Done some more digging:
T/O distances for Bf-109G6 trop, w/ 20 degrees flap:
3360 kg: 455/440 m (0.9 m/sec, 1.9 m/sec wind)
3340 kg: 457/431 m (0, 2.3 m/sec wind)
3320 kg: 411 m (2.5 m/sec wind)
3300 kg: 399 m (2.6 m/sec wind)
3280 kg: 408 m (1.7 m/sec wind)
Normal loaded weight was 3,360 kg.
Figures with 40 degrees of flap are actually longer.
Weight obviously makes a major difference to T/O performance, but I’m not sure how well this new info would gel with the earlier comments on 109D T/O performance. Given that the 109G-6 had a power to weight ratio of about 0.44 PS/kg and the 109D had a power to weight ratio of 0.35 PS/kg, I wonder how much this affected the T/O distance?
(These are obviously rough figures using best available power, not necessarily T/O power)
Then again, the other major consideration to balance is the much lower wingloading of the 109D
Sidestepping a little, and the Gloster Gladiator had a T/O run of 165 m with 2 bladed fixed pitch wooden prop, and 150 m with three bladed prop (not sure if fixed, two pitch or CSP). Power to weight was 0.50 PS/kg (better than the 109G-6

).
Surely the less heavily wing-loaded biplane would get off the ground faster than a 109D?