In addition, the TF30 uses two systems to improve reliable operation, the Mid Compression Bypass System (MCB) and the Mach Lever. This is accomplished using various sensor inputs run through a calculation using set schedules which decides the positions of the ramps. This system controls the variable geometry intakes by moving the variable ramps mounted in them to slow the airflow. To provide the engines with an even subsonic airflow the F-14 has the AICS or Air Inlet Control System. The F-14A is powered by two Pratt & Whitney TF30-P-414A while the F-14B is powered by two General Electrics F110-GE-400, both of which are afterburning turbofan engines. Weapons and Weapons Employment Overview.AN/ARA-50 UHF Automatic Direction Finder.AN/ARC-159 and AN/ARC-182 Remote Displays.Loading (saving) Preset Channel(s) on UHF 1 and V/UHF 2.Bearing Distance and Heading Indicator (BDHI).Attitude and Heading Reference Set (AHRS).AN/ALQ-100 AND 126 DECM (Defensive Electronic CounterMeasures).AN/ALE-39 Countermeasures Dispensing Set.Navigation Command and Control Grid (NAV GRID).Tactical Information Display (TID) and Associated Controls.Fire Detection and Suppression System Test. ![]() Engine Instrument Group (EIG), Related Indicators and Caution Lights. ![]()
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