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
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
Flap structure are front and rear spar, two more stringers , ribs 2-1 Flap
The aileron is of a mono-spar thin-spared , ribs structure. 2-2 A ileron
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 )
The nose & main landing gear is a strut type landing gear
5- Landing Gear مجموعة العجل
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