English for aircraft 1-1

AIR USED TO COOL HOT AIR. AIR COOLING. COOLING AIR.

TO TRANSFER FROM ONE CIRCUIT TO ANOTHER. SWITCHING CIRCUIT. CIRCUIT SWITCHING.

PROCEDURE TO CHECK LIGHTS. LIHGT TEST. TEST LIGHT.

SIGNAL SENT BACK BY THE SYSTEM. FEEDBACK SYSTEM. SYSTEM FEEDBACK.

LARGUE GROUPS (LOOMS) OF WIRES. WIRE LOOMS. LOOM WIRES.

NON-RETURN VALVE. CHECK VALVE. VALVE CHECK.

MOTOR TO MOVE A VALVE. VALVE DRIVE. DRIVE VALVE.

ACTIVATES A VALVE ELECTRICALLY. SELENOID VALVE. VALVE SELENOID.

AIR FROM ENGINE COMPRESSOR. BLEED AIR. AIR BLEED.

SYSTEM THAT PROVIDES HOT AIR. AIR BLEED. BLEED AIR.

HANDLE CONTROL SPOILER. SPOILER CONTROL HANDLE. CONTROL SPOILER HANDLE.

SYSTEM OXYGEN CREW FLIGHT. FLIGHT CREW OXYGEN SYSTEM. CREW OXYGEN SYSTEM FLIGHT.

UNIT DISPLAY LOWER. LOWER DISPLAY UNIT. DISPLAY UNIT LOWER.

BULKHEAD AFT PRESSURE. PRESSURE AFT BULKHEAD. AFT PRESSURE BULKHEAD.

PANEL LIGHTING EXTERIOR CONTROL. CONTROL PANEL LIGHTING EXTERIOR. EXTERIOR LIGHTING CONTROL PANEL. CONTROL EXTERIOR LIGHTING PANEL.

WING LEFT FAIRIN HAND TIP. HAND FAIRING LEFT WING TIP. LEFT HAND WING TIP FAIRING. TIP FAIRING LEFT HAND WING.

EDGE RIGHT TRAILING UPPER. UPPER RIGHT TRAILING EDGE. RIGHT TRAILING EDGE UPPER. TRAILING EDGE UPPER RIGHT.

FUEL INTEGRAL TANK. TANK FUEL INTEGRAL. FUEL TANK INTEGRAL. INTEGRAL FUEL TANK.

RECLINE BUTTON CONTROL. BUTTON CONTROL RECLINE. RECLINE BUTTON CONTROL. RECLINE CONTROL BUTTON.

DOOR CARRO LOCK FITTINGS. FITTINGS CARGO DOOR LOCK. CARGO DOOR LOCK FITTINGS. DOOR CARGO LOCK FITTINGS.

DISTRIBUTION CABIN CONDITIONED SYSTEM AIR AFT. DISTRIBUTION AFT AIR SYSTEM CONDITIONED CABIN. CONDITIONED CABIN SYSTEM AFT AIR DISTRIBUTION. AFT CABIN CONDITIONED AIR DISTRIBUTION SYSTEM.

MAIN DOOR GEARS. GEARS MAIN DOOR. DOOR GEARS MAIN. MAIN GEARS DOOR.

MARKER LIGHT INNER. INNER MARKER LIGHT. MARKER LIGHT INNER. LIGHT INNER MARKER.

BOX GEAR NOSE INTERPHONE. GEAR NOSE INTERPHONE BOX. GEAR BOX INTERPHONE NOSE. NOSE GEAR INTERPHONE BOX.

RECEPTACLE GROUND DOOR ACCESS POWER. ACCESS DOOR POWER RECEPTACLE GROUND. GROUND POWER RECEPTACLE ACCESS DOOR. POWER GROUND RECEPTACLE ACCES DOOR.

ENGINE No. 2 IS THE __________ ENGINE. RIGHT. LEFT.

SLAT N°1 IS THE __________ SLAT. INNER. UPPER.

ENGINE N° 2 IS THE_____ ENGINE. RIGHT. LEFT.

THE SELENOID VALVE IS MOUNTED_____ THE PUMP. OFF. ON.

THE CABIN IS_____ THE HOLD. UNDER. OVER.

INSERT THE MOTOR_____ THE MOTOR. INTO. OUT OF.

THE CABIN LIGHTS RUN _____ THE CELINIG. AWAY. ALONG.

THE PLATE RUNS _____ FRAME 32 _____ FRAME 57. FROM_____ TO. TO _____ FROM.

THE TANKS ARE LOCATED _____ RIBS AND 14. BETWEEN. OUTSIDE.

THE PURSER STATIO IS AT THE _____ OF THE CABIN. FRONT. REAR.

THE CENTER PEDESTAL IS _____THE PILOT STATIONS. BEYOND. BETWEEN.

THE FIRTS OFFICER IS _____ THE CAPTIAN. NEXT TO. UPPER.

THE INSULATOR IS _____ THE WIRE. ABOUT. AROUND.

THE CABLE PASSES _____ THE CUT-OUT. THROUGT. LARGUE.

THE INDICATION IS _____ TOLERANCE(OK). WHITIN. OUTSIDE.

THE POINTER IS _____ THE RED INDEX (FAULT). BEYOND. BESIDES.

THE BULK CARGO CORPARMENT IS AT THE _____. REAR. AFT.

THE APU IS _____ OF THE PRESSURE BULKHEAD. AFT. FWD.

THE SPOILER ARE ON THE _____ WING SURFACE. UPPER. LOWER.

WATER FLOWSN _____ THE DRAIN MAST. OUT OFF. SAFE.

THE AIRCRAFT HAS REACHED THE _____ OF ITS CLIMB. TOP. LOW.

POUR OIL _____ THE TANK TO TOP IT UP. OUT OF. INTO.

REMOVE THE CAP _____ THE OVERFLOW PIPE. FROM. WHIT.