Société des Avions Caudron/Caudron-Renault Aircraft Designations
Caudron 'C' Numbers Designations
C.02 - 1917 Single-seat high-altitude biplane fighter, span 6.425 m
- C.02: Nov 1917, 1 x 120 hp Le Rhône 9Jb rotary engine
- C.02: 1918, 1 x 150 hp Gnome 9N, 1 x 180 hp Le Rhône 9R rotary
C.17 - 1927 2-seat observation sesquiplane, span 14.50 m
- C.17 A2: 1 x 450 hp Lorraine 12E
Courlis, unarmed, x 6
-- Caudron's licensed-built 1923 Descamps-Brunet DB-17*
-- * Presumably explaining C.17 numerical designation
-- aka C.170
18
19
C.20 - 1917 single-seat army cooperation aircraft/light bomber
- C.20: 1 x 180 hp Gnome
Monosoupape rotary
C.21 - 1917 twin-engined multi-purpose biplane, span 13.50 m
- C.21 : Nov 1917, 2 x 80 hp Le Rhône 9C rotary
- C.21bis: 1919 1+3-seat airliner devel., x 1
C.22 - 1917 twin-engined two-seat light bomber, span 16.54 m, x 1
- C.22: 2 x 120 hp Le Rhône 9Jb or 130 hp Clerget 9B rotaries
-- C.22 was a scaled-up C.21, considered underpowered, no prod'n
C.23 - 1918 2-seat biplane light bomber (C.23 BN2), x 54
- C.23 : 2 x 260 hp Salmson CU 9Z, span 24.50 m
- C.23 : Postwar commercial mod, 12 pax, open cockpit
- C.23bis: Enclosed-cabin devel. of commerical C.23
24
C.25 - 1919 3-engined biplane 2+16 airliner, span 25.00 m
- C.25: 3 x Salmson 9Z, built but not flown, C.23 deriv.
C.26 - [Project] 1919 B.3 (3-seat day bomber) contender
--
http://www.secretprojects.co.uk/forum/index.php?topic=22273.0
C.27 - 1922 2-seat, 2-bay biplane trainer/tourer, span 12 m
- C.27 : 1 x 80 hp Le Rhône 9C rotary, Paul Deville design
-- To 1923 EP.2 contest, 39 x licensed C.27 for Turkish AF
- C.27bis: (??)
- C.27ter: (??)
--
https://www.flightglobal.com/pdfarchive/view/1922/1922 - 0765.html
28
29
30
C.31 - [Project] 1919 twin-engined 4-seat biplane tourer
32
C.33 - 1919 Twin-engined biplane 1+3-pax airliner, span 15.50 m
- C.33: 2 x 80 hp Le Rhône 9C, aka '
Landaulet Monsieur-Madame'
C.34 - [Project] 1920 3-seat recce/bomber, C.33 deriv.
- C.34: Submitted as contender for 1920 A.3/B.3 contests
C.35 - 19?? 4-seat light transport biplane, C.33 deriv.
- C.35: As C.33 (qv) except 2 x 60 hp Le Rhône 9Z rotaries
36
C.37 - 1920 trimotor 3-bay biplane 2+6 transport,span: 17.00 m
- C.37: 3 x 80 hp Le Rhône 9C rotaries, related to larger C.39
38
C.39 - 1921 3-engined biplane 2+6 civil transport a/c, x 1
- C.39: 3 x 130 hp Clerget 9B rotaries, span 20.92 m
-- * On wheels (4 pax on floats), Philippe Deville design
40
C.41 - 1922 4-seat biplane tourer, C.33 derivative
- C.41: 2 x Anzani radials
42
C.43 - 1921 5-engined 2+8 pax airliner, span 20.92 m, x 1
- C.43: 5 x 80 hp Le Rhône 9C (1 nose + 2 x push/pull pairs)
-- C.43 flown on wheeled undercarriage and twin float gear
-- C.43 was essentially a 5-engined vers. of 3-engined C.39
44
C.45 - 1922 2-seat colonial aircraft (To.2) contestant
46
47
48
C.49 - Trimotor 6-seat biplane light transport, C.39 deriv.
50
C.51 - 1921 biplane floatplane, 1 x Clerget (example: F-AIBL), x 1
--
https://www.flightglobal.com/FlightPDFArchive/1921/1921 - 0276.PDF
52
C.53 - [Project] 1921 2-seat night bomber, for BN.2 contest
- C.53: 4 x 260 hp Salmson CM9
54
C.55 - [Project] 1920 2-seat four-engined A.2 contender, C.53 deriv.
56
C.57 - 1921 2-seat biplane tourer, 1 x 130 hp Clerget, C.51 deriv.
- C.57: eg 5044.3 (F-AEAA) and 5045.2 (F-ADFV) and
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg287847.html#msg287847
58
C.59 - 1922 Single-engine 2-seat biplane scout/trainer aircraft
- C.59 : 1 x Hispano-Suiza 8Ab V-8 engine, ~1800+
- C.59/2: ET.2 trainer, 1 x 230 hp Lorraine 7Ma
Mizar, 1 x prototype
--
https://www.flightglobal.com/pdfarchive/view/1922/1922 - 0765.html
C.60 - 1921-1922 2-seat biplane scout/trainer, span 10.24 m
- C.60: Improved C.59, 1 × 130 hp Clerget 9B rotary engine
-- Exported, 36 x licensed-built by VL for Finnish AF
- C.60
??: Variant/re-engined with 230 hp radial (Salmson?)*
-- *
http://fandavion.free.fr/caudron.htm
C.61 - 1921 3-bay biplane 3-engined 6-8 pax airliner, span 24.14 m, x 12
- C.61 : 3 x 180 hp Hispano-Suiza 8Ac V-8, x 11 (8 x conv. to C.61bis)
--
https://www.flightglobal.com/pdfarchive/view/1923/1923 - 0004.html
- C.61bis: 1924-25 mod to wing-mounted Salmson CM9s, 9/5365 poss new-build
-- C.61bis conv's: 3/502, 5/5307, 6/5308, 9/5365, 9/5365, 1/5377, 2/5378
- C.61 :
?? [Project] Single-engined version
62
63
C.64 - 1922 2-seat biplane basic trainer, enlarged C.51 derivative
C.65 - 1922 Floatplane tourer biplane, 1 x 135 hp Clerget rotary, x 1
--
https://www.flightglobal.com/pdfarchive/view/1922/1922 - 0167.html
C.66 - 1922 Touring floatplane biplane, 1 x 140 hp HS 8Ab, x 1
--
https://www.flightglobal.com/pdfarchive/view/1922/1922 - 0167.html
C.67 - 1922 Single-seat light biplane, span 5.80 m
- C.67: Open cockpit, 1 x 25 hp Anzani 3-cyl, x 1
--
http://www.airwar.ru/image/idop/law1/c67/c67-1.gif
--
https://www.flightglobal.com/pdfarchive/view/1923/1923 - 0003.html
C.68 - 1922 2-seat biplane tourer, folding wings, span 7.65 m
- C.68 : 1 x 50 hp (60 hp?) Anzani 6-cylinder radial, x 4 (?)
- C.68bis: (??) no details - but five C.68s on French registery
-- 3094 F-ESAA, 6/3498 F-AFFH, 1/5148 F-AEIM, 2/5194 F-AEIL, 7/5363 F-AFFQ
69
70
C.71 - [Project] 1922 Transport, 4 x 180 hp HS 8Ab V-8s
C.72 - [Project] 1922 Transport, 4 x 180 hp HS 8Ab V-8s
73
C.74 - 1922 4-engined biplane 10-seat airliner, span 25 m, x 1
- C.74: 4 x 300 hp HS 8Fb push/pull V-8s, Paul Deville design
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg222899.html#msg222899
C.75 - [Project] 1923 trimotor transport biplane
- C.75: 3 x 240 hp Lorraine-Dietrich 8 Bb water-cooled V-8s
76
C.77 - 1923 single-seat basic trainer, variant of the C.59
- C.77: Intended for 1923 ET.1 competition
78
C.79 - 1923 single seat basic trainer, for ET.1
- C.79: Also intended for 1923 Coupe Michelin
C.80 - 192? 2-seat biplane trainer
- C.80: Intended for Spain and Argentina
C.81 - 1923 trimotor airliner, C.61 deriv., span 26.30 m, x 4 (5)*
– C.81: 1 x 400 hp Lorraine-Dietrich 12Db, 2 x 200 hp Salmson CM9
-- * At least one C.81 (F-AFBX, 5/5308) was conv. from a C.61
- C.81FR: 'Franco-roumaine' C-61a variant with diff. engine power
-- C.81FR: 1 x 370 hp LD 12D and 2 x 260 hp Salmson radials
- C.81
??: Poss. vers. with 380 hp Gnome-Rhône 9A Jupiter radials
-- **
http://gallica.bnf.fr/ark:/12148/bpt6k65555692/f53.highres
C.82 - 1924 trimotor passenger a/c, (poss. confusion with C.81?)
- C.82: 1 x Hispano-Suiza and 2 x Salmson CM9
C.83 - [Project] 1924 C.61 deriv., 1 x Salmson 508 (?), 2 x Salmson 260
- C.83: Designed for 1923 airliner/transport contest
84
C.85 - 192? 2-seat biplane tourer, derived from C.59
- C.85: 1 x 130 hp Clerget 9 Ba 9-cylinder rotary
86
C.87 - 1924 experimental single-engined pusher floatplane, F-ESAC
--
http://www.avions-bateaux.com/uploa...duit_178_59fa7e2e8ca255b10933e33707701f65.pdf
88
89
90
C.91 - 1923 biplane 1+4 pax cabin transport, span
?? m
- C.91 : (As 1st flown) 1 x 300 hp Renault 12F V-12
--
http://gallica.bnf.fr/ark:/12148/bpt6k65555692/f53.highres
- C.91bis: 1925 re-engining with 1 x 370 hp Lorraine 12D
C.92 - 1926 Passenger transport, 1 x 400 hp Lorraine-Dietrich 12 Db
- C.92: c/n 5499.1 (F-ESAC/F-AICY), discarded 7/1934
C.93 - 1923 4-seat light transport biplane a/c
- C.93: 1 x 300 hp Lorraine-Dietrich 12 Fe
C.94 - 192? biplane cabin transport, C.91 deriv.
- C.94: 1 x 400 hp Gnome-Rhône 9A
Jupiter radial
C.95 - [Project] 1924 2-seat military biplane trainer
- C.95: For 1924 ET.2 contest, derived from C.91
96
C.97 - 1924 2-seat biplane trainer, for Bolivian use
– C.97: 1 x 150 hp* or 180 hp Hispano-Suiza 8Ab V-8
-- *
http://gallica.bnf.fr/ark:/12148/bpt6k65554867/f170.highres
--
http://gallica.bnf.fr/ark:/12148/bpt6k6568021q/f22.highres
C.98 - Biplane racer, C.91 deriv., intended for Coupe Zenith
- C.98: 1 x 230 hp Salmson 9 Ab 9-cyl air-cooled radial
C.99 - 1924 2-seat observation-bomber for 1923 A.2 competition
- C.99: 1 x 450 hp Hispano-Suiza (
?? 12Ha type
??)
-- NB: Flight identifies C.99 as "a two-seater fighter"
--
https://www.flightglobal.com/pdfarchive/view/1924/1924 - 0786.html
100
C.101 - 1925 3-seat recce sesquiplane, to R.3 requirement
- C.101 : 1 x 450 hp Hispano-Suiza, span 14.56 m
- C.101GR: 'Grande reconnaissance' variant
C.102 - (??) possibly a C.101 development
C.103 - 1925 3-seat recce biplane, to R.3 requirement
– C.103: 1 x 450 hp Lorraine 12Db W-12, span 14.56 m
C.104 - 1925 3-seat recce biplane, to R.3 requirement*
- C.104: 1 x 420 hp G&R 9Ab Jupiter, span 14.56 m
- C.104 GR: 'Grand Raid', long-distance version
--
https://www.flightglobal.com/pdfarchive/view/1926/1926 - 0878.html
-- * Flight described C.104 as a "two-seater fighter"
--
https://www.flightglobal.com/pdfarchive/view/1926/1926 - 0974.html
C.105 - 1919 long-range a/c, 1 x 450 hp Renault 12 Ja*
-- *
Hydroretro lists 480 hp Renault type 12 Hd engine
C.106 - 1919 long-range a/c, 1 x 450 hp Renault 12 Ja*
-- *
Hydroretro lists 480 hp Renault type 12 Hd engine
C.107 - 1925 3-seat recce sesquiplane, to R.3 requirement
- C.107: 1 x 500 hp Salmson 18Cmb* engine, span 14.56 m
-- * Salmson 18Cmb was an 18-cyl water-cooled radial engine
108
C.109 - 1925 2-seat parasol trainer/tourer, span 11.50 m
- C.109: 1 x 40 hp Salmson 9Ad 9-cyl. radial, x 24
-- At least 1 x C.59 (c/n 400) rebuilt as C.109 (18/6221)
- C.109/1: eg F-AIQG, F-AIQO (8/6193, F-AITI, x 14
- C.109/1 raid: 1928 F-AISC (9/6194) long-range mod.
- C.109/2: C.109 re-engined with 85 hp Salmson 5Aq 5-cyl
--
https://www.flightglobal.com/pdfarchive/view/1925/1925 - 0520.html
C.110 - 1928 2-seat parasol trainer/utility, span 11.50 m
- C.110: 1 x 60 hp Salmson 5Ac 5-cyl radial, x 2
111
C.112 - 1928 2-seat parasol trainer/tourer, C.109 deriv.
- C.112: 1 x 80 hp Blackburn
Cirrus II or 50 hp Anzani
C.113 - 1928 2-seat parasol tourer, span 11.50 m, x 1
- C.113: 1 x 60 hp Anzani 6A-3 radial, C.110 deriv.
--
https://www.aviafrance.com/caudron-c-113-aviation-france-10201.htm
C.114 - 2-seat parasol tourer, C.109 deriv with Anzani 6-cyl. radial
-- F-AITI
https://www.flightglobal.com/pdfarchive/view/1928/1928 - 0854.html
115
C.116 - 1929 3-seat parasol-wing floatplane tourer version of C.109
- C.116: 1 x 95 hp Salmson 7 Ac 7- cylinder radial engine
C.117 - 1929 2-seat parasol tourer, C.109 deriv.
- C.117: 1 x 60 hp Salmson radial, span 11.50 m
118
119
120
121
122
123
124
C.125 - 1925 Biplane tourer deriv. from C.27, span 12.00 m, x 1
- C.125: Prototype only, 1 x 130 hp Clerget 9B rotary engine*
--
Wikipedia says "several" C.125 convers. from C.27 standard
C.126 - 1926 2-seat biplane tourer, deriv. from C.27, span 12.00 m
- C.116: 1 x 150 hp Clerget 9 Bd rotary, , C.126 led to C.127 & C.128
C.127 - 1924 2-seat biplane tourer, deriv. from C.27, span 12.00 m
- C.127: 1 x 80 hp Le Rhône 9C rotary or 120 hp Salmson *
-- *
http://gallica.bnf.fr/ark:/12148/bpt6k65554867/f170.highres
C.128 - 1925 biplane tourer deriv. from C.27/C.127, span 12.00 m, x 5
- C.128 : Slightly enlarged, 1 x 120 hp Salmson 9AC 9-cyl radial
- C.128bis: (
??) Poss 3-seat version of C.128
- C.128/2 : 1930 aerobatic biplane
C.129 - 19?? 2-seat biplane tourer deriv. from C.128, span 12.00 m
- C.129: 1 x 90 hp Anzani 10C 10-cyl radial engine
130
C.140 - 1928 tandem 2-seat sesquiplane liaison/observation trainer, x 1
- C.140: 1 x 230 hp Salmson 9Ab, span 11.30 m, Paul Deville design
C.141 - C.140 deriv., 1 x 230 hp Lorraine 7Ma
Mizar 7-cyl radial
150
C.154 - 1928 2-seat biplane trainer, some were C.59 conver., x 4 (?)
- C.154: F-AJOT & F-AJYT; C.59 conversions were F-AJMU & F-AJOS
C.155 - 1929 C.154 deriv. 2-seat sporting biplane, x 1 (?)
- C.155: 1 x 230 hp Lorraine 7Mc
Mizar, span (??) m
-- 6189.1 registered F-AIYY, 1929
156
C.157 - 1924 2-seat biplane trainer, some were conver.,* x 9 (?)
- C.157: 1 x 90 hp Anzani 6-cyl radial, span 10.24 m
-- * Caudron C.157 converted to C.59, C.320, and C.490 standards
C.158 - 1925 biplane trainer, 1 x Salmson 9AB radial
C.159 - 1924 2-seat biplane trainer, some were conver.,* x 2 (?)
- C.159: 1 x 230 hp Salmson 9Ab radial, span 10.24 m
-- * C.159 6174.2, F-AINA conv. to C.59, C.320, back to C.59
C.160 - 1926 2-seat biplane trainer, enlarged C.68
- C.160: 1 x by one 65 hp Salmson 5Ac 5-cyl radial
C.161 - 1927 2-seat wooden tourer, prototype only? *
– C.161: 1 x 60 hp Salmson 5Ac radial, span 9.00 m
-- * 1 x C.161 on French registry - c/n 5967.1 F-AIPV
162
163
164
C.165 - 1924 2-seat biplane tourer, C.68 derivative
- C.165: 1 x 70 hp Anzani 6-cyl two-row radial engine
166
167
C.168 - 1927 2-seat folding-wing biplane tourer/trainer
– C.168: 1 x 70 hp Anzani 6-cylinder radial, span 9.00 m
--
http://gallica.bnf.fr/ark:/12148/bpt6k65554867/f170.highres
-- NB:
Wikipedia mistakenly lists C.168 as C.61 airliner deriv.
C.169 - [Project] 1928 2-seat biplane tourer, C.68 deriv.
- C.165: 1 x 65 hp Salmson 5 Ac 5-cylinder radial engine
C.170 - See C.17
171
C.172 - 1928 2-seat observation biplane, C.17/C.170 deriv.
- C.172: 1 x 450 hp Lorraine 12Eb
Courlis water-cooled W-12
C.180 - 1930 trimotor* high-winged monoplane transport, x 1
- C.180: Metal constr., also submitted as colonial police a/c
-- * 3 x 300 hp Lorraine 9N
Algol 9-cyl radial, span 14.60 m
C.181 - 1931 trimotor colonial aircraft
- C.181: 3 x 300 hp Gnome-Rhône 7K
Titan Major radials
182
C.183 - 1923 trimotor biplane transport, span 26.30 m, x 2
- C.183: 1 x 550 hp Salmson CM19, 2 x 260 hp Salmsom CM9
-- C.183 was a C.61 deriv., 1 (c/n 5416) was a C.81 conv.
184
185
186
C.187 - 1923 biplane transport a/c developed from C.183, x 1
- C.187: Passenger transport, airframe modified from C.83
C.190 - 1928 2-seat, low-wing sport monoplane, span 11.50 m
- C.190: 1 x 80 hp Renault or 90 hp Aviation Michel*
-- * Presum. Aviation Michel A.M.14 Type I air-cooled 4-cyl
- C.191: 1928, 1 x 95 hp Salmson 7Ac,** 1 x prototype
-- **
Hydroretro lists as 90 hp Renault 4 Pa inline
-- pg 27
http://www.hydroretro.net/etudegh/renault.pdf
- C.192: 1 x 95 hp Salmson 7Ac radial, 1 x prototype
- C.193: 1929, 1 x 95 hp Renault 4Pb inline, x 6
-- 2 x C.193 mod. into Odier-Bessière
Clinogyre
--
http://www.secretprojects.co.uk/forum/index.php/topic,19577.msg189157.html#msg189157
- C.194 - (??) hypothetical designation
C.195 - 1930 low-wing monoplane trainer/tourer
- C.195: 1 x (??) hp Renault 4P (??), span 11.50 m
-- F-AJS(?) reg. suggest poss. C.193 conversion
--
http://aviadejavu.ru/Images6/FT/FT1930/12/1508-2.jpg
C.200 - [Project] 1930 single-engine high-wing tourer
210
C.220 - 1929 2-seat biplane trainer/tourer, span 9.90 m
- C.220: 1 x 95 hp Salmson 9Ac radial, wooden constr'n
C.221 - 1929 2-seat biplane trainer/tourer, span 9.90 m
- C.220 : 1 x 105 hp Lorraine-Dietrich 5Pb 5-cyl. radial
- C.221/2:
C.230 - 1930 2-seat biplane tourer, C.59 deriv., x 15
- C.230: 1 x 95 hp Salmson 7Ac radial, span 9.90 m
–- Different engines resulted in fresh designations
C.231 - 1930 2-seat biplane tourer, C.230 deriv.
- C.231: 1 x Lorraine (poss. 100 hp 5P as per C.221)
C.232 - 1931 2-seat biplane tourer, span 11.00 m, x 50
– C.232 : 1 x 95 hp Renault 4Pb, wooden construction
- C.232/2: As C.232 with added wheel brakes, x 3
- C.232/3: (
??) hypothetical designation
- C.232/4: Improved C.232/2, x 7
C.233 - Experimental engine testbed, c/n 15 F-AIKD, x 1
- C.233: 1 x 100 hp Michel 4a (poss. A.M.14 Type II?)*
-- * NB: Aviation Michel A.M.4a was 25 hp boat engine
C.234 -
no details
-- 6535.4 register F-ALDG
--
http://www.airhistory.org.uk/gy/reg_F-8.html
C.235 - C.230 testbed variant for Ministere de l'Air, x 1
- C.235: 1 x 150 hp Argus As 8R inverted V-8, span 12.70 m
C.240 - 1931 low-wing monoplane cabin tourer, x 1
- C.240: 1 x 120 hp Salmson 9Ac radial, span 15.00 m
- C.240: 1+3 pax, mixed constr., no customers found
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg179991.html#msg179991
C.250 - 193? 2-seat biplane trainer, prototype (
?)
- C.250: Poss. modified into sole C.251 (
confirm?)
-- Wind tunnel model tested, photo in TU issue 174
- C.250: 1 x (??) radial, span 10.24 m
--
https://commons.wikimedia.org/wiki/File:Caudron_C.250_wind_tunnel_model_Annuaire_de_L'Aéronautique_1931.jpg
C.251 - 1931 2-seat military training biplane, span 10.24 m, x 1
- C.251: 1 x 240 hp Lorraine 7Me
Mizair, to 1929 EP.2 contest*
-- * Military trainer to replace in-service Caudron C.59
--
http://gallica.bnf.fr/ark:/12148/bpt6k6554809h/f7.highres
260 - Poss. holding designation for Abrial A-260 project*
-- * Abrial A-260 was to be built by Caudron
--
http://www.secretprojects.co.uk/forum/index.php?topic=20862.0
C.270
Luciole - 1931 biplane tourer, various engine types
- C.270/1: [Project] 1934 biplane tourer, 105 hp Salmson 7Aca
- C.271 :
Luciole tourer variants with Lorraine engines
-- C.271/2: Biplane tourer, 1 x 110 hp Lorraine 5Pb, x 5
-- C.271/3: [Project] 1936 biplane, 1 x 110 hp Lorraine 5Pb
- C.272 :
Luciole tourer variants with Renault engines
-- C.272 : 1931 tourer, 95 hp Renault 4Pb
Bengali, x 52
-- C.272/2: 1933 trainer, 1 x 120 hp Renault 4Pei, x 22
-- C.272/3: 1933 trainer, 1 x Renault 4Pdi
Bengali, x 15
-- C.272/4: 1933 trainer, 1 x Renault 4Pei
Bengali, x 21
-- C.272/5: 1935 trainer, 1 x Renault 4Pgi
Bengali, x 80
- C.273 : 1931
Luciole trainer, 1 x Michel Type R,* x 14
-- * 100 hp Aviation Michel R At-3 (
any details on this?)
- C.274 : 1932 trainer, 1 x 120 hp Chaise Type H, x 1
- C.275 : 1936
Luciole trainer, 1 x Renault 4Pgi, x 433
-- NB: C.275 variants lacked the C.270's folding wings
-- C.275/1: 1937 trainer, 1 x Renault 4Pdi
Bengali, x 1
-- C.275R : 1945 trainer/tourer, 1 x Renault 4Pgi, x 1
- C.276 : 1932
Luciole trainer, 1 x DH
Gipsy III, x 7
-- C.276H: 1956 cabin tourer, 1 x Hirth HM 504, x 2
- C.277 - 1939
Luciole trainer, 1 x Renault 4Pei,** x 9
-- ** Some sources say 140 hp Renault 4Po3 engine
-- NB: C.277 vers. was C.272 without folding wing
-- C.277R: 1949 C.275 conversion to 1 x Renault Po3
- C.278 :
Luciole trainer, 1 x Salmson 9Ne, x 1
C.280 - 1932
Phalène high-wing monoplane utility aircraft
- C.280 : Prototypes, 1 x DH
Gipsy II inline, x 5
- C.280/2: 4-seat light tourer, Renault 4Pdi engine, x 21
- C.280/4:
Super Phalène, dual controls, auto slots/flaps, x 9
- C.280/6: 1933, 1 x 135 hp Salmson 9Nc 9-cyl radial, x 1
- C.280/9: Fuselage lengthened by 20cm, x 3
C.281 - (
??)
Phalène high-wing cabin monoplane
C.282 - 1932
Phalène cabin monoplane, C.280/4 deriv.
- C.282/1 : 1 x DH
Gipsy Major 4-cyl. inline, x 11
- C.282/2 :
Phalène IV, 1 x Renault 4Pdi
Bengali, x 10
- C.282/3 : As C.282/2, reduce fuel capacity, x 1
- C.282/4 :
Super Phalène, smaller airframe, dual control,
-- C.282/4 also featured automatic slots & flaps, x 9
- C.282/5 :
- C.282/6 :
- C.282/7 : 1 x Renault 4Pdi
- C.282/8 : 1933 defin. vers., 145 hp Renault 4Pdi, 89 + (3)
-- C.282/8 had longer fuselage, more fuel, and a tailwheel
- C.282/8-III :
- C.282/9 : 1 x Renault 4Pei, x 2
- C.282/10: Renault 4Pei, Merville 601 propeller* x 4**
-- * Replacing Merville Series 496 on earlier versions
-- ** Some sources claim that 11 x C.282/10 were built
283
C.284 - 1933
Phalène cabin monoplane, 1 x 135 hp Chaise 4*
-- OMI-built Chaise 4-Ba 4-cyl. was ultimately unsuccessful
C.285 - [Project] 1933 C.280 deriv., 1 x 120 hp Salmson 9Ac radial
C.286 -
Super Phalène high-wing cabin monoplane
- C.286 : DH
Gipsy III, redesig. vertical tail, x 1
- C.286/2 : 1933, 1 x Renault 4Pdi, rounded wingtips
-- 12 x C.286/2 (including x 10 conversions)
- C.286/2-S4 : 'Special', luxury vers. C.286/2
-- C.286/2-S4: 120 hp DH
Gipsy Major I, x 10
- C.286/3 : 1 x 120 hp DH
Gipsy Major I, x 1
- C.286/3-S4 : 'Special', luxury vers. C.286/3
- C.286/4 : C.280/6-style tail, DH
Gipsy Major I, x 5
- C.286/5 : 135 hp DH
Gipsy III, automatic slats, x 1
-- C.286/5 also had tailwheel and revised horiz. tail
- C.286/6 : DH
Gipsy Major I, Merville 501 prop, x 5
- C.286/7 : As C.286/6 except Ratier 1175 v-p prop, x 8
- C.286/8 - Longer C.280/9-type fuselage, C.286 tail
-- C.286/8 had 1 x 120 hp DH Gipsy Major I, x 4
- C.286/9 : Standard fuselage, DH
Gipsy Major III, x 1
287
288
C.289 - 1933
Phalène high-wing cabin monoplane, x 6 (?)
- C.289/1:
- C.289/2: 1 x 150 hp Hispano-Suiza 5Q radial, x 1
-- C.289/2 had C.286/9 structure with C.286 tail
- C.289/9: 1 x 120 hp Renault 4Pdi,* C.280/6 tail, x 5
-- *
Avia France has C.289/9 with 150 hp HS 5Q radial
290
300 -- Poss. not used to avoid confusion with R.300
-- [Project] 1931 OMI R.300 Coupe Deutch racing a/c*
-- R.300: 1 x 320 hp OMI Chaise 8C flat HO-8 engine
-- * Single-seat, mid-winged monoplane, span 6.20 m
-- Marcel Riffard & Georges Otfinovsky desig. R.300**
-- ** Prior to Riffard/Otfinovsky moving to Caudron
-- aka MR.300 (but
not 'CR.300')
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg92554.html#msg92554
--
http://www.secretprojects.co.uk/forum/index.php/topic,15856.msg213280.html#msg213280
310
C.320 - 1932 biplane trainer, rebuilt C.59s,* x 8
- C.320: 1 x250 hp Renault 9A 9-cyl, radial
-- * Or rebuilt from C.159 or C.179 airframes
330
C.340 - 1933
Micro Phalène, reduced-scale
Phalène light a/c, x 5
- C.340: Folding wings, 30 hp Chaise 4D motorcycle engine
- C.341: (??)
- C.342: (??)
- C.343: (??)
- C.344: C.340 re-engined with 1 x 40 hp Chaise 4E 2-cyl.
- C.345:
Phalène Junior, revised struts, 40 hp Train 4E, x 1
350
C.360 - 1933 low-wing monoplane racer, 1 x 170 hp Renault*
- C.360:
Atalante, longer-spanning R.300 development
-- * 4-cyl
Bengali Special, other sources say Régnier R6
361
C.362 - 1933 single-seat low-wing monoplane racer, x 2
- C.362: 1 x 170 hp Renault 4Pei
Bengali, span 6.80 m
- C.362: 7.00 m2 wings, fixed & spatted undercarriage
-- Built for the Coupe Deutch de la Meurthe 1933
C.363 - 1933 single-seat low-wing monoplane racer
- C.363: 1 x 120 hp Renault 4Pdi
Bengali 4-cyl
--
http://www.hydroretro.net/etudegh/renault.pdf
364
365
C.366 - 1933 single-seat low-wing monoplane racer, x 1
- C.366:
Atalante, 1 x 205-220 hp Régnier R6 6-cylinder
-- C.366
Atalante, came 2nd in the 1934 Coupe Deutsch
-- C.366 re-engined with Régnier
Martinet as Nennig C-3*
-- *
Have I garbled the Martinet part, was it Régnier engine??
--
http://www.secretprojects.co.uk/forum/index.php/topic,18670.msg179864.html#msg179864
C.370 - [Project] 1933) C-360 racer, 1 x Baudot
Complexe*
-- * ~600 hp liquid-cooled 32-cyl. multi-row** engine
-- ** Four rows of 8 cyl., designed by François Baudot
380
390
C.400 - 1934
Phalène, military desig. for C.282, x 40*
- C.400: 1 x 120 hp Renault Pdi, span 11.62 m
-- * 29 of 40 AdA C.400s went to Aviation Populaire
C.401 -
Phalène, higher power military liaison a/c
- C.401: 1 x 140 hp Renault Pei, span 11.62 m
C.410 -
Phalène, post-war civilian C.401 conv.
- C.401: 140 hp Renault Pei, span 11.62 m, x 11
420
C.430 - 1934
Rafale 1-2-seat tourer/racer, C.362 deriv.
- C.430: Tandem seats, 9.00 m2 low-wings, fixed/spatted u/c
- C.430: 1 x 120 hp Renault 4 Pdi, 2 x built (1 x conversion)
-- C.430 c/n 6885 (F-AMVA), c/n 6886 (F-AMVB)*
-- * Crashed 30 Nov 1934, killing Hélène Boucher
-- C.430/1: 1-seat F-AMVA conv., 180 hp Renault 438**
-- ** Oct 1934, for Coupe Deutsch de la Meurthe
--
https://www.flightglobal.com/pdfarchive/view/1934/1934
C.431 - 1979 replica of C.430/1 with 165 hp Régnier
C.432 - (??)
--
Aviocar: 'Roadable' vers. of C.432
--
http://gallica.bnf.fr/ark:/12148/bpt6k6555455p/f43.highres
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg234306.html#msg234306
C.440 - 1935
Goéland 6-seat twin-engine utility a/c, ~1702 built
- C.440: March 1935 prototype light passenger transport, x 3
-- C.440: 2 x 180 hp Renault 6Pdi
Bengali, span 17.60 m
-- C.440: Various engine installations tried, no wing diherdral
-- C.440: N° 1 prototype later converted into C.444 (qv)
- C.441: Pre-series, 3° dihedral on outer wing panels, x 4
-- C.441: To
Armee de l'air as VIP transport/liaison a/c
-- C.441: 2 x Renault 6Q-01 6-cyl inlines,* span 17.60 m
-- * Same righthand propeller rotation for both C.441 engines
-- *
hesham's source lists unhanded 220 hp 453-00
- C.442: [Project] 1935, 2 x 220 hp Renault 6Q-02/03 6-cyl.
-- C.442: Handed Renault 6Q-02/03 engines w/ superchargers
--
hesham's source lists 453-02 optimized for 2000 m
- C-443: [Project] 1935, 2 x 240 hp Renault 6Q-04 engines
-- C.443: 1st proposed Goéland vers. with handed propellers
--
hesham's source lists 453-02 optimized for 4000 m
- C.444: 1st built Goéland vers. with handed propellers
-- C.444: 2 x Renault 6Q-00/6Q-01 6-cyl.,** span 17.60 m
-- ** 220 hp usually quote
despite lacking compressors
- C.445: As per C.444 but with 4° wing dihedral, 114 x built
-- C.445/1: Civil, 2 x 200 hp Renault 6Q-10/6Q-11s, x 2
-- At least 1 x C.445/1 converted to modular C.445M std.
-- C.445/2: (Project) 1937
Super Goéland postal vers.
-- C.445/2: (Project) For Air Bleu, 2 x 360 hp Renault 456
-- C.445/2: Built transp. vers., 2 x 220 hp Renault 6Q-10/11
-- C.445/2: 3 x built (c/n 8617, 8618, and 8619)
-- C.445/3: Postwar production version, x 510
-- C.445EF: 1942-43 Vichy prod. as Luftwaffe training a/c
-- Unclear as to meaning of 'EF' designation suffix (
??)
-- C.445M : Modular-cabin militarized C.445/3,***, x 404
-- *** Unclear, 'M' for '
Modulaire' or '
Militaire'?
-- C.445R : Long-range version, fuel tanks in cabin, x 1
- C.446 : 1938
Super Goéland, higher-powered IV-12s, x 5
-- C.446
Grand Raid: 2 x 450 hp Renault 12R-00/-01s, x 1
-- C.446 (R): 2 x 600 hp (550 hp @ 4,000m) Renault 12R-02/03
-- C.446 (R): Listed as '
spéciaux' engines, reg. 420 hp
--
hesham's source lists 2 x 420 hp Renault 12R-00/01s
-- C.446 (R): Also feature '
spécial' reinforced u/c
-- C.446 (A): 2 x German 320 hp Argus As 410 IV-12 engines
--
hesham's source suggests As 410 have been sabotaged
- C.447: MedEvac vers., 4 x stretchers + 1 attendant, x 31
-- C.447 : 2 x 220 hp Renault 6Q-10/11 engines, (C.445 conv.??)
-- C.447/1: 2 x 240 hp Renault 6Q-20/21s, akin to C.449, x 10
-- C.447: aka
Goéland C (suggesting '
Goéland A'/-B'
- C.448: Trans./
Grande Tourisme, shortened span/no dihedral
-- C.448: Transport, 2 x 220 hp Renault 6Q-02 6-cyl., x 4
-- C.448-9: Poss. specific desig. for 'GT', out of sequence?
-- NB: C.448 'GT' developed in parallel with C.445R variant
- C.449: Final prod. vers., 2 x 240 hp Renault 6Qs, x 349
-- C.449/1: 1940 prod'n military transport, 295 x built
-- C.449/1: 2 x 240 hp Renault 6Q 20/21 6 cyl., span 17.60 m
-- C.449/2: (Project) Trainer, 2 x 410 hp Béarn 6D-03 6-cyl
-- C.449/2: To have reinforced u/c from C.446
Grand Raid
-- C.449/3: Lt transport vers., 2 x 240 hp Renault 6Q-20/-21
-- C.449/3: Lengthened fuselage, prototype never finished
-- C.449/4: Photo survey, 2 x 240 hp Renault 6Q-20/-21, x 8
-- C.449/4: Also '
police ccoloniale' + nav/bombing trainers
-- C.449/5: Postal variant (possibly for Air Bleu?), 7 x built
-- AA.1 : Postwar prod'n by AA (nationalized Caudron)****
-- **** Ateliers Aéronautiques d'Issy-les Molineaux
C.450 - 1934 single-engined racer based on C.362, x 1
- C.450: Single-seat, low-wing, fixed & spatted main u/c
- C.450: 1 x 330 hp Renault 433, span 6.74 m, area 700 m2
-- C.450 designed for Coupe Deutch de la Meurthe 1934
- C.450 R2: Mod. to tandem-seat speed record aircraft
C.460 - 1934
Rafale single-engined racer, C.362 deriv., x 3
- C.460 : Coupe Deutsch de la Meurthe 1934, spats, x 1
- C.460 : 1 x 360 hp Renault 456, span 6.75 m, area 7.00 m2
- C.460 R: c/n 6907 converted to fully retractable u/c, 1935
- C.461 : Flush cockpit version, 360 hp Renault 456 6-cyl., x 2
--
https://www.flightglobal.com/pdfarchive/view/1934/1934 - 0481.html
C.470 - [Project] 1938 4-engined
Goëland development
- C.470: 4 x 220 hp Renault 180 inline engines
C.480 - 1935 Frégate 5-seat high-wing cabin tourer, x 27
- C.480: 1 x 140 hp Renault 4Pei inline, span: 11.90 m
--
http://www.secretprojects.co.uk/forum/index.php/topic,18796.msg181475.html#msg181475
C.481 - 1935, (
??) poss. higher-powered
Frégate variant
- C.481: ? x 450 hp Renault Type 12R inverted V-12
- pg 19
http://www.hydroretro.net/etudegh/renault.pdf
C.490 - 1935 2-seat 2-bay biplane trainer, C.320 deriv.
- C.490: 1 x 170 hp Renault 6Pfi,* span 10.23 m, x 7
-- * C.490's
Bengali engine orig. from C.500
Simoun I
--
http://www.secretprojects.co.uk/forum/index.php/topic,15824.msg153806.html#msg153806
- C.491 - 1937 C.490 deriv, 1 x 180 hp Renault 6Pdi, span 10.23 m
- C.492 - 1935 C.320 deriv., 1 x 170 hp Renault 6Pfi, span 10.23 m, x 6
- C.493 - 1937 C.491 deriv, 1 x 180 hp Renault 6Pdi , span 10.23 m
C.500 - 1934
Simoun I prototype low-wing 4-seat cabin a/c
- C.500: 1 x 170 hp Renault 6Pfi, span 10.40 m, x 1
C.510 - 1934
Pélican 5-seat touring monoplane, x 62
- C.510: 1 x 140 hp Renault 4 Pdi Bengali 4-cyl inline
- C.511: (Project) C.510 with revised rigging* & u/c
-- * Possibly referring to wing struts, not rigging wire
C.520 - 1934
Simoun 4-seat low-wing cabin tourer, x 1
- C.520: 180 hp Renault 6Q air-cooled 6-cyl inline
C.530 - 1934
Rafale 2-seat sport/racer monoplane, x 7
- C.530: Primarily wooden const'n, fixed & spatted u/c
- C.530: 1 x 140-170 hp Renault 4Pd
Bengali Sport
- C.530: Wingspan 9.20 m, wing area 12.00 m2
-- C.530 was an enlarged version of C.430
Rafale
C.540 - (Project) monoplane racer in two versions
- C.540 : First version, based on C.500
Simoun I
- C.540 : Second version, based on C.530
Rafale
C.550 - (Project) Enlarged C.360 long-distance racer*
-- * Or a 2-seat racer variant of C.500/C.520
Simoun
- C.550: Meant for London-Melbourne race, not built
- C.550/II: Racer,
no other details
C.560 - 1935
Rafale II Coupe Deutsch racer, C.460 deriv. x 1
- C.560: 1 x 450 hp Renault 12R, span 6.67 m, area 7.00 m2
-- C.560 not ready for 1935 Coupe Deutsch race*
-- * Replaced by C.460 with 180 hp Renault 428
C.561 - 1936 single-seat Coupe Deutsch racer, C.461 deriv., x 1
- C.561: 1 x 450 hp Renault 446, span 6.67 m, area 7.00 m2
- C.561: Wood const., retract. u/c, flush cockpit
-- C.561 combine C.461 and C.560 features
C.570 - 1935
Kangourou twin-engined transport, x 1
- C.570: Military cargo transport, aka CR.570
-- aka R.570, 2 x 700 hp Renault W18 engines
--
https://www.flightglobal.com/pdfarchive/view/1936/1936 - 0645.html
C.580 - 1934 single-seat military fighter-trainer, 2 x built*
- C.580: 1 x 140 hp Renault 4Pdi,** span 7.70 m, area 9.00 m2
-- * c/ns 6939.1 (F-ANAS, see C.581) and 6940.2 (F-ANAT)
-- ** Avia France says 150 hp 4Pdi
Bengali; others say 4Pei
C.581 - 1935 Single-seat aerobatic monoplane, x 2
- C.581:
Rafale military aerobatic trainer
- C.581: 1 x 450 hp Renault 12R, span 7.70 m, area 9.00 m2
-- C.581 c/n 6939.1 (F-ANAS) converted C.580 airframe
590
C.600 - 1935
Aiglon 2-seat touring monoplane, x 178
- C.600G: 1 x DH
Gipsy Major-powered version, x 5
- C.601: Aiglon Senior, 2 x 100 hp Renault 4Pei, x 18
-- KXC: Japanese desig. for C.601 evaluated by IJN
- C.610: Single-seat long-distance 'Raid' vers., x 2
-- C.610: F-ANSK, ex-C.600, increased fuel tankage
C.620 - 1937
Simoun IV, 1 x 170 hp Renault 6Pfi, x 1
C.630 - 1935
Simoun, initial production vers., x 20
- C.630:
Simoun, 1 x 180 hp Renault 6Pdi
Bengali
- C.631:
Simoun, 1 x 220 hp Renault 6Q-01, x 3
- C.632:
Simoun, 1 x 220 hp Renault 6Q 6-cyl, x 1
-- C.632 was a long-range 'raid' vers., x 1 (F-ANXA)
- C.633:
Simoun, 1 x 220 hp Renault 6Q-07, x 6
-- C.633 had a modified fuselage
- C.634:
Simoun, 1 x Renault 6Q-01 or 6Q-09, x 3
-- C.634 had modified wing, increased take-off weight
- C.635:
Simoun, 1 x Renault 6Q-01 or 6Q-09, x 46
-- C.635 had improved cabin layout, conv. of earlier-models
-- C.635M: Mil. vers., Renault 6Q-09 or 6Q-19, x 489
C.636 - 1938 4-seat touring monoplane, C.630
Simoun deriv.
- C.636: Metal fuselage contruction (
?? monocoque ??)
C.637 - (Project) 193?, 1 x 300 hp Renault 6Q-20
- C.637: (??) C.63x
Simoun deriv./development (??)
C.638 - (Project) 193?, 1 x (??) hp Renault 6Q-20
- C.638: (??) C.63x
Simoun deriv./development (??)
C.639 - (Project)* 1943 C.635 with 240 hp Argus As 10
-- * C.639 poss. built or completed as C.635 conversion ??
--
http://www.secretprojects.co.uk/forum/index.php?topic=9932.0
C.640 - 1935
Typhon low-wing monoplane mail plane, x 7
- C.640: Single-seat, 2 x 220 hp Renault 6Q, span 11.50 m
-- Wooden constr'n, concept similar to DH-88
Comet
- C.641: 1935 single-seat record a/c, span 11.50 m, x 2
-- C.641 had raised canopy and increased fuel capacity
C.650 - [Project] 1935 3-seat fighter, C.640 derivative
--
http://www.secretprojects.co.uk/forum/index.php?topic=9932.0
C.660 - 1937
Rafale 2-seat racing monoplane, 4 x built*
- C.660: 1 x 140 hp Renault 4 Pei,** span: 9.20 m, area 9 m2
-- * At least two of the C.660s were C.530 conversions
-- ** According to
Hydroretro, others say 180 hp Renault 6
C.670 - 1937
Typhon high-speed bomber deriv., span 14.80 m
- C.670: 2 x 220 hp Renault 454, 3 x crew of three, x 1
-- Submitted for 1934 C.2/C.3/CN.2, 2 x 20 mm, 1 x 7.5 mm
--
http://www.airwar.ru/image/idop/bww2/c670/c670-1.jpg
--
http://www.secretprojects.co.uk/forum/index.php/topic,12771.msg125978.html#msg125978
C.680 - 1936
Super Rafale 2-seat sports monoplane, x 1
- C.680 : 1 x 140 hp Renault 4Pei 4-cyl., span 7.70 m, area 9 m2
- C.680-5: 1 x 220 hp Renault 6Q-03 6-cyl. engine
681
682
683
C.684 - 1936 2-seat sport monoplane, x 1
- C.684: Wooden constr., modified C.680
- C.684: 1 x 170 hp Renault 6Pfi, span 7.70 m
C.685 - 1936
Super Rafale 2-seat sport a/c, x 1
- C.685: Wooden construction, modified C.684
- C.685: 1 x 220 hp Renault 6Q, span 7.70 m, area 9 m2
C.686 - 193?
Super Rafale, C.685 mod.
- C.686 : 1 x 360 hp Renault (??), span 7.70 m, area 9 m2
- C.686: c/n 6933.4 (F-ANAM)
C.690 - 1936 fighter trainer, C.720 derivative, x 18
- C.690 : 1 x 220 hp Renault 6Q-03, span 7.70 m, area 9 m2
- C.690 : Single-seat fighter-trainer, x 4
- C.690M: Refined Armée de l'Air version, x 15
--
https://www.aviafrance.com/image.php?im=384
- C.691 : 1937 aerobatic vers. of C.690
- C.720 :
qv
692
693
694
C.695 - (Project) 1938 C.690 deriv.,
no other details
--
Le Trait d'Union no. 176
C.700 - (Project) 1935, marine C.640
Typhon derivative
C.700 - 1939 single-seat monoplane racer (
avion de course)
- C.700: 1 x 500 hp Renault 12Ro (or 12Rc) inverted V-12
-- Pg 19
http://www.hydroretro.net/etudegh/renault.pdf
C.710 - 1936 single-seat monoplane light fighter, x 3
- C.710: 1 x 500 hp Renault 12R-01 V-12, span 8.97 m
-- Submitted for 1934 C.1 fighter competition
- C.710: 2 x wing-mounted 20 mm HS-9 auto-cannons
C.711 - [Project] single-seat racer deriv. of C.710
- C.711: Longer fuselage and more powerful engine
C.712 - 1936 record-breaking C.710 derivative, x 1
- C.712: 1 x 730 hp Renault 12R special, span 8.97 m
-- aka C.712
Cyclone, aka C.712R ('R' for
Raid)
C.712 (II) - (Project) 193? 2-seat light bomber
-- C.712: aka C.712 B2, no other details
C.713 - 1937 single-seat monoplane light fighter, x 1
- C.713: C.710 with retract. u/c, to 1936 C.1 contest
- C.713: Armament, 2 x 20 mm HS-9 cannons in wings
-- C.713 considered development prototype for C.714s
--
http://www.airwar.ru/image/idop/fww2/c713/c713-1.gif
C.714 - 1938 single-seat monoplane light fighter, x 56
- C.714 : Cyclone, refined prod'n vers. of C.713 fighter
-- C.714.01: Prototype, 4 x 7.5 mm mgs in wing gondolas
- C.714R: 1 x 900 hp Renault 12R-03 inverted V-12, x 1
-- AdA desig. C.714 C1, sometimes seen as 'CR.714 C1'
C.714B - (Project) 2-seat light bomber
- C.714B: C.712 B2 derivative
C.715 - [Project] 1938 C-710 with 650 hp Renault*
-- * Some sources C.715 as orig. des. of CR.760
C.720 - 1936 single-seat fighter trainer aircraft, 1 x built
- C.720: 1 x 175 hp Renault
Bengali,* span 7.70 m, area 9 m2
-- Some sources say C.690 was derived from C.720
-- Other sources say C.720 was 2-seat C.714 deriv.
-- * C.720 planned for engines of 100 hp to 220 hp**
-- **
Hydroretro says 220 hp Renault 6Q installed
C.730 - [Project] 193? 2/3-seat fighter
-- Submitted for 1934 C.2/C.3/CN.2 competition
C.740 - (Project) 4-engined
Goéland devel.
C.750 - [Project] 4-seat vers. of C.800
Ramier tourer
- C.750: 1 x 140 hp Renault 4 Pei inverted 4-cyl.
C.760 - 1940 single-seat light fighter, C.714 deriv., x 1
- C.760: 1 x 760 hp Isotta-Fraschini
Delta RC.40 V-12
-- aka Caudron-Renault CR.760
-- 3v:
http://www.airwar.ru/image/idop/fww2/cr760/cr760-1.gif
- JN 760: 1999 replica, Ranger V-12, 'JN for builder Jean Noan
C.770 - 1940 single-seat light fighter, C.760 deriv., x 1
- C.770: 1 x 800 hp Renault-626 V-16
-- aka C.770-01 (prototype), Caudron-Renault CR.770
-- C.770/CR.770 used fuselage and tail of CR.760-03
C.780 - [Project] 1940 single-seat light fighter, C.770 deriv.
- C.780: As for C.770 except 1 x 500 hp Renault 468 V-12*
-- aka CR.780, armament 2 x 20 mm + 2-to-4 x 7.5 mm mgs
-- * Renault 468 fitted with contra-rotating propellers
C.790 - 1938 2-seat trainer, 1 x 220 hp Renault 6Q 6-cyl.
- C.790: Deriv. of single-seat C.690 fighter trainer (qv)
C.800 - (1st allocation) 1936
Ramier 2-seat tourer, x 2
- C.800
Ramier: 1 x 140 hp Renault 4 Pdi inverted 4-cyl
C.800 - 1942
Épervier 2-seat training glider, span 16.0 m
- C.800: 2 x 1942 prototypes, 302 C.800 built post-war*
-- * C.800 production was performed by Fouga
--
https://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/3vues/Caudron_C-800_Epervier_3v.jpg
- C.800: 1 x motorglider version (see 2nd C.850, below)
- C.801: 1951 improved prod'n version,
Épervier Ramier x 10
--
https://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/3vues/Caudron_C-801_3v.jpg
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg249934.html#msg249934
C.810 - (1st allocation) [Project] 1940 3-seat fighter
- C.810: 2 x Renault engines,
no other details
-- Submitted for 1934 C.2/C.3/CN.2 competition
C.810 - (2nd allocation) 1942 Colibri basic training glider
- C.810:
Colibri single-seat glider, span 14.00 m, x 1
--
https://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/3vues/Caudron_C-810_Colibri_3v.jpg
- C.811: Post-war improved C.810 single-seat glider, x 1
- C.812: [Project] Glider derived from C.811
813
814
C.815 - [Project] single-seat glider (desig. clashed with Fouga usage)
C.820 (I) - (Project) 1938 3-seat observation/utility a/c
C.820 (II) - (Project) Single-seat high-performance glider
- C.820: C.800
Épervier sailplane derivative
C.830 - [Project] 1936 trainer/army co-operation a/c (for T.3 competition)
- C.830: Prob. C.670 devel, 2 x 220 hp Renault 6Q 6-cyl, aka CR.830
--
http://www.secretprojects.co.uk/forum/index.php/topic,22273.msg248953.html#msg248953
C.830 - (Project) 1940 single-seat glider, no further details
C.840 - (Project) Aerobatic glider, developed from C.800
Épervier
C.850 - (Multiple apparent applications of this designation)
C.850 - (Project) 3-seat racer aircraft, 1 x 300 hp Renault 6Q 6-cyl
C.850 - (Project) 1937 twin-engined heavy fighter
- C.850: 2 x 450 hp* Renault 12R 00/01, span (??) m
-- * Some sources have power for 12R 00/01 as 500 hp
C.850 -
Mésange basic training glider, based on Grunau
Baby
- C.850: Built as Nord 1300
Norbaby, designation reassigned
C.850 - Motorglider development of C.800
Épervier (above), x 1
- C.850: C.800 w/ pylon-mounted pusher mounted before cockpit
C.860 - 1938 single-seat, long-range communication aircraft, x 1
- C.860: 'Grand Raids', range 7,100 km, 1 x 240 hp Renault 6Q-03
- C.860: Wooden struct., fabric-covered fuselage, span 10.40 m
--
http://gallica.bnf.fr/ark:/12148/bpt6k6554698t/f9.highres
C.870 - 1940 2-seat military advanced trainer, x 2
- C.870: 1 x 360 hp Renault 12R-09, span 10.20
C.880 - 1940 2-seat observation/artillery spotter a/c, x 2
- C.880: Monoplane of primarily wooden construction
- C.880: 1 x 220 hp Renault 6Q-01 6-cylinder, span 14.80 m
--
https://www.secretprojects.co.uk/threads/caudrons-rare-aircraft.15824/#post-187310
890
C.900 (I) - 1938 2-seat racer (biplace de course)
- C.900: 1 x 300 hp Renault 6Q air-cooled 6-cylinder
-- pg 29
http://www.hydroretro.net/etudegh/renault.pdf
C.900 (II) - (Project) 1939 twin-engined fighter studies
- C.900: 1st versions, studies for 1937 C.3 programme*
- C.900 : 1st version C1, single-seat heavy fighter
- C.900 : 1st version C2, two-seat heavy fighter
- C.900 : 2nd version, 2 x 1,200 hp I-F
Zeta X-24*
-- * Some sources say 1,250 hp (sic)
Zeta RC.42
-- * AC.3 in Gérard Hartmann's
Les réalisations de la SNCASE
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg222985.html#msg222985
C.900 (III) - (Project) 1943 monoplane light a/c studies
- C.900-2 : Conventional low-wing monoplane light a/c
- C.900-2 : 1 x 90 hp (??) inline engine, span (??) m
-- C.900-2 : 2-seat (?) tractor, fixed/spatted trike u/c
- C.900-2
hydro: Single main or twin float gear
- C.900-5 : 3-to-5 seat tractor, fixed/spatted trike u/c
- C.900-5 : 1 x 120-140 hp (??) inline, span (??) m
- C.900-6A: '
Léger' pusher, pod-and-boom fuselage
- C.900-6A: Retr. trike u/c, low boom, cruciform tail
--
https://www.secretprojects.co.uk/threads/various-caudron-projects.9932/page-3#post-348435
C.910 (I) - (Project) 1939 single-seat light fighter
- C.910: Mid-wing fighter (deriv. fro C.760 ??)
- C.910: 1 x 730 hp Isotta Fraschini
Delta IV-12
C.910 (II) - (Project) 1943 light transport monoplane
- C.910 (II): 2 x 300 hp Renault 6Q-20/21, span (??) m
- C.910 (II): 1943, low-wing twin-engined transport
- C.910-2: 1944, high-wing, twin tractors, fixed trike gear
- C.910-4: 1944, high-wing, twin pushers, fixed tricycle u/c
C.920 - (Project) High-winged light twin transport
- C.920: Multiple vers. (pax,
postale, cargo,
école)
-- Orig. vers. taildragger with inset windscreen
- C.920-1 : Top of engine nacelles align with wing
- C.920-2 :
Hypothetical designation
- C.920-3 :
Hypothetical designation
- C.920-4 : Higher engine nacelles (than C.920-1)
-- C.920-4 was bulkier, closer to unbuilt prototype
- C.920 (1941): Liaison/light transport, trike u/c
- C.920 (1941): 2 x 320 hp Argus As 410, span (??) m
-- May have inspired Messerschmitt-Caudron MeC 164*
- C.920 (May 1942): Two distinct variant evolved
- C.920-X: Enlarged, shoulder-winged C.920 devel.
-- C.920-X: Larger fuselage/tail, broader chord
- C.920-Y: Enlarged devel. high-winged transport
-- C.920-Y: Rounded nose/canopy, boxier fuselage
-- * MeC-164 prototype const. abandoned, Siebel Si 204 chosen
--
http://www.secretprojects.co.uk/forum/index.php/topic,12596.msg123605.html#msg123605
930
C.940 - [Project] 1941 low-wing, twin-engined postal monoplane
- C.940: 2 x 500 hp Renault 913 engines, span
?? m
--
http://www.secretprojects.co.uk/forum/index.php/topic,9932.msg287427.html#msg287427
- C.941: 194? C.940 deriv., 2 x 800 hp Renault engines*
-- * Prob. a ref. to 800 hp Renault 626 IV-16 engines
C.950 - (Project) 19?? single-engined colonial transport
C.960- (Project) 1941 twin-engined transport seaplane
- C.960: 2 x (??) hp Renault 6Q 6-cyl., span (??) m
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