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Curtiss Hawk 75

Table of Contents


Introduction

Prototype and Development

Curtiss P-36

Curtiss Model 75 Hawk

Surviving Examples

Production Figures

Further Reading and Bibliography

A Curtiss Hawk H75A-2 of the 1ere Escadrille, of GC II/5 intercepting a Heinkel He 111 during the first days of the German attack on France, May 1940.


Curtiss Hawk Key Data
Country of Origin: United States of America
Manufacturer: Curtiss Airplane Division, Curtiss-Wright Corporation, Buffalo, New York, United States of America
Major Variants: P-36A, P-36C, P-36G, Hawk 75A, Hawk 75H, Hawk 75M, Hawk 75N, Hawk 75O, Hawk 75Q
Role: Pursuit Fighter
Operated by: United States, Great Britain, France, Norway, Finland, Germany, Brazil, Netherlands, China, Siam, Persia, Argentina, Peru, Portugal, South Africa
First Flight: Early 1935
In Service: April 1938 (first delivery to the USAAC)
Number Built: 1,088

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Introduction

The Curtiss H75 Hawk was one of a class of aircraft which set new fighter design standards in the mid 1930s. Low-winged monoplanes with all-metal construction, retractable undercarriage and enclosed cockpits; first with radial engines and later in-lines, this design standard applied to most World War Two fighters, and indeed was also the basic design of the fighters during the first ten years of the jet-age.

The Hawk 75 line was distinguished by seeing early combat in every war theatre between 1938 and 1942. Chinese Hawks first flew against the Japanese in 1938, side by side with Soviet Polikarpovs; aircraft they later flew against in Finnish hands in the Continuation War.

Siamese (Thai) Hawk 75s flew against French Morane-Saulnier M.S.406s in Indo-China in 1940; then later, flying alongside M.S.406s in France, scored the first kills for the French Armée de l'Air in 1939. P-36s, the United States Army Air Corps (USAAC) version of the Hawk 75 were airborne within 15 minutes of the Japanese attack at Pearl Harbor, scoring some of the earliest air combat victories of the Pacific War; Thai Hawk H75s also flew combat against the Japanese on the Malay Peninsula on the 7th December 1941, as did the Netherlands East Indies Hawks in January 1942 on Sumatra and Java.

After their Government had formed an alliance with Japan, the Thai Hawk 75s then faced Allied forces in Burma who themselves were later flying Mohawks (H75s). The final act of the Hawk as a first-line combat fighter was when it was flown by Vichy French forces against Allied airforces during the invasion of Morocco in 1942 - "Operation Torch" -the first US land operation in the West.

In spite of this proud combat heritage, the Curtiss Model 75 is often dismissed as simply "the precursor to the P-40 Kittyhawk" and no further interest taken in it.

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Prototype and Development

The Hawk design originated in November 1934 (the same year as the Bf 109, the Hurricane and Spitfire) as a private-venture development of a single-seat fighter by Curtiss-Wright. It was a low-winged, all-metal monoplane, and originally had a 900-hp radial engine; the Wright XR-1670-5. This aeroplane was named the Curtiss Design 75 and was entered into a design competition against the Seversky P-35 (also privately developed) in April, 1936, which looked to select a replacement for the Boeing P-26 Peashooter pursuit fighter.

Due to delays with the Seversky prototype time was available for Curtiss to re-engine the original Model 75, and a new 850-hp engine; the Wright XR-1820-39 (G5) radial, was fitted and the type designated the Model 75B. The original prototype was later retrospectively designated the Model 75D, but has also sometimes been wrongly named the XP-36.

Curtiss Model 75 prototype

The Curtiss Model 75 prototype in slow flight. It is painted with the standard USAAC scheme of the time - yellow wings and blue fuselage. This type was later designated as Model 75D. (Photo: Curtiss Wright Corporation)

The Model 75 had a number of features more typical of Northrop designs due to Donovan Berlin, the Chief Engineer, having recently come from that company. One innovative feature was the main landing gear rotating through 90° as it retracted to lay flush in the relatively thin wing section. Other features were fabric covered control surfaces, enclosed cockpit, hydraulic split-flaps, monocoque fuselage construction, and a wing built in two halves and joined at the centre-line. Initial combat fit was two .30 in machine guns in the top engine cowl, but it had no pilot armour or self-sealing fuel tanks fitted.

In April 1936 when the competitive assessment was finally done, Seversky's P-35 won the competition. The Curtiss Model 75B had been only able to achieve a top speed of 285 mph at 10,000 ft, in spite of the specification requirement to achieve 294 mph. The USAAC eventually operated a total of 137 of the competing Seversky P-35s before the type was retired from front-line service after being hopelessly outclassed by the Japanese Air Forces during the invasion of the Philippines in December 1941.

Although by losing the design competition Curtiss-Wright had missed out on a full production order for pursuit fighters in 1936, they were given a contract to manufacture three further Model 75s for testing and evaluation. These were designated as Model H75E (Army designation Y1P-36) and had 1,050-hp Pratt and Whitney R-1830-13 Twin Wasp radial engines fitted (de-rated to 950 hp). They also had improved pilots' visibility and retractable tail-wheels. This engine installation was very effective, and although being 362 lbs heavier than the earlier 75B (5,437 lbs vs 5,075 lbs gross weight) the first aircraft achieved 294.5 mph at 10,000 ft. The Army were impressed with this performance, and other characteristics of the aircraft, and on the 7th of July 1937, ordered 210 production aircraft - designated the P-36A. This order was worth over four million dollars - the largest fighter order ever placed by the Army Air Corps at that time. The US Government then allowed Curtiss to accept foreign orders and various models of the Model 75 ultimately flew in at least fifteen air forces.

A simplified version was developed for export which was based on the Model H75E. It was called the Hawk 75 (Model 75H) - the first model to use the name Hawk - and had fixed undercarriage shrouded in streamlined spats, wing bomb racks and an 875 hp Wright GR-1820-G3 radial engine. The engine could be changed to suit customer requirements, and this model was exported to a number of countries, some of which assembled it under license.

During the construction of the Y1P-36s (Model 75E) for the USAAC the Model 75I was also being built. It was a conversion of the prototype 75B aircraft designed to demonstrate an in-line liquid cooled engine. Curtiss was aware that air-cooled radial engines would eventually become limiting so added an Allison V-12 engine (V-1710-11) capable of developing 1,150 hp when supercharged (at 20,000 ft). The resulting prototype fighter exceeded 300 mph, the first US fighter to do so. Test flights began in April 1937, and the Army took delivery of the aircraft as the XP-37 in June. The cockpit was moved back to balance the plane, and other modifications made. It was eventually retired to a mechanics school after 152 flying hours. It cost $104,352 when purchased from Curtiss. Thirteen further test aircraft were ordered as YP-37s. They incorporated changes derived from the XP-37 tersting, including a lengthened fuselage, nose cowling reshaping, a V-1710-21 engine and new supercharger and aerodynamic modifications. The unsatisfactory engine/supercharger performance continued, and all were eventually retired with the highest time aircraft only having logged 212 hours. They had cost $34,481 each.

One of the thirteen YP-37 trial aircraft. (Photo: Curtiss Wright Corporation)

The fourth P-36A was used for aerodynamic research into streamlining engine cowls around radial engines. By extending the propeller drive shaft, the cowl could be shaped more like that of an in-line engine. This aircraft was designated as the XP-42 (Model 75S) and continued in this research role until scrapped in 1947.

The most significant development of the Model 75 was the fitting of an Allison V-1710-19 in-line supercharged engine to the tenth production P-36A as the Model 75P. Redesignated as XP-40 (Hawk 81) this aircraft became the first P-40 Warhawk, a type which was to later play an important role during World War Two.

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Curtiss P-36

The three Y1P-36s (Model 75E) delivered to the USAAC had Pratt and Whitney R-1830-13 Twin Wasp engines, one .50 cal and one .30 cal machine-gun in the cowl with no bulged fairing, view panels behind the cockpit and no cowl flaps. They were valued at $43,432, $43,477 and $73,477 respectively. During the trials at Wright Field they achieved speeds of 294.5 mph at 10,000 ft with 900 hp, and 256 mph with 660 hp at gross weight of 5,437 lbs. The 1050 hp twin Wasps were derated to 950 hp at take off, and a Hamilton Standard constant speed propeller was fitted. At the completion of the test program the three Y1P-36s were re-designated P-36.

Two hundred and ten P-36As were ordered by the USAAC with the first delivery in April 1938. These production machines differed from the Y1P-36s by having cowl flaps, bulbous fairings over the nose guns, a Curtiss constant speed propeller and a fully rated Wasp engine. Normal ammunition load was 500 rounds of .30 cal and 200 rounds of .50 cal. With the fully rated engine these aircraft achieved 313 mph at 10,000 ft with a full combat weight. However in little over a year from the first delivery there had been 81 changes to the design giving a gross weight of 5,650 lbs and the maximum available speed at 10,000 was then 300 mph. One hundred and seventy six were completed as P-36As.

One of the production P-36As was temporarily converted to trial an 8:1 supercharger gearing modification and designated as P-36B in 1938. It was later returned to its original configuration. Two were converted on the production line to the XP-40 (Model 75P) and XP-42 (Model 75S) respectively. They are described in the Prototype and Development section above.

In December 1938 the eighty-fifth P-36A was converted to a prototype P-36C with the addition of a .30 cal gun with 500 rounds to each wing. The ammunition storage was in a slim streamlined magazine projecting underneath the wing and became a visible characteristic of the P-36C. The final 30 aircraft of the original 210 ordered were completed as P-36Cs and were also up-engined to a 1,200 hp Pratt and Whitney R-1830-17 Twin Wasp. Although the gross weight had now climbed to 5,734 lbs, the P-36C could still achieve 311 mph at 10,000 ft.

Curtiss P-36C fighters of the 27th Pursuit Squadron, 1st Pursuit Group at the Cleveland Air Races on 1 September, 1939, the day Germany invaded Poland. These aircraft had been painted with washable paint in different trial camouflage schemes. The two vertical fuselage bands indicate the Squadron leader's aircraft. (Photo: Curtiss Wright Corporation)

Three further P-36As were converted for weapons trials. The XP-36D was fitted with 2 .50 cal guns in the nose, each with 400 rounds, and two .30 cal guns in each wing with 500 rounds each. This was the same armament as the Hawk 75A-2. The XP-36E had one .50 cal with 200 rounds in the nose and three .30 cal guns with 500 rounds each in each wing for a total of seven. This aircraft was retired and used for mechanic training after 1942.

The final trial aircraft, the XP-36F, was the most heavily armed with the original .50 and .30 cal in the nose, and a Masden 23 mm cannon with 100 rounds mounted in a gondola under each wing. It was only tested briefly before the cannon were removed and it reverted to a P-36A.

The only example of the XP-36F which was trialled. It had a 23 mm Masden cannon mounted in each under-wing gondola. When testing was finished the cannon were removed and the aircraft reverted to a P-36A. (Photo: Curtiss Wright Corporation)

The P-36G aircraft were simply redesignated Model 75A-8s originally destined for Norway. The USAAC retained thirty of them, but because of their Wright Cyclone engines they were considered unsuitable for USAAC combat use. Eventually they were transferred to Peru as P-36Gs.

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Curtiss P-36 Variants

These variants were not designated in alphabetical order as they were designed. They are listed here in order of manufacture.

Model 75D - The first prototype, which was later converted to the Model 75B
Model 75B - Entered unsuccessfully in the original 1936 design competition, and later converted to the Model 75I
Model H75E Y1P-36 The three Model 75 evaluation aircraft supplied to the USAAC
Model 75L P-36A First production model for the USAAC
P-36B Temporary research supercharger conversion from a P-36A
P-36C Final production version for the USAAC
P-36G Hawk 75A-8s taken on strength by the USAAC
XP-36D Converted from a P-36A
XP-36E Converted from a P-36A
XP-36F Temporary research conversion from a P-36A
Model 75P XP-40 Converted from a P-36A.
Model 75J - Converted from one of the Model 75A demonstrators. A trial supercharger fitting
Model H75R - Converted from the Model 75J aircraft. A supercharger trial.
Model 75K - Project only, not built. Pratt and Whitney 910 hp R-2180 Twin Hornet engine
Model 75I XP-37 Converted from the original Model 75B aircraft
YP-37 Pre-production evaluation examples of the XP-37
Model 75S XP-42 Converted from a P-36A.

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Curtiss P-36 Specifications

Model
75D prototype
Y1P-36
P-36A
P-36C
P-36G
Engine 900 hp Wright SCR-1670-G5 1,050 hp P&W R-1830-13 1,050 hp P&W R-1830-13 1,200 hp P&W R-1830-17 1,200 hp Wright GR-1820-G3 Cyclone
Span 37 ft 0 in
11.27 m

37 ft 3.5 in
11.35 m

37 ft 3.5 in
11.35 m
37 ft 3.5 in
11.35 m
37 ft 0 in
11.27 m
Length 28 ft 3.5 in
8.62 m

28 ft 10 in
8.78 m

28 ft 6 in
8.68 m
28 ft 10 in
8.78 m
28 ft 6 in
8.68 m
Height 9 ft 1 in
2.76 m
9 ft 0 in
2.74 m
9 ft 3 in
2.81 m
9 ft 3 in
2.81 m
9 ft 3 in
2.81 m
Wing area 237 sq ft
22 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
Empty weight 3,760 lbs
1,705 kg
4,267 lbs
1,935 kg
4,567 lbs
2,076 kg
4,619 lbs
2,095 kg
4,675 lbs
2,121 kg
Gross weight 4,843 lbs
2,106 kg
5,414 lbs
2,456 kg
5,689 lbs
2,586 kg
5,829 lbs
2,644 kg

5,880 lbs
2,667 kg

Maximum speed 281 mph at 10,000 ft
452.2 kph at 3,048 m
293 mph at 10,000 ft
471.5 kph at 3,048 m
300 mph at 10,000 ft
480 kph at 3,048 m
311 mph at 10,000 ft
497.6 kph at 3,048 m
322 mph at 15,200 ft
518.2 kph at 4,572 m
Cruising speed 250 mph
402.3 kph
261 mph
420 mph
270 mph
434.5 kph
270 mph
434.5 kph
240 mph
386.2 kph
Climb No data 10,000 ft (3,048 m) in 3 min 45 sec 3,400 ft/min
1,036 m/min
15,000 ft (4,572 m) in 4.9 min 15,000 ft (4,572 m) in 6 min
Service ceiling 30,000 ft
9,144 m
31,500 ft
9601 m
33,000 ft
10,058 m
33,700 ft
10,272 m
32,350 ft
9,860 m
Range 537 miles
864 km
790 miles
1,271 km

825 miles
1,327 km

820 miles
1,319 km
650 miles
1,046 km
Armament 2 x .30 guns 2 x .30 guns 2 x .30 guns 4 x .30 guns 6 x .30 guns

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Curtiss P-36 in Operation

United States of America

The United States Army Air Corps was operating P-36s at the outbreak of the war with Japan. More data will be added at a later stage.

Peru

P-36s were operated in Peru during and after WWII.

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Curtiss Model 75 Hawk

At the same time as Curtiss were preparing the three Model 75E's (Y1P-36) for the USAAC, they were also developing a prototype export model to meet the demand for modern combat aircraft throughout the world. This aircraft differed from the Model 75E by having fixed undercarriage with spats, a variable armament fit, bomb racks fitted, and a Wright 875 hp GR-1820-G3 Cyclone engine. It was marketed as the "Hawk 75" and designated Model 75H by Curtiss. Two demonstrators were built.

One of the two Hawk 75 demonstrators. This aircraft was sold to China. (Photo: Curtiss Wright Corporation)

The main export model was the Hawk H75A. It had retractable undercarriage and four guns - a nose-mounted .50 cal and.30 cal. and a .30 cal in each wing. This was a weak armament by current European standards, and the Hawk 75A was also relatively slow. However it was maneuverable and of very rugged construction. Two models of each of the Wright Cyclone and Pratt and Whitney Twin Wasp were available for installation. France alone ordered 1,130 Hawk H75As of various models from 75A-1 to 75A-4, although 511 of these were not manufactured due to the German defeat of France. At least 91 further Hawk H75As of various models were built to order for other countries, the designators finally reaching A-9. The sub-types of the Hawk H75A differed in armament fit and engines and are listed on the table below.

China, which was already fighting a desperate war against the invading Japanese, showed early interest in the Hawk 75, and purchased one of the demonstration 75Hs, and then ordered more, with delivery starting in May 1938. This order was designated as the Model 75M and 112 were supplied in total. They had fixed undercarriage and two wing mounted .30 cal guns as well as the cowl mounted .50 and .30 cals. Two further demonstrators, designated as Model 75Q, were later built for sale to China, one of them being converted to retracting undercarriage.

The Royal Thai Air Force took delivery of twelve Hawk 75s designated as Model H75N. These had an extra pair of .30 cal guns mounted in gondolas outboard of the fixed wheels making six guns in all.

The second Hawk 75H demonstrator was purchased by Argentina. They ordered 29 further aircraft which Curtiss designated as Model H75O, and also built twenty under licence.

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Curtiss Model 75 Hawk Variants

These variants were not designated in alphabetical order as they were designed. They are listed here in order of manufacture.

The prefix "H" was added to export variants.

Model 75D
-
The first prototype, which was later converted to the Model 75B
Model 75B
-
Entered unsuccessfully in the original 1936 design competition, and later converted to the Model 75I
Model 75H
-
Prototype export model. Wright 875 hp GR-1820-G3 Cyclone
Model H75A
H75-A1
Pratt and Whitney 1,050 hp R-1830-SC3G Twin Wasp; 4 x 7.5 mm FN Browning guns; French cockpit equipment. Mohawk I in RAF service
-
H75-A2
Pratt and Whitney 1,050 hp R-1830-SC3G Twin Wasp; 6 x 7.5 mm FN Browning guns; French cockpit equipment. Mohawk II in RAF service.
-
H75-A3
Pratt and Whitney 1,200 hp R-1830-S1C3-G Twin Wasp; 6 x 7.5 mm FN Browning guns; French cockpit equipment. Mohawk III in RAF service
-
H75-A4
Wright 1,200 hp GR-1820-G205A Cyclone 9; 4 x 7.5 mm FN Browning guns; French cockpit equipment. Mohawk IV in RAF service
-
H75-A5
Some as Mohawk IV in RAF service.
-
H75-A6
Pratt and Whitney 1,200 hp R-1830-S1C3-G Twin Wasp; 4 x 7.9 mm guns
-
H75-A7
Wright 1,200 hp GR-1820-G205A Cyclone 9; 1 x .50 cal and 3 x .30 cal factory fitted - the .50 cal was replaced by a .30 cal in service.
-
H75-A8
Wright 1,200 hp GR-1820-G205A Cyclone 9; 2 x 12.7 mm and 4 x 7.9 mm guns. P-36G in US service
-
H75-A9
Wright 1,200 hp GR-1820-G205A Cyclone 9. Mohawk IV in RAF service
Model H75M
-
Wright 850 hp GR-1820-G3; 1 x .50 cal and 3 x .30 cal guns
Model H75N
-
Wright 850 hp GR-1820-G3; 1 x .50 cal and 3 x .30 cal guns
Model H75O
-
Wright 875 hp GR-1820-G3;
Model 75Q
-
Additional demonstrators of the 75H. Wright 875 hp GR-1820-G3 Cyclone

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Curtiss Model 75 Hawk Specifications

Model
75D prototype
Hawk 75
H75A-3
H75A-4
H75A-8
H75M
Engine 900 hp Wright SCR-1670-G5 875 hp Wright GR-1820-G3 Cyclone 1,200 hp P&W R-1830-17 Twin Wasp 1,200 hp Wright GR-1820-G205A Cyclone 9 1,200 hp Wright GR-1820-G3 Cyclone 875 hp Wright GR-1820-G3 Cyclone
Span 37 ft 0 in
11.27 m
37 ft 0 in
11.27 m
37 ft 3.5 in
11.35 m
37 ft 3.5 in
11.35 m
37 ft 0 in
11.27 m
37 ft 0 in
11.27 m
Length 28 ft 3.5 in
8.62 m
28 ft 7 in
8.71 m
28 ft 6 in
8.68 m
28 ft 7 in
8.71 m
28 ft 6 in
8.68 m
28 ft 7 in
8.71 m
Height 9 ft 1 in
2.76 m
9 ft 3 in
2.81 m
9 ft 3 in
2.81 m
9 ft 3 in
2.81 m
9 ft 3 in
2.81 m
9 ft 3 in
2.81 m
Wing area 237 sq ft
22 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
236 sq ft
21.92 sq m
Empty weight 3,760 lbs
1,705 kg
3,975 lbs
1,803 kg
4,620 lbs 4,541 lbs 4,675 lbs
2,121 kg
3,975 lbs
1,803 kg
Gross weight 4,843 lbs
2,106 kg
5,172 lbs
2,345 kg
5,734 lbs 5,750 lbs 5,880 lbs
2,667 kg
5,305 lbs
2,406 kg
Maximum speed 281 mph at 10,000 ft
452.2 kph at 3,048 m
239 mph (384.6 kph) at sea level

280 mph at 10,700 ft
450.6 kph at 3,261 m

311 mph at 10,000 ft
497.6 kph at 3,048 m

323 mph at 15,000 ft
519.8 kph at 4,572 m
322 mph at 15,200 ft
518.2 kph at 4,633 m

280 mph at 10,000 ft
450.6 kph at 3,048 m

Cruising speed 250 mph
402.3 kph
No data 270 mph
432 kph
262 mph
419.2 kph
261 mph
420 kph
240 mph
386.2 kph
Climb No data 2,340 ft (713 m) in 1 min

22,960 ft (6,998 m) in 12.5 min.

15,000 ft (4,572 m) in 4.9 min 15,000 ft (4,572 m) in 4.9 min 15,000 ft (4,572 m) in 6 min No data
Service ceiling 30,000 ft
9,144 m
31,800 ft
9,693 m
33,700 ft
10,272 m
32,700 ft
9,967 m
32,350 ft
9,860 m
31,800 ft
9,693 m
Range 537 miles
864 km
547 miles at 240 mph at 10,700 ft
880 km at 386.2 kph at 3261 m
820 miles at 200 mph
1,312 km at 320 kph
603 miles at 248 mph
965 km at 397 kph
650 miles
1,046 km
1,210 miles (fuel overload)
1,947 km
Armament 2 x .30 guns 1 x .50 gun and 1 or 3 .30 guns

Bombs:
10 x 25 lb (11.36 kg), or
10 x 30 lbs (13.63 kg), or
6 x 50 lb (22.72 kg)

1 x .50 and 3 x .30 guns 6 x 7.5 mm guns 2 x .50 and 4 x .30 guns 1 or 2 .50 and 2 or 3 .30 guns

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Curtiss Model 75 Hawk in Operation

France

French Hawks were modified by the installation of FN Browning machine guns, metric instruments, a Munerelle oxygen supply, modified seat backs to fit the French Lemercier back-mounted parachute, a Radio-Industrie 537 radio, a Baille-Lemaire gunsight and reversed throttle controls. All Curtiss Hawks were numbered in a single sequence starting at No. 1 for the first H75A-1, and continuing with No. 101 for the first 75A-2 and 201 for the first 75A-3.

H75A-1

100 were ordered, and all delivered. First deliveries were in December 1938. The first sixteen aircraft were tested at Buffalo before dispatch, and then checked on arrival at the SNCAC factory at Bourges. Later aircraft were shipped in a broken down form and assembled by SNCAC. They first entered squadron service in March 1939 with Groupe de Chasse (G.C.) 4 and G.C.5.

H75A-2

100 were ordered and all delivered. Deliveries started in May 1939.

H75A-3

135 were ordered of which approximately 60 were delivered. Some were delivered to French Morocco and Britain received more than 20 after the French surrender.

H75A-4

795 were ordered, of which only 6 reached France before its defeat by Germany. 4 were lost at sea, 17 disembarked in Martinique, and 6 in Guadeloupe in the West Indies. The 23 in the West Indies were eventually shipped to Morocco in 1944 and used there for training by the Free French forces.

The French Hawk H75A-1s were delivered in natural metal finish and the camouflage was applied after assembly in France. (Photo: Curtiss Wright Corporation)

Curtiss H75A-1 Hawks of the French Groupe de Chasse II/4 scored the first recorded fighter-to-fighter combat kills on the Western Front in World War Two. On the 8th of September 1939 they flew into battle against a schwarm of Bf 109Es from I/JG53, shot down two 109s, and then forced Oberleutnant Werner Mölders to a forced landing with a damaged engine. The Hawks had opened their account in the west.

By the end of 1939 France had ordered over 2,000 aircraft from companies in the United States, among them 1,150 Hawks for operation by the Armée de l'Air. During May 1940, with war looming, France desperately sought more combat aircraft from the United States. However they were informed on the 16th that Curtiss P-36s would not be released to France from US military stocks because the US Army was opposed to it. In the meantime however, on the 18th of May, the US Administration indicated to the British that they were prepared to release some of the 150 P-36s then possessed by the Army Air Corps to the RAF. France was obviously considered a lost cause.

When the German forces finally attacked France in May 1940, only 101 Hawks were operational with four Groupes de Chasse and some Headquarters flights, all in metropolitan France. They were:

Unit Aircraft and Status Base
G.C. I/4 30 Hawks of which 29 were operational. Wez-Thuisy (Dept. Champagne, near Reims) under command of Comandant Heurtaut.
G.C. II/4 31 Hawks of which 29 were operational. Xaffévillers (Dept. Vosages) under command of Comandant Bourne F.A.105 (5e Armée).
G.C. I/5 29 Hawks of which 25 were operational. Suippes (Dept. La Marne) under command of Comandant Murtin F.A. 102 (2e Armée)
G.C. II/5 26 Hawks of which 14 were operational. Toul-Criox-de-Metz (Dept. Meurthe et Moselle) under command of Comandant Hugues F.A.103 (3e Armée).
HQ Gpt 22 2 Hawks, both operational. Velaine-en-Haye under command of Col. Dumèmes.
HQ Z.O.A.E. (Eastern Zone of Air Operations) 1 Hawk which was not operational. Nancy under command of Gal. Bouscat.
HQ Gpt 23 2 Hawks, both operational. Laon-Chambry under command of Gal. Romatet.

[note that these numbers are those given by Leulliot, 1999. Milde gives figures which are the same in total but distributed differently; GC I/4 32 Hawks (25 operational), GC II/4 32 (22), GC I/5 32 (27) and GC II/5 30 (23).]

These four Groupes de Chasse remained operational with Hawks for the entire campaign, and were later joined in operations by G.C. III/2 which had given up their Moraine 406s and re-equiped with Hawks during early June.

The performance of the Hawks in comparison to the Luftwaffe's Messerschmitt Bf 109s is open to question. Gunston says that; "they wrote a glorious chapter over France in May 1940", however Terraine considers their effectiveness relative to the Bf 109E fighter to be questionable. They were slower and less effectively armed than the Bf 109E, although their pilots liked them because of their maneuverability and ruggedness. They were able to take considerable punishment in battle and still survive.

However, the Hawks certainly performed well against the Luftwaffe bombers. On the first day of the attack on France, GC I/5 shot down eight Dornier Do 17s from KG 3 and GC II/5 shot down three Heinkel He 111s of I./JG53. Between May 10th and June 24th the Groupes de Chasse operating Hawks claimed a total of 230 confirmed and 81 probable kills. These were distributed among the Groupes de Chasse as follows:

C.G. I/4 37 confirmed and 5 probable
C.G. II/4 48 confirmed and 23 probable
C.G. I/5 85 confirmed and 26 probable
C.G. II/5 48 confirmed and 22 probable
C.G III/2 not known.

The Hawk equipped units performed much better than other French fighter units in May and June 1940. This was, at least in part, because they also had the elite pilots. There were at least six aces in C.G. I/5 alone:

Sous Lieutenant Plubeau 15 victories
Captaine Marin La Meslée 20 victories
Captaine Accart 15 victories
Sergent Chef Morel 12 victories
Captaine Vasatko 15 victories
Sous Lieutenant Perina 13 victories

[Perina and Vasatko were both Czechoslovakians who had fled the German invasion of their own country and volunteered for service in the Armée de l'Air.]

The Hawk units had performed well and with replacement aircraft becoming available during the period of fighting, all remained at nearly full strength when the Armistice was signed. Their status in June 1940 was:

Unit Aircraft and Status Base
G.C. I/4 22 Hawks of which 20 were operational Evreux-Fauville
G.C. II/4 37 Hawks of which 30 were operational Orconte
G.C. I/5 26 Hawks of which 22 were operational Saint-Dizier-Robinson
G.C. II/5 22 Hawks of which 17 were operational Toul-Croix-de-Metz
G.C. III/2 30 Hawks of which 28 were operational La Perthe

After the liberation of France in 1945, Hawks continued to operate within the Armée de l'Air. They were being used by the Fighter Training School - Ecole de Chasse - in Morocco in 1945, and later in metropolitan France at Cazaux in 1946. The last Hawk was retired in 1951.

Norway

H75-A6

Norway first ordered Curtiss Hawks in late 1939. These were engined with the 1200 hp Pratt and Whitney R-1830-SC3-G Twin Wasp, and armed with four 7.9 mm machine-guns. Delivery of the first batch of 12 commenced in February 1940, two months before the German invasion in April 1940. A second order had also been placed for 12 more H75-A6s, but only some of these 24 aircraft arrived before Norway was overrun by German forces. It is thought that 19 H75A-6s had been delivered to the Army's aircraft maintenance base at Kjeller Airfield by the 9th of April when Germany invaded. None of these aircraft were combat-ready and only 6 are believed to have been flyable, although still without weapons. Those capable of flying tried to fly-off to escape bombing, but the field had a packed snow surface which had softened during the day, and as they were not ski-equipped, but had wheeled undercarriage, they were unable to gain flying speed. None were damaged during Luftwaffe attacks so most of the aircraft which had been delivered were captured, some of them still in their shipping crates. Eight of these captured H75-A8s were later supplied to Finland by the Germans.

H75-A8

Just before the invasion of Norway, the Government had ordered 36 Hawk H75-A8s, equipped with Wright Cyclone 1200 hp R-1820-G205A engines and two 12.7 mm, and four 7.9 mm machine guns. Delivery could not proceed after Norway was over-run by Germany, and the USAAC requisitioned 30 of them, designating them as P-36G. The remaining six H75-A8s were issued to the Free Norwegian Forces air training facility near Toronto in Canada during February 1941. The H75-A6s which remained undelivered to Norway (probably five) were also used at that facility for fighter pilot training by Norwegian forces.

Netherlands

H75-A7

The Dutch Government had ordered 20 Hawk H75-A7s with Wright Cyclone 9 R-1820-G205A engines of 1200 hp and 3 x .30 cal and 1 x .50 cal machine guns, but they had not been delivered by the time Germany had invaded. These aircraft were all diverted to the Netherlands East Indies Army Air Corps.

Germany

Germany captured a number of Hawks and passed some on to Finland to use in combat against the Soviet Union. More data will be added at a later stage.

Finland

More data will be added at a later stage.

Africa, Mediterranean and the Middle East

The South African Airforce and the Vichy French operated Hawk 75s in East Africa and Morocco respectively. More data will be added at a later stage.

Vichy France (Morocco)

More data will be added at a later stage.

South Africa

More data will be added at a later stage.

The China/Burma/India Theatre

Hawk 75s flew in combat with the Royal Siamese Air Force, the Royal Air Force in India and the Netherlands East Indies Army Air Force during the early part of the Pacific War. More data will be added at a later stage.

Siam (now Thailand)

More data will be added at a later stage.

China

More data will be added at a later stage.

Great Britain

More data will be added at a later stage.

Netherlands East Indies (now Indonesia)

More data will be added at a later stage.

Other Operators

Hawk 75s were supplied to four further Air Forces; those of Argentina, Brazil, Persia and Portugal.

Argentina

More data will be added at a later stage.

Brazil

More data will be added at a later stage.

Persia (now Iran)

More data will be added at a later stage.

Portugal

More data will be added at a later stage.

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Appendix A: Surviving Examples

One Thai Hawk H75N was in the Royal Thai Air Force Museum in Bangkok in 1979.

A P-36G was held in the Peruvian Air Force Museum in 1977.

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Appendix B: Production Figures

Numbers in brackets show aircraft converted from an existing airframe.

Model Variant
Number built
Curtiss Construction numbers
Model 75D -
1
11923
Model 75B -
(1)
11923
Model 75H -
2
12327, 12328
Model 75A -
1
12931
Model H75A H75-A1
100
12798 - 12897
- H75-A2
100
12932 - 13031
- H75-A3
135
13671 - 13805
- H75-A4
284
13806, 13808 - 14090
- H75-A5
6
13807
5 assembled under licence
- H75-A6
24
13643 - 13654, 13659 - 13670
- H75-A7
20
14424 - 14443
- H75-A8
36
14546 - 14581
- H75-A9
10
15252 - 15261
Model H75M -
112
12625 - 12554
82 under licence
Model H75N -
12
12756 - 12767
Model H75O -
49
12769 - 12797
20 under licence
Model 75Q -
2
12898, ?
Model H75E Y1P-36
3
12240 - 12242
Model 75L P-36A
176
12415 - 12417, 12419 - 12424, 12426 - 12624
- P-36B
(1)
12435
- P-36C
30
(1)
12594 - 12624
(12500)
- P-36G
(30)
30 of 14546 - 14581
- XP-36D
(1)
12589
- XP-36E
(1)
12562
- XP-36F
(1)
12587
Model 75P XP-40
1
12425
Model 75J -
(1)
12931
Model H75R -
(1)
12931
Model 75K -
0
Proposal only
Model 75I XP-37
(1)
11923
- YP-37
13
12655 - 12667
Model 75S XP-42
1
12418
- -
-
-
Total listed all types (1,127)
Total airframes built 1,088

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Appendix C: Further Reading and Bibliography

Bibliography

Aerospace Publishers, 1980, 'Blitzkreig part 7: the race to the channel', in Illustrated Encyclopedia of Aviation, Volume Two, Orbis, London

Aerospace Publishers, 1980, 'Curtiss Model 75 (P-36)', in Illustrated Encyclopedia of Aviation, Volume Six, Orbis, London

Leulliot, N., 15 February 2000, Armée de l'Air Order of Battle, 10th May 1940
http://members.tripod.com/~France40/adla/ada_may.html

Leulliot, N., 15 February 2000, Armée de l'Air Order of Battle, June 1940
http://members.tripod.com/~France40/adla/ada_june.html

Beauchamp, G. and Cuny, J., Curtiss Hawk 75, VIP Publishers, Colorado.

Bowers, P.M., 1979, Curtiss Aircraft 1907-1947, Putnam, London.

Caven, W.F., and Cate, J.L., editors, 1948-1958, The Army Air Forces in World War II, Volume One, Plans and Early Operations, January 1939 to August 1942, Office of Air Force History, Washington.

Cull, B., Lander, B. and Weiss, H., 1995, Twelve Days in May, Grub Street, London.

Cuny, J. and Danel, R., 1974, L'Aviation de Chasse Française, 1918-1940, Docavia, Paris.

Dias da Cunha, R., 10 April 2000, História da Força Aérea Brasileira, the Curtiss P-36 in FAB Service
http://www.mat.ufrgs.br/~rudnei/FAB/eng/p-36a.html

Ehrengardt, C-G. and Shores, C., 1983, L'aviation de Vichy au Combat, Vol.1: Les Campagnes Oubliées, Lavauzelle, Paris.

Ganszauge, M. and Ripatti, P., 16 May 2000, Curtiss Hawk 75A (P-36)
http://www.jyu.fi/~mg/history/fafwwii.shtml

Green, W., 1960, Warplanes of the Second World War, Volume Four, Fighters, Hanover House, New York.

Gunfeldt, C., 1990, Fornebu .9 April, Wings, Oslo.

Gunston, W., 1976, Encyclopedia of the World's Combat Aircraft, Salamander, London.

Hall, H.D., 1955, North American Supply, History of the Second World War, United Kingdom Civil Series, Her Majesty's Stationary Office, London.

Hooton, E.R., 1994, Phoenix Triumphant: the rise and rise of the Luftwaffe, Arms and Armour Press, London.

Hsu, L. and Chang, M., 1971, History of the Sino-Japanese War (1937-1945), Chung Wu Publishing Co., Taipei.

Jervås, B., 16 May 2000, Norwegian Aircraft in 1940
http://home.sol.no/~kurtmon/norwair1940.html

Long, J., 16 May 2000, Curtiss H-75A Hawk
http://www.geocities.com/CapeCanaveral/2072/Finnaf.html

Martin, P., 1991, Invisibles Vainqueurs: Exploits et Sacrifice de l'Armee de l'Air en 1939-1940, Editions Yves Michelet, Paris.

Milde, J-P., 2000 update, "Curtiss H75A", in The French Campaign
http://home.worldnet.fr/gaeroy/usav_fr.html

Milde, P., 7 March 2000, Personal Communication.

O'Hara, D.P., 16 May 2000, The Royal Thai Airforce, 1940-41
http://www.netcomuk.co.uk/~dpohara/frthaf.htm

Prasad, B, editor, 1956, Expansion of the Armed Forces and Defence Organisations, Official History of the Indian Armed Forces in the Second World War 1939-45, Orient Longmans,

Rawlings, J., 1969, Fighter Squadrons of the RAF and their Aircraft, McDonald, London.

Swanborough, G. and Bowers, P.M., 1989, United States Military Aircraft Since 1909, Putnam, London.

Terraine, J., 1997, The Right of the Line, Wordsworth Editions Limited, Ware.

Thornburg, C, 30 January 2000, The World's Airforces
http://www.geocities.com/CapeCanaveral/Cockpit/7930/

Further Reading

Keskinen, K., Stenman, K. & Niska, K. 1975: Suomen Ilmavoimien historia 5. Curtiss Hawk 75 A. P-40M. Tietoteos, Espoo, Finland.

Beauchamp, G., 1985, Mowhawks over Burma, Canada's Wings, Ontario.

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