Manufacturer models Unless otherwise noted, the engines fitted are
Pratt & Whitney R-985 radials. ;Model 18A :First production model with seating for two pilots and seven or eight passengers, fitted with
Wright R-760E-2 engines of , MTOW: •
Model S18A :Version of Model 18A capable of being fitted with skis or
Edo 55-7170
floats; MTOW: ;Model A18A :Version fitted with Wright R-760E-2 engines, MTOW: Twelve aircraft built. ;Model B18S :Nine-passenger pre-World War II civil variant, served as basis for USAAF F-2 ;Model D18S :First post-World War II variant introduced in 1945, with seating for eight passengers and MTOW of , 1,035 built ;Model D18C :Variant with
Continental R9-A engines of and MTOW of , introduced in 1947, 31 built. ;Model E18S :Variant with redesigned wing and MTOW of ; 403 built ;C-45A :Eight-seat utility transport based on C18S; ;C-45C :Two Model 18S aircraft impressed into the USAAF, redesignated UC-45C in January 1943 ;C-45D :Designation given to two AT-7 aircraft converted as passenger transports during manufacture, redesignated UC-45D in January 1943 ,
Platte Valley Airpark, Hudson, Colorado, June 2007 ;C-45E :Designation given to two AT-7 and four AT-7B aircraft converted as passenger transports during manufacture, redesignated UC-45E in January 1943 ;C-45H :AT-7s and AT-11s remanufactured in the early 1950s for the USAF to similar standard as civil D18S, with no autopilot and R-985-AN-14B engines; 432 aircraft rebuilt ;TC-45H ;AT-11A :Conversion of AT-11 as navigation trainer; 36 converted at least one conversion from impressed civil B18S some transferred from USAAF C-45A stocks ;JRB-3 :Photographic version, similar to C-45B; 23 obtained, ;JRB-6 :Remanufactured JRB ;SNB-1 :Similar to AT-11; 110 built ;SNB-2 :Navigation trainer similar to AT-7, 299 built ;SNB-2C :Navigation trainer similar to AT-7C, 375 built ;SNB-2H :Ambulance conversion ;SNB-2P :Photo-reconnaissance trainer conversion ;SNB-3Q :Electronic countermeasures trainer conversion ;SNB-5 ;SNB-5P ;Expeditor 3N: navigation trainer – 88 built ;Expeditor 3NMT: 3NM converted to a transport aircraft – 67 built ;Expeditor 3NMT(Special): navigation trainer/personnel transport – 19 built ;Expeditor 3TM: transport with fittings so it could be converted to a navigation trainer – 44 built ;Expeditor 3TM(Special): modified RCAF Expeditors used overseas in conjunction with Project WPB6 – three built
Canadian Armed Forces ;CT-128 Expeditor: 1968 redesignation of existing RCAF aircraft upon
unification of the Canadian Armed Forces Brazilian Air Force designations ;U-45 :Designation for the C-45.
Royal Thai Air Force designations ;B.L.1 :() designation for the C-45B and C-45F.
Conversions ;Conrad 9800 :Modification increasing the gross weight to 9,800 pounds with a single piece windshield ;Dumod I : Executive conversion with Volpar tricycle landing gear, new wing tips, enlarged fight deck and refurbished 6–7 seat cabin with larger windows. Originally named
Infinité I. 37 converted by 1966. ;Dumod Liner :Stretched airliner conversion. Similar to Dumod I but with forward fuselage stretched by , allowing up to 15 passengers to be carried. Originally named
Infinité II. ;Hamilton Westwind :Turboprop conversions with various engines ;Hamilton Westwind II STD: Stretched conversion powered by two 840-hp
PT6As, and with accommodation for up to 17 passengers ;Hamilton Westwind III:two 579-hp
PT6A-20s or 630-hp
PT6A-27s or 630-hp
Lycoming LTS101s. ;Hamilton Westwind IV:two 570-hp
Lycoming LTP101s or 680-hp
PT6A-28s or 750-hp
PT6A-34s or 1020-hp
PT6A-45s ;PacAero Tradewind :Conversion of Beech D18S/C-45 to five- to 11-seat executive transport with single fin by
Pacific Airmotive ;Rausch Star 250 :Built as C-45F 44-47231, this aircraft was re-manufactured at Wichita by Beech in 1952, to become TC-45G 51-11544. From 1959 Rausch Engineering Inc. of South San Francisco, California, converted N8186H to tricycle undercarriage, using forward retracting main gear from a P-51 and rearward-retracting nose-leg from a T-28, adding a nose extension, rear fuselage extension, re-roofed fuselage for increased headroom and enlarged cabin windows. The modifications did not obtain FAA certification despite 58 hours of flight testing, with the aircraft eventually being broken up at Antioch, CA, in 1978. ;SFERMA-Beechcraft PD.18S :Modification of Beech 18S powered by two
Turboméca Bastan turboprops ;Volpar (Beechcraft) Model 18 :Conversion of Model 18 with nosewheel undercarriage ;Volpar (Beechcraft) Super 18: ;Volpar (Beechcraft) Turbo 18:Beech Model 18s fitted with the Volpar MkIV tricycle undercarriage and powered by two 705-hp
Garrett TPE331-1-101B turboprop engines, flat-rated to , driving
Hartzell HC-B3TN-5 three-bladed, reversible-pitch, constant-speed feathering propellers ;Volpar (Beechcraft) Turboliner II :Turboliners modified to meet
SFAR 23 ==Operators==