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| The aerobatic team “Krasnaya pyaterka” (the Red Fives) first performed publicly for the first time during the May 1st parade in 1935. The team existed up to 1940 and many famous pilots were members of the team. They used different I-16s during this time. The I-16s here are Type 24s painted gloss red with silver stars and unpainted propeller blades. 1940. |
The Polikarpov I-16 is a
Soviet single-engine single-seat fighter aircraft. It is a low-wing cantilever
monoplane fighter with retractable landing gear, and was the first such aircraft
to attain operational squadron status. It "introduced a new vogue in
fighter design". The I-16 was introduced in the mid-1930s and formed the
backbone of the Soviet Air Force at the beginning of World War II. The
diminutive fighter, nicknamed "Ishak" or "Ishachok"
("donkey" or "burro") by Soviet pilots, figured prominently
in the Second Sino-Japanese War, the Battle of Khalkhin Gol, Winter War and the
Spanish Civil War – where it was called the Rata ("rat") by the
Nationalists or Mosca ("fly") by the Republicans. The Finns called
the aircraft Siipiorava "(flying squirrel)".
General Information
Type: Fighter
National origin: Soviet Union
Manufacturer: Plant No. 21 (Gorky),
Plant No. 39 (Moscow), Plant No. 153 (Novosibirsk), Plant No. 458
(Rostov-on-Don/Baku), (Spain)
Designer: N. N. Polikarpov Design Bureau
Primary users: Soviet Air Force, Spanish
Republican Air Force, Chinese Nationalist Air Force
Number built: 10,292 (6,848 fighters
and 3,444 trainers)
Manufactured: November 1933 – 1942
Introduction date: March 1935
First flight: 30 December 1933
(TsKB-12)
Retired: 1945 (Soviet Air Force), 1953
(Spanish Air Force)
Developed into: Polikarpov I-180
Design and Development
While working on the Polikarpov
I-15 biplane, Nikolai Nikolaevich Polikarpov began designing an advanced
monoplane fighter. It featured cutting-edge innovations such as retractable
landing gear and a fully enclosed cockpit, and was optimized for speed with a
short, stubby fuselage, and a Wright R-1820 radial engine in a NACA cowling.
The aircraft is small, light and simple to build.
Full-scale work on the
TsKB-12 prototype began in June 1933, and the aircraft was accepted into production
on 22 November 1933, a month before it took to the air. The TsKB-12 was of
mixed construction, using a wooden monocoque fuselage and wings employing a
KhMA chrome-molybdenum steel alloy wing spar, dural ribs and D1 aluminum alloy
skinning on the center and leading edges, with the remaining portions of the
wings fabric-covered. Another modern feature were the ailerons which ran along
almost the entire trailing edge of the wing and also operated as flaps (in the
manner of more modern flaperons) by drooping 15°. The cockpit was covered by a
40-centimeter-wide (16 in) canopy which featured an Aldis-type tubular gun
sight which could slide back and forth on runners fitted with rubber bungee
cords. A 225 L (59.4 US gal) fuel tank was fitted directly in front of the
cockpit. The main landing gear is fully retractable by a hand crank. The
armament consisted of a pair of 7.62×54mmR (0.30 in) ShKAS machine guns in the
wings, mounted on the outboard side of the main gear and 900 rounds of
ammunition.
These features were
proposed at first by Andrei Tupolev; however, the NII VVS (Air Force Scientific
Test Institute) was more concerned about the stresses a typical combat aircraft
was subjected to in combat, and initially considered the risk too great.
However, TsAGI, with the help of the 3rd Design Brigade under the leadership of
Pavel Sukhoi and Aleksandr Putylov, eventually convinced NII VVS that what was
being proposed was not only feasible, but would enhance the aircraft's performance.
The TsKB-12 was designed
for the Wright Cyclone SR-1820-F-3 9-cylinder radial engine (rated at 529
kW/710 hp); a license to build this engine under the supervision of the OKB-19
Shvetsov design bureau in the Soviet Union was being negotiated. As the license
was not yet approved, Polikarpov was asked to settle for the less powerful M-22
(Soviet-built version of the Gnome-Rhone Jupiter 9ASB, which itself was a
licensed version of the Bristol Jupiter VI) with 358 kW (480 hp). This was
deemed acceptable because the projected top speed still exceeded 300 km/h (185
mph).
The M-22-powered TsKB-12
first took to the air on 30 December 1933 with the famous Soviet test pilot
Valery Chkalov at the controls. The second TsKB-12, with a Cyclone engine and
three-bladed propeller, flew in January of the following year. Initial
government trials in February 1934 revealed very good maneuverability, but the
aircraft did not tolerate abrupt control inputs. Thus the TsKB-12 was deemed
dangerous to fly and all aerobatics were forbidden. The M-22 version was
preferred due to the vibration of the Cyclone-powered aircraft. Pilots
commented early on about the difficulty of climbing into the cockpit, a trait
that persisted through the I-16's service life. Before continuing test flights
the designers had to answer the question of spin behavior. Wind tunnel testing
suggested that the TsKB-12, with its short tail, would enter an unrecoverable
spin, but real-life trials were necessary to confirm this. Since Cyclone
engines were rare, it was decided to risk the M-22 prototype for this purpose.
On 1 and 2 March 1934, Chkalov performed 75 spins and discovered that the
aircraft had very benign stall behavior (dipping a wing and recovering without
input from the pilot when airspeed increased) and intentional spins could be
easily terminated by placing the controls in the neutral position. The stories
of vicious spin behavior of the I-16 perpetuated in modern literature is
unfounded (perhaps extrapolated from Gee Bee experience). In fact, the I-16's
stablemate, the biplane Polikarpov I-153, exhibited much worse spin characteristics.
Service trials of the
new fighter, designated I-16, began on 22 March 1934. The M-22 prototype
reached 359 km/h (223 mph). The pioneering presence of a complex, triple-strut manually
retracted main landing gear design was prone to jamming and required
considerable strength from the pilot, who directly operated the rearmost
strut's upper end, moved with a manually turned jackscrew running spanwise
within the wing structure, to "slide" outwards and inwards on each
side to respectively get the main gear retracted and extended, with the main
strut (the forward-most of the trio) needing to shorten its length during its
retraction to fit the main wheel into the lower fuselage, performed by the
middle-location strut's geometric arrangement and pivot locations. Most of the
test flights were performed with the gear extended. On 14 April 1934, the
Cyclone prototype was damaged when one of the landing gear legs collapsed while
it was taxiing. On 1 May 1934, the M-22 prototype participated in the flyover
of Red Square. Approximately thirty I-16 Type 1 aircraft were delivered, but
were not assigned to any VVS fighter squadron. Most pilots who flew the I-16
Type 1 for evaluation purposes did not find the aircraft to have many redeeming
characteristics. Regardless of pilot opinion, much attention was focused on the
Cyclone-powered aircraft and the M-25 (the license-built Cyclone).
The third prototype with
a Cyclone engine incorporated a series of aerodynamic improvements and was
delivered for government trials on 7 September 1934. The top speed of 437 km/h
(270 mph) no longer satisfied the Air Force, who now wanted the experimental
Nazarov M-58 engine and 470 km/h (290 mph). Subsequently, the M-22-powered
version entered production at Factory 21 in Nizhny Novgorod and Factory 39 in
Moscow. Because it was the fourth aircraft produced by these factories, it
received the designation I-16 Type 4. Aircraft fitted with these new engines required
a slightly changed airframe, including armor plating for the pilot and changes
to the landing gear doors (particularly, the hinged lower main wheel door) to
allow for complete closure.
The M-25 fitted I-16,
the I-16 Type 5, featured a new engine cowling which was slightly smaller in
diameter and featured nine forward-facing, radially-set shuttered openings to
control cooling airflow, a redesigned exhaust with eight individual outlet
stubs, and other changes. The M-25 was rated at 474 kW (635 hp) at sea level
and 522 kW (700 hp) at 2,300 m (7,546 ft). Due to the poor quality of the
canopy glazing, the I-16 Type 5 pilots typically left the canopy open or
removed the rear portion completely. By the time the Type 5 arrived, it was the
world's lightest production fighter (1,460 kg/3,219 lb), as well as the world's
fastest, able to reach speeds of 454 km/h (282 mph) at altitude and 395 km/h
(245 mph) at sea level. While the Type 5 could not perform the high-G maneuvers
of other fighters, it possessed superior speed and climb rates, and had
extremely responsive aileron control, which gave it a very good roll rate,
which led to precision maneuvers in loops and split-Ss.
A total of 10,292
single-seat aircraft were produced between 1935 and 1942; the number of two-seat
trainer variants produced varies between 843 and 3,189.
Operational History
Initial service
experience revealed that the ShKAS machine guns had a tendency to jam. This was
the result of the guns being installed in the wings upside-down to facilitate
the fit. The problem was addressed in later modifications. Evaluations from
pilots confirmed the experience with prototypes. Controls were light and very
sensitive, abrupt maneuvers resulted in spins, and spin behavior was excellent.
An aileron roll could be performed in under 1.5 seconds (roll rate over 240
degrees/second). The machine guns were fired via a cable and the required
effort, coupled with sensitive controls, made precision aiming difficult. The
rear weight bias made the I-16 easy to handle on unprepared airfields because
the aircraft was rather unlikely to flip over the nose even if the front wheels
dug in.
The I-16 was a difficult
fighter to fly. The pilots had poor visibility, the canopy tended to become
fouled with engine oil, and the moving portion was prone to slamming shut
during hard maneuvers, which caused many pilots to fix it in the open position.
The front section of the fuselage, with the engine, was too close to the center of gravity, and the pilot's cockpit too far to the rear. The Polikarpov had
insufficient longitudinal stability and it was impossible to fly the aircraft
"hands off".
Spanish
Civil War
At the start of the
Spanish Civil War in 1936, Republican forces pleaded for fighter aircraft.
After receiving payment in gold, Joseph Stalin dispatched around 475 I-16 Type
5s and Type 6s. The first I-16s appeared in Spanish skies in November 1936. The
Polikarpov monoplanes had their baptism of fire on 13 November 1936, when
twelve I-16s intercepted a Nationalist bombing raid on Madrid. Soviet pilots
claimed four air victories and two German Heinkel He 51 pilots were killed. The
Soviets suffered losses too; the group commander collided with an enemy
aircraft and another I-16 pilot crash landed. The Polikarpovs immediately began
dominating the enemy Heinkel He 51 and Arado Ar 68 biplanes and remained unchallenged
until the introduction of the Messerschmitt Bf 109. The arrival of the newest
Bf 109Bs and the overwhelming numerical superiority of Nationalist fighters
were the primary cause of the heavy I-15 and I-16 combat losses suffered
throughout 1937. A number of aviation publications called the new Soviet
fighter a "Boeing" due to the incorrect assumption that it was based
on the Boeing P-26's design. The Nationalists nicknamed the stubby fighter Rata
(Rat), while the Republicans affectionately called it Mosca (Fly).
Combat experience showed
that the I-16 had deficiencies; several aircraft were lost after structural
failure of the wings, which was quickly remedied by reinforced structures.
Heavy machine gun bullets could sometimes penetrate the armored backrest, and
fuel tanks occasionally caught fire in spite of being protected. The hot
Spanish summers required the addition of oil radiators, and dust adversely affected
the life of the engines. Although some aircraft accumulated up to 400 hours of
flying time, the average life of an I-16 was 87 days, of which one sixth was
spent on maintenance. The biggest complaint in service was the light armament
of only two 7.62 mm (0.30 in) machine guns. This was urgently addressed with
the Type 6 which added a third ShKAS in the bottom of the fuselage. The
four-gun Type 10 was nicknamed "Super Mosca" or simply
"Super". The total number of I-16s delivered to Spain from 1936 to
1938 amounted to 276. When the war ended on 1 April 1939, 187 had been lost in
Spain: 112 lost in combat, one shot down by anti-aircraft fire, eleven
destroyed on the ground, one force-landed and 62 lost in accidents.
China,
the Far East, and Battles at Khalkhin Gol
Between October 1937 and
September 1939 the USSR delivered 885 aircraft (rising to 1,250 by 1941),
including 216 Polikarpov I-16s, predominately Type 5s and Type 10s. At first
the Soviet pilots would have to fly the aircraft over 1,500 miles across China
to get them to their destination of Lanzhou, however this was a risky journey
and so future batches of aircraft would be disassembled and transported to Hami
(closer to Lanzhou), before final assembly and delivery to Lanzhou. The first
I-16s were delivered in November 1937, however rushed training of the Chinese
pilots meant many were lost to crashes. In Chinese service the I-16 became
known as the "Lastochka" or "Swallow". In the early years
of the war the I-16 was a capable fighter, however from 1939 onwards its
performance was deemed to be lacking in comparison to newer fighters.
A number Chinese aces
flew the I-16; among them Lo Ying-Teh who in 1938 shot down Japanese unit
leader Lt Ryohei Ushioda's A5M2 in his I-16 Type 5. Another ace to fly the I-16
was Liu Chi-Sheng who achieved 3 of his 10 kills while flying the I-16 Type 5,
along with another shared kill.
Another 250 I-16 Type
10s were supplied to China. This model added a second set of 7.62 mm (0.30 in)
ShKAS machine guns, armor behind the pilot, and had a slightly upgraded 560 kW
(750 hp) M-25 engine. In 1939, of the 500 I-16s deployed to the fighting at
Nomonhan, approximately 112 were lost during the battles of Khalkhin Gol, of
which 88 were destroyed in aerial combat, primarily against the all-metal
Nakajima Ki-27 Japanese fighters. During test trials in Russia of a captured
Ki-27, the aircraft proved superior to the Soviet I-152 (I-15bis), I-153, and
the I-16 in aerial combat, as well as having a faster take-off and lower landing
speed, requiring shorter airstrips than the I-16, which needed 270 meters (890
ft) to stop and 380 meters (1,250 ft) for take-off.
Further attempts were
made to upgrade the firepower of the aircraft using 20 mm (0.79 in) ShVAK
cannons, making the I-16 one of the most heavily armed fighters of the period,
able to fire 28 rounds of ammunition in three seconds. Pilots loved the
results, but the cannons were in short supply, and only a small number of the
I-16 Type 12, 17, 27, and 28 were built. The Chung 28 is an unlicensed I-16
built from the spare parts of I-16s provided to the Nationalists, delivered in
1941 and did not include upgraded cannons. The cannons adversely affected
performance, with 360° turn time increasing from fifteen seconds in the Type 5
to eighteen seconds. The Type 24 replaced the skid with a tailwheel and
featured the much more powerful 670 kW (900 hp) Shvetsov M-63 engine. The Type
29 replaced two of the ShKAS guns with a single 12.7 mm (.50 in) UBS. Ten Type
17 fighters were supplied to the Chinese Air Force where on 20 May 1940, they
effectively shot down a C5M scout-attack plane and three G3M bombers during the
Battle of Chongqing.
Types 18, 24, 27, 28,
and 29 could be fitted to carry RS-82 unguided rockets. The first successful
use of air-to-air missiles in air combat was on August 20, 1939. A Ki-27 was
hit by an RS-82 rocket launched from a distance of about a kilometer. The shot
was fired by Captain N. Zvonarev.
A 1939 government study
found the I-16 had exhausted its performance potential. The addition of armor,
radio, battery, and flaps during the aircraft's evolution exacerbated the rear
weight distribution problems to the point where the aircraft required
considerable forward pressure on the stick to maintain level flight and at the
same time developed a tendency to enter uncontrolled dives. Extension and
retraction of the landing flaps caused a dramatic change in the aircraft's
attitude. Accurate gunfire was difficult.
Soviet
Union
The pilots nicknamed the
aircraft Ishak because it was similar to the Russian pronunciation of
"I-16" ("ee-shestnadtset"). When Operation Barbarossa
erupted on 22 June 1941, 1,635 of 4,226 VVS aircraft were I-16s of all
variants, fielded by 57 fighter regiments in frontier areas. The main assault
delivered by the Luftwaffe's Luftflotte 2 (in support of Wehrmacht Army Group Center) was directed against the Soviet Western Special Military District, that
deployed 361 (424 according to other sources) I-16s. During the early phase of
the campaign the I-16 bases were the main targets for the German aircraft and
after 48 hours of combat, of the 1,635 Polikarpov monoplanes in service on 21
June 1941, only 937 were left. By 30 June the number of I-16s in western front
line units had dropped to 873, including 99 that required repairs. To stem the
Luftwaffe aerial assault several I-16 pilots adopted the taran tactic and
sacrificed their lives, ramming German aircraft.
Its main opponent in the
sky in 1941 was the German Messerschmitt Bf 109. The I-16 was slightly more
maneuverable than the early Bf 109s and could fight the Messerschmitt Bf 109E,
or Emil, on equal terms in turns. Skilled Soviet pilots took advantage of the
Polikarpov's superior horizontal maneuverability and liked it enough to resist
the switch to more modern fighters. The German aircraft, however, outclassed
its Soviet opponent in service ceiling, rate of climb, acceleration and,
crucially, in horizontal and diving speed, due to better aerodynamics and a
more powerful engine. The main versions of the I-16 had a maximum speed of
450–470 km/h (279–291 mph), while the Bf 109E had a maximum speed of 560–570
km/h (347–353 mph), and the more streamlined Bf 109F Friedrich could hit
615–630 km/h (372-390-plus mph). German pilots held the initiative and could
decide if they wanted to chase their opponents or attack them from above and
behind and then gain altitude for a new attack. Meanwhile, Polikarpovs could
only defend each other by forming a defensive circle or via horizontal
maneuverability.
Moreover, in terms of
armament, Messerschmitts had a slight edge on the I-16. The Emil carried two
wing-mounted 20mm MG FF cannons and two synchronized 7.92 mm MG-17s with a weight
of a one-second salvo of 2.37 kg, while the most common version of the
I-16—armed with just two synchronized and two wing-mounted 7.62 ShKAS—could
deliver 1.43 kg of bullets each second. Finally, the ammunition storage on a
Messerschmitt exceeded that of the I-16, carrying 1,000 rounds for each machine
gun (plus sixty drum-housed rounds for each cannon), while the Polikarpov
carried just 450 rounds for each ShKAS gun.
Around half of all
produced I-16s were still in service in 1943, when they were finally replaced.
Specially modified I-16s
were used in the Zveno parasite aircraft experiments using the Tupolev TB-3 as
a mothership. These I-16s carried two 250 kg bombs for dive bombing. This was
more than double the bomb load an I-16 could take off with under its own power.
Once the bombs were dropped, they could perform as normal I-16s, and could
re-attach to the TB-3 for the return journey.
The Luftwaffe was known
to have captured some I-16 and UTI-4 two-seat trainers (two of which were
marked with the Stammkennzeichen codes DM+HC and DM+HD) and flown from the
Erprobungstelle Rechlin central Luftwaffe test facility by Kampfgeschwader 200
(KG 200). The Luftwaffe was not the only air force able to test its fighters
against the I-16; the Japanese captured a few I-16s as well, and the Romanian
Air Force also got one when a Soviet pilot defected. The Finnish Air Force
(FAF) captured some I-16s (along with several other Soviet types). During the
Winter War and the Continuation War, the Finns captured six I-16s and one
I-16UTI. Two of the captured I-16s and I-16UTIs were put back into flying condition
and flight tested.
Variants
TsKB-12: First prototype, M-22 engine,
336 kW (450 hp), two unsynchronized ShKAS machine guns in the wings with 900
rpg.
TsKB-12bis: Second prototype, Wright
SGR-1820-F-3 Cyclone engine, 533 kW (715 hp)
TsKB-12P (I-16P): Prototype armed with two
ShVAK cannon in the wings, 150 rpg.
TsKB-18: Ground attack prototype with
M-22 engine and armored cockpit. Armed with four ShKAS or PV-1 machine guns and
100 kg (220 lb) of bombs. Two additional Type 5s were fitted with six ShKAS machine
guns of which four could decline to 20° for ground strafing.
TsKB-29 (SPB): Pneumatically-operated
landing gear and flaps, Wright Cyclone engine, armament of two ShKAS machine
guns, used as a high-speed dive bomber in the Zveno project
I-16 Type 1: Pre-production series,
M-22 engine with 358 kW (480 hp).
I-16 Type 4: First production
version, M-22 engine.
I-16 Type 5: Type 4 with a
streamlined and tapered engine cowling, Shvetsov M-25 engine with 522 kW (700
hp). 2 prototypes tested with M-62 engine as well. Mass-produced.
I-16 Type 6: Shvetsov M-25B engine,
545 kW (730 hp). Weight reduction down to 1383 kg.
I-16 Type 10: Four ShKAS machine guns
(two synchronized in the fuselage and two in the wings), windscreen replaced
the sliding canopy, could be fitted with retractable skis for winter
operations, M-25B engine with 560 kW (750 hp). Hispano-Suiza-built aircraft
were powered by the Wright Cyclone R-1820-F-54 engine.
I-16 Type 12: Version of I-16 Type 5
with 2 ShKAS machine guns and 2 ShVAK cannons.
I-16 Type 16: Type 10 with
synchronized ShVAK 12.7mm prototypes. Only three were built, all in January
1939, with serial numbers 16211-16213. They passed factory trials and were delivered
to the VVS for military trials.
I-16 Type 17: Type 10 with two ShKAS
machine guns and two ShVAK cannon, rubber tail wheel, M-25V engine with 560 kW
(750 hp). Some aircraft were fitted with an additional 12.7 mm (0.5 in) Berezin
UB machine gun for strafing.
I-16 Type 18: Type 10 with Shvetsov
M-62 engine producing 620 kW (830 hp), with a two-speed supercharger and a
variable-pitch propeller. Capable of carrying two 100 L (26 US gal) underwing
fuel tanks.
I-16 Type 19: Identical to the Type
10, except for the replacement of their wing-mounted ShKAS machine guns with
Savin–Norov machine guns; the propeller-synchronized ShKAS were not replaced.
Only three aircraft were built in this configuration, all in January 1939. They
had serial numbers 19211-19213. They were first used as test platform for the
new gun and then delivered to the VVS as I-16SN. They saw action during the
Winter War.
I-16 Type 20: This designation was
first applied to four prototypes built in February 1939 at Factory 21 and armed
with Savin–Norov (SN) machine guns synchronized to fire through the propeller.
This type was however rejected in August 1939, and then the designation reused
for the first I-16 version (otherwise the same as the type 10) capable of
carrying drop tanks. These 93 L (25 US gal) tanks were designated PSB-21.
Eighty aircraft of this specific type were delivered. Additionally, all I-16
types built after January 1940 could use these drop tanks.
I-16 Type 21 and Type 22: These were planned to
have four synchronized machine guns all firing through the propeller. Type 21
was to use only ShKAS, while type 22 was supposed to use a mixture of ShKAS and
SN machine guns. Both types however existed only on paper; no aircraft of these
types went into service.
I-16 Type 23: Type 10 additionally
armed with RS-82 rockets; 35 were built starting in May 1939. Further production
of this type was cancelled in August 1939.
I-16 Type 24: Four ShKAS, landing
flaps replaced drooping ailerons, tailwheel added, second cockpit door added on
the starboard side, Shvetsov M-63 engine with 670 kW (900 hp).
I-16 Type 27: Type 17 with an M-62
engine.
I-16 Type 28: Type 24 with two ShKAS
and two ShVAK.
I-16 Type 29: Two synchronized ShKAS
in the nose and a single 12.7 mm (0.50 in) UBS in the bottom of the fuselage;
it had no guns in wings which were reserved for ground attack weapons. Three
rocket racks were mounted in each wing. Additionally, starting in 1941, the
external fuel tank hard point was changed so that it became multipurpose: it
could carry the new type of drop tank, PLBG-100, or a FAB-100 bomb. Wartime
photographs from the summer of 1941 show two configurations: one with 6 RS-82
rockets and two FAB-100 bombs and another with four RS-132 rockets.
I-16 Type 30: Re-entered production in
1941–42, M-63 engine.
I-16TK: Type 10 with a turbocharger for
improved high-altitude performance, reached 494 km/h (307 mph) at 8,600 m (
28,200 ft), did not enter production.
UTI-1: Two-seat trainer version of
Type 1.
UTI-2: Improved UTI-1 with fixed
landing gear.
UTI-4 (I-16UTI) also known as I-16 Type 15: Two-seat
trainer version of Type 5, most with fixed landing gear. This model was built
in significant numbers, approximately 3,400 were produced.
Chung 28A: Chinese product version, base
on the I-16 Type 6 with 712hp Wright R-1820-F3 engine (Maximum speed 455 km/h),
armed with two Browning machine gun. total 30 built (3 fighter & 30
Trainer).
Operators
China: Chinese Nationalist Air Force
Nazi Germany: Luftwaffe operated
captured aircraft
Finland: Finnish Air Force operated
captured aircraft.
Mongolia: Mongolian People's Army
Aviation operated one I-16 used for training
Poland: Polish Air Force operated one
I-16 (1 Pułk Lotnictwa Myśliwskiego) and two UTI-4 aircraft (15 Samodzielny
Zapasowy Pułk Lotniczy and the Techniczna Szkoła Lotnicza.
Romania: Royal Romanian Air Force one
captured aircraft, one I-16 was captured near Dorohoi in 1941.
Soviet Union: Soviet Air Forces, Soviet
Naval Aviation
Spanish Republic: Spanish Republican Air
Force
Spanish State: Spanish Nationalist Air
Force operated I-16 and UTI-4 aircraft captured from the Spanish Republican Air
Force, returned by French government and 30 built in Jerez de la Frontera.
I-16s were still operated in 1952. Group 1-W, 26th Group, Morón Fighter School.
Surviving Aircraft
Commencing in 1993, New
Zealand pilot and entrepreneur Sir Tim Wallis' Alpine Fighter Collection organized
the restoration of six I-16s and three I-153s, found in Russia, to an airworthy
condition by the Soviet Aeronautical Research Institute (Sibnia) in Novosibirsk.
The flight of the first restored aircraft (I-16 9) took place in October 1995.
Once restored the aircraft were transported by rail to Vladivostok and from
there shipped via Hong Kong to New Zealand. This project was completed in 1999
when the third and final I-153 arrived in New Zealand. In addition a seventh
I-16 was later restored for American collector Jerry Yagen.
China: Unknown – I-16 on static
display at the Chinese Aviation Museum in Datangshang. It is believed to be a
replica incorporating original parts.
Finland: UT-1 – I-16 UTI-4 on static
display at the Finnish Aviation Museum in Vantaa, Uusimaa.
Germany: 2421319 – I-16 Type 24
airworthy with a private owner in Germany as D-EPRN.
Russia: 2421234 – I-16 Type 24
airworthy with a private owner in Russia as RA-1561G; 2821395 – I-16 on static
display at the Central Naval Museum in Saint Petersburg; Replica – I-16 on static
display at the Museum of the Great Patriotic War in Moscow; Unknown – I-16 on
static display at the Central Air Force Museum in Monino.
Spain: 2421039 – I-16 Type 24
airworthy at the Fundación Infante de Orleans in Madrid as EC-JRK; Replica –
I-16 on static display at the Museo del Aire in Madrid.
United States: 2421014 – I-16 Type 24
airworthy at the Flying Heritage Collection in Everett, Washington as N7459; 2421028
– I-16 Type 24 airworthy at the Military Aviation Museum in Virginia Beach, Virginia
as N1639P; 2421645 – I-16 Type 24 under restoration to airworthy at Fantasy of
Flight as N30425.
Specifications (I-16 Type 24)
Crew: One
Length: 6.13 m (20 ft 1 in)
Wingspan: 9 m (29 ft 6 in)
Height: 3.25 m (10 ft 8 in)
Wing area: 14.5 m2 (156 sq ft)
Airfoil: TsAGI R-II (16% at root)
Empty weight: 1,490 kg (3,285 lb)
Gross weight: 1,941 kg (4,279 lb)
Powerplant: 1 × Shvetsov M-63 9-cylinder
supercharged air-cooled radial engine, 820 kW (1,100 hp)
Propellers: 2-bladed variable-pitch
propeller
Maximum speed: 489 km/h (304 mph, 264
kn) at 3,000 m (9,800 ft)
Range: 700 km (430 mi, 380 nmi) with
drop tanks
Service ceiling: 9,700 m (31,800 ft)
Rate of climb: 14.7 m/s (2,890 ft/min)
Time to altitude: 5,000 m (16,000 ft) in
5 minutes 48 seconds
Wing loading: 134 kg/m2 (27 lb/sq ft)
Power/mass: 0.43 kW/kg (0.26 hp/lb)
Armament: 2 × fixed forward-firing 7.62
mm (0.300 in) ShKAS machine guns in upper cowling; 2 × fixed forward-firing
7.62 mm (0.300 in) ShKAS machine guns in the wings/20 mm (0.787 in) ShVAK
cannons (type-28); 6 × unguided RS-82 rockets or up to 500 kg (1,100 lb) of
bombs
Bibliography
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Nina Gut. Fighting Polikarpov: Eagles of the East No. 2. Lynnwood, WA: Aviation
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Fighter Pilots on the Eastern Front. Barnsley, South Yorkshire, UK: Pen &
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Gordon, Yefim and Keith
Dexter. Polikarpov's I-16 Fighter: Its Forerunners and Progeny (Red Star,
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Khazanov. Soviet Combat Aircraft of the Second World War, Volume One:
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sokolov (I-16 Fighter. A Restive "Donkey" of Stalin's Falcons).
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| I-16 Type 24 of a naval aviation unit, 1939. |
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| I-16, Kola Peninsula, 1941. |
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| Soviet aircraft from the 15th Fighter Regiment of the 8th Mixed Air Division, destroyed by Luftwaffe strikes, abandoned in the southern part of the Kaunas airfield, June 22, 1941. |
.jpg) |
| A fully operational Russian fighter captured as a war prize from the airport on the banks of the Syväri River, camouflaged in the middle of the forest. (The photo shows a Polikarpov I-16, type 15 (UTI-4)) Location: Aunus, Lotinanpelto, Finland. |
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| I-16 fighters on patrol over Russia. |
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| Hook up of one of the two Polikarpov I-16 SPBs (dive-bomber) Type 5 under a Tupolev TB3 4M-34RN during official testing in the summer of 1938. |
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| I-16 and other destroyed Soviet aircraft. |
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| Polikarpov I-16 captured by the Nationalists during the Spanish Civil War and repainted in their own colors. |
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| I-16. |
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| I-16 with Chinese insignia, flown by Chinese pilots and Soviet volunteers |
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| Soviet pilots Kurbatov and Moshin near I-16. Khalkhin Gol. August 1939. |
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| Operation Barbarossa: Russian and German planes destroyed on the ground. In the front Russian Polikarpov UTI-4 a two-seater training version of I-16 Soviet fighter. In the back a plane with German markings is likely Henschel Hs 126. 1941. |
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| Operation Barbarossa: Germans inspecting Russian planes. The plane in the front is Yakovlev UT-1 and the one in the back is Polikarpov I-16. 31 December 1940. |
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| Japanese armed forces’ aircraft engineers study Soviet I-16 fighter used by National Revolutionary Army. Nanking, 22 December 1937. |
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| I-16, Pruzany, 1941. |
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| I-16s at Pruzany, 1941. Aircraft in above photo is at left in background. |
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| I-16s over Leningrad during the siege. |
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| I-16s on airfield with GAZ-AA fire truck. |
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| TsKB-12 in the yard of the Central Design Office. |
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| The TsKB-12 fitted with skis and a three-bladed Hamilton Standard propeller, and Evgenii Chalow in the cockpit. The plane was armed with two PV-1 machine guns in the wings. |
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| TsKB-12 M-22 is in the air, spring of 1934. |
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| TsKB-12 with “Wright Cyclone” F-3 engine. |
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| Assembly line of I-16 type 4, 1934. |
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| I-16. |
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| I-16s in flight. |
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| I-16 of one of the Republican units during the Spanish Civil War. |
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| Modified I-16 of Antonio Arias, Republican Air Force, Spanish Civil War. |
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| View from a German bomber of a Republican I-16 attacking as a Me 109 comes up behind to attack the I-16. |
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| I-16 assembly line in Spain. |
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| CM-177 (I-16 type 10), 4th Fighter Squadron, Republican Air Force, Spanish Civil War, 1938. Note “Popeye” on the tail. |
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| Captured I-16, 1W-1, Nationalist Air Force. |
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| Captured I-16, Nationalist Air Force, Morocco, 1939. |
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| Captured I-16, 1W-6, Nationalist Air Force. |
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| Captured I-16s, Nationalist Air Force, Group 22, Tablada airfield. |
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| The last I-16 in service in the Spanish Air Force, C.8-25. |
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| Captured I-16 in Finnish Air Force as VH-201. |
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| Squadron commander of 7th IAP, Soviet Air Force, Fedor Shinkarenko, in front of his I-16. |
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| Damaged I-16 of 122nd IAP, Soviet Air Force, Lida, 22 June 1941. |
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| An airfield captured by German forces crowded with I-16s. |
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| Lieutenant Chirkov from 158th IAP LenVO is giving instructions to his wingmen before a flight. July 1941. |
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| Line of pilots from 154th IAP LenVO, which was a part of the Leningrad PVO system. |
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| Ski-equipped Type 5 ‘Red 3’ of the 13th Avia Escadrille of the 61st Avia Brigade of the Red Banner Baltic Fleet Air Force during the Winter War. The plane was flown by Senior lieutenant Novikov. The slogan means “For the Constitution of the SSSR!” probably painted in silver. It is not known if there were other slogans on the other side. |
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| TsKB-12 with two-blade propeller in spring 1934. |
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| The inscription 3s means that this is the third I-16 Type 4 built in factory n.39. Unlike the prototype, it has complete landing gear doors. National insignia have not yet been applied. A visible difference compared to the prototype was that the cowling appears extended more backward on the top and sides, but not on its lower part. |
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| Another view of the same I-16 Type 4 as shown above. |
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| A very early Type 5 ‘Red 1’ at NII VVS with an experimental fuel tank. The new cowling of the M-85A with drop-sized exhaust recesses is clearly recognizable. The wing still has only 11 ribs, as on the Type 4; later during its evolution, the Type 5 received a stronger wing with 22 ribs. |
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| These I-16 Type 5 of the Baltic Fleet were photographed in June 1939 but built around 1936. This version is immediately recognizable due to its angular sliding hood and its telescope-style gunsight; as well as the lack of guns, oil and carburetor intakes on the engine cowling distinguishes the Type 5/6 from successive variants of the I-16. |
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| Another view of the I-16 Type 5s of the Baltic Fleet. |
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| Ski-equipped Type 5 of 13th Avia Escadrille of the 61st Avia Brigade of the Red Banner Baltic Fleet Air Force during the Winter War. The plane was flown by Major Gubanov. The slogan on the right side means “Freedom to the Oppressed!”; the one on the opposite side means “Za VKP(b)” = “For the All-Union Communist Party,” and probably are painted in silver. 1940. |
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| View of the left side of the same plane as above. |
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| I-16 Type 5 ‘Red (?) 891.’ The unusual position of the number is noteworthy. The sides of the cowling looks to have been repainted with the same green of the fuselage, while the front, spinner and propellers seem to be painted black. |
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| I-16 “3-1” wrecked after the outbreak of the war. Note the unusual double number on the rudder and the white transversal band, apparently not extending to the lower surface of the fuselage. The plane features the characteristic black cowling of the Type 5s. |
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| I-16 Type 5 with light gray finish and black cowling. Probably utilized for training. |
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| I-16 Type 5 wrecked at the outbreak of the war. |
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| Another view of the same aircraft as above. |
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| I-16 Type 5s (first two) and Type 17s (last three planes), 1939. |
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| I-16 Type 5 captured at Kaunas, Lithuania, summer 1941. |
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| Rare uncamouflaged I-16 Type 5, possibly from a training unit. |
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| Another view of the same I-16 as shown above. |
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| I-16 Type 5 or Type 10, IAP, Khalkin Gol, 1939. |
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| I-16 pilots prepare for a flight. |
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| I-16 Type 10 and later introduced retractable ski landing gear. The tips of the skis entered in a recess visible under the engine cowling. |
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| Testing the retraction of the ski gear. |
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| Another view of the I-16 with retractable ski gear showing the partially closed wheel bays. |
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| Gray I-16 crudely camouflaged with green strokes. The emblem on the tail may be of a flight school. |
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| I-16 Type 17 “White 301.” |
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| The I-16 Type 17 nose. Note the “T”-shaped oil cooler inlet. |
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| I-16 Type 17, 2nd Lt. Katalov, 22nd IAP, crashed during the fighting against the Japanese in Nomonhan, Manchuria, in 1939. |
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| I-16 Type 17, Grigoriy Sergeyevich Zhuikov, commander of a squadron of the 191st IAP that defended Leningrad in September 1941. He obtained seven victories flying I-16s. |
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| I-16 Type 28 being examined by German soldiers. |
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| Captured I-16 without a propeller spinner next to an Me 109. |
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| Wreck of an I-16 Type 24. |
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| Damaged I-16 Type 24. |
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| I-16 Type 24, summer 1941. |
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| PAK-1 gunsight on an I-16. |
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| I-16 Type 28. |
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| I-16 Type 28. |
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| I-16 Type 29. This model had a radio and radio mast on the side of the nose. |
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| I-16 Type 29. |
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| UTI-4 with the same front windshield as a single-seat I-16. |
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| UTI-4 with the rear windshield of a UTI-2. |
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| I-16 Type 24 but with a UTI trainer windshield. |
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| Multi-colored camouflage scheme on I-16s was tested in mid-1940, but never adopted due to the difficulty providing in the necessary paint to the units. |
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| I-16 Type 18 of Lt. S.G. Surzhenko, 72 SAP(“Smeshanii Aviatsionii Polk” = Mixed Aviation Regiment) of the Northern Fleet, Vaenga airport, summer 1941. |
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| I-16 Type 5 (first plane) and Type 10 (second plane). 1941. A starter truck is in front of each plane. |
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| Rocket-armed I-16 Type 29, IAP, Leningrad Front, fall 1941. Camouflage pattern appears to have been created by adding stripes of black to the basic overall green. |
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| I-16 Type 29, Sgt. V.P. Segalayev, 71 IAP, Baltic Fleet, with underwing rocket rails. |
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| I-16 Type 17, Senior Lt. J. Vasilev, squadron commander, 4 GvIAP, Red Banner Baltic Fleet, spring 1942., in unusual three-tone camouflage scheme of green/black/light brown. |
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| I-16 in black/green camouflage, the only stars being those on the fuselage. |
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| I-16 Type 28s with unusual black bands on green background. |
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| I-16s with black/green camouflage, PVO, Moscow, 1943. |
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| I-16 in black/green camouflage in non-standard pattern. |
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| I-16 Type 5 with gun camera above rear of cockpit, red star on propeller spinner, and unusual green/black camouflage. |
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| I-16 Type 29 with unusual black/green camouflage pattern. |
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| I-16 Type 10 in unusual striped camouflage pattern, summer/fall 1941. |
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| I-16 Type 24, Lt. Ivan K. Bratushki, 286th IAP, Leningrad front, Ladoga area, summer 1942. Note the wire aerials from the stabilizer to the right side of the fuselage and the right wing. |
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| I-16 in unusual camouflage pattern, 1943. |
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| Finnish soldiers pose with an I-16 that belly landed. |
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| Captured I-16 Type 5 with non-retractable skis, underwing rocket rails, in brush-painted winter camouflage. |
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| The same aircraft as above being examined by Finnish technicians. |
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| I-16 Type 10 with underwing rockets and lacking landing gear doors. Many obsolete aircraft were converted to ground attack duty. |
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| I-16s, 4th GvIAP, Baltic Fleet, winter 1942. The first aircraft has underwing rockets. |
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| I-16 Type 24, Lt. G. Tsokolayev, 13th IAP VVS-KBF, which was made a Guards units as 4th GvIAP VVS-KBF on 18 January 1942. |
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| I-16 in heavy winter washable paint camouflage, northeast front, November 1942. |
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| I-16 Type 24 in winter camouflage paint. |
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| I-16 Type 29 undergoing maintenance, spring 1942. |
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| I-16 Type 5 with underwing rockets, Mozdok airport, northern Caucasus, 1943. |
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| I-16 Type 5 with underwing rockets of the same unit as the above photo. |
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| I-16 Type 5, Baltic Fleet, New Peterhof airfield, 1937. |
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| I-16s, Baltic Fleet. |
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| I-16 Type 10 with M-25V and two TK-1 turbochargers. |
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| I-16P prototype with fixed landing gear. |
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| I-16 Type 24, Lt. Krichevsky, Bugogoshch airfield, Leningrad Front, 1943. |
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| I-16 Type 29 during testing. |
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| I-16 Type 20, an experimental version of the I-16 Type 10 with two 200-liter underwing fuel tanks. |
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| I-16 Type 10 with M-25V and two TK-1 turbochargers. |
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| I-16. |
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| I-16. |
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| Captured. I-16 UTI two-seat trainer in Finnish service. |
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| I-16. |
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| I-16 UTI two-seat trainer. |
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| I-16. |
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| I-16. |
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| I-16. A member of the ground crew runs alongside to guide the pilot whose vision is restricted. |
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| I-16. |
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| Soviet poster: “The act of heroism of Hero of the Soviet Union comrade Kharitonov” depicting an I-16 ramming a German Ju 88 bomber. |
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| Soviet poster including I-16 fighters: “On any aggression and strike we will answer by triple strikes with all power of our valiant Red Army,” quoting K. Voroshilov. |
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| I-16. |
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| I-16 Type 4. |
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| I-16 Type 5 |
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| I-16 Type 10 |
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| I-16 Type 29. |
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| I-16 Type 10 cockpit details. |
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| I-16 Type 24 cockpit details. |
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| I-16. |
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| I-16. |
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| I-16. |
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| I-16. |
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| I-16 fuselage. |
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| I-16 wing. |
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| I-16 fuselage with wing. |
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| I-16 wing and fuselage. |
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| I-16 landing gear in wing. |
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| I-16. |
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| I-16. |
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| I-16. |
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| I-16. |
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| I-16. |
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| I-16 rudder. |
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| I-16 tail fin. |
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| I-16 horizontal stabilizer. |
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| I-16. |
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| I-16 tail skid. |
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| Tail skid for ski-eqipped I-16. |
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| I-16 front windshield for pilot trainee. |
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| I-16 pedals. |
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| I-16 pilot's seat. |
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| I-16 pilot's seat padding and harness. |
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| I-16 Type 24 main undercarriage. |
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| UTI-4 two-seat trainer. |
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| RO-82 rocket launcher mounted underneath wing. |
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| Right side view of ski-equipped I-16. |
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| Front view of ski-equipped I-16. |
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| Underside view of ski-equipped I-16. The upper ski is shown extended; the lower ski is shown retracted. |
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| RO-82 (top) and RO-132 (bottom) wing-mounted rocket launchers. |
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| RS-82, RS-132, M-8 and M-13 rockets (left to right). |
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| Restored I-16 in the colors of Republican Spain. |
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| I-16 in Spanish Republican colors with “Popeye” on the tail. Museo de Cuatrovientos, Madrid, Spain. |
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| I-16 at the EAA AirVenture, Oshkosh, 2003. |
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| Polikarpov I-16 at the China Aviation Museum, 2011. |
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| I-16 on display in Moscow, 2005. |
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| Polikarpov UTI-4, two-seater training version of I-16 Soviet fighter. Displayed in Helsinki Aviation Museum, with Finnish markings. 2006. |
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| Polikarpov I-16 at Warbirds Over Wanaka International Airshow 2008 (Lorne Douglas) |
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| I-16 at Wanaka, New Zealand, 15 Apr 2006. (Jeff Gilbert) |