| Parade Ground Aircraft | |||||||||||
| A7 | A10 | B17 | B24 | B25 | B26 | B29 | C45 | C47 | C118 | C119 | C121 |
| C123 | F15 | F16 | F82 | P38 | P47 | P51 | P63 | SR71 | T6 | T28 | T34 |
| Other USAF Aircraft | |||||||||||
| Bombers | |||||||||||
| B1 | B2 | B45 | B47 | B50 | B52 | B58 | F111 | - | - | - | - |
| Cargo, VIP, & Tanker | |||||||||||
| C5 | C17 | C21 | C24 | C46 | C97 | C130 | C133 | C140 | C141 | KC10 | KC135 |
| Experimental & Prototype | |||||||||||
| D558 | F107 | X1 | X2 | X3 | X4 | X5 | X15 | XB70 | YC14 | - | - |
| Fighters | |||||||||||
| A1 | F4 | F5 | F22 | F84 | F84F | F86 | F86D | F100 | F101 | F102 | F104 |
| F105 | F106 | F117 | P40 | P80 | - | - | - | - | - | - | - |
| Helicopters | |||||||||||
| CH3E | CH21 | CH54A | H5A | HH43 | MH60 | R4B | R6A | UH1P | UH13 | UH19 | V22 |
| Reconnaissance | |||||||||||
| E3 | O1G | OV2 | OV10 | RF4 | RF101 | U2 | - | - | - | - | - |
| Trainers | |||||||||||
| T6A | T33 | T37 | T38 | T41 | - | - | - | - | - | - | - |
North American F-107A

The F-107A was originally designed as a tactical fighter-bomber version of the F-100, with a recessed weapon bay under the fuselage. However, extensive design changes resulted in its redesignation from F-100B to F-107A before the first prototype flew. Special features included an all-moving vertical fin; a control system which permitted the plane to roll at supersonic speeds; and a system (Variable Area Inlet Duct) which automatically controlled the amount of air fed to the jet engine. On Sept. 10, 1956, the No. 1 F-107A made its initial flight, attaining Mach 1.03 (The speed of sound, Mach 1, is about 760 mph at sea level). The aircraft first achieved Mach 2 (twice the speed of sound) in tests on Nov. 3, 1956. Three F-107As were built as prototypes and were test flown extensively, but the aircraft did not go into production, the Republic F-105 having been selected as the standard fighter-bomber for the Tactical Air Command. In late 1957, Nos. 1 and 3 were leased to the National Advisory Committee for Aeronautics (NACA) for high-speed flight research.
SPECIFICATIONS Span: 36 ft. 7 in. Length: 60 ft. 10 in. Height: 19 ft. 8 in. Weight: 41,537 lbs. max. Armament: Four 20mm cannons, 108 2.75 in. rockets and up to 4,000 lbs. of bombs Engine: Pratt & Whitney J75 of 23,500 lbs. thrust (with afterburner) Crew: One
PERFORMANCE Maximum speed: Mach 2-plus Cruising speed: 600 mph. Range: 1,570 miles Service Ceiling: 48,000 ft.




| Parade Ground Aircraft | |||||||||||
| A7 | A10 | B17 | B24 | B25 | B26 | B29 | C45 | C47 | C118 | C119 | C121 |
| C123 | F15 | F16 | F82 | P38 | P47 | P51 | P63 | SR71 | T6 | T28 | T34 |
| Other USAF Aircraft | |||||||||||
| Bombers | |||||||||||
| B1 | B2 | B45 | B47 | B50 | B52 | B58 | F111 | - | - | - | - |
| Cargo, VIP, & Tanker | |||||||||||
| C5 | C17 | C21 | C24 | C46 | C97 | C130 | C133 | C140 | C141 | KC10 | KC135 |
| Experimental & Prototype | |||||||||||
| D558 | F107 | X1 | X2 | X3 | X4 | X5 | X15 | XB70 | YC14 | - | - |
| Fighters | |||||||||||
| A1 | F4 | F5 | F22 | F84 | F84F | F86 | F86D | F100 | F101 | F102 | F104 |
| F105 | F106 | F117 | P40 | P80 | - | - | - | - | - | - | - |
| Helicopters | |||||||||||
| CH3E | CH21 | CH54A | H5A | HH43 | MH60 | R4B | R6A | UH1P | UH13 | UH19 | V22 |
| Reconnaissance | |||||||||||
| E3 | O1G | OV2 | OV10 | RF4 | RF101 | U2 | - | - | - | - | - |
| Trainers | |||||||||||
| T6A | T33 | T37 | T38 | T41 | - | - | - | - | - | - | - |