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Additional info for ADC Standards (HVAC, Flexible,American Duct Council)

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A separate engine bleed air system, internal to the engine and from a different compressor stage than the aircraft bleed air, is used for engine anti-ice. 1 Engine Anti-Ice Switch ON Activates the engine anti-ice system. OFF Deactivates the engine anti-ice system. TEST Checks ice detector operation and turns on INLET ICE display. 1 Engine Crank Switch. An engine crank switch is on the left console. The switch has positions of L (left), OFF and R (right). During engine start, placing the switch to L or R starts engine crank for the corresponding left or right engine.

1 Meet The Hornet. The F/A-18A/C Hornet is a single-place fighter/attack aircraft built by McDonnell Douglas Aerospace. See figure 1-1 for general arrangement and Cockpits Foldout section, for cockpit arrangement. It is powered by two General Electric F404-GE-400 or F404GE-402 (enhanced performance) turbofan engines with afterburner. The aircraft features a variable camber mid-wing with leading edge extensions (LEX) mounted on each side of the fuselage from the wing roots to just forward of the windshield.

THE UPRIGHT/POSITIVE AOA FALLING LEAF MODE IS THE MOST COMMON FALLING LEAF MODE. LARGE ALTITUDE LOSS MAY OCCUR BECAUSE OF THE HIGH RATE OF DESCENT, WHICH MAY EXCEED 20,000 FT/MIN. POSITIVE INDICATIONS THAT THE AIRCRAFT IS RECOVERING ARE AN INCREASINGLY NOSE LOW ATTITUDE AND AN INCREASING PEAK AIRSPEED. " E. 4 TO READ AS FOLLOWS: "INVERTED FALLING LEAF. " F. 5 TO READ AS FOLLOWS: "FALLING LEAF AND TRANSIENT SPIN ARROWS. DURING THE FALLING LEAF MODE TRANSIENT SPIN ARROWS MAY BE PRESENT. " G. 5 DELETE THE WARNING WHICH STATES: "CHASING THE AOA WITH LONGITUDINAL STICK DELAYS RECOVERY.

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