجموعة العجل
    • rigid control for aileron, rudder and elevator controls and a booster for the aileron control
    • فى اسطح التحكم المختلفة نظام التحكم
    • extending slotted flaps القلابات
    • a single- piece speed brake installed under the center of the fuselage الفرامل الهوائية
  • 4.  
  • 5. 1-Fueslage Structure جسم الطائرة
    • frames 1 and 4 is the nose landing gear well and the front & equipment bay.
    • frames 4 and 9 is the front and rear cockpits and the second equipment bay.
    • No.1 and No.2 fuel tank baths, air intake duct, air brake bay and the fuselage/wing
    • gun pod is suspended between frames 7 and 12.
    • frames 21 and 32 is for engine mounting & fitting of horizontal and vertical stabilizer
  • 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 )
  • 10.
    • Vertical Fin structure are spars 1 and 2, stringers 1, 2 and 3, skin and ribs structure
    • The rudder is of a mono-spar thin-spared structure and ribs
    4- Vertical Tail الذيل الراسى ( الموازن الراسى )
  • 11.
    • The nose & main landing gear is a strut type landing gear
    5- Landing Gear مجموعة العجل
  • 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
  • 13.
    • gun pod is suspended under the fuselage between frames 7 and 12.
    7- Gun Pod المدفع
  • 14. 8- Ejection Seat الكرسى المنقذ ف
  • 15. 8- Engine المحرك
    • Turbofan Engine type
  • 16. هذه المحاضرات للتدريب فقط و لا تستخدم فى التجميع بل يتم استخدام المواصفات المعتمدة شكرا