I notice that all ranges on internal fuel were estimated using the fuel economy achieved with external tanks. In reality the range on internal fuel only will result in better fuel economy than with external tanks.
In other words you will fly further per liter on internal fuel than you will on external tanks. There are two obvious reasons for this... First, you don't need to carry the extra weight of the drop tank & its fuel, and secondly it cuts down on aerodynamic drag.
Therefore estimating the range on internal tanks by using the range with drop tanks as a guide will result in a shorter estimated range than reality.
Here are the ranges of some of the A6M variants, including actual ranges on internal fuel only.
Source: Aero Detail 7, Mitsubishi A6M Zero Fighter
A6M2:
518L internal only = 2220km
518L (internal) + 330L (external) = 3350km
A6M3 model 32:
470L internal only = 1800km
470L (internal) + 330L (external) = 2380km
A6M3 model 22: No data given for the model 22, but the extra 100L as compared to the model 32 should give the A6M3 model 22 considerably longer range.
A6M5 model 52:
570L internal only = 1550km
570L (internal) + 320L (external) = 1920km
From the A6M5 onwards the external tank design was changed from metal to wood, which might account for the slightly different fuel capacity.
The external tank design was changed again from the A6M5c onwards to a design using four support points.
The A6M5c and A6M7 could in addition to a centerline tank also carry drop tanks underneath the wings, extending range further.
All speed & climb performance data below was achieved using military power (without WEP) as per Japanese Navy convention.
For the range data (red arrows) the first value is range on internal fuel only, while the second value is range with drop tanks. Max Range for the A6M5c & A6M7 is with multiple drop tanks.
