Lockheed L-100 Hercules Information & Lockheed L-100 Hercules Links at HealthHaven.com
advertise
add site
services
publishers
database
health videos
Bookmark and Share

search wiki for    ?
web dir firms image gallery news pdf wiki shop video 
about
toolbar
stats
live show
health store
more stuff
JOIN/LOGIN
Featured Results:
SweetLeaf $13.99 SteviaPlus Fiber 100 pkts-Buy SteviaPlus Fiber 100 pkts...
SweetLeaf $13.99 SteviaPlus Fiber 100 pkts-Buy SteviaPlus Fiber 100 pkts...
mynaturalmedicineclinic.c...
 Lipoic Acid 100 mg (100 caps) : : HPDI Product Page
Lipoic Acid 100 mg (100 caps) : : HPDI Product Page
integratedhealth.com
 Beckman TL 100, Beckman TL Centrifuge, TL 100 Beckman Ultra Centrifuge,...
Beckman TL 100, Beckman TL Centrifuge, TL 100 Beckman Ultra Centrifuge,...
blockscientific.com
 
L-100 Hercules
A Tepper Aviation L-382 taking off from Mojave Spaceport, California
Role Transport aircraft
National origin United States
Manufacturer Lockheed
First flight 20 April 1964
Introduction 30 September 1965
Developed from C-130 Hercules
Northwest Territorial Airways L-100-30 at London Stansted Airport
Civil-owned C-130A of TBM Inc.

The Lockheed L-100 Hercules was the Lockheed Corporation's less successful civilian variant of the prolific C-130 military transport aircraft. Its first flight occurred in 1964. Longer L-100-20 and L-100-30 versions were developed. L-100 production ended in 1992 with 114 aircraft delivered.[1][2]

Contents

[edit] Development

In 1959 Pan American ordered 12 GL-207 Super Hercules to be delivered by 1962, it was to be powered by four 6,000 eshp Allison T61 turboprops. It was to be 23 ft 4 in (7.11m) longer than the C-130B, a variant powered by 6,445 Rolls-Royce Tynes and a jet-powered variant with four Pratt & Whitney JT3D-11 turbofans were also under development. Both Pan American and Slick Airways (who had ordered six) cancelled their orders and the other variants did not evolve past design studies. The company then decided to produce a commercial variant which was just a de-militarised version of the C-130E Hercules. The prototype L-100 (N1130E) first flew on the 20 April 1964 when it carried out a 25 hour 1 minute flight. The type certificate was awarded on 16 February 1965. Twenty-one production aircraft were then built with the first delivery to Continental Air Services on 30 September 1965.

Slow sales led to the development two new, longer versions, the L-100-20 and L-100-30, both of which were larger and more economical than the original model. Deliveries totaled 114 aircraft, with production ending in 1992. An L-100J variant of the updated C-130J was cancelled in 2000.[1][2]

[edit] Variants

Civilian variants are equivalent to the C-130E model without pylon tanks or military equipment.

L-100 (Model 382)
One prototype powered by four Allion 501-D22s and first flown in 1964
L-100 (Model 382B)
Production variant, equivalent to the C-130E without underwing fuel tanks and without military equipment.
L-100-20 (Model 382E and Model 382F)
Stretched variant certified in 1968 with a new 5 ft (1.5 m) section forward of the wing and 3 ft 4 in (1.02 m) section aft of the wing.
L-100-30 (Model 382G)
A further stretched variant with an addition 6 ft 8 in (2.03 m) fuselage section.

[edit] Operators

In July 2009 a total of 36 Lockheed L-100 Hercules aircraft were in commercial service. Operators include Safair (9),[3] Lynden Air Cargo (6), Transafrik (5), Libyan Arab Air Cargo (3), First Air (2), and other operators with fewer numbers of the type.[4]

In January 2009, 35 Lockheed L-100s were in use with military operators, including Indonesian Air Force (10), Libyan Air Force (5), Algerian Air Force (3), Kuwait Air Force (3), Peruvian Air Force (3), Royal Saudi Air Force (3), and other users with fewer aircraft.[5]

[edit] Specifications (L-100-30)

C-130-3-view.png

Data from International Directory of Civil Aircraft,[1] Complete Encyclopedia of World Aircraft[6]

General characteristics

  • Crew: 3-4: (two pilots, navigator, flight engineer/loadmaster)
  • Payload: 51,050 lb (23,150 kg)
  • Length: 112 ft 9 in (34.37 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: 77,740 lb (35,260 kg)
  • Max takeoff weight: 155,000 lb (70,300 kg)
  • Powerplant:Allison 501-D22A turboprops, 4,510 shp (3,360 kW) each

Performance

[edit] See also

Related development

Comparable aircraft

[edit] References

  1. ^ a b c Frawley, Gerald. The International Directory of Civil Aircraft, 2003/2004. Fishwick, Act: Aerospace Publications, 2003. ISBN 1-875671-58-7.
  2. ^ a b Lockheed L-100 Hercules. airliners.net
  3. ^ http://www.safair.co.za/index.php?option=3&id=1&com_id=47&parent_id=47&com_task=1
  4. ^ "World Airliner Census". Flight International, 18-24 August 2009.
  5. ^ "World Military Aircraft Inventory". 2009 Aerospace Source Book. Aviation Week and Space Technology, January 2009.
  6. ^ Donald, David, ed. "Lockheed C-130 Hercules". The Complete Encyclopedia of World Aircraft. Barnes & Nobel Books, 1997. ISBN 0-7607-0592-5.

[edit] External links




Product Results (view all...)

search wiki for    ?
web dir firms image gallery news pdf wiki shop video 



↑ top of page ↑about thumbshots