A PARTIALLY BLOCKED AIR FILTER WILL CAYTE THE AIR DRIVEN TURN INDICATOR TO

THE VALUES OF COEFFICIENT A,B,C IN ORDER ARE

THE GYRO IS SET TO READ 356 IN AN AIRCRAFT WHICH IS STATIONARY ON THE GORUND IN THE LATITUDE 50N, THE READING AFTER 1 HOUR AND 45 MIN IS ?

THE GYRO IS SET TO READ THE CORRECT MAGNETIC HEADING WHEN THE AIRCRAFT IS HEADING 090 T VARIATION 10E THE GYRO HEADING AFTER 45 MINYTES FLIGHT ON TRACK OF 090 T WITH NIL DRIFT ALONG THE PARALLEL OF 62 N AT 545 KT IS

THE ROTOR AIR DRIVEN AH ROTATES ANTI CLOCKWISE WHEN VIEWED FROM ABOVE,

ON THE AIRCRAFT ACCELERATING........... WILL CAUSE THE BOTTOM OF THE ROTOR AXIS TO LAG, RESULTING IN A ......WING.......INDICATION.
THE CORRECT WORDS TO COMPLETE THE ABOVE STATEMEN

AN AIRCRAFT IS CLIMBING AT A CONSTANT MACH NO, BELOW THE TROPOPAUSE IN ISA CONDITONS DURING THE CLIMB THE RAS WILL

AN AIRCRAFT IS FLYING AT FL390 TEMPERATURE 207 A AT MACH 0.85 THE TAS OF THE AIRCRAFT IS

THE RATE OF PRECESSION OF A GYRO VARIES:

AN AIRCRAFT FLYING AT A CONSTANT FL AND MAINTAINING A CONSTANT TAS FLIES INTO AN AREA OF WARMER AIR THE AIR DENSEITY IS........CAUSING THE RAS TO

REFERRING TO THE TURN AND SLIP INDICATOR SHOWN ABOVE THE INDICATONS ARE A 90 DEGREE TURN WILL BE COMPLETE IN ------ SECS AND THERE IS -----------BANK FOR THE -----------

IN A CLIMB THE PITOT BECOMES BLOCKED, THE VERTICAL SPEED INDICATOR(VSI) WILL INDICATE:

AN AIRCRAFT ACCELERATES ON A WESTERLY HEADING IN THE N HEMISPHERE THE COMPASS NEEDLE ROTATES000000INDICATING A TURN TOWARDS--------

AN AIRCRAFT PASSIN 6500 FT IN A DESCENT WHEN THE STATIC LINE BECOMES BLOCKED. THE ALTIMETER THEN READS:

IN A HIGH SPEED FLIGHT AT HIGH ALTITUDE THE STATIC SOURCE WILL SUFFER

A FLIGHT PLANNNED ALONG A TRACK OF 235(M) WHICH PASSES OVER A MOUNTAING HAVING AN ELEVATION OF 3900 METERS...THE REGIONAL QNH is 998 MB ASSUME 1 MB EQUALS 30 FT. THE LOWEST USUBLE FLIGHT LEVEL ACCORDING TO THE QUADRANT RULE SYSTEM WHICH WILL PROVIDE MINIM

AN INCREASE OF A 0.15 IN A MACH NUMBER RESULTIS IN A NA INCREASE OF 93 KTS IN TAS. IF THE TEMPERATURE DEVIATION FROM ISA IS 9+ C THE FL IS

IN A STABLE PLATAFORM NORH REFERECEND INS THE MEAN GROUNDSPEED IS 550 KTAFTER 21.1 MINS THE INDICATED GROUNDSPEED WAS OVERREADING BY 5 KTS THE INDICATED GROUNDSPEED AFTER 63.3 MINUTES WAS:

A VSI METERING UNIT INCORPORATES A CAPILLARY TUBE TO COMPESATE FOR

IN THE ABOVE DIAGRAM OF A GYRO MAGNETIC COMPASS THE COMPONENTS LABELLED B,H AND D IN ORDER ARE

IF THE PITOT LINE BECOMES BLOCKED IN THE DESCENT THE ASI WILL INDICATE:

AFTER AN 8,5 HR FLIGHT AN AIRCRAFT IS PARKED ON RAMP POSITION N47 59 4 E011 20.0 IF THE INS POSITION READOUT WAS N48 08 0 E011 40.5 THE HOURLY RADIAL ERROR RATE WAS

A GYROSCOPE WHICH UTILISES GRAVITY TO CONTROL A VERTICAL REFERENCE IS TERMED A

THE PRODUCT OF THE FIRST INTEGRATION OF THE E/W ACCELERATON SENSED BY AN INS SYSTEM IS

IN THE ABOVE DIAGRAM OF A SERVO ALTIMETER THE COMPONENTS LABELLED B,C,D IN ORDER ARE

WITH REFERENCE TO THE ABOVE DIAGRAM OF A MACHMETER THE CORRECT DESCRIPTIONS OF THE COMPONENTS LABELLED A,B AND C IN ORDER ARE