An old wish of mine, I just shined it up some. 
A6M3 (Navy Type 0 Carrier Fighter Model 22) "Hamp"Engine: x1 Nakajima Sakae 21 engine w/two-stage supercharger [1,130hp at take-off, 1,100hp at 9,350ft, 980hp at 19,685ft] w/ 3-bladed constant speed Sumitomo propeller
Speed: Altitude         TAS          Man. Press.
Ft.                 MPH         " Hg.                   Blower
------------------------------------------------------------------------------------------
0                   280             36.0                    Low
5,000            296             36.0                    Low
*9,300          310             36.0                    Low
10,000          310             35.2                    Low
15,000          304             29.3                    Low
15,000          307             36.0                    High
**15,300      308             36.0                    High
20,000          305             31.0                    High
25,000          300             25.6                    High
30,000          294             20.3                    High
* Low blower critical altitude for climb
** High blower critical altitude for climb
Climb Rate:Alt.            Climb Rate      Climb Time     Blower         Man. Press.               TAS
Ft.             Ft./min            Min.                                   " Hg.                          MPH
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0               3,260              0                    Low             36.0                          140
5,000        3,060              1.58               Low             36.0                          151
*7,000      2,980              2.24               Low             36.0                          155
10,000      2,460              3.35               Low             32.8                          159
10,000      2,340              3.35               High             36.0                          159
**15,000  2,180              5.55               High             36.0                          168
20,000      1,650              8.19               High         28.8                          177
25,000      1,120              11.84             High             23.2                          185
30,000      600                 17.79             High             19.2                          193
* Low blower critical altitude for climb
** High blower critical altitude for climb
Ceiling: 11,050 m
Fuel: 570 liters internal + 330 liters in a centerline drop tank
Range: 1,284 naut miles
Weight: 4,107lb empty, 5,835lb loaded
Dimensions:Span                  36 ft. 2 1/4 in.
Length               29 ft. 9 in.
Height               9 ft. 2 in.
Wing area               232 sq. ft.
CG            Approx. 31% MAC, 0.075 in. forward of main spar
Air foil (root)             NACA 2315
Air foil (tip)                NACA 3309
Max. chord thickness, center line   8 1/4 in.
Max. chord thickness, tip       4 1/8 in.
Chord, centerline             8 ft. 3 in.
Chord, fuselage side (20 in. from centerline)    8 ft. 1 in.
Chord, tip                4 ft. 1 1/4 in.
Mean chord                6 ft. 4.8 in.
Aspect ratio                5.5
Dihedral, on 30% chord          6.5 deg.
Taper ratio                44
Wing loading             21.3 lb/sq/ft
Power loading             5.42 lb/hp/sq/ft
Aileron area, total             20.2 sq. ft.
Aileron span, each          9 ft. 7 5/8 in.
Flap area, total             16.44 sq. ft.
Flap span, each             5 ft. 3 3/4 in.
Horizontal tail area, total          51.68 sq. ft.
Stabilizer area, total          40.84
Airfoil, root                NACA-.0009-64 approx.
Airfoil, tip                NACA-.0010
Span                   15 ft. 5 in.
Mean chord               3 ft.
Aspect ratio                5.7
Taper ratio                .439
Elevator area, total          10.85 sq. ft.
Percent balance             11.35
Trim tab area             1.19 sq. ft.
Fin area                7.92 sq. ft.
Rudder height             4 ft. 6 in.
Rudder area             7.7 sq. ft.
Rudder area forward hinge line       0.7 sq. ft.
Rudder trim tab area          .065 sq. ft.
Percent balance             9.64
Armament: 2x 7.7mm Type 97 machine guns in upper cowl, 2x 20mm Type 99 Model 1 Mark 3 cannon w/100rpg in wings, 2x wing rack 132lb bombs
# Built: 560 Aircraft
Notes: Late production aircraft fitted with long barrel 20mm, Type 99 Model 2 Mark 3 cannon. (Perk Option?)
Sources:http://www.j-aircraft.com/research/zerofacts.htmhttp://www.wwiiaircraftperformance.org/japan/hamp-eb201.htmlhttp://rwebs.net/avhistory/history/Zeke32.htmWhy?Well, the two models of the zero we have already need a face-life eventually, and I'm sure with that being done this one could be modeled in as well. It would flesh out the IJNAF most used fighter plane of the war and help with expand the the Japanese plane-set during scenarios and in general.
(Sorry for the jammed together look of the speed and climb data, for some reason it doesn't want to put in my spaces... If anyone sees anything wrong with this info and/or would like to add anything, don't hesitate to say anything!)