767 Rec

(ATA 23- 25) THE POWER SOURCE FOR EMERGENCY EVACUATION SYSTEM IS. A. STANDBY AC BUS. B. HOT BATTERY BUS. C. STANDBY DC BUS.

(ATA 23) WHAT IS THE CHIME SOURCE WHEN THE PASSENGER SINGS “ FASTEN SEAT BELTS” AND “NO SMOKING” ACTIVATE?. A. AUDIO MANAGEMENT UNIT. B. PASSENGER ADDRESS AMPLIFIER. C. AUDIO ACCESSORY UNIT.

(ATA 23) IF ONE ATTENDANTS HANDSET IS BEING USED FOR PA ANNOINCEMENTS MAY THE OTHER HANDSETS STILL BE USED TO COMMUNICATE BETWEEN ATTENDANTS STATIONS ?. A. YES, AT ANY TIME. B. NO, ONLY ONE HANDSET CAN BE USED. C. YES, BUT ONLY IN THE ALERT MODE.

(ATA23) HOW MANY COMMUNICATION AND NAVEGATION SYSTEMM CAN BE MONITORED AT THE SAME TIME?. A. ANY COMBINATION. B. ONLY 5 COMMUNICATION STATIONS. C. ONLY 1 NAVIGATION OR COMMUNICATION STATION.

(ATA 23) WHAT IS THE DATA SOURCE OF NAVIGATION DATA FOR SATCOM SDU (SATELITE DATA UNIT). A. INERTIAL REFERENCE UNIT (IRU). B. FLIGHT MANAGEMENT (FMS). C. GLOBAL POSITION SYSTEM (GPS).

(ATA 23 ) WHEN DOES THE COCKPIT VOICE RECORDER ERASE SWITCH ACTIVATE THE BULK ERASE FEATURE?. A. AUTOMATICALLY DURING CVR TEST. B. WHEN PARKING BRAKE IS SET AND AIR-GROUND RELAY SENSES GROUND. C. WHEN THE MEMORY OF FLIGHT DATA RECORDER IS FULL.

(ATA 23) HOW LONG DOES A HORN IN THE NOSE WHEEL WELL AREA SOUND IF CREW AND H..THE GND CALL SWITCH?. A. AS LONG AS THE SWITCH IS PRESSED. B. UNTIL THE GROUND CREW PRESSED RESET BUTTON ON P40 PANEL. C. FOR 30 SEC ONLY .

(ATA 23) HOW DOES THE GROUND STATION CALL A CERTAIN AIRPLANE USING SELCAL SYSTEM?. A. BY UNIQUE DIGITAL CODE. B. BY SET OF FOUR AUDIO TONES. C. BY MODULATING THE SPECIAL FREQUENCY SIGNAL.

ATA 23) HOW IS POSSIBLE TO ADJUST THE RF SENSITIVITY LEVEL OF THE LEFT HF TRANSCEIVER. A. ONLY FROM THE LEFT RADIO CONTROL PANEL (RCP). B. FROM THE LEFT OR CENTER RADIO CONTROL PANEL (RCP). C. FROM THE ANY RADIO CONTROL PANEL (RCP).

(ATA 23) WHAT IS THE POWER SUPPLY FOR LEFT VHF SYSTEM?. A. RIGHT DC BUS. B. LEFT DC BUS. C. DC STANDBY BUS.

(ATA 23) HOW IS AN OPERATIONAL TEST OF THE PASSENGER ENTERTAINMENT AND SERVICE PERFORMED?. A. USING PUSHBUTTONS ON THE FACE PANEL OF THE COLUMN TIMER DECODER. B. USING SWITCH ON THE FOWARD ATTENDANT PANEL. C. USING PUSHBUTTONS ON THE MAINTENANCE PANEL P61 IN THE COCKPIT.

(ATA 23) WHAT DOES A PINK LIGHT AND A HI-LO CHIME IN THE CABIN INTERPHONE SYSTEM INDICATE?. A.CABIN CALL FROM FLIGHT DECK OR CABIN. B. CABIN TO FLIGHT DECK CALL. C. LAVATORY CALL.

(ATA 30) WHICH POWER USES WINDSHIELD WIPER MOTOR - CONVERTER?. 28V AC. 115V AC. 28V DC.

(ATA 30) WHAT PROVIDES INFLIGHT THERMAL ANTI-ICING TO OUTBOARD SLATS?. A. ELECTRICAL POWER FROM MAIN AC BUSES. B. LP ( LOW PRESSURE) COMPRESSOR AIR. C. PNEUMATIC SYSTEM BLEED AIR.

(ATA 30) ENGINE INLET COWL ANTI-ICE VALVE CAN BE LOCKED IN FOLLOWING POSITIONS. FULLY CLOSED AND PARTIALLY OPEN. FULLY OPEN AND FULLY CLOSED. FULLY OPEN AND PARTIALLY OPEN.

(ATA 30) GE CF6. WHAT TYPE OF SWITCHES ARE THE ENGINE ANTI-ICE CCONTROL PANEL. A. PUSH ON/ PUSH-OFF TYPE WITH A WHITE ON LIGHT AND AN AMBER VALVE LIGHT. B. ROTARY SWITCHES WITH TO POSITIONS ONLY ON AND OFF. C. ROTARY SWITCHES WITH TREE POSITION ON, OFF AND AUTO.

( ATA 28) WHAT IS THE PURPOSE OF THE SURGE TANK PRESSURE RELIEF VALVE?. PREVENTS RUPTURE OF THE FUELING MANIFOLD WHEN THE FUELING VALVES CLOSE. MODULATES THE PRESSURE WITHIN THE TANKS TO MAINTAIN A NOMINAL VALUE. SUPPLIES A BACKUP VENT IF THE VENT FLAME ARRESTOR IS PLUGGED.

(ATA 28) WHAT ACTION IS REQUIRED TO START THE DC FUEL PUMP IF THE APU IS BEING STARTED WITH BATTERY POWER ONLY?. THE LEFT FORWARD DC PUMP MUST BE REPLACED ON. THE DC FUEL PUMP MUST BE SWITCHED O BEFORE APU START. NO ACTION IS REQUIRED, THE DC FUEL PUMP STARTS AUTOMATICALLY.

(ATA 28) WHERE IS THE FUEL TEMPERATURE MEASURED?. IN THE FUEL DISTRIBUTION MANIFOLD. IN THE LEFT MAIN TANK. IN THE BOTH MAIN TANKS.

(ATA 28) WHICH BUS WILL POWER THE FUELING STATION AUTOMATICALLY WHEN THE DOOR IS OPENED?. A. GROUND HANDLING BUS. B. BATTERY BUS. C. GROUND SERVICE BUS.

( ATA 28) THE “SYSTEM TEST” SWITCH ON THE FUELING CONTROL PANEL IS USED TO. A. CHECK IF THE BLUE FUELING VALVE LIGHT ARE OPERATING. B. VERIFY THE ABILITY OF THE FQIS TO STOP THE FUELING. C. DO A TEST FOR OVERFILL SYSTEM.

(ATA 28) WHERE DOES THE NORMAL APU FUEL FEED COME FROM?. A. LEFT ENGINE FEED MANIFOLD. B. LEFT AND RIGHT CROSSFEED MANIFOLD. C. APU DC FUEL PUMP.

(ATA 28) CODE A DISPLAYED ON LH MAIN FUEL TANK QUANTITY INDICATOR DURING TEST. WHAT DOES IT REPRESET?. FQIS CHANNEL A FOR LH MAIN TANK IS ACTIVE. FQIS CHANNEL A FOR LH MAIN TANK IS BEING TESTED. FQIS CHANNEL A FOR LH MAIN TANK FAILED.

(ATA 47) WHAT DOES THE BITE DISPLAY MENU “ EXISTING FAULTS” SHOW?. A. FAULTS THAT ARE PRESENT IN THE SYSTEM. B. SPECIAL DETAILS OF THE NITROGEN GENERATION SYSTEM. C. FAULTS THA ARE IN THE MEMORY AND THAT HAVE NOT BEE CLEARED.