Open Flight School

Tactical Information Display (dt.: Taktische Informationsanzeige)

Das TID ist ein Bildschirm in der zentralen Konsole des RIO. Die Anzeige kann auf dem HSD, mittels eines Schalters vom Piloten aus, gespiegelt werden.

Weiterführende Informationen:

• F-14 Tomcat Piloten-Basiskurs (DCS) / Cockpiteinweisung / Cockpitübersicht / VKR

Turbine Inlet Temperature (dt.: Turbineneinlasstemperatur)

Die TIT ist die Temperatur der Gase nach der Brennkammer des Triebwerkes, bevor sie auf die Turbine treffen.

Weiterführende Informationen:

• F-14 Tomcat Piloten-Basiskurs (DCS) / Cockpiteinweisung / Cockpitübersicht / KKL

Transition Layer (TLYR)

Additional Information:

• Wikipedia
• OFS: QNH and QFE

Throttles Panel (dt.: Schubkontrollenpanel)

Weiterführende Informationen:

• A-10C Warthog Basiskurs (DCS) / Cockpiteinweisung / Cockpitübersicht / LK

Transition Level

Additional Information:

• Wikipedia
• OFS: QNH and QFE

Up Front Controller

The Up Front Controller was introduced in the A-10C so that important settings can be made quickly without having to look too far away from the HUD. It is a control unit whose buttons control and input of settings to other cockpit units.

For the F/A-18C this concept has been extended so that entries can only be made via the centrally located UFC.

Ultra High Frequency (dt.: Dezimeterwelle)

Weiterführende Informationen:

• Wikipedia

Vertical Display Indicator (dt.: vertikale Displayanzeige)

Das VDI zeigt Lage- und Waffendaten an.

Weiterführende Informationen:

• F-14 Tomcat Piloten-Basiskurs (DCS) / Cockpiteinweisung / Cockpitübersicht / MK

Visual Flight Rules

Additional Information:

• Wikipedia

Very High Frequency

Additional Information:

• Wikipedia

The Vikhr is a Russian laser guided anti-tank missile.

Further Information:

• Wikipedia 9K121 Vikhr

Velocity Vector (dt.: Geschwindigkeitsvektor)

Der VV im HUD zeigt an, wohin sich das Flugzeug bewegt.

Weiterführende Informationen:

• F-14 Tomcat Piloten-Basiskurs (DCS) / Cockpiteinweisung / Cockpitübersicht / HUD 

(AH-64D Apache) Aircraft Survivability Equipment (Page)

The ASE page provides a de-cluttered, azimuth-only display of any radar or laser threats detected by the aircraft defensive systems, and allows the aircrew to manage the survivability equipment onboard the aircraft, such as the RLWR and chaff dispenser.

(AH-64D Apache) Back-Up Control System

Normally, the pilot and CPG flight controls are mechanically linked. The mechanical linkages are protected by shear pins and mis-track sensors to prevent a control jam or severance from affecting both sets of flight controls. If the flight controls are decoupled by the shear pin, or a mis-track is otherwise sensed, the Back-Up Control System is automatically activated. The BUCS is a single-channel, four-axis, non-redundant electric fly-by-wire (FBW) system. The FBW system is designed to replicate the feel of the hydromechanical controls but does not replicate SCAS functionality. BUCS can only be active for the pilot or the CPG station. Either the pilot or the CPG can transfer BUCS control to their station if necessary, depending on the nature and location of the jam or severance within the flight controls.

(A-10C Warthog) Counter Measures Set

The A-10C has a defensive system that helps alert and protect you against enemy weapon systems with radar and laser illumination. This includes support for Electronic Counter Measure (ECM) pods, chaff and flare dispensers, a radar warning receiver set, and a Missile Warning System (MWS). These systems are combined to form the CounterMeasures Set (CMS). The CMS has two primary panels: the Countermeasures Signal Processor (CMSP) panel and the Countermeasures Set Control (CMSC) panel.

(AH-64D Apache) Environmental Control System

The ECS provides crewmember comfort through ventilation, heating, and air conditioning. Ventilation is provided by pilot and CPG gaspers, which can be opened to admit outside air into the cockpit. The ECS also powers ventilation fans that provide forced air exchange between the cockpits and for avionics cooling.

(AH-64D Apache) Electronic Control Unit

Detects overspeed and overcurrent anomalies, as well as abnormal oil pressure. The ECU will automatically shut down the APU when an anomaly is detected. The ECU also controls the power takeoff (PTO) clutch engagement to the accessory section of the main transmission.

(AH-64D Apache) Electrical Power Management System

Electrical aircraft power is managed by the EPMS. The EPMS is a fully redundant and automatic power system consisting of a distributor for battery, AC, and DC power.

(AH-64D Apache) Flight Management Computer

The FMC provides rate damping to smooth flight control inputs and command augmentation. It also provides limited attitude and altitude hold capability for hands-off flying.

(AH-64D Apache) Generator Control Unit

AC power is provided by two brushless, air-cooled generators. Each generator outputs 45 kVA three-phase four-wire power at 115 or 200 volts and 400 Hz. Each generator has its own Generator Control Unit. A single generator is capable of handling full flight loads without shedding. The generators are mounted to the transmission accessory gearbox.