Aircraft manuals

I only have one manual, the MiG-23ML manual, i will translate it and if some one wants to discuss it well is welcome

This is from the page 9 of the MiG-23 manual, in this page has in very few words the MiG-23ML and MiG-23UB main specifications:

We can see that the MiG-23ML has a weight with four R-3S missiles of 14670 kg and with two bombs of 500kg each of 15190kg, an internal fuel reserve of 3700kg, with an external fuselage tank it reaches 4360 kg, with external wing pod fuel tanks 5020 kg and with three fuel tank is 5680 kg, the MiG-23ML has a max speed at sea level of 1400 km/h, a Max speed of 2500 km/h or in Mach number of Mach 2.35, a practical ceiling of 17000 mtrs, a Max G limit of 8.5 at speeds below Mach 0.85 and 7.5Gs at speeds above Mach 0.85

The MiG-23ML has a flight range on internal fuel at the speed of Mach 0.74-0.77 with the wings set at a sweep angle of 16 degrees at ceiling of 14km-16km, of 1450km, this increases to 2360km with three fuel tanks

The MiG-23ML has a Max range with three external fuel tanks and two R-24/AA-7 Apex of 900km at a ceiling of 200 meters

The MiG-23 will accelerate at the altitude of 1 km from the speed of 630km to 1300km in just 30 seconds and at the altitude of 10km-12km will accelerate from Mach 1 to Mach 2 in just 160 seconds

The other page is the page number 1 and its the cover of the MiG-23ML manual