Spitfire IIA with 40 gal tank.
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Tested at Boscombe Down in Sept 1941 (?) .
Some were flown by Sqadron Nos 66, 118, and 154.
I don't know if any squadron was fully equipped or not.
This was the 2nd attempt at fitting the wing tank. It had been tried on a MK I.
Somewhere there was a report on the MK I. The Report on the MK IIA gives speeds and climbs.
The MK IIB had metal alerions and handling was a marked improvement over the MK I and the plane was considered satisfactory as a fighter.
Granted this tank has a fair amount of drag and cost a bit over 20mph in speed. It also cost about 700fpm in climb under 20,000ft.
How much was drag and how much was weight can be argued. Fitting the fuel tanks inside would get rid of the drag (except for a few mph) but the weight is still a problem.
Engaging the enemy over the French/Belgian coast is problematic. Near the end of the misson/sweep (longer than a normal Spitfire) there isn't going be much difference.
At the start or entry into enemy airspace the planes carrying the extra fuel are going to have much degraded climb.
Early MK Vs (eight gun) show a bit better climb using standard 2850rpm and 9lbs climb compared to the MK IIs with Merlin XII engines. Above 20,000ft the MK Vs show more advantage.
MK Vs seem to show rather different performance from each other.
A MK Vb with standard tanks was within 15lbs of the MK IIA with the fuel tank. Extend range Vb might have had similar performance to a standard IIa? Or IIb? Is that good enough in late 1941?