![]() ![]() These cockpits are also available on AVSIM. Looking for a high resolution F-4 Phantom cockpits for your flightĬombatACE F-4E Hi-res Cockpit. Streak Eagle has designed very nice high resolution F-4C, D and EĬockpits, that are partly based on the images shown below. Click on the images to view larger versions.į-4C Phantom II front cockpit layout and instrument panel.į-4C Phantom II rear cockpit layout and instrument panel.į-4C, F-4D and F-4E Phantom II high resolution cockpits for The images below show typical F-4C Phantom II cockpit layouts and Another restored F-4C instrument panel is shown on Dale's General arrangement of the F-4C and F-4D.īob Dwyer's web site shows very nice and detailed images of an F-4C instrument The production stopped in 1966 when 583 F-4Cs were Radar set consisted of a AN/APQ-100 radar and there was a AN/APA-157 It used two J79-GE-15 engines and had a RAM air turbine. Tailhook, radome and hydraulic folding wings were The rear cockpit was reconfigured so that the rear-seat crewman couldĪlso fly the plane. Modified with larger tyres as compared to its Navy counterpart and The first F-4C prototype flew in Mayġ963 and production deliveries began in November 1963. Its main tactical fighter aircraft and decided to approve of a USAF The USAF tested the Navy F-4B in 1961 to see if it could serve as At 1-1.McDonnell USAF F-4C, RF-4C, F-4D and F-4E Phantom II aircraft.At 45 degrees from final altitude should be 450ft MSL.Maintain 30 degrees of bank during turn to final.Maximum carrier landing gross weight: 34,000lbs upon touchdown deploy drag chute (use the toggle cabin seat belt lights key).Maximum runway landing gross weight: 38,000lbs For every 1 000lbs below 38,000 subtract 2 knots.At 38,000lbs gross weight approach speed is 145 knots (early F-4B)/138 knots (late F-4B and F-4N).Landing speeds can be calculated using the following rule-of-thumb: This provides an on speed angle of attack light with a 3 degree glideslope and 700-800fpm descent rate. When on final approach maintain power setting of 84-88% RPM depending on gross weight. ![]() Using the angle of attack indexer maintain an on speed indication amber light. When the airspeed is below 250 knots CAS lower the landing gear and extend the flaps. When the yaw rate stops neutralize all controls and fly out of the unusual attitude.Apply full rudder opposite to the direction of the spin.If out of control and below 10 000ft AGL: EJECT.When aircraft is unloaded (5-10 units angle of attack) center the ailerons.Make judicious use of rudder to avoid inducing excessive yaw.Then vary the pitch attitude to maintain mach until reaching cruise altitude Vary pitch to maintain 400 knots CAS until reaching final cruise mach.Maintain 10 to 12 degrees nose-up until reaching 400 knots CAS.Raise flaps at 300 feet or 200 knots CAS while maintaining 10 to 12 degrees nose-up.Raise landing gear when definitely airborne.At high gross weights beware of over-rotation immediately after leaving the deck.When nosewheel is past catapult shuttle.Verify sufficient pneumatic pressure for nosewheel strut extension.Upon nosewheel lift off relax back pressure on the stick to avoid exceeding 10 to 12 degrees of pitch.Verify pin unlock handle down and wing pin unlock lights out check ARI is 10 degrees with yaw SAS off, 15 degrees with yaw SAS on.Flight control surfaces: cycle and check travel.Throttle IDLE after ignition is achieved.14%, move throttle to 40-50% and wait for ignition Starter switch: Right right click and hold.Throttle: IDLE (right click to move from cut).Start cart air and power connected to the aircraft ( see chapter: payload manager).Wing fold switch coincides with wing position.Communications function selector switch: STBY.Navigation function selector panel: SET.Centerline station safety switch: SAFE and guard down.Missile jettison selector switch (MSP): OFF.Wing flap switch coincides with flap position.External transfer switch: OUTBD or CENTER. ![]()
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