109E-1 weighed 2500kg, E-3 - 2610, E-4 - 2570.Change from 109C/D to 109E was about 450kg, mostly due the DB 601 engine and accessories (and fuel). But the bigger engine allowed for almost 100kph more speed.
The 109E-3 weighed 2608kg, useful load was 555kg (1224lbs) But the 109E carried a bit less fuel but more guns/ammo than old Curtiss.
Surprisingly, our opinions are in agreement.I am sorry, I am failing to follow the logic of an old obsolete aircraft being being demoted to ground support somehow allows a "standard" fighter to be transferred to the Light fighter catagory?
So what's the problem with accepting the definition offered above as a definition? Only "true" "light" fighters - C.710/713/714, Potez 230 (with HS12Xcrs), MB.700, XP-77 (thanks, SaparotRob!), SAM-13, R.30, SAI 207/403 - would be included . Even the VG.30 can no longer be considered as "light" - it was supposed to be equipped with HS 12Y-49 and Allison V-1710 in serial production, its weight corresponded to the contemporary Bf.109s. The CW-21, still, was a "colonial" fighter, and was not considered as an alternative to "conventional" fighters. Therefore, it is also outside the scope of the concept.
It is impossible to achieve a reasonable compromise between flight performance, operational characteristics, avionics equipment and armament within the "light fighter" concept. Sacrificing one of these characteristics for the sake of the others results in a deliberately inferior airplane. The flight performance of the unarmed prototypes should not be misleading - it would have inevitably deteriorated if armament had been installed. Why consider alternatives to something that was fundamentally unsuitable?
