Autonomy is not good, I made a return flight from Augusta-Malta (a roughly 300km) and my aircraft did not have enough fuel to return mid-flight return ???
Source Wikipedia:
Specifications (Z.501)
Data from The Encyclopedia of Weapons of World War II
General characteristics
Crew: 4-5
Length: 14.30 m (46 ft 11 in)
Wingspan: 22.50 m (73 ft 9¾ in)
Height: 4.40 m (14 ft 6 in)
Wing area: 62 m² (670 ft²)
Empty weight: 3,850 kg (8,490 lb)
Max. takeoff weight: 7,050 kg (15,300 lb)
Powerplant: 1 × Isotta-Fraschini Asso XI.RC RC2C.15 liquid-cooled V12 engine, 656 kW (880 hp)
Performance
Maximum speed: 275 km/h (148 kn, 170 mph)
Range: 2,400 km (1,300 nmi, 1,500 mi)
Service ceiling: 7,000 m (23,000 ft)
Armament
Guns: 3 × 7.7 mm (0.303 in) Breda-SAFAT machine guns (initially Vickers), but many had only two when the nose position was removed
Bombs: 640 kg (1,400 lb) carried externally
How can we modify the characteristics of reservoirs in IL-2?
Thanks