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McDonnell Douglas F-4 Phantom II Supersonic Aircraft Family

The McDonnell Douglas F-4 Phantom II is a two-seat, twin-engine supersonic aircraft family that first flew in 1958. Developed by McDonnell for U.S. Navy fleet defense, it expanded into a widely operated family for air defense, reconnaissance, training, electronic-warfare, and other military duties. National and service variants introduced different sensors, structures, and engine installations while retaining the common Phantom II design.

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Identity

Aliases
McDonnell F4H Phantom IIF4H-1F-4 Phantom IIF-4BF-4CF-4DF-4EF-4EJF-4FF-4GF-4JF-4KF-4MF-4NF-4SFG.1 PhantomFGR.2 PhantomRF-4CRF-4EQF-4
Family Name
McDonnell Douglas F-4 Phantom II
Full Name
McDonnell Douglas F-4 Phantom II Supersonic Aircraft Family
Roles
militaryreconnaissancetrainerresearch
Status
active
Type
aircraft

Details

Aircraft Specs
Configuration
fixed_wing
Operating Modes
land
Takeoff Landing Capabilities
conventional
Description
The McDonnell Douglas F-4 Phantom II is a two-seat, twin-engine supersonic aircraft family that first flew in 1958. Developed by McDonnell for U.S. Navy fleet defense, it expanded into a widely operated family for air defense, reconnaissance, training, electronic-warfare, and other military duties. National and service variants introduced different sensors, structures, and engine installations while retaining the common Phantom II design.
First Flight Year
1,958
Manufacturer
Propulsion Configurations
  • Entries
    • Nested value
    Name
    J79-powered Phantom II variants
    Notes
    Applies to the principal U.S. and most export Phantom II variants; exact J79 dash number and rating vary by variant.
  • Entries
    • Nested value
    Name
    British Spey-powered Phantom variants
    Notes
    Applies to the Royal Navy F-4K/FG.1 and Royal Air Force F-4M/FGR.2.

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Creation Time
July 30, 2026 at 04:00:22 UTC
Updated Time
July 30, 2026 at 04:00:22 UTC