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North American F-86D Sabre Dog
Single-engine single-seat swept-wing tri-gear all-weather jet fighter/interceptor, U.S.A.


Archive Photos [1]


Archive Photos 1,2,3


[North American F-86D-15-NA Sabre Dog (NA-165, AF 50-560, c/n 165-106) on display (9/15/2004) at the March Field Air Museum, Riverside, California (Photo by John Shupek copyright © 2004 Skytamer Images)]

[North American F-86D-35-NA Sabre Dog (NA-173, AF 51-6261, c/n 173-405, painted as AF 52-10115) displayed (3/15/2011) on a pylon at Chandler, Arizona (Photos by Ron Strong, 12/2007)]

[North American F-86D-35-NA Sabre Dog (NA-173, AF 51-6261, c/n 173-405, painted as AF 52-10115) displayed (3/15/2011) on a pylon at Chandler, Arizona (Photo by Lt. Col. Dr. Marc Matthews, USAF (ret.), 3/15/2011)]

[North American F-86D-40-NA Sabre Dog (NA-190, AF 52-3598, c/n 190-266) on display (5/4/1995) at the National Museum of the United States Air Force, Wright Patterson AFB, Dayton, Ohio (Photo by John Shupek copyright © 1995 Skytamer Images)]

[North American F-86L-60-NA Sabre Dog (NA-201, AF 53-1060, c/n 201-504, converted to F-86L, painted as AF 52-366) on display (9/25/2003) at the Yankee Air Museum, Belleville, Michigan (Photo by John Shupek copyright © 2003 Skytamer Images)]

[North American F-86L-55-NA Sabre (AF 53-0700, c/n 201-144) on display (8/2/2012) at the Ehlert Memorial Park, Brookfield, Illinois (Photo by Lt. Col. Dr. Marc Matthews, USAF (ret.), 8/2/2012)]

North American F-86D Overview [4]
From Wikipedia, the free encyclopedia


    North American F-86D “Sabre Dog”
  • Role: Fighter interceptor
  • Manufacturer: North American Aviation
  • First flight: 22 December 1949
  • Primary users: United States Air Force; Italian Air Force; SFR Yugoslav Air Force; Venezuelan Air Force
  • Number built F-86D: 2,504
  • Number built F-86D/K/L: 2,847
  • Unit cost: USD $343,839 (F-86D)
  • Developed from: North American F-86 Sabre

The North American F-86D Sabre (sometimes called the “Sabre Dog” or “Dog Sabre”" was a transonic jet all-weather interceptor of the United States Air Force and others. Based on North American's F-86 Sabre day fighter, the F-86D had only 25 percent commonality with other Sabre variants, with a larger fuselage, larger afterburner engine, and a distinctive nose radome.

Design and Development [4]


The North American YF-95 was a development of the F-86 Sabre, the first aircraft designed around the new 2.75-inch (70 mm) “Mighty Mouse” Folding-Fin Aerial Rocket (FFAR). Begun in March 1949, the unarmed prototype, AF 50-577, first flew on 22 December 1949, piloted by North American test pilot George Welch and was the first U.S. Air Force night fighter design with only a single crewman and a single engine, a J47-GE-17 with afterburner rated at 5,425 lbf (24.1 kN) static thrust. Gun armament was eliminated in favor of a retractable under-fuselage tray carrying 24 unguided Mk.4 rockets, then considered a more effective weapon against enemy bombers than a barrage of cannon fire. A second prototype, AF 50-578, was also built, but the YF-95 nomenclature was short-lived as the design was subsequently redesignated North American YF-86D.

Rocket Tray [4]


The fuselage was wider and the airframe length increased to 40 ft 4 in (12.29 m), with a clamshell canopy, enlarged tail surfaces and AN/APG-36 all-weather radar fitted in a radome in the nose, above the intake. Later models of the F-86D received an uprated J-47-GE-33 engine rated at 5,550 lbf (24.7 kN) (from the F-86D-45 production blocks onward). A total of 2,504 D-models were built.

Operational History [4]


On 18 November 1952, F-86D, AF 51-2945, set a speed record of 698.505 mph (1,124.1 km/h). Captain J. Slade Nash flew over a three km (1.8 mi.) course at the Salton Sea in southern California at a height of only 125 ft (38 m). Another F-86D broke this world record on 16 July 1953, when Lieutenant Colonel William F. Barns, flying F-86D AF 51-6145, in the same path of the previous flight, achieved 715.697 mph (1,151.8 km/h).

Variants [4]


  • North American YF-95A (NA-164): Prototype all-weather interceptor; two built; designation changed to YF-86D.
  • North American YF-86D (NA-164): Originally designated YF-95A.
  • North American F-86D: (NA-165/173/177/190/201) Production interceptor originally designated F-95A, 2,504 built.
  • North American F-86G (NA-177): Provisional designation for F-86D variant with uprated engine and equipment changes, 406 built as F-86Ds.
  • North American YF-86K (NA-205): Basic version of F-86D intended for export with rocket tray replaced by four 20 mm cannon and simplified fire control system, two conversions.
  • North American/Fiat F-86K (NA-201/201/213/221/232/242): NATO version of F-86D; MG-4 fire control system; four 20 mm M24A1 cannon with 132 rounds per gun; APG-37 radar. 120 were built by North American, 221 were assembled by Fiat.
  • North American F-86L: Upgrade conversion of F-86D with new electronics, extended wingtips and wing leading edges, revised cockpit layout, and uprated engine; 981 converted.

Operators [4]


  • Denmark: Royal Danish Air Force. Received 59 ex-USAF F-86Ds 1958-1960; assigned to 723, 726 and 728 Squadrons.
  • France: French Air Force. Fiat built 62 F-86Ks for France (1956-1957), assigned to EC 1/13 Artois, EC 2/13 Alpes, and EC 3/13 Squadrons. Serials were 55-4814/4844, 55-4846/4865, 55-4872/4874, 55-4876/4879.
  • West Germany: German Air Force. Acquired 88 U.S. F-86Ks 22 July 1957-23 June 1958. The Ks were assigned to Jagdgeschwader 75/renamed 74.
  • Greece: Greek Air Force. Acquired 35 F-86Ds from U.S. Were received in 1961 and retired in 1967 but kept as back up until 1969. the North American F-86D was the first all weather fighter in Greek Air Force. North American F-86Ds were assigned to 337 & 343 Squadrons. Until 1964 were in natural metal. After retirement were in NATO camouflage.
  • Honduras: Honduran Air Force. Acquired Six Venezuelan F-86Ks in 1970.
  • Italy: Italian Air Force. Fiat produced 121 F-86Ks for Italy, 1955-1958. Also, 120 U.S. F-86Ks were acquired. F-86s were assigned to the AMI air groups: 6 Gruppo COT/1 Stormo, 17 Gruppo/1 Stormo, 23 Gruppo/1 Stormo, 21 Gruppo/51 Aerobrigata, 22 Gruppo/51 Aerobrigata and 12 Gruppo/4 Aerobrigata.
  • Japan: Japanese Air Self-Defense Force. Acquired 122 US F-86Ds, 1958-1961; assigned to four all-weather interceptor Hikotai, and Air Proving Ground at Gifu.
  • Netherlands: Royal Netherlands Air Force (Koninklijke Luchtmacht) (KLu). Acquired 57 U.S.-built and six Fiat-built F-86K Sabres, 1955-1956; and assigned to three squadrons, No. 700, 701 and 702. Operated until 1964.
  • Norway: Royal Norwegian Air Force. Acquired 60 U.S.-built F-86K Sabres, 1955-1956, and four Italian-assembled Fiat F-86K-models.
  • Philippines: Philippine Air Force. Acquired 20 F-86Ds, assigned to 8th Fighter Interceptor Squadron "Vampires" beginning 1960; part of the U.S. military assistance package.
  • South Korea: Republic of Korea Air Force. Acquired 40 F-86Ds, beginning 20 June 1955.
  • Republic of China (Taiwan): Republic of China Air Force.
  • Turkey: Turkish Air Force. Acquired 50 US-built F-86Ds, and 40 F-86Ks.
  • Thailand: Royal Thai Air Force. Acquired 20 F-86Ls.
  • United States: United States Air Force.
  • Venezuela: Venezuelan Air Force. Acquired 32 US-built F-86Fs, October 1955-December 1960; 1965 acquired 79 Fiat-built F-86Ks from West Germany.
  • Yugoslavia: SFR Yugoslav Air Force. Acquired 130 U.S.-made F-86Ds and operated them between 1961 and 1974.

North American F-86D-40-NA Specifications [4,5,6,7]


Type:

  • Single-seat jet-propelled fighter.

Wings:

  • Low-wing cantilever monoplane with 35° sweep-back.
  • Thin laminar-flow wing section.
  • All-metal structure of sandwich type construction in which the structural material is laminated between the inner and outer tapered skins.
  • No ribs in inboard halves of wing panels and skin is milled from 0¼-in. material at roots.
  • Auto slots on leading-edge.
  • Slotted flaps.
  • Hydraulic aileron boost.
  • Gross wing area 274 ft&Sup2; (25.4 m²)

Fuselage:

  • Oval section all-metal structure with flush-riveted stressed skin.
  • Air intake pre-positioned under nose, which closed radar scanner.[5]

Tail Unit:

  • Cantilever monoplane type.
  • All-metal structure.
  • All surfaces have 35° sweep-back.
  • Dihedral tailplane.
  • Hydraulic elevator boost.

Landing Gear:

  • Retractable tricycle type with steerable nose-wheel.
  • Hydraulic retraction.
  • Cleveland 8657 air-oil shock struts.
  • Bendix 26-in. (66 cm) magnesium wheels and Bendix rotor-disc hydraulic brakes on main wheels.
  • Track 8 ft. 3 in. (2.5 m.).

Powerplant:

  • One General Electric J-47-GE-17 axial-flow gas turbine (5,425-lb-thrust); 7,500-lb-thrust with afterburner.*
  • External long-range drop-tanks may be carried under wings outboard of landing-gear.

Accommodation:

  • Pressurized pilot's cockpit with “clamshell”[5] canopy.
  • ] canopy.
  • Pilot ejection seat.

Armament and Equipment:

  • Six 0.50-in. (12.7 mm) machine-guns in nose.
  • Provision for 16 5-in. (127 mm) rockets under wings.
  • Latest radio, radar and navigation equipment.

Dimensions: [4]

  • Span: 37 ft. 1½ in. (11.3 m).
  • Length: 40 ft. 3 in.
  • Height: 15 ft.

Weights: [4]

  • Empty weight: 13,518 lb.
  • gross weight: 19,975 lb.

Performance: [7]

  • Cruising speed: 533 mph
  • Maximum speed: 679 mph
  • Climb rate: 7,470 ft/min
  • Ceiling: 48,000 ft
  • Combat radius: 330 miles
  • Ferry range: 1,052 miles

References


  1. Shupek, John. The Skytamer Archive, photos from the Shupek Photo Collection, copyright © 1998-2019 Skytamer Images (Skytamer.com)
  2. Photos: Ron Strong, 12/2007
  3. Photos: Lt. Col. Dr. Marc Matthews, USAF (ret.), 3/15/2011
  4. Wikipedia, the free encyclopedia, North American F-86 Sabre
  5. Bridgman, Leonard. Jane's All The World's Aircraft 1950/51, Sampson Low, Marston & Company, Ltd., London, 1951, pp 262c-264c
  6. Bridgman, Leonard. Jane's All The World's Aircraft 1950/51, Sampson Low, Marston & Company, Ltd., London, 1951, pp 271c
  7. Avery, Norm, North American Aircraft 1934-1998, Volume 1, Santa Ana, CA: Narkiewicz//Thompson, 1998, ISBN 0-913322-05-9, pp 148

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