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Catalog #: 182305
Catagory: Aircraft -->Rotor (Helicopters)

Price: CONTACT US
Date Added: March 21, 2026

HERCULES D-130 Aircraft 1: C-130-H (Airworthy/Currently Flying) Crew: 5 (two pilots, navigator, flight engineer, and loadmaster) Payload: 45,000 lb (20,000 kg) Length: 97 ft 9 in (29.8 m) Wingspan: 132 ft 7 in (40.4 m) Height: 38 ft 3 in (11.6 m) Wing Area: 1,745 ft² (162.1 m²) Empty Weight: 75,800 lb (34,400 kg) Maximum Speed: 320 knots (366 mph, 592 km/h) at 20,000 ft (6,060 m) Cruise Speed: 292 knots (336 mph, 540 km/h) Range: 2,050 nautical miles (2,360 mi, 3,800 km) Service Ceiling: 33,000 ft (10,060 m) empty; 23,000 ft (7,077 m) with 42,000 pounds (19,090 kilograms) payload Rate of Climb: 1,830 ft/min (9.3 m/s) The C-130H has been a workhorse, supporting various missions worldwide ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1962. ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft airframe structure has 17,113 flight hours. ? Aircraft engines have 1,500 hours. ? Aircraft requires PDM which will be paid for by the seller at close of sale. ? Aircraft asking price is offered at $ 19,300,000USD 1 ? Aircraft 2: C-130-E (Airworthy/Currently Flying) DESCRIPTION: Military tactical transport POWER PLANT: Four 3,020 kw (4,050 eshp) Allison T56-A-7A turboprops SPECIFICATIONS: Wingspan: 40.25 m (132 ft 7 in) Length: 29.78 m (97 ft 9 in) Height: 11.68 m (38 ft 4 in) Wing area: 161.12 m² (1,745 sq ft) Max cruising speed: 587 km/h (365 mph) Rate of climb at sea level at max loaded weight: 472 m/min (1,550 ft/min) Take-off distance to 15 m (50 ft) at 70,310 kg (155,000 lb): 1,783 m (5,850 ft) Landing distance from 15 m (50 ft) at 45,360 kg (100,000 lb): AUW 732 m (2,400 ft) Range with 14,830 kg (32,700 lb) payload at 547 km/h (340 mph): 5,875 km (3,650 miles) Range with max fuel and 8,980 kg (19,800 lb) payload at 547 km/h (340 mph): 7,805 km (4,850 miles) Empty weight: 32,795 kg (72,300 lb) Max payload weight: 14,833 kg (32,700 lb) Loaded weight: 70,310 kg (155,000 lb). ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft requires PDM which will be paid for by the seller at close of sale. ? Aircraft asking price is offered at $19,300,000USD 2 Aircraft 3: C-130-H-30 (Airworthy/Currently Flying) Length: 112 feet 9 inches (34.37 meters) Height: 38 feet 10 inches (11.83 meters) Wingspan: 132 feet 7 inches (40.38 meters) Power Plant: Four Rolls-Royce AE 2100D3 4,691 pshp turboprop engines with GE-Dowty Aerospace R391 6-blade propellers Max Take-off Weight (2.5g): 164,000 pounds (74,389 kilograms)Payload (2.5g): 41,333 pounds (18,748 kilograms) Operating Weight (Empty): 87,667 pounds (39,765 kilograms) Zero Fuel Weight: 129,000 pounds (58,513 kilograms) Landing Distance (135,000 lbs.): 3,100 feet Range (40,000 lbs. payload, 2.25g): 2,450 nautical miles Maximum Cruise Speed: 355 KTAS (660 km/hr) The C-130H-30 is an updated version of the legacy C-130, offering enhanced capabilities and performance. ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1983. ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft airframe structure has 17,076 flight hours. ? Aircraft has fully integrated avionics system. ? Aircraft has digital fuel quantity upgrade. ? Aircraft has provisions for self-protection system. ? Aircraft has Engine Instrument Display System EIDS ? Aircraft has Fuel tank System Fault Tolerance Evaluation System per SFAR 88 SBs. ? Aircraft has 4A cargo handling system. ? Aircraft has engine and propeller data available. ? Aircraft requires C Check per SPM 515C38. Included in price. ? Aircraft asking price is offered at $ 17,900,000USD 3 Aircraft 4: KC-130-H (Airworthy/Currently Flying) Specifications (C-130H) Data from USAF C-130 Hercules fa ct sheet, International Directory of Military Aircraft, Complete Encyclopedia of World Aircraft, Encyclopedia of Modern Military Aircraft General characteristics Crew: 5 (two pilots, navigator, flight engineer and loadmaster) Capacity: C-130E/H/J cargo hold: length, 40 feet (12.31 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters) C-130J-30 cargo hold: length, 55 feet (16.9 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters) 92 passengers or 64 airborne troops or 74 litter patients with 2 medical personnel or 6 pallets or 2–3 Humvees or 2 M113 armored personnel carriers Payload: 45,000 lb (20,000 kg) Length: 97 ft 9 in (29.8 m) Wingspan: 132 ft 7 in (40.4 m) Height: 38 ft 3 in (11.6 m) Wing area: 1,745 ft² (162.1 m²) Empty weight: 75,800 lb (34,400 kg) Useful load: 72,000 lb (33,000 kg) Max. takeoff weight: 155,000 lb (70,300 kg) Powerplant: 4 × Allison T56-A-15 turboprops, 4,590 shp (3,430 kW) each Performance Maximum speed: 320 knots (366 mph, 592 km/h) at 20,000 ft (6,060 m) Cruise speed: 292 kn (336 mph, 540 km/h) Range: 2,050 nmi (2,360 mi, 3,800 km) Service ceiling: 33,000 ft (10,060 m) empty; 23,000 ft (7,077 m) with 42,000 pounds (19,090 kilograms) payload Rate of climb: 1,830 ft/min (9.3 m/s) Takeoff distance: 3,586 ft (1,093 m) at 155,000 lb (70,300 kg) max gross weight; 1,400 ft (427 m) at 80,000 lb (36,300 kg) gross weight ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1976. ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft airframe structure has 16,084 flight hours. ? Aircraft has fully integrated avionics system. ? Aircraft has digital fuel quantity upgrade. ? Aircraft has provisions for self-protection system. ? Aircraft has Engine Instrument Display System EIDS 4 ? Aircraft has Fuel tank System Fault Tolerance Evaluation System per SFAR 88 SBs. ? Aircraft has 4A cargo handling system. ? Aircraft has engine and propeller data available. ? Aircraft requires C Check per SPM 515C38. Included in price. ? Aircraft asking price is offered at $ 16,200,000USD Aircraft 5: C-130-H ? Length: 112 feet 9 inches (34.37 meters) ? Height: 38 feet 10 inches (11.83 meters) ? Wingspan: 132 feet 7 inches (40.38 meters) ? Power Plant: Four Rolls-Royce AE 2100D3 4,691 pshp turboprop engines with GE-Dowty Aerospace R391 6-blade propellers (all composite) ? Max Take-off Weight (2.5g): 164,000 pounds (74,389 kilograms) ? Payload (2.5 g): 41,333 pounds (18,748 kilograms) ? Operating Weight (Empty): 87,667 pounds (39,765 kilograms) ? Zero Fuel Weight: 129,000 pounds (58,513 kilograms) ? Landing Distance (135,000 lbs.): 3,100 feet ? Range (40,000 lbs. payload, 2.25g): 2,450 nautical miles ? Maximum Cruise Speed: 355 KTAS (660 km/hr) Airworthy/Currently Flying) ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1979. ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft airframe structure has 17,596 flight hours. ? Aircraft has fully integrated avionics system. ? Aircraft has digital fuel quantity upgrade. ? Aircraft has provisions for self-protection system. ? Aircraft has Engine Instrument Display System EIDS ? Aircraft has Fuel tank System Fault Tolerance Evaluation System per SFAR 88 SBs. ? Aircraft has 4A cargo handling system. ? Aircraft has engine and propeller data available. ? Aircraft requires C Check per SPM 515C38. Included in price. ? Aircraft asking price is offered at $ 17,200,000USD 5 Aircraft 6: C-130-H( Airworthy/Currently Flying) Length: 112 feet 9 inches (34.37 meters) Height: 38 feet 10 inches (11.83 meters) Wingspan: 132 feet 7 inches (40.38 meters) Power Plant: Four Rolls-Royce AE 2100D3 4,691 pshp turboprop engines with GE-Dowty Aerospace R391 6-blade propellers (all composite) Max Take-off Weight (2.5g): 164,000 pounds (74,389 kilograms) Payload (2.5 g): 41,333 pounds (18,748 kilograms) Operating Weight (Empty): 87,667 pounds (39,765 kilograms) Zero Fuel Weight: 129,000 pounds (58,513 kilograms) Landing Distance (135,000 lbs.): 3,100 feet Range (40,000 lbs. payload, 2.25g): 2,450 nautical miles Maximum Cruise Speed: 355 KTAS (660 km/hr) ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1979. ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft airframe structure has 19,296 flight hours. ? Aircraft has fully integrated avionics system. ? Aircraft has digital fuel quantity upgrade. ? Aircraft has provisions for self-protection system. ? Aircraft has Engine Instrument Display System EIDS ? Aircraft has Fuel tank System Fault Tolerance Evaluation System per SFAR 88 SBs. ? Aircraft has 4A cargo handling system. ? Aircraft has engine and propeller data available. ? Aircraft requires C Check per SPM 515C38. Included in price. ? Aircraft asking price is offered at $ 17,200,000USD 6 Aircraft 7: C-130E (Airworthy) Lockheed C-130E Hercules: Length: 29.78 meters (97 feet 9 inches) Height: 11.68 meters (38 feet 4 inches) Wingspan: 40.25 meters (132 feet 7 inches) Power Plant: Four 3,020 kW (4,050 eshp) Allison T56-A-7A turboprop engines Max Take-off Weight (2.5g): 70,310 kilograms (155,000 pounds) Payload (2.5g): 14,833 kilograms (32,700 pounds) Empty Weight: 32,795 kilograms (72,300 pounds) Max Cruising Speed: 587 kilometers per hour (365 miles per hour) Rate of Climb at Sea Level (max loaded weight): 472 meters per minute (1,550 feet per minute) Take-off Distance to 15 meters (50 feet) at 70,310 kg (155,000 lb): 1,783 meters (5,850 feet) Landing Distance from 15 meters (50 feet) at 45,360 kg (100,000 lb): 732 meters (2,400 feet) Range with 14,830 kg (32,700 lb) payload at 547 km/h (340 mph): 5,875 kilometers (3,650 miles) Range with max fuel and 8,980 kg (19,800 lb) payload at 547 km/h (340 mph): 7,805 kilometers (4,850 miles) ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1962. ? Aircraft has been confirmed as airworthy and currently flyable. ? Aircraft has been upgraded to H capability with -15 engines. ? Aircraft has ARC 164V UHF, ARC 190V HF and ARC 186 VHF radios ? Aircraft has digital flight data recorder. ? Aircraft has auto-pilot. ? Aircraft has Flight Management System. ? Aircraft has Ground Proximity Warning System GPWS 88 SBs. ? Aircraft has Bendix King IVA 81D Traffic Collision Avoidance System TCAS ? Aircraft has APN 59 Radar System ? Aircraft has engine and propeller data available. ? Aircraft asking price is offered at $ 16,300,000USD 7 Aircraft 8-10 C- H-30 Hercules: Length: 112 feet 9 inches (34.37 meters) Height: 38 feet 10 inches (11.83 meters) Wingspan: 132 feet 7 inches (40.38 meters) Power Plant: Four Rolls-Royce AE 2100D3 4,691 pshp turboprop engines with GE-Dowty Aerospace R391 6-blade propellers (all composite) Max Take-off Weight (2.5g): 164,000 pounds (74,389 kilograms) Payload (2.5 g): 41,333 pounds (18,748 kilograms) Operating Weight (Empty): 87,667 pounds (39,765 kilograms) Zero Fuel Weight: 129,000 pounds (58,513 kilograms) Landing Distance (135,000 lbs.): 3,100 feet Range (40,000 lbs. payload, 2.25g): 2,450 nautical miles Maximum Cruise Speed: 355 KTAS (660 km/hr) The C-130H-30, an extended version of the C-130 Hercules, offers superior performance and versatility. Whether transporting troops, cargo, or conducting special missions, the C-130H-30 remains a reliable workhorse ? 3 C130 H-30s (Airworthy/Currently Flying) ? Aircraft was delivered to end user by Lockheed Martin Marietta in 1976-79. ? Aircraft asking price is offered at $ 16,700,000USD It is lacking an APU, however, which is why is retains a Super E designation. The owner is asking $11 million, and aircraft inspection / records review may occur once the proper licensing is presented, along with mandate and appropriate proof of funds. Note: Please note that our aircraft, as well as the 10 others we have, are all former military and will require an end user certificate or ITAR license to purchase. We would need a copy of either to proceed.