Avionics 2a352g Volume 1
- 1.ON THE F-16 AIRCRAFT, FUSELAGE STATION ZERO IS LOCATED
- A.
AT THE AFT END OF THE NOSE RADOME
- B.
AT THE FORWARD END OG THE NOSE RADOME
- C.
5.0 INCHES AFT OF THE FORWARD END OF THE NOSE RADOME
- D.
5.0 INCHES FORWARD OF THE FORWARD END OF THE NOSE RADOME
- 2.ON THE F-16, WATERLINE 65.0 IS LOCATED 65.0 INCHES IN WHICH DIRECTION FROM WATERLINE 0.0?
- A.
AFT
- B.
ABOVE
- C.
BELOW
- D.
FORWARD
- 3.WHEN SHOULD WORN DOOR/PANEL FASTENERS BE REPLACED?
- A.
IMMEDIATELY
- B.
BEFORE THE AIRCRAFT TAXIS
- C.
WHEN SHEET METAL SHOP SEES FIT
- D.
THE NEXT TIME YOU PERFORM MAINTENANCE UNDER THAT DOOR/PANEL
- 4.WHICH OF THE FOLLOWING STRUCTURES IS NOT A PART OF THE EMPENNAGE GROUP?
- A.
WINGS
- B.
RUDDER
- C.
VENTRAL FINS
- D.
HORIZONTAL STABS
- 5.THE LEADING EDGE FLAPS FOR THE F-16 ARE LOCATED ON THE
- A.
WING ASSEMBLY
- B.
EMPENNAGE GROUP
- C.
FUSELAGE ASSEMBLY
- D.
HORIZONTAL STABS
- 6.ON THE F-16 INSTALLIG THE EMERGENCY POWER UNIT SAFETY PIN WILL
- A.
NOT PREVENT THE FIRING OF THE EPU IN FLIGHT
- B.
PREVENT THE ACCIDENTAL FIRING OF THE EPU ONLY IN FLIGHT
- C.
NOT PREVENT THE FIRING OF THE EPU IF THE EXTERNAL SOURCE SHUTS DOWN
- D.
PREVENT THE ACCIDENTAL FIRING OF THE EPU DURING GROUND MAINTENANCE
- 7.TO OPERATE THE AIRCRAFT PRIMARY FLIGHT CONTROLS, THE F-16 HYDRAULIC SYSTEMS PROVIDE HYDRAULIC PRESSURE AT APPROXIMATELY WHAT PSI
- A.
1100
- B.
2100
- C.
3100
- D.
4100
- 8.AT AIRCRAFT ALTITUDES BETWEEN 800 AND 2300 FEET, THE F-16 CABIN PRESSURE IS REGULATED TO
- A.
8000 FOOT AIR PRESSURE
- B.
THE 23000 FOOT AIR PRESSURE
- C.
AMBIENT AIR PRESSURE
- D.
5 PSI ABOVE AMBIENT AIR PRESSURE
- 9.THE DIGITAL FLIGHT CONTROL SYSTEM USES WHAT MEANS TO TRANSFER INPUTS TO THE CONTROL SURFACES?
- A.
CONTROL CABLES
- B.
FULL FLY BY WIRE
- C.
MECHANICAL LINKAGE
- D.
A COMBINATION OF CONTROL CABLES AND ELECTRICAL WIRE
- 10.ARTIFICIAL FEEL IN THE DIGITAL FLIGHT CONTROL SYSTEM IS PROVIDED BY BEAMS AND COIL SPRINGS
- A.
INTERNAL TO THE HANDGRIP ASSEMBLY
- B.
INTERNAL TO THE TRANSDUCER ASSEMBLY
- C.
EXTERNAL TO THE HANDGRIP ASSEMBLY
- D.
EXTERNAL TO THE TRANSDUCER ASSEMBLY
- 11.IN ADDITION TO RUDDER CONTROL, THE RUDDER PEDALS ARE ALSO USED TO GENERATE
- A.
BRAKE COMMAND SIGNALS ONLY
- B.
NOSEWHEEL STEERING SIGNALS ONLY
- C.
BRAKE COMMAND AND NOSEWHEEL STEERING SIGNALS
- D.
ANTI-SKID COMMAND AND NOSEWHEEL STEERING SIGNALS
- 12.YAW TRIM ON THE F-16 IS ACCOMPLISHED BY USING THE
- A.
YAW TRIM CONTROL ON THE MANUAL TRIM PANEL
- B.
YAW TRIM CONTROL ON THE SIDE STICH CONTROLLER
- C.
RUDER TRIM CONTROL ONTHE MANUAL TRIM PANEL
- D.
RUDDER TRIM CONTROL ON THE SIDE STICK CONTROLLER
- 13.WHAT HAPPENS IF THE FLIGHT DATA RECORDER MEMORY CAPACITY IS EXCEEDED?
- A.
WRITE OVERWILL WILL OCCUR
- B.
CAUTION-CAUTION IS HEARD IN THE HEADSETS
- C.
THE FLIGHT DATA RECORDER AUTOMATICALLY SHUTS OFF
- D.
THE FLIGHT DATA RECORDER CAUTION LIGHT ILLUMINATES
- 14.WHICH OF THE FOLLOWING FUNCTIONS DOES THE STORES MANAGEMENT SET PERFORM?
- A.
QUICK REACTION FINGERTIP CONTROL OF NAVIGATION DISPLAYS
- B.
PROBVIDES TARGET DATA TO THE FIRE CONTROL AVIONICS SUBSYSTEM
- C.
SWITCHING VIDEO AND POWER CONTROLS AT THE WEAPONS STATIONS
- D.
GENERATES SYMBOLS FOR ESSENTIAL AIRCRAFT PERFORMANCE DATA INCLDING ALTITUDE, AIRSPEED, ATTITUDE, AND HEADING
- 15.ON THE F-16, 10JG PROCEDURES MUST BE AVVOMPLISHED PRIOR TOHYDRAULIC POWER APPLICATION: INSURE THE AIRCRAFT EXTERIOR IS SAFE, THE AIRCRAFT COCKPIT IS SAFE FOR ENTRY, AND THE AIRCAFT IS SAFE FOR
- A.
COOLING AIR
- B.
AVIONICS SYSTEMS POWER APPLICATION
- C.
ELECTRICAL AND HYDRAULIC POWER APPLICATION
- D.
COOLING AIR AND AVIONIC SYSTEMS POWER APPLICATION
- 16.WHAT ARE YOU VERIFYING WHEN YOU INSURE THE AIRCRAFT EXTERIOR IS SAFE FOR MAINTENANCE?
- A.
THAT THE CREW CHIEF DID THEIR JOB
- B.
THAT ITS OK TO APPLY ELECTRICAL POWER
- C.
THAT AVIONIC SYSTEMS ARE SAFE FOR MAINTENANCE
- D.
BASICALLY THAT ALL APPLICABLE SAFETY/LOCKPINS ARE INSTALLED
- 17.YOU PERFORM THE SAFE FOR COCKPIT ENTRY PROCEDURE
- A.
STANDING ON THE GROUND
- B.
SITTING IN THE PILOTS SEAT
- C.
DURING AIRCRAFT WALKAROUND
- D.
STANDING ON THE CREW LADDER
- 18.AFTER ENGINE ENGINE SHUTDOWN THE ENGINE EXHAUST NOZZLE SHOULD E AVOIDED FOR AT LEAST
- A.
2 MIN
- B.
5 MIN
- C.
15 MIN
- D.
45 MIN
- 19.WHAT HAZARDS DOES THE JFS POSE?
- A.
JFS ELECTRIC STARTER SEPARATION OR DISINTEGRATION
- B.
JFS ELECTRIC STARTER SEPARATION AND DISINTEGRATION
- C.
HIGH TEMP HIGH VELOCITY EXHAUST AND NOISE ONLY
- D.
INTAKE SUCTION, HIGH TEMP HIGH VELOCITY EXHAUST AND NOISE
- 20.WHO IS RESPONSIBLE FOR FOD PREVENTION?
- A.
EVERYONE
- B.
EXPEDITERS
- C.
CREW CHIEFS
- D.
INDIVDUALS WHO CREATED FOD
- 21.THE MOST COMMON INJURY ASSOCIATED WITH MOVING FLIGHT CONTROL SURFACES IS
- A.
A BLOW TO THE HEAD
- B.
A DEEP THIGH BRUISE
- C.
A SEVERED FINGER
- D.
A LACERATION USUALLY BELOW THE HEAD
- 22.IN THE FIRST FEW MINUTES AFTER AN AIRCRAFT WITH HOT BRAKES COMES TO A STOP, THE DANGER OF A TIRE BLOWOUT
- A.
DECREASES
- B.
INCREASES
- C.
IS ELIMINATED
- D.
STAYS THE SAME
- 23.IN AIRCRAFT MAINTENANCE A NO STEP AREA IS AN AREA
- A.
WHERE WALKING IS PROHIBITED
- B.
THAT IS RESTRICTED AROUND AIRCRAFT MUNITIONS
- C.
WHERE NO MAINTENANCE STANDS ARE PERMITTED
- D.
IN FRONT OF, OR BEHIND AN AIRCRAFT WERE VARIOUS AIRCRAFT HAZARDS EXISTS
- 24.WHAT IS THE PROPER WAY TO REMOVE EXCESSIVE SOLDER FROM A SOLDERING IRON OR GUN?
- A.
SWING OR SHAKE IT
- B.
USE A SOLDER SUCKER
- C.
DIP THE HOT TIP IN WATER
- D.
WIPE THE HOT TIP ACROSS A DAMP RAG OR SPONGE
Questions: 25 | Attempts: 2783 | Last updated: Mar 22, 2022
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Sample QuestionThe ADF requires two seperate antenna?
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