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Aviation
CF-188A
VIII
Rank
AB
12.7
RB
12.7
SB
12.7
AB
RB
12.3
SB
12.3
AB
12.7
RB
12.7
SB
Battle rating
Great Britain
Research country
Fighter
Main role
Premium vehicle
Status
Canada
Operator
General information

The McDonnell Douglas F/A-18 Hornet is an American carrier-based fighter jet. In the late 1970s, the Royal Canadian Air Force launched the New Fighter Aircraft program to replace its aging CF-101 Voodoo, CF-104 Starfighter, and CF-116 Freedom Fighter. Among the candidates considered were the Tornado, the Mirage F.1, and the American F-14, F-15, F-16, and F-18. Although the F-14 was considered the most capable option, it was ruled out due to its high price and political factors, leading to the adoption of the McDonnell Douglas F/A-18A/B Hornet. The Hornet proved optimal for Canadian conditions with its two reliable engines, rugged landing gear for operation at austere airfields, and sufficient range to cover vast territories.

In 1980, Canada ordered 98 single-seat CF-188As and 40 two-seat CF-188Bs. The aircraft received some modifications, including an altered lighting system and modernized avionics. The CF-188’s combat debut took place during the Persian Gulf War. Subsequently, they were used in NATO operations in the Balkans, Libya, Iraq, and Syria.

The Canadian CF-188A was introduced in Update 2.49 "Tusk Force", and is located in the British aviation research tree. Similar to the American Hornet, the Canadian fighter is equally effective in air and mixed battles due to its extensive range of weaponry and excellent flight characteristics. Pilots have access to familiar AIM-7P SARH air-to-air missiles, AIM-9L IR missiles, Paveway guided bombs, and two variants of the AGM-65 Maverick air-to-surface missiles. Disadvantages include the lack of an HMD and advanced ARH air-to-air missiles.


Where to purchase

Flight performance
Max speed
at 10,668 m 1,7891,7621,8381,762 km/h
Rate of Climb 205161253.5161 m/s
Turn time 2425.52325 s
Max altitude 16,764 m
Takeoff Run 750 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 17.1 m
Wingspan 11.5 m
Wing Loading 413 kg/m²

Weight:
Base weight 11.0111.3710.7211.31 t
Fuel in main tanks 4.69 t (35m)
Fuel in drop tanks 2.78 t (20m)

Limits:
Max Speed Limit (IAS) 1,477 km/h
Mach Number Limit 2.1 M
G limit ≈ -5/11 G
Flap Speed Limit (IAS) L / T
463 / 935 km/h
Gear Speed Limit (IAS) 700 km/h
Offensive armament
20 mm M61A1 cannon
Ammunition 578 rounds
Fire rate 6,000 shots/min
One-second Burst Mass 10.02 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
HEF-I/API-T/AP-I/SAPHEI4036221263
HEF-I/HEF-I/API-T/HEF-I/HEF-I/AP-I4036221263
SAPHEI3733201164
HEF-I/AP-I/AP-I/SAPHEI4036221263
Suspended armament
Max weight 7,700 kg
Wing loading left / right
Maximum 4,000 kg
Max. difference 3,000 kg

NameWeightSlot
84.5 kg
2 × 168.9 kg
231.3 kg
38 × 527.9 kg
8 × 560.6 kg
240.9 kg
2 × 481.8 kg
446.8 kg
2 × 893.6 kg
893.6 kg
254 kg
2 × 508 kg
446.8 kg
2 × 893.6 kg
235.9 kg
2 × 471.8 kg
277.1 kg
2 × 554.3 kg
495.3 kg
943.9 kg
1,079.6 kg
303.5 kg
226.8 kg
Drop tank (330 gal.)110 kg
AN/AAS-38B targeting pod158 kg
Economy
Repair cost
AB 2,275 SL
RB 6,411 SL
SB 7,527 SL
Crew training 10,000 SL
Experts 1,770,000 SL
Aces 3,400 GE
Research Aces 2,560,000 RP
Reward multiplier AB / RB / SB
2 x (95 / 315 / 495) % SL
2 x 250 % RP
Premium vehicle
All modifications are unlocked

Flight performance
Survivability
Weaponry
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Settings
Settings
Characteristics:
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