| Performance Metric | Early Serie I (This Overhaul) | Later C.200 Production Batch | Engineering / Operational Notes |
|---|---|---|---|
| Sea Level Top Speed | 122.2 m/s (440–465 km/h) | 122.2 m/s (440–465 km/h) | Identical deck speed; lower drag offsets slightly lower max horsepower. |
| Peak Rated Altitude | 3,600 m (~500 km/h) | 4,200 m (504 km/h) | Early supercharger ducting hits optimal efficiency lower down. |
| Service Ceiling | 8,300 m | 8,900 m | Enforced via adjusted high-altitude power tables. |
| Acceleration & Climb | Decent / Moderate | Crisp / Improved | Lower power-to-weight ratio slows energy recovery in vertical loops. |
| Dead-Stick Glide Ratio | Flatter / Cleaner (L/D) | Steeper / Draggier | Spinner cone and sealed canopy reduce parasite drag when engine conked out. |
| Stall Departure | More abrupt (constant profile wings) | Slightly smoothed (cf. "Stefanutti fix" with balsa shims to create variable profile wings) | Unmodified early wing roots trigger more stubborn wing drop under heavy G. |
While early Serie I Saettas underwent initial desert trials with the 4° Stormo in North Africa in August 1939, pilot concerns over the unannounced stall break led to their temporary withdrawal back to Italy and Sicily prior to June 1940. Historically accurate combat encounters between the early Serie I C.200 and RAF Hurricane Mk.Ia occur during the Malta / Central Mediterranean campaign (1940), the Balkan / Greek invasion (Spring 1941), and subsequent Western Desert operations (April 1941 onward) following tropical filter retrofits (although by that time the later-production C.200 would have been dominant). In terms of broad historical realism, it is possible to present rare skirmishes between the early C.200 and Mk.Ia Hurricane in the North African theater as early as the September-October 1940 window.