| AP-1 | 1937 | SEV-1XP modified as SEV-7 then as AP-1; became the prototype for the P-35; also modified P-35 for trials [NR1390] | [1] |
| EP-1 | | GUARDSMAN. Export version of P-35 ("EP" for export pursuit); diverted to USAAC as the P-43A. | |
| EP-1-106 | 1939 | GUARDSMAN. New designation of EP-1 in USAAC service (also found as DS-1, Republic Model 106 and "AP-35"!). Became RP-35A | |
| AP-2 | 1937 | Racer [R1250]; proposed as pursuit with flush, rectracting gear, lost out in 1937 competition | 1 |
| AP-2 | 1939 | XP-41; a P-35 modified with new streamlined canopy, a Wright R-1830-19 engine with a two-speed supercharger, and revised landing gear | [1] |
| AP-3 | | Pursuit proposal, an unbuilt P-35 version with liquid cooled Allison V-1710 engine, abandoned in favour of AP-4 | |
| AP-4 | 1939 | XP-43-RE LANCER. Adaptation of P-35 [NX2597]. Procured as P-43 series. | 1 |
| AP-4(A) | 1940 | YP-43 LANCER. Pre-production version of AP-4 prototype delivered in September 1940 (13 built) | |
| ? | | P-43 LANCER. Production version (80 built?). Also P-43, (R)P-43A, P-43A/B/C/D/E | |
| ? | | P-43A-1 LANCER. Production version for RAF, sent to China and India (125 built). | |
| AP-4J | 1939 | P-44-1 ROCKET proposal. 400 hp Pratt &Whitney R-2180-1; 80 ordered in Sept 13,1939 as the P-44; cancelled and transfered to P-43 | 0 |
| AP-4B | | XP-44 project; was to incorporate the R-2180 engine; cancelled | |
| AP-4C | | P-44-IV project with R-2600 engine; mockup with XR-2800; not built | |
| AP-4L | | P-44-2 WARRIOR proposal with 2000Hp R-2800-7; 200 ordered, also cancelled, and transfered to P-47B/C | 0 |
| AP-5/A | 1938 | Single seat fighter project; appears in the Sarah Clark collection and US National Archives II | 0 |
| AP-6/A | 1938 | Single seat fighter project; appears in the Sarah Clark collection and US National Archives II | 0 |
| AP-7/A | 1938 | Speed record aircraft used by Major de Seversky to establish a new transcontinental speed record [NX1384] | 1 |
| AP-8 | | Fighter proposal; never completed; formed the basis for the AP-9 | 0 |
| AP-9 | 1939 | Entrant in the 1939 Air Corps fighter competition, based on AP-8, used improved airfoil; lost to XP-39 [NX2598] | 1 |
| AP-10 | 1939 | XP-47 THUNDERBOLT. Response to AC CP 39-770; light weight fighter to be powered by Allison V-1710 liquid cooled engine. | 0 |
| ? | | XP-47A THUNDERBOLT | |
| ? | | XP-47B THUNDERBOLT | |
| ? | | P-47B THUNDERBOLT (171 built) | |
| ? | | P-47C THUNDERBOLT (154 built) | |
| AP-11 | | | |
| AP-12 | | ROCKET. R-40C specification; highly streamlined design, engine behind the cockpit, driving tractor contraprop in nose via long shaft (competitor of XP-55) | 0 |
| AP-13 | 1940 | | |
| AP-14 | | | |
| AP-15 | | | |
| AP-16a | | P-47M THUNDERBOLT. / plain "AP-16" possibly allocated to XP-47B | |
| AP-16b | 1944 | P-47N THUNDERBOLT | |
| AP-17 | | | |
| AP-18 | 1941 | XP-69. Development of AP-12; intended powerplant Wright R-2160; ordered in July 1941; scale mock-up June 1942, cancelled 1943 | 0 |
| AP-19 | 1944 | XP-72. Two built. | |
| AP-20 | | | |
| AP-21a | 1946 | Seems to be related to North American's XT-28 (XT-28 Proposal for Rep. Model AP-21a); appears in the Sara Clark collection and US National Archives II | |
| AP-22 | | JB-2 THUNDERBUG (by Willys-Overland), a copy of the Fieseler Fi.103 "V-1" flying bomb (1000 built); became KUW-1, then LTV-2 "Loon" (LTV-A-1) | |
| AP-23 | 1944 | XP-84 THUNDERJET. Includes initial designs. Three XP-84 aircraft ordered on 11 November 1944 | |
| AP-23F | | F-84C THUNDERJET variant. | |
| AP-23X | 1947 | Preliminary design for a swept-wing F-84 (March 1947); not accepted by the Air Force Material Command | 0 |
| AP-23M | 1949 | YF-96 (F-84F) THUNDERSTREAK. Final swept wing proposal; ordered as the YF-96 on the November 10, 1949 | |
| AP-23T | 1952 | YRF-84F THUNDERFLASH. | |
| AP-24 | 1945 | YOA-15 SEABEE. Aircraft developed from RC-1, powered by one 215 hp Lycoming O-425-5 engine (and not with XO-425-7) | |
| AP-25 | | | |
| AP-26 | | | |
| AP-27 | | | |
| AP-28 | | | |
| AP-29 | | | |
| AP-30 | | engineering designation for F-84? | |
| AP-31 | 1946 | XP-91 proposal for high performance research aircraft and day interceptor [MX-909]. Became the XF-91 THUNDERCEPTOR after redesign. | 2 |
| AP-31-N1 | 1949 | F-91A THUNDERCEPTOR [MX-1658] | 0 |
| AP-32 | | | |
| AP-33 | | | |
| AP-34 | | | |
| AP-35 | | | |
| AP-36 | | engineering designation for F-84? | |
| AP-37 | | engineering designation for F-84? | |
| AP-38 | | Cargo and personnel land-based transport | 0 |
| AP-39 | | | |
| AP-40 | | | |
| AP-41 | | RAINBOW. The original proposal for the XF-12, drawing dated 15.10.47 | |
| AP-42 | 1945? | Large USAF swept wing jet bomber proposal as follow-up to B-47 | 0 |
| AP-43 | | | |
| AP-44A | 1948 | Mach 3 all-weather high altitude interceptor (led to AP-57) | 0 |
| AP-45 | | | |
| AP-46 | | XF-84H (initially XF-106) THUNDERSCREECH. Development of F-84F fitted with turboprop engine and first flown 22.7.55. No production. | |
| AP-47 | 1948 | Mixed-power ground support airplane proposal | 0 |
| NP-48 | 1948 | Proposal to the U.S.Navy against F3H, closely resembling the XP-91, with butterfly tail, wing with inverse taper but without wing tanks / rocket engines | 0 |
| NP-49 | 1948 | Proposal to the U.S.Navy against F3H, same tail and wing arrangement as NP-48 but with two engines below the wing; nose partly glazed | 0 |
| NP-50 | 1948 | US Navy bomber project similar in configuration to the Skywarrior, for USN's OS-115 VA class LRSA (Long Range Special Attack) proposal | 0 |
| AP-51 | | | |
| NP-52 | 1950 | Twin-engine anti-submarine aircraft for OS-117 competition | 0 |
| AP-53 | | | |
| AP-54 | 1949 | Single engine swept wing all-weather interceptor fighter study with F-91-style wing and large tip fittings | 0 |
| AP-55 | 1950 | Twin-boom inverted V-tail lightweight fighter/interceptor project (F-91 derivative) against F-104. Several versions drawn, none built. | 0 |
| AP-56 | | | |
| AP-57 | 1951 | XF-103 AWI Interceptor proposal and full development into Mach 3 (1954). 3 prototypes ordered, one started; cancelled Aug. 1957 | 0 |
| AP-58 | | | |
| AP-59 | | | |
| AP-60 | 1949 | Four-engine turboprop aircraft – bomber variant of the Rainbow*; appears in Sara Clark | 0 |
| AP-61 | | (*could there be also a transport variant for the XC-Heavy Transport and Parasite/Missile carrier competition?) | |
| AP-62 | | | |
| AP-63 | 1951 | F-105A/B THUNDERCHIEF. Swept wing fighter-bomber. Numerous layouts before final design was chosen | |
| AP-63-5 | | F-105C THUNDERCHIEF | |
| AP-63-10 | | Two-place all-weather variant | |
| AP-63-19 | 1960 | proposal for British, French, German co-production; the British offered option of Olympus B.01.22R. Anderton states F-105D (July 1960) | |
| AP-63-19E(?) | | proposal to Canada for strike attack Interceptor Day Fighter, limited all-weather F-105 with Orenda engine | |
| AP-63-26 | | proposal to Luftwaffe for F-105D version | |
| AP 63-31 | 1957 | F-105D THUNDERCHIEF. All-weather version of F-105B, revised avionics/radar | |
| AP-63-32 | | proposal to Canada, an F-105 with advanced Iroquois engine | |
| AP 63-33 | 1957-58 | F-105E THUNDERCHIEF. Two-seat, reduced fuel version of F-105D | |
| AP-63-36 | 1958 | proposal for SR-196 Tactical Strike Reconnaissance System. Fuselage stretch may have been basis for F-105F (September 1958) | |
| AP-64 | | | |
| AP-65 | | | |
| AP-66 | | | |
| AP-67 | | | |
| AP-68 | | | |
| AP-69 | | | |
| AP-70 | | | |
| AP-71 | 1954 | RF-105B THUNDERCHIEF. Reconnaissance version | |
| AP-72 | | | |
| AP-73 | | | |
| AP-74 | | | |
| AP-75 | 1954 | Long range interceptor (LRI) project to WS-202A | 0 |
| AP-76 | 1955 | research airplane project competing with North American X-15 (Project 1226 competition; MX-1554A; Preliminary Model Specification ES-348) | 0 |
| AP-77 | | | |
| AP-78 | | | |
| AP-79 | | | |
| AP-80 | | | |
| AP-81 | | | |
| AP-82 | | | |
| AP-83 | | | |
| AP-84 | | | |
| AP-85 | 1955 | Two-seat swept-wing development of F-84F Thunderstreak | 0 |
| AP-86 | | | |
| AP-87 | | | |
| AP-88 | | | |
| AP-89 | | | |
| AP-90 | | UCX/UTX contender against the Lockheed JetStar and North American Sabreliner; was to have used a General Electric engine and a "bending" tailpipe. | 0 |
| AP-91 | | | |
| AP-92 | | | |
| AP-93 | | | |
| AP-94 | | | |
| AP-95 | | Air-to-Surface ballistic Missile (to fit in F-105 weapons bay) | |
| AP-96 | | Man-in-Space vehicle, proposed to Air Force | |
| AP-97 | | | |
| AP-98 | | | |
| AP-99 | | Strategic air-to-surface ballistic missile | |
| AP-100/A | 1959 | Large V/STOL fighter-bomber proposal with three large lift fans mounted in centre of wide fuselage | 0 |
| | | | |
| AP-106 | | Parametric study for VTOL aircraft | |