Therefore, I would have ensured that my Fw 190T's were compatible with whatever size of carrier was necessary, and used them to clear the skies so the U-boats could function. The carrier would be concentrated around a single type, carying only one type of engine, propeller, landing gear, wings, tail assembly, etc. for repairs. There would not be much confusion around different types, because everyone would know all the routines for the Fw 190T.
I fully recognize the attractiveness of this idea but I am afraid that this would have been the most impractical solution of all.
At first, the Fw-190 was just appearing in the frontline services by mid 1941 in her early A-versions with the bugs not beeing worked out until mid 1942 with the introduction of the A-4 subvariant. This were general fighter variants and by no means specialized naval variants, whiches development time requirements are not taken into account so far.
Second, the BMW-801 radial engines of the Fw-190A required replacement after a nominal 20 hours flighttime until late in 1942, which would require about four spare engines per plane to be shipped by the CVL extra to account for very low level air operations, enduring CAP-missions are not sustainable in these conditions.
Thirdly, a navalized Fw-190, albeit possible, would require major modification of fuselage wing, an entirely new airframe as a result.
A)The cockpit needs to be placed more towards the frontal area in order to improve visibility to the fwd. arcs (esspeccially the sub horizon arcs, which are decisive for landing ops) and eventually higher.
B)The rear fuselage needs reinforcements to take the arrestor hook with structu ral reserves.
C) The low speed handling charckteristics of the Fw-190A are abysmal poor. The plane is generally treated for improved high speed handling but low slow, the Fw-190 shows severe weaknesses: The stall does develope rapidily from the mid of the wing outwards with little associated earlier stick warnings. That are bad news in the landing deck capabilities. It would need some kind of outer wing slats to compensate for this.
D) The Fw-190A as designed has a low wingarea conception (the V-5 prototype was tried with large and small wings and eventually the small wing was choosen for all serial Fw-190´s due to increased agility and better high speed performances). The resulting netto effects showed a comparably high landing speed and in combination with the constraints summerized under C), the advisable approach speed was 150 Km/h, a good tad bit faster than the navalized Bf-109, which wouldn´t be usable on the CVL.
E) development times for a navalized Fw-190A would take three years lowest (if started early in 1940) and you couldn´t expect serial production planes to roll of from the assembly lines any sooner than mid 1943. By this time it´s already (much) to late to send CVL´s out into the Atlantic.
Best regards,