Close this search box.

North American A-36

The North American A-36 (listed in some sources as “Apache” or “Invader”, but generally called Mustang) was the ground-attack/dive bomber version of the North American P-51 Mustang, from which it could be distinguished by the presence of rectangular, slatted dive brakes above and below the wings.

A total of 500 A-36 dive bombers served in the Mediterranean and Southeast Asia theatres during World War II before being withdrawn from operational use in 1944.

The A-36 project was a stopgap measure intended to keep North American Aviation (NAA) assembly lines running during the first half of 1942 despite the US having exhausted its funds earmarked for fighter aircraft.

When the order came for more P-51s in June 1942, the NAA workforce was thoroughly experienced.

With the introduction of the North American Mustang Mk.I with the Royal Air Force’s Army Co-operation Squadrons in February 1942, the new fighter began combat missions as a low-altitude reconnaissance and ground-support aircraft.

Supplementing the Curtiss P-40 Tomahawks already in service, Mustang Mk Is were first supplied to No. 26 Squadron RAF, then rapidly deployed to 10 additional squadrons by June 1942.

First used in combat over the Dieppe Raid on 19 August 1942, a Mustang of No. 414 (RCAF) Squadron downed one of the formidable Focke-Wulf Fw 190s, the first victory for a Mustang. 

Despite the limited high-altitude performance of the Allison V-1710 engine, the RAF was enthusiastic about its new mount, which “performed magnificently”.

During the Mustang Mk. I’s successful combat initiation, North American’s president Howard “Dutch” Kindelberger pressed the newly redesignated U.S. Army Air Forces (USAAF) for a fighter contract for the essentially similar P-51, 93 of which had passed into the USAAF when the Lend-Lease contract with Britain ran out of funds.

The Mustang Mk IA/P-51 used four 20 mm Hispano wing cannon in place of the original armament, a combination of four wing-mounted .30 in (7.62 mm) M1919 Browning machine guns and four .50 in (12.7 mm) M2 Browning machine guns, two of which were mounted in the wings, while the second pair was mounted in the “chin”, or lower engine cowling, and synchronized to fire through the propeller.

No funds were available for new fighter contracts in fiscal year 1942, but General Oliver P. Echols and Fighter Project Officer Benjamin S. Kelsey wanted to ensure that the P-51 remained in production.

Since appropriations were available for an attack aircraft, Echols specified modifications to the P-51 to turn it into a dive bomber.

The contract for 500 A-36A aircraft fitted with bomb racks, dive brakes, and heavier-duty wing, was signed by Kelsey on 16 April 1942, even before the first flight of the first production P-51 in May 1942.

With orders on the books, North American Aviation (NAA) began modifying the P-51 to accept the bomb shackles which had already been tested in a “long-range ferry” program that the RAF had stipulated.

Engineering studies totalling 40,000 hours and wind tunnel testing with a ⅛-scale model were completed in June 1942.

Utilizing the basic P-51 airframe and Allison engine, structural reinforcing “beefed up” several high stress areas and “a set of hydraulically operated dive brakes were installed in each main wing plane”.

Due to the slightly inboard placement of the bomb racks and unique installation of four cast aluminium dive brakes, a complete redesign of the P-51 wing was required.

The first A-36A (42-83663) was rolled out of the NAA Inglewood plant in September 1942, rapidly going through flight testing with the first flight in October, with deliveries commencing soon after of the first production machines.

The A-36A continued the use of nose-mounted .50 in (12.7 mm) machine guns along with wing armament of four .50 in (12.7 mm) calibre machine guns.

The USAAF envisaged that the dive bomber would operate mainly at altitudes below 12,000 ft (3,700 m) and specified the use of a sea level-rated Allison V-1710-87, driving a 10 ft 9 in (3.28 m)-diameter three bladed Curtiss-Electric propeller and delivering 1,325 hp (988 kW) at 3,000 ft (910 m).

The main air scoop inlet was redesigned to become a fixed unit with a larger opening, replacing the earlier scoop which could be lowered into the airstream.

In addition, the A-36 carburettor air intake was later fitted with a tropical air filter to stop sand and grit being ingested into the engine.

The USAAF later ordered 310 P-51As, which were essentially A-36s without the dive-brakes and nose-mounted weapons, leaving an armament of four wing-mounted .50 in (12.7 mm) Browning machine guns. 

An Allison V-1710-81 1,200 hp (890 kW) was fitted and used the same radiator and air intake as the A-36A.

The P-51A was still fitted with bomb racks although it was not intended to be used primarily as a fighter-bomber and the racks were mainly used to carry drop tanks.





32 ft 3 in (9.83 m)


37 ft 0.25 in (11.28 m)


12 ft 2 in (3.71 m)

Gross weight

10,000 lb (4,535 kg)


1 × Allison V-1710-87 liquid-cooled piston V12 engine,

1,325 hp (988 kW)


Maximum speed

365 mph (590 km/h, 315 kn)

Cruise speed

250 mph (400 km/h, 215 kn)


550 mi (885 km, 478 nmi)

Service ceiling

25,100 ft (7,650 m)


6 × 0.50 in (12.7 mm) M2 Browning machine guns

Up to 1,000 lb (454 kg) of bombs on two underwing hardpoints.


Share on facebook