STATUS: Active, Limited Service
MANUFACTURER(S): Lockheed - USA
OPERATORS: Algeria; Argentina; Canada; Ecuador; Gabon; Indonesia; Kuwait; Libya; Peru; Philippines; Saudi Arabia; South Africa; United Arab Emirates; United States
LENGTH: 112.86 feet (34.4 meters)
WIDTH: 131.23 feet (40 meters)
HEIGHT: 38.06 feet (11.6 meters)
WEIGHT (EMPTY): 77,713 pounds (35,250 kilograms)
WEIGHT (MTOW): 154,985 pounds (70,300 kilograms)
ENGINE: 4 x Allison 501-D22A turboprop engines developing 4,510 horsepower each.
SPEED (MAX): 354 miles-per-hour (570 kilometers-per-hour; 308 knots)
RANGE: 5,592 miles (9,000 kilometers; 4,860 nautical miles)
CEILING: 22,966 feet (7,000 meters; 4.35 miles)
RATE-OF-CLIMB: 1,830 feet-per-minute (558 meters-per-minute)
Detailing the development and operational history of the Lockheed L-100 Hercules Civilian Cargo Transport Aircraft.
Entry last updated on 9/2/2018.
Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The excellent hauling capabilities and military market success that was the Lockheed C-130 Hercules transport eventually yielded a civilian market form as the L-100 Hercules. Its prototype first flew on April 20th, 1964 to which the aircraft was introduced for civilian airspace operations on September 30th, 1965. The L-100 retains the same form and function of the original C-130 including its excellent handling capabilities and short-field hauling qualities. Production netted 114 aircraft in all with the last built in 1992. The L-100 was recognized by Lockheed as company "Model 382", the production form based on this as the "Model 382B".
Following the original L-100s was the L-100-20 of 1968 which included a fuselage stretch for additional internal volume. The L-100-30 saw a further lengthening of the fuselage that added nearly seven feet. The entire line was then modernized in the LM-100J.
In the L-100-30, the crew numbers three minimum and includes two pilots and a flight engineer. Patload capacity is 51,000lbs with a Maximum Take-Off Weight (MTOW) of 155,000lbs. Power is served through 4 x Allison 501-D22A series turboprop engines developing 4,500 horsepower each. Maximum speed is 355 miles per hour with a cruise speed of 335 miles per hour. Round-trip range is 1,535 miles with a ferry range of 5,555 miles out. The aircraft features a service ceiling of 23,000 feet and a rate-of-climb of 1,830 feet per minute.
Dimensions include a length of 112 feet, 9 inches, a wingspan of 132 feet, 7 inches and a height of 38 feet, 3 inches.
Despite its civilian-minded design, the L-100 was still adopted by the militaries of Algeria, Kuwait, Indonesia, Philippines and Saudi Arabia among others. Despite the military shift towards the much improved C-130J "Super Hercules", the L-100 has not followed suit to date - though a February 2014 report suggests Lockheed will reactivate the initiative soon. This would then produce the L-100J designation.
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Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
This entry's maximum listed speed (354mph).
Graph average of 300 miles-per-hour.
Graph showcases the Lockheed L-100-30 Hercules's operational range (on internal fuel) when compared to distances between major cities.
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units