AT THE AFT END OF THE NOSE RADOME
AT THE FORWARD END OG THE NOSE RADOME
5.0 INCHES AFT OF THE FORWARD END OF THE NOSE RADOME
5.0 INCHES FORWARD OF THE FORWARD END OF THE NOSE RADOME
AFT
ABOVE
BELOW
FORWARD
IMMEDIATELY
BEFORE THE AIRCRAFT TAXIS
WHEN SHEET METAL SHOP SEES FIT
THE NEXT TIME YOU PERFORM MAINTENANCE UNDER THAT DOOR/PANEL
WINGS
RUDDER
VENTRAL FINS
HORIZONTAL STABS
WING ASSEMBLY
EMPENNAGE GROUP
FUSELAGE ASSEMBLY
HORIZONTAL STABS
NOT PREVENT THE FIRING OF THE EPU IN FLIGHT
PREVENT THE ACCIDENTAL FIRING OF THE EPU ONLY IN FLIGHT
NOT PREVENT THE FIRING OF THE EPU IF THE EXTERNAL SOURCE SHUTS DOWN
PREVENT THE ACCIDENTAL FIRING OF THE EPU DURING GROUND MAINTENANCE
1100
2100
3100
4100
8000 FOOT AIR PRESSURE
THE 23000 FOOT AIR PRESSURE
AMBIENT AIR PRESSURE
5 PSI ABOVE AMBIENT AIR PRESSURE
CONTROL CABLES
FULL FLY BY WIRE
MECHANICAL LINKAGE
A COMBINATION OF CONTROL CABLES AND ELECTRICAL WIRE
INTERNAL TO THE HANDGRIP ASSEMBLY
INTERNAL TO THE TRANSDUCER ASSEMBLY
EXTERNAL TO THE HANDGRIP ASSEMBLY
EXTERNAL TO THE TRANSDUCER ASSEMBLY
BRAKE COMMAND SIGNALS ONLY
NOSEWHEEL STEERING SIGNALS ONLY
BRAKE COMMAND AND NOSEWHEEL STEERING SIGNALS
ANTI-SKID COMMAND AND NOSEWHEEL STEERING SIGNALS
YAW TRIM CONTROL ON THE MANUAL TRIM PANEL
YAW TRIM CONTROL ON THE SIDE STICH CONTROLLER
RUDER TRIM CONTROL ONTHE MANUAL TRIM PANEL
RUDDER TRIM CONTROL ON THE SIDE STICK CONTROLLER
WRITE OVERWILL WILL OCCUR
CAUTION-CAUTION IS HEARD IN THE HEADSETS
THE FLIGHT DATA RECORDER AUTOMATICALLY SHUTS OFF
THE FLIGHT DATA RECORDER CAUTION LIGHT ILLUMINATES
QUICK REACTION FINGERTIP CONTROL OF NAVIGATION DISPLAYS
PROBVIDES TARGET DATA TO THE FIRE CONTROL AVIONICS SUBSYSTEM
SWITCHING VIDEO AND POWER CONTROLS AT THE WEAPONS STATIONS
GENERATES SYMBOLS FOR ESSENTIAL AIRCRAFT PERFORMANCE DATA INCLDING ALTITUDE, AIRSPEED, ATTITUDE, AND HEADING
COOLING AIR
AVIONICS SYSTEMS POWER APPLICATION
ELECTRICAL AND HYDRAULIC POWER APPLICATION
COOLING AIR AND AVIONIC SYSTEMS POWER APPLICATION
THAT THE CREW CHIEF DID THEIR JOB
THAT ITS OK TO APPLY ELECTRICAL POWER
THAT AVIONIC SYSTEMS ARE SAFE FOR MAINTENANCE
BASICALLY THAT ALL APPLICABLE SAFETY/LOCKPINS ARE INSTALLED
STANDING ON THE GROUND
SITTING IN THE PILOTS SEAT
DURING AIRCRAFT WALKAROUND
STANDING ON THE CREW LADDER
2 MIN
5 MIN
15 MIN
45 MIN
JFS ELECTRIC STARTER SEPARATION OR DISINTEGRATION
JFS ELECTRIC STARTER SEPARATION AND DISINTEGRATION
HIGH TEMP HIGH VELOCITY EXHAUST AND NOISE ONLY
INTAKE SUCTION, HIGH TEMP HIGH VELOCITY EXHAUST AND NOISE
EVERYONE
EXPEDITERS
CREW CHIEFS
INDIVDUALS WHO CREATED FOD
A BLOW TO THE HEAD
A DEEP THIGH BRUISE
A SEVERED FINGER
A LACERATION USUALLY BELOW THE HEAD
DECREASES
INCREASES
IS ELIMINATED
STAYS THE SAME
WHERE WALKING IS PROHIBITED
THAT IS RESTRICTED AROUND AIRCRAFT MUNITIONS
WHERE NO MAINTENANCE STANDS ARE PERMITTED
IN FRONT OF, OR BEHIND AN AIRCRAFT WERE VARIOUS AIRCRAFT HAZARDS EXISTS
SWING OR SHAKE IT
USE A SOLDER SUCKER
DIP THE HOT TIP IN WATER
WIPE THE HOT TIP ACROSS A DAMP RAG OR SPONGE