Lockheed CC-130 Hercules

In the early 1990s, as part of a broader modernization and restructuring effort within the Royal Canadian Air Force, 418 Squadron began the process of transitioning to the CC-130 Hercules, in collaboration with 435 Squadron. This robust four-engine turboprop aircraft, designed for versatile roles ranging from troop transport and cargo delivery to aerial refueling, was set to enhance the squadron's capabilities significantly. The Hercules is renowned for its exceptional payload capacity, long-range capabilities, and ability to operate from rough, undeveloped runways—traits that would have supported 418 Squadron's expanding operational scope, particularly in training.

• Wing Span: 40.41 m (132 ft 7 in)

• Length: 29.79 m (97 ft 9 in)

• Height: 11.66 m (38 ft 3 in)

• Weight, Empty: 33,060 kg (72,885 lb)

• Weight, Gross: 70,310 kg (155,000 lb)

• Cruising Speed: 555 k/h (345 mph)

• Max Speed: 618 k/h (384 mph)

• Rate of Climb: 558 m (1,830 ft) /min

• Service Ceiling: 7,040 m (23,100 ft)

• Range: 7,220 km (4490 mi)

• Power Plant: 4 Allison T56-A-7A turboprop engines, 4,050 shp