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Heinkel He 111

Discussion in 'Axis Bomber Planes' started by Spitfire XIV-E, Sep 15, 2010.

  1. Spitfire XIV-E

    Spitfire XIV-E New Member

    Jul 26, 2007
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    Heinkel He 111

    Role Medium bomber
    Manufacturer Heinkel Flugzeugwerke
    Designed by Siegfried and Walter Günter
    First flight 24 February 1935
    Introduced 1935
    Retired 1945 (Luftwaffe)
    Primary user Luftwaffe
    Produced 1935–1944
    Number built 32 V series prototype aircraft
    12 civilian airliners
    808 pre war aircraft
    5,656 aircraft (1939–1945)
    Total: 6,508.
    Variants CASA 2.111

    The Heinkel He 111 was a German aircraft designed by Siegfried and Walter Günter in the early 1930s in violation of the Treaty of Versailles. Often described as a "Wolf in sheep's clothing", it masqueraded as a transport aircraft, but its purpose was to provide the Luftwaffe with a fast medium bomber.

    Perhaps the best-recognised German bomber due to the distinctive "greenhouse" nose of later versions, the Heinkel was the most numerous and the primary Luftwaffe bomber during the early stages of World War II. It fared well until the Battle of Britain, when its weak defensive armament, relatively low speed, and poor manoeuvrability were exposed. Nevertheless, it proved capable of sustaining heavy damage and remaining airborne. As the war progressed, the He 111 was used in a variety of roles on every front in the European Theatre. It was used as a strategic bomber during the Battle of Britain, a torpedo bomber during the Battle of the Atlantic, and a medium bomber and a transport aircraft on the Western, Eastern, Mediterranean, Middle Eastern, and North African Fronts.

    Although constantly upgraded, the Heinkel He 111 became obsolete during the latter part of the war. It was to have been replaced by the Luftwaffe's Bomber B project, but the delays and eventual cancellation of the project forced the Luftwaffe to continue using the He 111 until the end of the war. Manufacture ceased in 1944, at which point, piston-engine bomber production was largely halted in favour of fighter aircraft. With the German bomber force defunct, the He 111 was used for transport and logistics.

    The design of the Heinkel endured after the war in the CASA 2.111. Its airframe was produced in Spain under license by Construcciones Aeronáuticas SA. The design differed significantly in powerplant only. The Heinkel's descendant continued in service until 1973, when it was retired.

    Design and development
    Design conception

    In the early 1930s Ernst Heinkel decided to build the world's fastest passenger plane, a goal met with scepticism by Germany's aircraft industry and political leadership. Heinkel entrusted development to Siegfried and Walter Günter, both fairly new to the company and untested. In June 1933 Albert Kesselring visited Heinkel's offices. Kesselring was head of the Luftwaffe Administration Office: at that point Germany did not have a State Aviation Ministry but only an aviation commissariat, the Luftfahrtkommissariat. Kesselring was hoping to build a new air force out of the Flying Corps being constructed in the Reichswehr and convinced Heinkel to move his factory from Warnemunde to Rostock and turn it over to mass production with a force of 3,000 employees who would produce the first He 111. Heinkel began a new design for civil use in response to new American types that were appearing, the Lockheed 12, Boeing 247 and Douglas DC-2.

    The first single-engined Heinkel He 70 Blitz ("Lightning") rolled off the line in 1932 and the type immediately started breaking records. In its normal four-passenger version its speed reached 380 km/h (230 mph), powered by a 447 kW (600 hp) BMW VI engine. The elliptical wing that the Günther brothers had already used in the Bäumer Sausewind sports plane before they joined Heinkel became a feature in this and many subsequent designs they developed. The design drew the interest of the Luftwaffe, which was looking for an aircraft with dual bomber/transport capabilities.

    Heinkel He 111 in flight. Note the elliptical wing.The He 111 was a twin-engine version of the Blitz, preserving the elliptical inverted gull wing, small rounded control surfaces and BMW engines, so that the new design was often called the Doppel-Blitz ("Double Blitz"). When the Dornier Do 17 displaced the He 70, Heinkel needed a twin-engine design to match its competitors. Heinkel spent 200,000 hours developing it. The fuselage length was extended to just over 17.4 m/57 ft (from 11.7 m/38 ft 4½ in) and wingspan to 22.6 m/74 ft (from 14.6 m/48 ft).

    First flight
    The first He 111 flew on 24 February 1935, piloted by chief test pilot Gerhard Nitschke, who was ordered not to land at the company's factory airfield at Rostock-Marienehe, as this was considered too short, but at Rechlin. He ignored these orders and landed back at Marienehe. He said that the He 111 performed slow manoeuvres well and that there was no danger of overshooting the runway. Nitschke also praised its high speed "for the period" and "very good-natured flight and landing characteristics", stable during cruising, gradual descent and single-engined flight and having no nose-drop when the undercarriage was operated. However during the second test flight Nitschke revealed there was insufficient longitudinal stability during climb and flight at full power and the aileron controls required an unsatisfactory amount of force.

    By the end of 1935, prototypes V2 V4 had been produced under civilian registrations D-ALIX, D-ALES and D-AHAO. D-ALES became the first prototype of the He 111A-1. On 10 January 1936, and received recognition as the "fastest aircraft in the world", as its speed exceeded 402 km/h (250 mph). However, this was incorrect; the fastest aircraft at that time was the Macchi M.C.72, which broke the record in 1934. The design would have achieved a greater total speed had the DB 600 engines of 746 kW (1,000 hp) been added. However, German aviation industries lacked power plants with more than 447 kW (600 hp). Heinkel were forced to use the BMW VI glycol-cooled engine.

    During the war, test pilot Eric Brown evaluated many Luftwaffe aircraft. Among them was a He 111H-1 of Kampfgeschwader 26 which force landed at the Firth of Forth on 9 February 1940. Brown described his impression of the He 111s unique greenhouse nose:

    The overall impression of space within the cockpit area and the great degree of visual sighting afforded by the Plexiglas panelling were regarded as positive factors, with one important provision in relation to weather conditions. Should either bright sunshine or rainstorms be encountered, the pilot's visibility could be dangerously compromised either by glare throwback or lack of good sighting.

    Taxiing was easy and was only complicated by rain, when the pilot had to slide back the window panel and look out to establish direction. On take off, Brown reported very little "swing" and the aircraft was well balanced. On landing, Brown noted that approach speed should be above 145 km/h (90 mph) and should be held until touch down. This was to avoid a tendency by the He 111 to drop a wing, especially on the port side.

    In the mid-1930s, Dornier Flugzeugwerke and Junkers competed with Heinkel for RLM contracts. The main competitor to the Heinkel was the Junkers Ju 86. In 1935, comparison trials were undertaken with the He 111. At this point, the Heinkel was equipped with two BMW V1 engines while Ju 86A was equipped with two Jumo 205Cs, both of which had 492 kW (660 hp). The He 111 had a slightly heavier takeoff weight of 8,220 kg (18,120 lb) compared to the Ju 86's 8,000 kg (17,640 lb) and the maximum speed of both aircraft was 311 km/h (193 mph).[10] However the Ju 86 had a higher cruising speed of 177 mph, 9 mph faster than the He 111. This stalemate was altered drastically by the appearance of the DB 600C, which increased the He 111's power by 164 kW (220 hp). The RLM awarded both contracts, and Junkers sped up development and production at a breathtaking pace, but the financial expenditure for the Junkers was huge. In 1934-1935, 3,800,000 RM (4½% of annual turnover) was spent. The Ju 86 appeared at a large amount of flight displays all over the world which helped sales to the RLM and abroad. Dornier, also currently competing with their Do 17, and Heinkel were not as successful. However in production terms the He 111 dominated with 8,000 examples produced. Just 846 Ju 86s were produced, and the Ju 86's weak performance could not match that of the He 111. Having dropped out of the race, Junkers concentrated on the Junkers Ju 88 design. It would be the He 111 that entered the Luftwaffe as the dominant numerical type at the beginning of the Second World War.

    In view of this disaster [failure of the Ju 86], it was understandable that the Luftwaffe encouraged with particular urgency and attention conversion of the He 111 into a standard bomber. This was pursued in a similar manner to the Ju 86. Three machine-gun stands were installed that, spacewise, were more favourable, especially when the entire fuselage nose, including the cockpit, was later expanded to make provision for an all-round-vision canopy. Nobody sang praises to my fast commercial aircraft, something that eventually happened.

    "The sheep": early civilian variants
    He 111C
    The first prototype, He 111 V1 (W.Nr. 713, D-ADAP), first flew from Rostock-Marienehe on 24 February 1935.[13] It was followed by the civilian-equipped V2 and V4 in May 1935. The V2 (W.Nr. 715, D-ALIX) used the bomb bay as a four-seat "smoking compartment", with another six seats behind it in the rear fuselage. V2 entered service with Lufthansa in 1936, along with six other newly-built versions known as the He 111 C. The He 111V4 was unveiled to the foreign press on 10 January 1936. Nazi propaganda inflated the performance of the He 111C, announcing its maximum speed as 400 km/h (249 mph), in reality its performance standing at 360 km/h (224 mph). The He 111C-0 was a commercial version and took the form of the V4 prototype design. The first machine, designated D-AHAO "Dresden". It was powered by the BMW VI engine and could manage a range (depending on the fuel capacity) of 1,000 km (621 mi) to 2,200 km (1,367 mi) and a maximum speed of 310 km/h (193 mph). The wing span on the C series was 22.6 m (74 ft 1¾in). The fuselage dimensions stood at 17.1 m (56 ft 1¾in) in the He 111V1, but changed in the C to 17.5 m (57 ft 5 in). The Jumo 205 diesel-type powerplant engine replaced the BMW VI. Nevertheless, the maximum speed remained in the 220–240 km/h (137–149 mph) bracket. This was increased slightly when the BMW 132 engines were introduced.

    A general problem existed in powerplants. The He 111 was equipped with BMW VI glycol-cooled engines. The German aviation industry lacked powerplants that could give an output more than 600 hp. The engines that were of suitable quality were kept for military use, frustrating German airline Lufthansa and forcing it to rely on the BMW VI or 132s.

    He 111G
    The He 111G was an upgraded variant and had a number of differences to its predecessors. To simplify production the leading edge of the wing was straightened, like the bomber version. Quite a few different engine types were used, among them the BMW 132, BMW VI, DB 600 and DB601A. Some C variants had been upgraded with the new wing modifications. A new BMW 132H engine was also used in a so-called Einheitstriebwerk (unitary powerplant). These radial engines were used in the Junkers Ju 90 and the Focke-Wulf Fw 200. The wing units and engines were packed together as complete operating systems, allowing for a quick change of engine. The He 111G was the most powerful as well as the fastest commercial version. The G-0 was given the BMW VI 6.0 ZU. Later variants had their powerplants vary. The G-3 for example was equipped with the BMW 132. The G-4 was powered by DB600G inline 950 hp engine and the G-5 was given the DB601A with a top speed of 410 km/h (255 mph). By early 1937, eight G variants were in Lufthansa service. The maximum number of He 111s in Lufthansa service was 12. The He 111 operated all over Europe and flew flights as far away as South Africa. Commercial development ended with the He 111G.

    Basic design (based on the He 111 H-3)
    The design of the He 111A-L initially had a conventional stepped cockpit. The introduction of the P variant meant that the He 111P and following production variants would be fitted with a fully glazed "bullet" or "fishbowl"-like nose. The stepped cockpit now merged into the glazed nose which housed the pilot, bombardier, and navigator. Within the cockpit the pilot was on the left and the navigator/bomb aimer on the right. The navigator went forward to the prone bomb-aiming position, or could tilt his chair to one side so that he could move into the rear of the aircraft. There was no cockpit floor below the pilots feet - the rudder pedals being on arms - giving very good visibility below.

    The fuselage contained two major bulkheads. The cockpit was at the front of the first bulkhead. The nose was fitted with a rotating machine gun mount which was offset to allow the pilot a better field of forward vision. The cockpit was fully glazed, with the exception of the lower right section, which acted as a platform for the bombardier-gunner to be positioned. The bombsight penetrated through the cockpit floor into a protective housing on the external side of the cockpit area. Between the forward and rear bulkhead was the bomb bay, which was constructed with a double-frame to strengthen it for carrying the bomb load. The space between the bomb bay and rear bulkhead was used up by Funkgerät radio equipment and contained the dorsal and ventral gunner positions. The rear bulkhead itself contained a hatch which led to the rest of the fuselage which was held together by a series of stringers. The wing was a two spar design. The fuselage was formed of stringers to which the fuselage skin was riveted. Internally the frames were fixed only to the stringers which made for simpler construction but at the loss of some rigidity.

    Inside Wk Nr 701152 He 111 H-20. Looking forward to the first bulkhead from the ventral gunner's position. The control column and cockpit glazing is visible in the central backgroundThe wings' leading edges were swept back to a point inline with the engine nacelles, while the trailing edges were angled forward slightly. The wing contained two 700 L (190 US gal) fuel tanks between the inner wing main spars, while at the head of the main spar the oil coolers were fitted. Between the outer spars, a second pair of reserve fuel tanks were located carrying an individual capacity of 910 L (240 US gal) of fuel. The outer trailing edges were formed by the ailerons and flaps, which were met by smooth wing tips which curved forward into the leading edge. The outer leading edge sections were installed in the shape of a curved "strip nosed" rib, which was positioned ahead of the main spar. Most of the interior ribs were not solid, with the exception of the ribs located between the rear main spar and the flaps and ailerons. This was of solid construction, though even they had lighting holes.

    The control systems also had some innovations. The control column was centrally placed and the pilot sat on the port side of the cockpit. The column had an extension arm fitted and had the ability to be swung over to the starboard side in case the pilot was incapacitated. The control instruments were located above the pilot's head in the ceiling which allowed viewing and did not block the pilot's vision. The fuel instruments were electrified. The He 111 used the inner fuel tanks closest to the wing root. The outer tanks acted as reserve tanks. The pilot would be alerted to the fuel level when the tank had 100 L (26 US gal) left. A manual pump was available in case of electrical or power failure, but the delivery rate of just 4½ L (1.2 US gal) per minute demanded that the pilot fly at the lowest possible speed and just below 3,048 m (10,000 ft). Fortunately, the He 111 handled well at low speeds.

    The defensive machine gun positions were located in the glass nose, the ventral, dorsal and lateral positions in the fuselage and all offered a significant field of fire. The design of the nose allowed the machine gun position to be moved 10° upwards from the horizontal and 15° downwards. The gun can also traverse some 30° laterally. Both the dorsal and ventral machine guns can move up and downwards by 65°. The dorsal position can also move the 13 mm (.51 in) MG 131 machine gun 40° laterally, but the ventral 7.92 mm (.312 in) MG 81Z machine gun could be moved 45° laterally. Each MG 81 single machine gun mounted in the side of the fuselage could move laterally by 40°, and could move upwards from the horizontal by 30° and downwards by 40°.

    Military variants

    He 111 A - D

    A He 111E in Luftwaffe service, 1940. The early variants had a conventional, stepped cockpit.The initial reports from the test pilot, Gerhard Nitschke, were favourable. The plane's flight performance and handling were impressive although it dropped its wing in the stall. As a result, the passenger variants had their wings reduced from 25 m (82 ft) to 23 m (75 ft). The military aircraft - V1, V3 and V5 - spanned just 22.6 m (74.1 ft).[13] The first prototypes were underpowered, as they were equipped with 431 kW (578 hp) BMW VI 6.0 six-cylinder in-line engines. This was eventually increased to 745 kW (999 hp) with the fitting of the DB (Daimler-Benz) 600 engines into the V5, which became the prototype of the "B" series.

    Only 10 He 111A-0 models based on the V3 were built, but they proved to be underpowered and were eventually sold to China. The type had been lengthened by 1.2 m (3.9 ft) due to the added 7.92 mm (.312 in) MG 15 machine gun in the nose. Another gun position was installed on top of the fuselage, and another in a ventral position, which could retract. The bomb bay was divided into two compartments and could carry 680 kg (1,500 lb) of bombs. The problem with these additions was that the weight of the aircraft reached 8,200 kg (18,080 lb). The He 111's performance was seriously reduced; in particular, the BMW VI 6.0 Z engines were not now powerful enough. The increased length also altered the 111's aerodynamic strengths and reduced its excellent handling on takeoffs and landings. The crews found the aircraft difficult to fly, and its top speed was reduced significantly. Production was shut down after the pilots reports reached the RLM. However, a Chinese delegation was visiting Germany and they considered the He 111 A-0 fit for their needs and purchased seven machines.

    The first He 111B made its maiden flight in the autumn of 1936. The first production batch rolled off the production lines that summer, at Rostock. Seven B-0 pre-production aircraft were built, bearing the Werknummern (Works numbers) 1431 to 1437. The B-0s were powered by DB 600C engines fitted with variable pitch airscrews.[24] The screws increased output by 149 kW (200 hp).[24] The B-0 had a MG 15 machine gun installed in the nose. The B-0 could also carry 1,500 kg (3,310 lb) in their vertical cells.[24] The B-1 had some minor improvements. The installation of the revolving gun-mount in the nose and a flexible Ikaria turret under the fuselage.[24] After improvements, the Reichsluftfahrtministerium (RLM- Reich Air Ministry) ordered 300 He 111B-1s; the first were delivered in January 1937. The B-2 variant had its engines upgraded to the supercharged 634 kW (850 hp) DB 600C, or in some cases, the water-cooled 690 kW (925 hp) 600G. The B-2 began to roll off the production lines at the Heinkel works in Oranienburg in 1937. The He 11B-3 was a modified trainer. Some 255 B-1s were ordered. However, the production orders were impossible to fulfill and only 28 B-1s were built. Owing to the production of the new He 111E, only a handful of He 111B-3s were produced. Due to insufficient capacity, Dornier, Arado and Junkers built the He 111B series at their plants in Wismar, Brandenburg and Dessau. The B series compared favourably with the capacity of the A series. The bomb load increased to 1,500 kg (3,300 lb), while there was also an increase in maximum speed and altitude to 215 mph (344 km/hr) and 22,000 ft (6,700 m) The armament was settled at three machine gun positions. Save for the windshield, the dorsal gunner's position was exposed to the elements.

    In late 1937, the D-1 series entered production. However, the DB 600Ga engine with 781 kW (1,047 hp) planned for this variant was instead allocated to the Bf 109 and Bf 110 production lines. Heinkel then opted to use Jumo engines, and the He 111 V6 was tested with Jumo 210 G engines, but was vastly underpowered. However, the improved 745 kW (999 hp) Jumo 211 A-1 powerplant prompted the cancellation of the D series altogether and concentration on the design of the E series.

    [edit] He 111 E
    The pre-production E-0 series were built in small numbers. Fitted with Jumo 211 A-1 engines loaded with retractable radiators and exhaust systems. The variant could carry 1,700 kg (3,748 lb) of bombs giving it a take off weight og 10.300 kg (22,707 lbs). The development team for the Jumo 211 A-1 engines managed to increase engine power to 930 hp, subsequently the He 111 E-1s bomb load capacity increased to 2,000 kg (4,410 lb) and a top speed of 242 mph (390 km/hr).

    The E-1 variant with Jumo 211A-1 engines was developed in 1937, the He 111 V6 being the first production variant. The E-1 had its original powerplant, the DB 600 replaced with the Jumo 210 Ga inline engines. The more powerful Jumo 211 A-1 engines desired by the RLM were not yet ready for installation. Another trial aircraft, He 111 V10 (D-ALEQ) was to be fitted with two oil coolers necessary for the Jumo 211 A-1 installation. The lubricant coolers being installed into the engine fairing in a streamline manner.

    The E-1s came off the production line in February 1938, in time for a number of these aircraft to serve in the Condor Legion during the Spanish Civil War in March 1938. In a way, the positive performance influenced later variants. The Luftwaffe believed that because the E variant could outrun enemy fighters, there was no need to upgrade the defensive weaponry, which would prove a mistake from the Battle of Britain onward. The defensive armament of the ten ton heavy aircraft corresponded to the He 111B-2 variant. The fuselage bomb bay used four bomb racks, in later versions eight modular standard bomb racks designed to carry one SC 250 kg (550 lb) bomb, or four SC 50 kg (110 lb) bombs each in nose up orientation (which resulted in the bombs doing a flip as they were dropped out of the aircraft). These modular standard bomb racks were a common feature on the first generation of Luftwaffe bombers (including the Junkers Ju 52), but it turned out that they limited the ordnance selection to bombs of only two sizes. Since they had to be built strong enough to carry heavy bombs without contributing to the structural integrity of the aircraft, these racks were abandoned in later designs.

    The E-2 series was not produced, and was dropped in favour of producing the E-3. with only a few modifications, such as external bomb racks. Its design features were distinguished by improvements FuG radio systems, and the Jumo 211 A-3 installed in place of the A-1, albeit experimentally. The E-3 series was equipped with the Jumo 211 A-3 for the duration of the series which packed 1,100 hp.

    He 111E of the Legion Kondor. Note the early variants conventional "stepped" cockpitThe E-4 variant was fitted with external bomb racks also and the empty bomb bay space was filled with a 835 L (221 US gal) tank for aviation fuel and a further 115 L (30 US gal) oil tank. This increased the loaded weight to nearly 9.9 tonnes (11 tons), but increased its range to 1,800 km (1,130 mi). The modifications allowed the He 111 to perform both long and short range missions.[30] The E-4s eight internal vertically aligned bomb racks could each carry a 250 kg (550 lb). The last E Variant, the He 111E-5, was powered by the Jumo 211A-3, and retained the 835 L (221 US gal) fuel tank on the port side of the bomb bay. Only a few of the E-4 and E-5 were built.

    The RLM had acquired an interest in rocket boosters fitted for the sake of simplicity below the wings of a heavily loaded bomber to cut down the length of runway needed for take-off. Once in the air the booster canisters would be jettisoned by parachute for re-use. The firm of Hellmuth Walter, at Kiel, handled this development. The first standing trials and tests flights of the boosters were held in 1937 at Neuhardenberg with test pilot Erich Warsitz at the controls of Heinkel He 111E AMUE.

    He 111 F
    The He 111 design quickly ran though a series of minor design versions to fix one sort of problem or another. One of the more obvious changes started with the He 111 F models, which moved from the elliptical wing to one with straight leading and trailing edges, which could be manufactured more efficiently. The dimensions of the new design had a wing span of 22.6m (74 ft 1¾in) and an area of 87.60m² (942.90 ft). The industrial capacity of Heinkel was limited and production was delayed. 24 machines of the F-1 series, fitted with DB 600 engines, were exported to Turkey. Another 20 of the F-2 variant were built. The Turkish interest, prompted by the fact the tests of the next prototype, He 111 V8, was some way off, prompted the RLM to order 40 F-4s with Jumo 211 A-3 engines. These machines were built and entered service in early 1938. This fleet was used as a transport group during the Demyansk Pocket and Battle of Stalingrad. At this time, development began on the He 111 J. It was powered by the DB 600 and was intended as a torpedo bomber. As a result, it lacked an internal bomb bay and carried two external torpedo racks. The RLM gave an order for the bomb bay to be retrofitted; this variant became known as the J-1. In all but the powerplant, it was identical to the F-4. The final variant of the F series was the F-5. The F-5 was designed as a bomber. Its bombsight and powerplant configuration equipment was identical to the E-5. The F-5 was rejected as a production variants owing to the superior performance of the He 111P-1 which was being developed.

    He 111 J
    The He 111's low-level performance attracted the interest of the Kriegsmarine. The navy believed the He 111 would make an excellent torpedo bomber, and as a result, the He 111 J was produced. The J was capable of carrying torpedoes and mines. The Kriegsmarine eventually dropped the program as they deemed the four man crew too expensive in terms of manpower. The RLM however, had progressed too far with the development, and continued to build the He 111 J-0. Some 90 (other sources claim 60 were built in 1938 and were then sent to Küstenfliegergruppe 806. The He 111J-0 was powered by the DB 600G without retractable radiators. It could carry a 2,000 kg (4,410 lb) payload. Few of the pre-production J-0s were ever fitted with the DB 600G. Instead, the DB 600 was used and the performance of the powerplant left much to be desired. The torpedo bomber was not pursued. The J-1 was identical to the F which the exception of the powerplants. The J was used in training schools until 1944. Some J-1s were used as test beds for Blohm & Voss L 10 radio-guided air-to-ground torpedo missiles.

    He 111 P

    He 111P dropping bombs over Poland, September 1939The He 111 P incorporated the updated Daimler-Benz DB 601A-1 water cooled engine and featured a newly designed nose section, including an asymmetric Ikaria nose mounting for an MG 15 machine gun that replaced the 'stepped' cockpit with a roomier and aerodynamically favourable glazed "dome" over the front of the aircraft. These improvements allowed the aircraft to reach 475 km/h (295 mph) at 5,000 m (16,400 ft) and a cruise speed of 370 km/h (230 mph), although a full bombload reduced this figure to 300 km/h (190 mph) The design was implemented in 1937 because pilot reports indicated problems with visibility. The pilot's seat could actually be elevated, with the pilot's eyes above the level of the upper glazing, complete with a small pivoted windscreen panel, to get the pilot's head above the level of the top of the "glass tunnel" for a better forward view for takeoffs and landings.

    One of Heinkel's rivals, Junkers, built 40 He 111Ps at Dessau. On 8 October 1938, the Junkers Central Administration commented:

    Two aircraft were able to be inspected on 6th October in Bernburg. Apparent are the externally poor, less carefully designed components at various locations, especially at the junction between the empennage and the rear fuselage. All parts have an impression of being very weak; especially when one is used to taking a long look at Junkers' designs, one cannot dispel a feeling of uncertainty. The visible flexing in the wing must also be very high. The left and right powerplants are interchangeable. Each motor has an exhaust-gas heater on one side, but it is not connected to the fuselage since it is probable that as a result of incorrect air feed, the warm air in the fuselage is not free of carbon monoxide (CO). The fuselage is not subdivided into individual segments, but is attached over its entire length, after completion, to the wing centre section. Outboard of the powerplants, the wings are attached by universal joints. The latter can in no way be satisfactory and have been the cause of several failures.

    The new design was powered by the DB 601 Ba engine with 1,175 PS and reduced the length of the aircraft by 1.1 m (3.6 ft). The He 111P's DB601 powerplant exhaust pipes had a second outlet on the top of the engine which pumped hot air back into the aircraft to warm crews. It was designated as P-0, and the first production lines reached their units in Fall 1938. In May 1939, the P-1 and P-2 went into service with improved radio equipment. The P-1 variant was produced with two DB 601Aa powerplants of 1,150 hp. The fuel tanks had the added innovation of self-sealing fuel tanks to protect them from enemy fire. The Nose department itself was now fully glazed and the "stepped up" cockpit was dispensed with. The P-1 was powered by a DB 601Aa engine and given a semi-retractable tail wheel to decrease drag. Armament consisted of a MG 15 mounted in the Ikaria A Stand mount in the nose, and a sliding hood for the fuselage's dorsal B-Stand position. Installation of upgraded FuG III radio communication devices were also made and a new ESAC-250/III vertical bomb magazine was added. The overall takeoff weight was now 13,300 kg (29,321 lb).

    The P-2, like the later P-4, was given stronger armour and two MG 15 machine guns on either side of the fuselage and two external bomb racks. Radio communications consisted of FuG IIIaU radios and the DB601 A-1 replaced the 601Aa powerplants. The Lotfernrohr 7 bombsights, which became the standard bombsight for German bombers, were also fitted to the P-2. The P-2 was also given "field equipment sets", to upgrade the weak defensive armament to four or five MG 15 machine guns. The P-2 had its bomb capacity raised to 4 ESA-250/IX vertical magazines. The P-2 thus had an empty weight of 6,202 kg (13,272 lb), a loaded weight increased to 12,570 kg (27,712 lb) and a maximum range of 2,100 km (1,305 mi).

    The P-3 was powered with the same DB601A-1 engines. The aircraft was also designed to take off with a land catapult (KL-12). A towing hook was added to the fuselage under the cockpit for the cable. Just eight examples were produced, all without bomb equipment. The P-4 contained many changes from the P-2 and P-3. The jettisonable loads were capable of considerable variation. Two external SC 1800 kg (3,960 lb) bombs; two LMA air-dropped anti-shipping mines; one SC 1,800 kg plus four SC 250 kg; or one SC 2,500 kg external bomb could be carried on a ETC Rüstsatz rack. Depending on the load variation, a 835 L fuel and 120 L oil tank could be added in place of the internal bomb bay. The armament consisted of three defensive MG 15 machine guns. But these were not sufficient, so a further six MG 15s and one MG 17 machine gun was added. The radio communications were standard FuG X(10), Peil G V direction finding and FuBI radio devices. Because of the increase in defensive firepower, the crew numbers increased from four to five. The empty weight of the P-4 increased to 6,775 kg (14,936 lb), and the full takeoff weight increased to 13,500 kg (29,762 lb) owing to the mentioned alterations. The P-5 was powered by the DB601A. The variant was mostly used as a trainer and at least 24 production variants were produced before production ceased. The P-5 was alleged to have been fitted with PVC bomb racks, which cannot be confirmed. The P-5 was fitted with meteorological equipment, and was used in Luftwaffe weather units. Many of the He 111 Ps served during the Polish Campaign. With the Junkers Ju 88 experiencing technical difficulties, the He 111 and the Do 17 formed the backbone of the Kampfwaffe. On 1 September 1939, Luftwaffe records indicate the Heinkel strength at 705 (along with 533 Dorniers).

    The P-6 variant was the last production model of the He 111 P series. In 1940, the RLM abandoned further production of the P series in favour of the H versions, mostly because the P-series' Daimler-Benz engines were sorely needed for Messerschmitt Bf 109 and Bf 110 fighter production. The remaining P-6s were redesignated P-6/R2s and used as heavy glider tugs. The most notable difference with previous variants was the upgraded DB608N powerplants.

    The P-7 variant's history is unclear. German archives do not produce any reliable information for this variant, if it existed. The P-8 was said to have been similar to the H-5 fitted with dual controls. Its existence cannot be established. The P-9 was produced as an export variant for the Hungarian Air Force. Due to the lack of DB608E engines, the line was terminated in Summer 1940.

    He 111H, the main variant
    He 111H-1 to H-10
    The H variant of the He 111 series was more widely produced and saw more action during World War II than any other Heinkel variant. Owing to the uncertainty surrounding the delivery and availability of the DB 601 engines, Heinkel began tests with the 820 kW (1,100 hp) Junkers Jumo 211 powerplants. The somewhat larger size and greater weight of the Jumo 211 engines were unimportant considerations for a twin engine design, and the Jumo was used on almost all early-war bomber designs. When the Jumo was fitted to the P model it became the He 111 H.

    He 111H on a torpedo training exercise, 10 October 1941The He 111H-1 was fitted with a standard set of three 7.92 mm (.312 in) MG 15s and eight SC 250 250 kg (550 lb) or 32 SC 50 50 kg (110 lb) bombs. The same armament was used in the H-2 which started production in August 1939. The P-series was gradually replaced on the eve of war with the new the H-2, powered by improved Jumo 211 A-3 engines of 820 kW (1,100 hp). A count on 2 September 1939 revealed that the Luftwaffe had a total of 787 He 111s in service, with 705 combat ready, including 400 H-1 and H-2s that had been produced in a mere four months. Production of the H-3, powered by the 895 kW (1,200 hp) Jumo 211 D-1, began in October 1939. The experiences during the Polish Campaign lead to an increase in defensive armament. MG 17s were fitted whenever possible and the number of machine guns was increased to seven. Normally one MG 17 would be installed in the nose, one in the ventral position, dorsal position and one in each waist window position. The two waist positions received an additional MG 15 or 17. On some Heinkels a permanent belt-fed MG 17 was installed in the tail.

    After the Battle of Britain, smaller scale production of the H-4s began. The H-4 was virtually identical to the He 111P-4 with the DB 600s swapped for the Jumo 211D-1s. This variant also differed from the H-3 in that could either carry 2,000 kg (4,410 lb) of bombs internally or mount one or two external racks to carry one 1,800 kg (3,970 lb) or two 1,000 kg (2,210 lb) bombs. As these external racks blocked the internal bomb bay doors, a combination of internal and external storage was not possible. A PVR 1006L bomb rack was fitted externally and a 835 L (221 US gal) tank added. The PVR 1006L was capable of carrying a SC 1000 1,000 kg (2,210 lb) bomb. Some H-4s had their PVC racks modified to drop torpedoes. Later modifications enabled the PVC 1006 to carry a 2,500 kg (5,510 lb) "Max" bomb. But 1,000 kg (2,200 lb) "Hermann" or 1,800 kg (3,970 lb) "Satans" were used more widely. The H-5 series followed in February 1941, with heavier defensive armament. Like the H-4, it retained a PVC 1006 L bomb rack to enable it to carry heavy bombs under the fuselage. The first ten He 111H-5s were pathfinders, and selected for special missions. The aircraft sometimes carried 25 kg flashlight bombs which acted as flares. The H-5 could also carry heavy fire bombs, either heavy containers or smaller incendiary devices attached to parachutes. The H-5 also carried LM A and LM B aerial mines for anti-shipping operations. After the 80th production aircraft, the PVC 1006 L bomb rack was removed and replaced with a heavy-duty ETC 2000 rack, enabling the H-5 to carry the SC 2500 "Max" bomb, on the external ETC 2000 rack, which enabled it to support the 5,000 lb bomb. Some H-3 and H-4s were equipped with barrage balloon cable-cutting equipment in the shape of cutter installations forward of the engines and cockpit. They were designated H-8, but later named H8/R2. These aircraft were difficult to fly and the production stopped. The H-6 initiated some overall improvements in design. The Jumo 211 F-1 engine of 1,007 kW (1,350 hp) increased its speed while the defensive armament was upgraded with one 20 mm MG FF cannon in the nose position, one MG 15 in the ventral turret, and in each of the fuselage side windows (optional). Some H-6 variants carried tail-mounted MG 17 defensive armament. The performance of the H-6 was much improved. The climb rate was higher and the machine could reach a slightly higher ceiling of 8,500 m (27,200 ft). When heavy bomb loads were added, this ceiling was reduced to 6,500 m (20,800 ft). The weight of the H-6 increased to 14,000 kg (30,600 lb). Some H-6s received Jumo 211F-2s which improved a low-level speed of 226 mph (365 km/h). At an altitude of 6,000 m (19,200 ft) the maximum speed was 270 mph (435 km/h). If heavy external loads were added, the speed was reduced by 21.75 mph (35 km/h) Other designs of the mid-H series included the He 111 H-7 and H-8. The airframes were to be rebuilds of the H-3/H-5 variant. Both were designed as nightbombers and were to have two Jumo 211F-1s installed. The intention was for the H-8 to be fitted with cable-cutting equipment and barrage ballon deflectors on the leading edge of the wings. The H-7 was never built. The H-9 was intended as a trainer with dual control columns. The airframe was a H-1 variant rebuild. The powerplants consisted of two JumoA-1s or D-1s. The H-10 was also designated to trainer duties. Rebuilt from an H-2 of H-3 airframe, it was installed with full defensive armament including 13 mm (.51 in) MG 131 and 7.92 mm (.312 in) MG 81Z machine guns. It was to be powered by two Jumo 211A-1s, D-1s or F-2s.

    Later H variants, H-11 to H-20

    A formation of He 111Hs, circa 1940In the summer of 1942, the H-11, based on the H-3 was introduced. With the H-11, the Luftwaffe had at its disposal a powerful medium bomber with heavier armour and revised defensive armament. The drum-fed 7.92 mm (.312 in) MG 15 was replaced with a belt-fed 13 mm (.51 in) MG 131 in the now fully enclosed dorsal position (B-Stand); the gunner in the latter was now protected with armoured glass. The single MG 15 in the ventral C-Stand was also replaced, with a belt-fed 7.92 mm (.312 in) MG 81Z with much higher rate of fire. The beam positions originally retained the single MG 15s, but the H-11/R1 replaced these with twin MG 81Z as well; this latter arrangement was standardized in November 1942. The port internal ESAC bomb racks could be removed, and an 835 L (221 US gal) fuel tanks installed in its place. Many H-11s were equipped with a new PVC rack under the fuselage, which carried five 250 kg (550 lb) bombs. Additional armour plating was fitted around crew spaces, some of it on the lower fuselage and could be jettisoned in an emergency. Engines were two 1,000 kW (1,340 hp) Junkers Jumo 211F-2, allowing this variant to carry a 2,000 kg (4,410 lb) payload to a range of 2,340 km (1,450 mi). Heinkel built 230 new aircraft of this type and converted 100 H-3s to H-11s by the summer of 1943.

    The third mass production model of the He 111H was the H-16, entering production in late 1942. Armament was as on the H-11, with some differences. The 20 mm MG FF cannon was deleted, as the H-16s were seldom employed on low-level missions, was replaced with a single MG 131 in a flexible installation in the nose (A-Stand). On some aircraft, designated He 111H-16/R1, the dorsal position was replaced by DL 131 electrically-powered turret, armed with a MG 131. The two beam and the aft ventral positions were provided with MG 81Zs, as on the H-11. The two 1,000 kW (1,340 hp) Jumo 211 F-2 provided a maximum speed of 434 km/h (270 mph) at 6,000 m (19,690 ft); cruising speed was 390 km/h (242 mph), service ceiling was 8,500 m (27,900 ft).[55] Funkgerät (FuG) radio equipment. FuG 10P, FuG 16, FuBl Z and APZ 6 were fitted for communication and navigation at night, while some aircraft received the FuG 101a radio altimeter. The H-16 retained its eight ESAC internal bomb cells; four bomb cells, as on previous versions could be replaced by a fuel tank to increase range. ETC 2000 racks could be installed over the bomb cell openings for external weapons carriage. Empty weight was 6,900 kg (15,210 lb) and the aircraft weighed 14,000 kg (30,860 lb) fully loaded for take off. German factories built 1,155 H-16s between the end of 1942 and the end of 1943; in addition, 280 H-6s and 35 H-11s were updated to H-16 standard.

    The last major production variant was the H-20, which entered into production in early 1944. It was powered by two 1,305 kW (1,750 hp) Junkers Jumo 213E-1 engines, turning three-blade, Junkers VS 11 wooden variable-pitch propellers. Heinkel and its licenses built 550 H-20s through the summer of 1944, while 586 H-6s were upgraded to H-20 standard. In contrast to the H-11 and H-16 the H-20, equipped with two Jumo 211F-2s, was given more powerful armament and radio communications. The defensive armament consisted of one MG 131 in an A-Stand gun pod for the forward mounted machine gun position. One rotatable DL 131/1C (or E) gun mount in the B-stand was standard and later MG 131 machine guns were added. Navigational direction finding gear was also installed. The Peil G6 was added to locate targets and the FuBI 2H blind landing equipment was built in to help with night operations. The radio was a standard FuG 10, TZG 10 and FuG 16Z for naviagational direction to the target. The H-20 also was equipped with barrage balloon cable-cutters. The bomb load of the H-20 could be mounted on external ETC 1000 racks, or four ESAC 250 racks. The sub variant H-20/R4 could carry 20 50 kg (110 lb) bombs as external loads.

    One of the most interesting variants was a glider tug, the He 111 Z, standing for Zwilling or twin. It was built from two 111 H-6s joined together with a connecting wing and a fifth engine and used to tow the giant Messerschmitt Me 321 or tow Gotha Go 242 gliders. Ten He 111 Zs were built, and all served until destroyed.

    The He 111H had to be kept in production until 1944 because the RLM failed to provide a successor: the He 177 Greif heavy bomber was plagued by engine problems, and the Bomber B program was eventually abandoned. The vast majority of the 7,300 He 111s produced were the H models, largely identical to the first H introduced in 1939.

    He 111Z
    The He 111Z Zwilling was a design that entailed the merging of two He 111s. The design was originally conceived to tow the Messerschmitt Me 321 glider. Initially, four He 111H-6s were modified. This resulted in a twin-fuselage, five-engine aircraft. They were tested at Rechlin, and the pilots rated them highly. A batch of 10 were produced and five were built from existing H-6s. The machines were joined by a centre wing formed by two sections 6.15 m (20 ft) in length. The powerplants were five Jumo 211F engines at 1,000 kW (1,340 hp) each. Total fuel capacity was 8,570 L (2,260 US gal). This was increased with the addition of four 600 L (160 US gal) drop tanks. It could tow a Gotha Go 242 glider or Me 321 for up to 10 hours at cruising speed. It could also remain airborne if the three centralised powerplants failed. The He 111Z-2s and Z-3s were also planned as heavy bombers carrying 1,800 kg (3,970 lb) of bombs and having a range of 4,000 km (2,500 mi). The ETC extensions allowed for a further four 600 L (160 US gal) drop tanks to be installed.

    The He 111Z-2 could carry four Henschel Hs 293 anti-shipping guided missile, which were guided by the FuG 203b Kehl III missile control equipment. With this load the He 111Z had a range of 1,094 km (680 mi) and a speed of 314 km/h (195 mph). Its maximum bombload was 7,200 kg (15,870 lb). To increase power the five Jumo 211F-2 powerplants were to be fitted with Hirth TK 11 superchargers. The armament was the same as the H-6 with the addition of one 20 mm MG 151/20 in a rotating gun-mount of the centre section. The variant did not display any convincing (stable) flight performance. The layout of the He 111Z had the pilot and his controls in the port fuselage only. Only the controls themselves and essential equipment remaining in the starboard section. The aircraft had a crew of seven; a pilot, first mechanic, radio operator and gunner in the port fuselage, and the observer, second mechanic and gunner in the starboard fuselage. The Z-3 was to be a reconnaissance version and was to have additional fuel tanks increasing its range to 6,000 km (3,730 mi). Production was due to take place in 1944, just as bomber production was being abandoned. The long-range variant designs failed to come to fruition. The He 111Z was to have been used in an invasion of Malta in 1942 and as part of an airborne assault on the Soviet cities Astrakhan and Baku in the Caucasus in the same year. During the Battle of Stalingrad their use was cancelled due to insufficient airfield capacity. Later in 1943 it helped evacuate German equipment and personnel from the Caucasus region and during the Allied invasion of Sicily attempted to deliver reinforcements to the island.[61] During operations, the He 111Z did not have enough power to lift a fully loaded Me-321. The He 111s in RATO (rocket assisted takeoff) units were supplemented by rocket pods. Two were mounted beneath each fuselage and one underneath each wing. This added 500 kg (1,100 lb) in weight, but gave additional thrust to the engines. The pods were then released by parachute after takeoff. The He 111Z's operational history was minimal. One such machine was caught by RAF fighter aircraft over France on 14 March 1944. The He 111Z was towing a Gotha Go 242, and was shot down. Eight were shot down or destroyed on the ground in 1944.

    To meet demand for numbers, Heinkel constructed a factory at Oranienburg. On 4 May 1936, construction began, and exactly one year later the first He 111 rolled off the production line. The RLM Luftwaffe administration office suggested that Ernst Heinkel lend his name to the factory. The "Ernst Heinkel GmbH" was established with a share capital of 5,000,000 Reichsmarks (RM). Heinkel was given a 150,000 RM share. The factory itself was built and belonged to the German state. From this production plant, 452 He 111s and 69 Junkers Ju 88s were built in the first year of the war. German production for the Luftwaffe amounted to 808 He 111s by September 1939. According to Heinkel's memoirs, a further 452 were built in 1939, giving a total of 1,260. But "1940's production suffered extreme losses during the Battle of Britain, with 756 bombers lost". Meanwhile, the He 111's rival - the Ju 88 - had increased production to 1,816 aircraft, some 26 times the number from the previous year. Losses were also considerable the previous year over the Balkans and Eastern Fronts. To compensate, He 111 production was increased to 950 in 1941. In 1942, this increased further to 1,337 He 111s. The Ju 88 production figures were even higher still, exceeding 3,000 in 1942, of which 2,270 were bomber variants. In 1943, He 111 increased to 1,405 aircraft. But the Ju 88 still outnumbered it in production terms as its figures reached 2,160 for 1943. The Allied bomber offensives in 1944 and in particular Big Week failed to stop or damage production at Heinkel. Up until the last quarter of 1944, 756 Heinkel He 111s had been built. While Junkers produced 3,013 Ju 88s, of which 600 were bomber versions. During 1939-1944, a total of 5,656 Heinkel He 111s were built compared to 9,122 Ju 88s. As the Luftwaffe was now on the strategic defensive, bomber production and that of the He 111 was suspended. Production in September 1944, the last production month for the He 111, included 118 bombers. Of these 21 Junkers Ju 87s, 74 Junkers Ju 188s, 3 Junkers Ju 388s and 18 Arado Ar 234s were built. Of the Heinkel variants, zero Heinkel He 177s were produced and just two Heinkel He 111s were built.

    He 111 production in 1939
    A He 111 in the preliminary stage of wing installationQuarterly production 1942-1944.

    Year 1942 1943 1944
    Quarter Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4
    Number Produced 301 350 356 330 462 340 302 301 313 317 126 0

    In 1937, 24 He 111F-1s were bought by the Turkish Air Force. The Turks also ordered four He 111G-5s. China also ordered 12 He 111A-0s, but at a cost 400,000 Reichsmark (RM). The aircraft were crated up and transported by sea. At the end of the Spanish Civil War, the Spanish Air Force acquired 59 He 111 "survivors" and a further six He 111s in 1941-1943. Bulgaria was given one He 111H-6, Romania received 10 E-3s, 32 H-3s and 10 H-6s. Two H-10s and three H-16s were given to Slovakia, Hungary was given 3 He 111Bs and 12-13 He 111s by 6 May 1941. A further 80 P-1s were ordered, but only 13 arrived. Towards the end of 1944, 12 He 111Hs were delivered. The Japanese were due to receive 44 He 111Fs, but in 1938 the agreement was cancelled.

    Operational history
    Main article: Heinkel He 111 operational history
    The Heinkel He 111 served on all the German military fronts in the European Theatre of World War II. Beginning the war as a medium bomber it supported the German campaigns in the field until 1943 when, owing to Western Allied and Soviet air superiority, it reverted to a transport aircraft role. Small numbers of Kampgeschwader did continue to operate a small number of He 111s until 1945 in various roles, but mostly at night to avoid Allied fighter aircraft.

    ■He 111 A-0: 10 aircraft built based on He 111 V3, two used for trials at Rechlin, rejected by Luftwaffe all 10 were sold to China".

    ■He 111 B-0: Pre-production aircraft, similar to He 111 A-0, but with DB600Aa engines.

    ■He 111 B-1: Production aircraft as B-0, but with DB600C engines. Defensive armament consisted of a flexible Ikaria turret in the nose A Stand, a B Stand with one DL 15 revolving gun-mount and a C Stand with one MG 15.

    ■He 111 B-2: As B-1, but with DB600GG engines, and extra radiators on either side of the engine nacelles under the wings. Later the DB 600Ga engines were added and the wing surface coolers withdrawn.

    ■He 111 B-3: Modified B-1 for training purposes.

    ■He 111 C-0: Six pre-production aircraft.

    ■He 111 D-0: Pre-production aircraft with DB600Ga engines.

    ■He 111 D-1: Production aircraft, only a few built. Notable for the installation of the FuG X, or FuG 10, designed to operate over longer ranges. Auxiliary equipment contained direction finding Peil G V and FuBI radio blind landing aids.

    ■He 111 E-0: Pre-production aircraft, similar to B-0, but with Jumo 211A-1 engines.

    ■He 111 E-1: Production aircraft with Jumo 211 A-1 powerplants. Prototypes were powered by Jume 210G as which replaced the original DB 600s.

    ■He 111 E-2: Non production variant. No known variants built. Designed with Jumo 211 A-1s and A-3s.

    ■He 111 E-3: Production bomber. Same design as E-2, but upgraded to standard Jumo 211A-3s.

    ■He 111 E-4: Half of 2,000 kg (4,410 lb) bomb load carried externally.

    ■He 111 E-5: Fitted with several internal auxiliary fuel tanks.

    ■He 111 F-0: Pre-production aircraft similar to E-5, but with a new wing of simpler construction with a straight rather than curved taper, and Jumo 211A-1 engines.

    ■He 111 F-1: Production bomber, 24 were exported to Turkey.

    ■He 111 F-2: 20 were built. The F-2 was based on the F-1, differing only in installation of optimised wireless equipment.

    ■He 111 F-3: Planned reconnaissance version. Bomb release equipment replaced with RB cameras. It was to have Jumo 211A-3 powerplants.

    ■He 111 F-4: A small number of staff communications aircraft were built under this designation. Equipment was similar to the G-5.

    ■He 111 F-5: The F-5 was not put into production. The already available on the P variant showed it to be superior.

    ■He 111 G-0: Pre-production transportation aircraft built, featured new wing introduced on F-0.

    ■He 111 G-3: Also known as V14, fitted with BMW 132Dc radial engines.

    ■He 111 G-4: Also known as V16, fitted with DB600G engines.

    ■He 111 G-5: Four aircraft with DB600Ga engines built for export to Turkey.

    ■He 111 J-0: Pre-production torpedo bomber similar to F-4, but with DB600CG engines.

    ■He 111 J-1: Production torpedo bomber, 90 built, but re-configured as a bomber.

    ■He 111 L: Alternative designation for the He 111G-3 civil transport aircraft.

    ■He 111 P-0: Pre-production aircraft featured new straight wing, new glazed nose, Db601Aa engines, and a ventral gondola for gunner (rather than "dust-bin" on previous models).

    ■He 111 P-1: Production aircraft, fitted with three MG 15s as defensive armament.

    ■He 111 P-2: Had FuG 10 radio in place of FuG IIIaU. Defensive armament increased to five MG 15s.

    ■He 111 P-3: Dual control trainer fitted with DB601A-1 powerplants.

    ■He 111 P-4: Fitted with extra armour, three extra MG 15s, and provisions for two externally mounted bomber racks. Powerplants consisted of DB601A-1s. The internal bomb bay was replaced with a 835 L fuel tank and a 120 L oil tank.

    ■He 111 P-5: The P-5 was a pilot trainer. Some 24 examples were built. The variant was powered by DB 601A engines.

    ■He 111 P-6: Some of the P-6s were powered by the DB 601N engines. The Messerschmitt Bf 109 received these engines, as they had greater priority.

    ■He 111 P-6/R2: Conversions later in war of surviving aircraft to glider tugs.

    ■He 111 P-7: Never built.

    ■He 111 P-8: Its existence and production is in doubt.

    ■He 111 P-9: It was intended for export to the Hungarian Air Force, by the project founder for lack of DB 601E engines. Only a small number were built, and were used in the Luftwaffe as towcraft.

    ■He 111 H-0: Pre-production aircraft similar to P-2 but with Jumo 211A-1 engines.

    ■He 111 H-1: Production aircraft. Fitted with FuG IIIaU and later FuG 10 radio communications.

    ■He 111 H-2: This version was fitted with improved armament. Two D Stands (waist guns) in the fuselage giving the variant some five MG 15 Machine guns.

    ■He 111 H-3: Similar to H-2, but with Jumo 211A-3 engines. Like the H-2, five MG 15 machine guns were standard. One A Stand MG FF cannon could be installed in the nose and an MG 15 could be installed in the tail unit.

    ■He 111 H-4: Fitted with Jumo 211D engines, late in production changed to Jumo 211F engines, and two external bomb racks. Two PVC 1006L racks for carrying torpedoes could be added.".

    ■He 111 H-5: Similar to H-4, all bombs carried externally, internal bomb bay replaced by fuel tank. The variant was to be a longer range torpedo bomber.

    ■He 111 H-6: Torpedo bomber, could carry two LT F5b torpedoes externally, powered by Jumo 211F-1 engines, had six MG 15s and one MG FF cannon in forward gondola.

    ■He 111 H-7: Designed as a night bomber. Similar to H-6, tail MG 17 removed, ventral gondola removed, and armoured plate added. Fitted with Kuto-Nase barrage balloon cable-cutters.

    ■He 111 H-8: The H-8 was a rebuild of H-3 or H-5 aircraft, but with balloon cable-cutting fender. The H-8 was powered by Jumo 211D-1s.

    ■He 111 H-8/R2: Conversion of H-8 into glider tugs, balloon cable-cutting equipment removed.

    ■He 111 H-9: Based on H-6, but with Kuto-Nase balloon cable-cutters.

    ■He 111 H-10: Similar to H-6, but with 20 mm MG/FF cannon in ventral gondola, and fitted with Kuto-Nase balloon cable-cutters. Powered by Jumo 211 A-1s or D-1s.

    ■He 111 H-11: Had a fully-enclosed dorsal gun position and increased defensive armament and armour. The H-11 was fitted with Jumo 211 F-2s.

    ■He 111 H-11/R1: As H-11, but with two 7.92 mm (.312 in) MG 81Z twin-gun units at beam positions.

    ■He 111 H-11/R2: As H-11, but converted to a glider tug.

    ■He 111 H-12: Modified to carry Hs 293A missiles, fitted with FuG 203b Kehl transmitter, and ventral gondola deleted.

    ■He 111 H-14: Pathfinder, fitted with FuG FuMB4 Samos and FuG 16 radio equipment.

    ■He 111 H-14/R1:Glider tug version.

    ■He 111 H-15: The H-15 was intended as a launch pad for the Blohm & Voss BV 246.

    ■He 111 H-16: Fitted with Jumo 211F-2 engines and increased defensive armament of MG 131 machine guns, twin MG 81Zs, and a MG FF cannon.

    ■He 111 H-16/R1: As H-16, but with MG 131 in power-operated dorsal turret.

    ■He 111 H-16/R2: As H-16, but converted to a glider tug.

    ■He 111 H-16/R3: As H-16, modified as a pathfinder.

    ■He 111 H-18: Based on H-16/R3, was a pathfinder for night operations.

    ■He 111 H-20: Defensive armament similar to H-16, but some aircraft feature power-operated dorsal turrets.

    ■He 111 H-20/R1: Could carry 16 paratroopers, fitted with jump hatch.

    ■He 111 H-20/R2: Was a cargo carrier and glider tug.

    ■He 111 H-20/R3: Was a night bomber.

    ■He 111 H-20/R4: Could carry twenty 50 kg (110 lb) bombs.

    ■He 111 H-21: Based on the H-20/R3, but with Jumo 213E-1 engines.

    ■He 111 H-22: Re-designated and modified H-6, H-16, and H-21's used to air launch V-1 flying-bombs.

    ■He 111 H-23: Based on H-20/R1, but with Jumo 213A-1 engines.

    ■He 111 R: High altitude bomber project.

    ■He 111 U: A spurious designation applied for propaganda purposes to the Heinkel He 119 high-speed reconnaissance bomber design which set an FAI record in November 1937. True identity only becomes clear to the Allies after World War II.

    ■He 111 Z-1: Two He 111 airframes coupled together by a fifth engine, used a glider tug for Messerschmitt Me 321.

    ■He 111 Z-2: Long-range bomber variant based on Z-1.

    ■He 111 Z-3: Long-range reconnaissance variant based on Z-1.
    CASA 2.111

    The Spanish company CASA also produced a number of heavily modified He 111s under license for indigenous use. These models were designated CASA 2.111 and served until 1975.

    Military operators

    A Chinese He 111A equipped with unidentified radial engines. Bulgaria
    ■Bulgarian Air Force.

    ■Chinese Nationalist Air Force.
    ■Czechoslovak Air Force operated one aircraft post-war.
    ■Royal Hungarian Air Force.
    ■Royal Romanian Air Force.
    ■Slovak Air Force
    Spanish State
    ■Spanish Air Force.
    ■Turkish Air Force operated He 111F variant.
    United Kingdom
    ■Royal Air Force operated various captured variants during and after the war.
    United States
    ■United States Army Air Force operated several captured aircraft after the war. One pictured H-20 - 23, may be the machine currently on display at the RAF Museum Hendon, minus the DL131 turret.

    Civil operators
    ■Lufthansa operated 12 aircraft.
    ■Unknown civilian user operated one converted bomber. The registration of the He 111 was YR-PTP. It is unknown whether this was a German or Romanian designation. Works, or factory number is unknown.


    He 111, Werknr. 701152, RAF Hendon, London. This H-20, built in 1944, was modified to drop paratroops (Fallschirmjäger)
    The He 111P-2, Wk Nr 1526, built in 1939Only three original German built He 111 survivors are on display or stored in museums around the world (not including major sections):[79]

    ■He 111E-3 series (Wk Nr 2940) with the 'conventional' cockpit is on display at Museo del Aire, Madrid, Spain, having served in the Condor Legion.
    ■A mostly complete He 111P-2 (Wk Nr 1526), is on display at the Norwegian Air Force Museum at Gardermoen.[79]
    ■A He 111H-20, Wk Nr 701152, is on display at the RAF Museum Hendon, London.
    In 2005 another He 111 was salvaged from a Norwegian lake and has since been moved to Germany for restoration, and may be the most complete wartime He 111 to date.[79] Unrelated to this effort are efforts by several organizations to restore one to flyable condition.

    Specifications (He 111 H-6)
    Data from Nowarra, Heinz J. Heinkel He 111: A Documentary History[80]

    General characteristics

    ■Crew: 4 (pilot, navigator/bombardier/nose gunner, ventral gunner, dorsal gunner/radio operator)[81]
    ■Length: 16.4 m (53 ft 9½ in)
    ■Wingspan: 22.60 m (74 ft 2 in)
    ■Height: 4.00 m (13 ft 1½ in)
    ■Wing area: 87.60 m² (942.92 ft²)
    ■Empty weight: 8,680 kg (19,136lb lb)
    ■Loaded weight: 12,030 kg (26,500 lb)
    ■Max takeoff weight: 14,000 kg (30,864 lb)
    ■Powerplant: 2× Jumo 211F-1 or 211F-2 liquid-cooled inverted V-12, 986 kW (1,300 hp (F-1) or 1,340 (F-2)) each

    ■Maximum speed: 440 km/h (273 mph)
    ■Range: 2,300 km (1,429 mi) with maximum fuel
    ■Service ceiling: 6,500 m (21,330 ft)
    ■Rate of climb: 20 minutes to 5,185 m [82] (17,000 ft [82])
    ■Wing loading: 137 kg/m² [82] (28.1 lb/ft² [82])
    ■Power/mass: .082 kW/kg [82] (.049 hp/lb [82])


    ■up to 7 × 7.92 mm MG 15 or MG 81 machine guns, some of them replaced or augmented by
    ■1 × 20 mm MG FF cannon (central nose mount or forward ventral position)
    ■1 × 13 mm MG 131 machine gun (mounted dorsal and/or ventral rear positions)

    ■up to 2,000 kg (4,409 lb) carried internally (eight 250 kg max), or:
    ■up to 2,500 kg (5,512 lb) on two external racks
    [edit] Specifications (He 111 C-0)
    Data from Regnat, Karl-Heinz. Black Cross Volume 4: Heinkel He 111
    General characteristics

    ■Crew: 2
    ■Length: 17.5 m (57' 5")
    ■Wingspan: 22.60 m (74 ft 2 in)
    ■Height: 4.10 m (13' 5⅜")
    ■Wing area: 87.60 m² (942.92 ft²)
    ■Empty weight: 5,400 kg (11,905lb lb)
    ■Loaded weight: 9,610 kg (21,186 lb)
    ■Powerplant: 2× BMW VI liquid-cooled inverted V-12, (660hp) each

    ■Maximum speed: 310 km/h (193 mph)
    ■Range: 2,400 (1,491 mi)
    ■Service ceiling: 4,800 m (15,750 ft)
    ■Wing loading: 109.7 kg/m² (22.45 lb/ft²)

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