Latécoère Late 28

Developed from the Latecoere 26, the Latecoere 28.0 was a braced high-wing monoplane powered by a Renault 12Jbr engine. The enclosed cockpit accommodated a pilot and co-pilot/ engineer, and the cabin was furnished for eight passengers. Seventeen Late 28.0s were followed by 29 Late 28.1 aircraft with a 373kW Hispano-Suiza 12Hbxr engine. A number of Late 28.0s were converted subsequently to Late 28.1 standard.
The sole Late 28.2 was a mail carrier and established several payload/speed world records in 1931. The first of five Late 28.3 mail carriers was flown by Jean Mermoz on 11/12 April 1930 to achieve a world closed-circuit distance record for seaplanes of 4308km.
The remaining Late 28.3s were used on Mediterranean routes and charter services. The Late 28.1/H was a wheel landing gear version of the Late 28.3. Two one-off aircraft were the Late 28.3-I, a passenger version of the Late 28.3, and the Late 28.4-I, also developed from the Late 28.3 but powered by a Gnome-Rhone 14Kbr radial engine of 522kW. In 1930 there appeared the Late 28.5, structurally strengthened and powered by a 485kW Hispano-Suiza 12Nbr, followed by three Late 28.6 aircraft, also Hispano-powered and built for Venezuela, which had already purchased two Late 28.1s.

Variants:

Laté 28
Laté 28-0: 1 x 500 hp Renault 12Jb V12, 2 crew + 8 pax
Laté 28-1: 1 x 500 hp Hispano-Suiza 12Hbr, 2 crew + 8 pax
Production of Laté 28-0 and ’28-1 totalled at least 47 a/c*
Laté 28-2: record aircraft (5 Int’l speed records, 1 x 650 hp HS.12Nbr, 1 built
Laté 28-2 had Lamblin radiators, carried twice Laté 28-1’s payload
Laté 28-3: twin-float seaplane airmail transport, 600 hp HS.12Lbr V12
Laté 28-3 ‘Comte-de-La Vaulx’ F-AJNQ, trans-South Atlantic, 12-13 May 1930
Laté 28-4: Laté 28-4-01, 1 x 700 hp Gnome-Rhone 14KB radial, 1 built
Laté 28-5: military floatplane for Aéronavale, 1 x 650 hp Hispano-Suiza 12Nb
Laté 28 c/n 92 ‘La Frégate’ record breaker flown by Lt de Vaisseau Pâris
Laté 28-6: Laté 28-6-1, 3 x HS.12Nb-powered a/c for Venezuela, conv to Laté 28-9
Laté 28-7: [Project] Laté 28-0 with 700 hp Renault 12Mc, not built
Laté 28-8: 1930 record attempt a/c, 1 x 650 hp Hispano-Suiza 12 Nbr, 1 built
Laté 28-8 c/n 916** F-AJXL had and enlarged wing, it broke up in flight
Laté 28-9: Laté 28-9-1, 3-seat bomber with dorsal machine gun mounting

  • Production for Aéropostale x 38, Aviacion Nacional Venezolana x 3, Linea Aeropostal Venezolana x 2, and Aeroposta Argentina (an Aéropostale subsidiary) x 4.

Aéropostale Laté 28-0: c/n 910 F-AJOU, 916 ‘OV, 917 ‘OX, 923 ‘OY, 924 ‘OZ, 925 F-AJPA, 926 ‘PB, 927 ‘PC, 929 F-AJUV, 930 ‘UX, 931 ‘UY, 932 ‘UZ, 933 F-AJVB, 934 F-AJVH, 935 ‘VI, 936 ‘VJ, and 937 ‘VK (all conv. to Laté 28-1 standards, 1933-35 except 917, 931, 923, & 937).

Aéropostale Laté 28-1: c/n 902 F-AJHS, 903 F-AJIO, 904 F-AJIX, 905 F-AJIP, 906 F-AJIQ, 908 F-AJJM, 911 F-AJLB, 912 F-AJLE, 913 F-AJLM (YV-ABU, 914 F-AJLN, and 915 F-AJLO.

Air France Laté 28/1H: c/n 941 F-AMX, 943 F-AMXV, and 944 F-AMXX

Aéropostale Laté 28-3 c/n 921 F-AJPF, 922 ‘PG (conv. to Laté 28-1), & 940 ‘PH

** NB: It’s difficult to pin down exact Laté 28 variant numbers. In part, this is because of individual airframes being modified between variants. In other cases there is c/n duplication in registration records – eg: c/n 918 is listed both as the record-breaking Laté 28-8 airframe and as Aeroposta Argentina’s F-AJPD which crashed in Rio Plate estuary.

Specifications:

Late 28.1
Engine: 1 x Hispano-Suiza 12Hbxr, 500hp
Max take-off weight: 4040 kg / 8907 lb
Empty weight: 2440 kg / 5379 lb
Wingspan: 19.25 m / 63 ft 2 in
Length: 13.64 m / 44 ft 9 in
Height: 3.58 m / 11 ft 9 in
Wing area: 48.60 sq.m / 523.13 sq ft
Max. speed: 232 km/h / 144 mph
Cruise speed: 200 km/h / 124 mph
Ceiling: 5200 m / 17050 ft
Range: 1000 km / 621 miles
Range w/max.fuel: 1000 km / 621 miles
Crew: 3
Passengers: 8

Latécoère Late 26

The Late 26 (about 70 were built during 1928-30 mainly for Aeropostale) was primarily a mailplane, although it accommodated two passengers. A Laté 25 development, the Late 26 featured three open cockpits in line and power was provided by a 450hp Renault 12Ja engine in the Late 26.2R and a 500hp Renault 12Jb in the Late 26.6R. Square- replaced the round-section fuselage of the Laté 25.

Late 26.2R
Engine: 1 x 450hp Renault 12Ja
Max take-off weight: 3364 kg / 7416 lb
Empty weight: 1590 kg / 3505 lb
Wingspan: 17.40 m / 57 ft 1 in
Length: 12.20 m / 40 ft 0 in
Height: 3.90 m / 12 ft 10 in
Wing area: 48.60 sq.m / 523.13 sq ft
Max. speed: 188 km/h / 117 mph
Cruise speed: 157 km/h / 98 mph
Ceiling: 4500 m / 14750 ft
Range: 680 km / 423 miles

Latécoère Late 25

The 1926 Latecoere 25 monoplanes had a four-seat cabin, single 450hp Renault and a one ton payload.

Laté 25-1R: 1927 prototype Laté 25-1 conv. from Laté 17 (603/F-AIEH)
Laté 25-2R: 1929 production version, 1 x 450 hp Renault 12Ja
Laté 25-2R were conv. from Laté 17, Laté 17, and Laté 17-3R
Laté 25-3R: 1931, 1 x 450 hp Renault 12Ja
Laté 25-3R were conv. from Laté 17, Laté 17-1J, Laté 17-3R
NB: Laté 25/4R listed as Laté 17-1J 607/F-AIHF conv. [typo?]

Latécoère Late 23

The Late 23 was an enlarged version of the Late 21 (conv. from Laté 21bis F-AIHP 73/2) for 4-6 pax, powered by Farman engines and spanning 28.00m. With accommodation for eight passengers, it had a maximum take-off weight of 7503kg, but the sole prototype broke up on take-off on 31 December 1927, killing its crew of four.

Engines: 2 x 500hp Farman 12We
Max take-off weight: 7503 kg / 16541 lb
Empty weight: 4627 kg / 10201 lb
Wingspan: 28.00 m / 91 ft 10 in
Length: 16.60 m / 54 ft 6 in
Height: 4.80 m / 15 ft 9 in
Wing area: 123.00 sq.m / 1323.96 sq ft
Max. speed: 178 km/h / 111 mph
Cruise speed: 152 km/h / 94 mph
Ceiling: 3800 m / 12450 ft
Range: 1200 km / 746 miles

Latécoère Late 21

The first flying-boat produced by Latecoere was the Late 21, built for Aéropostale for its Marseille-Algiers postal and passenger routes. The prototype, first flown in 1926, had a parasol wing with lower stub wings which acted as stabilising sponsons. Two 313kW Gnome-Rhone Jupiter 9Ab radials were mounted in tandem on the wing, and the single-step hull terminated in a large single fin and rudder. Open side-by-side pilots’ cockpits were located in line with the wing leading edge and there was cabin accommodation for seven passengers. Successful tests with the Late 21 led to the construction in 1927 of five slightly modified Late 21bis and a single Late 21ter, with Farman 12We engines. The Late 21 bis spanned 22.00m, had a maximum take-off weight of 5730kg and possessed a maximum speed of 172km/h.
The Late 23 was an enlarged version of the Late 21, powered by Farman engines and spanning 28.00m.

Variants:
Laté 21 – 1926 parasol monoplane flying boat, 2 x push-pull 420 hp GR Jupiter 9Ab, 21 m span

Laté 21: prototype N°1/72 F-ESDH, conv. into Laté 21bis F-AIHN

Laté 21bis: production model, different hull length, fins shortened
1 x Laté 21 conv., plus F-AIIE, ‘FH, ‘HN, ‘HP (conv. to Laté 23), ‘HQ

Laté 21ter: 2 x 500 hp Farman 12We W12 engines
F-AIKL N°1/76 ,1927 to Aéropostale, discarded Oct 1931

Engine: 2 x Gnome-Rhone Jupiter 9Ab , 420hp
Max take-off weight: 5730 kg / 12633 lb
Empty weight: 3530 kg / 7782 lb
Wingspan: 22.00 m / 72 ft 2 in
Length: 17.95 m / 58 ft 11 in
Height: 4.85 m / 15 ft 11 in
Wing area: 88.00 sq.m / 947.22 sq ft
Max. speed: 172 km/h / 107 mph
Cruise speed: 144 km/h / 89 mph
Ceiling: 3600 m / 11800 ft
Range:
800 km / 497 miles
Crew: 3
Passengers: 5-7

Latécoère Late 17

Laté 17: 1924 high-winged monoplane mailcarrier, 4 pax cabin, 23 built

Laté 17
Prototype, 1 x 300 hp Renault 12Fe, 2 built (F-ESDF & F-AHFG)

Laté 17-1R
280 hp Renault 12Fc

Laté 17-1J
380 hp GR Jupiter 9Aa

Laté 17-3J
380 hp GR Jupiter 9Aa

Laté 17-3R
300 hp Renault 12Fe

Laté 17 prototype 601/F-AIEG (ex-Laté 15) becomes first Laté 17-3R conv.

Laté 17-4R
450 hp Renault 12Ja