MEMORY ITEMS Flashcards
GPWS/EGPWS WARNINGS
“PULL UP”
“TERRAIN TERRAIN PULL UP”
“TERRAIN AHEAD PULL UP”
“OBSTACLE OBSTACLE PULL UP”
“OBSTACLE AHEAD PULL UP”
SIMULTANEOUSLY:
AP…..OFF
PITCH…..PULL UP
-PULL TO FULL BACKSTICK AND MAINTAIN IN THAT POSITION.
THRUST LEVERS…..TOGA
SPEED BRAKES LEVER…..CHECK RETRACTED
BANK…..WINGS LEVEL OR ADJUST
-AIRCRAFT OBTAIN THE BEST CLIMB PERFORMANCE WHEN THE WINGS ARE AS LEVEL AS POSSIBLE. THE FLIGHT CREW CAN ADJUST BANK WHILE CLIMBING, PROVIDED THAT TURNING IS THE SAFEST ACTION.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.
EMERGENCY DESCENT
CREW OXY MASKS…..USE
SIGNS…..ON
EMER DESCENT…..INITIATE
^IF A/THR NOT ACTIVE:
THR LEVERS.....IDLE
SPD BRK…..FULL
^WHEN DESCENT ESTABLISHED:
SPEED…..MAX/APPROPRIATE
**^IF STRUCTURAL DAMAGE SUSPECTED:**
MANEUVER WITH CARE
CONSIDER L/G EXTENSION
ENG MODE SEL….IGN
ATC…..NOTIFY
-NOTIFY ATC OF THE NATURE OF THE EMERGENCY, AND STATE INTENTION. THE FLIGHT CREW CAN COMMUNICATE WITH THE ATC USING VOICE, OR CPDLC WHEN THE VOICE CONTACT CANNOT BE ESTABLISHED OR HAS POOR QUALTIY.
EMER DESCENT (PA)…..ANNOUNCE
-THE FLIGHT CREW MUST INFORM THE CABIN OF EMERGENCY DESCENT ON THE PA SYSTEM.
ATC XPDR 7700…..CONSIDER
-SQUAWK 7700 UNLESS OTHERWISE SPECIFIED BY ATC.
CREW OXY MASKS DILUTION…..NORM
-TO SAVE OXYGEN, SET THE OXYGEN DILUTER SELECTOR TO THE N POSITION
-IF THE OXYGEN DILUTER SELECTOR REMAINS SET TO 100 %, OXYGEN QUANTITY MAY BE INSUFFICIENT TO COVER THE ENTIRE EMERGENCY DESCENT PROFILE
-ENSURE THAT CREW COMMUNICATION IS ESTABLISHED WITH OXYGEN MASKS. AVOID THE CONTINUOUS USE OF INTERPHONE TO MINIMIZE INTERFERENCE WITH THE BREATHING NOISE IN THE OXYGEN MASK.
MAX FL: 100/MEA-MORA
^IF CAB ALT ABOVE 14,000 FEET:
OXYGEN PAX MASK MAN ON…..PRESS
-THIS ACTION CONFIRMS THAT THE PASSENGER OXYGEN MASKS ARE RELEASED. NOTE: NOTIFY THE CABIN CREW, WHEN THE AIRCRAFT REACHES A SAFE FLIGHT LEVEL, AND WHEN CABIN OXYGEN IS NO MORE NECESSARY.
LOSS OF BRAKING
^IF NO BRAKING:
REV…..MAX
-IF NEEDED, THE FLIGHT CREW MAY KEEP MAXIMUM REVERSE THRUST UNTIL FULL AIRCRAFT STOP.
BRAKE PEDALS…..RELEASE
- WHEN THE FLIGHT CREW SETS THE A/SKID & N/W STRG SW TO OFF, THE CONTROL OF THE BRAKING SYSTEM IS TRANSFERRED FROM THE BSCU TO THE ABCU, AND THE ALTERNATE BRAKING MODE IS ACTIVATED. CONSEQUENTLY THE PF SHOULD RELEASE THE BRAKE PEDALS BEFORE THE PM SELECTS THE A/SKID OFF. THIS ACTION AVOIDS BRUTAL BRAKING APPLICATION.
A/SKID OFF…..ORDER
-THE PF ORDERS THE PM TO SET THE A/SKID & N/W STR SW TO OFF.
A/SKID & N/W STRG…..OFF
BRAKE PEDALS…..PRESS
MAX BRK PR…..1,000 PSI
-THE ABCU AUTOMATICALLY LIMITS THE BRAKE PRESSURE TO 1,000 PSI. MONITOR BRAKE PRESSURE ON THE BRAKES PRESS INDICATOR.
**^IF STILL NO BRAKING:** PARK BRAKE.....USE -USE SHORT SUCCESIVE PARKING BRAKE APPLICATIONS TO STOP THE AIRCRAFT.
TCAS CAUTION - TRAFFIC ADVISORY
“TRAFFIC, TRAFFIC”
^IF THE A/THR IS OFF AND AVAILABLE:
AUTOTHRUST…..ON -IT IS RECOMMENDED TO SET THE A/THR TO ON IN ORDER TO AVOID THE AUTO FLT A/THR LIMITED ALERT AT THE AUTOMATIC A/THR ACTIVATION THAT OCCURS IN THE CASE OF AN RA.
-DO NOT PERFORM A MANEUVER BASED ON A TA ALONE.
TCAS WARNING - RESOLUTION ADVISORY
“CLIMB”
“DESCEND”
“MAINTAIN VERTICAL SPEED MAINTAIN”
“LEVEL OFF, LEVEL OFF”
“ADJUST VERTICAL SPEED ADJUST”
“MONITOR VERTICAL SPEED”
-ALWAYS FOLLOW RA ORDERS, EVEN IF THIS RESULTS IN CROSSING THE INTRUDER ALTITUDE, BECAUSE THESE ORDERS ENSURE THE BEST ALTITUDE SEPARATION.
CAUTION: BE AWARE THAT THE INTRUDER MAY HAVE A TCAS, AND MAY MANEUVER IN RESPONSE TO A COORDINATED RA ORDER. THEREFORE, NOT FOLLOWING AN RA ORDER COULD COMPROMISE SAFE OPERATION.
^ALL RA, EXCEPT ANY CLIMB RA DURING APPROACH IN CONF 3 OR FULL:
AP (IF ENGAGED)…..OFF
BOTH FDS…..OFF
-RESPOND PROMPTLY AND SMOOTHLY
NOTE: THE FD WILL REENGAGE WITH THE OCCURANCE OF A CORRECTIVE RESOLUTION ADVISORY AND MUST BE RESELECTED OFF.
VERTICAL SPEED…..ADJUST OR MAINTAIN
-ADJUST OR MAINTAIN THE VERTICAL SPEED AS REQUIRED, TO REACH THE GREEN AREA AND/OR AVOID THE RED AREA OF VERTICAL SPEED SCALE.
NOTE: AVOID EXCESSIVE MANEUVERS WHILE ATTEMPTING TO MAINTAIN THE VERTICAL SPEED JUST OUTSIDE THE RED AREA OF THE VERTICAL SPEED SCALE, AND WITHIN THE GREEN AREA. IF NECESSARY, USE THE FULL SPEED RANGE BETWEEN VA MAX AND VMAX.
^ANY CLIMB RA DURING APPROACH IN CONF 3 OR FULL:
GO-AROUND…..PERFORM
-THE AP/FD TCAS MODE DISENGAGES (THE AP/FD NO LONGER FOLLOWS THE RA ORDERS). FOLLOW THE SRS GA.
VERTICAL SPEED…..MONITOR
-CHECK THAT THE VERTICAL SPEED REMAINS OUT OF THE RED AREA OF THE VERTICAL SPEED SCALE AND TAKE OVER IF NECESSARY.
-RESPECT STALL, GPWS, OR WINDSHEAR WARNINGS.
ATC…..NOTIFY
^WHEN THE “CLEAR OF CONFLICT” AURAL ALERT SOUNDS:
ATC…..NOTIFY
LATERAL AND VERTICAL GUIDANCE…..ADJUST
-ADJUST THE LATERAL AND VERTICAL GUIDANCE TO RESUME NORMAL NAVIGATION, IN ACCORDANCE WITH ATC CLEARANCE.
AP/FD…..AS RQRD
-IF NECESSARY, REENGAGE THE AP/FD.
UNRELIABLE SPEED INDICATION
^IF THE SAFE CONDUCT OF THE FLIGHT IS IMPACTED:
AP…..OFF
A/THR…..OFF
FD…..OFF
PITCH/THRUST:
-BELOW THRUST RED ALT…..15 DEGREES / TOGA
-ABOVE THRUST RED ALT AND BELOW FL100…..10 DEGREES / CLB
-ABOVE THRUST RED ALT AND ABOVE FL100…..5 DEGREES / CLB
FLAPS (IF CONF 0(1)(2)(3))…..MAINTAIN CURRENT CONF
FLAPS (IF CONF FULL)…..SELECT CONF 3 AND MAINTAIN
SPEEDBRAKES…..CHECK RETRACTED
L/G…..UP
-WHEN AT, OR ABOVE MSA OR CIRCUIT ALTITUDE: LEVEL OFF FOR TROUBLESHOOTING.
^TO LEVEL OFF:
AP…..OFF
A/THR…..OFF
FD…..OFF
SPEEDBRAKES…..CHECK RETRACTED
PITCH/THRUST TABLE…..APPLY
^WHEN FLIGHT PATH IS STABILIZED:
AP…..OFF
A/THR…..OFF
FD…..OFF
SPEEDBRAKES…..CHECK RETRACTED
FLIGHT PATH…..KEEP STABILIZED
RESPECT STALL WARNING
GPWS/EGPWS CAUTIONS
“TERRAIN TERRAIN”
“TOO LOW TERRAIN”
“TERRAIN AHEAD”
“CAUTION TERRAIN”
“CAUTION OBSTACLE”
“OBSTACLE AHEAD”
^AT ANY POINT THE ABOVE CAUTIONS ARE ANNUNCIATED:
SIMULTANEOUSLY:
AP…..OFF
PITCH…..PULL UP
-PULL TO FULL BACKSTICK AND MAINTAIN IN THAT POSITION.
THRUST LEVERS…..TOGA
SPEED BRAKES LEVER…..CHECK RETRACTED
BANK…..WINGS LEVEL OR ADJUST
-AIRCRAFT OBTAIN THE BEST CLIMB PERFORMANCE WHEN THE WINGS ARE AS LEVEL AS POSSIBLE. THE FLIGHT CREW CAN ADJUST BANK WHILE CLIMBING, PROVIDED THAT TURNING IS THE SAFEST ACTION.
NOTE: FOR SOME AIRPORTS, THE OPERATOR MAY DEFINE A SPECIFIC PROCEDURE.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.
GPWS/EGPWS CAUTIONS
“SINK RATE”
^ABOVE 1,000 FEET AFE:
FLIGHT PATH…..ADJUST
-ADJUST PITCH AND THRUST TO SILENCE THE ALERT.
^BELOW 1,000 FEET AFE:
GO-AROUND…..CONSIDER
GPWS/EGPWS CAUTIONS
“DON’T SINK”
FLIGHT PATH…..ADJUST
-ADJUST PITCH AND THRUST TO SILENCE THE ALERT
GPWS/EGPWS CAUTIONS
“TOO LOW GEAR” - “TOO LOW FLAPS”
GO-AROUND…..PERFORM
GPWS/EGPWS CAUTIONS
“GLIDESLOPE”
^ABOVE 1,000 FEET AFE IN IMC OR ABOVE 500 FEET AFE IN VMC:
FLIGHT PATH…..ADJUST
-ADJUST THE PITCH AND THRUST TO REDUCE THE VERTICAL DEVIATION FROM THE GLIDESLOPE.
**^WHEN CONDITIONS REQUIRE A DELIBERATE APPROACH BELOW GLIDESLOPE:** G/S MODE…..OFF
^BELOW 1,000 FEET AFE IN IMC OR BELOW 500 FEET AFE IN VMC:
GO-AROUND…..CONSIDER
STALL RECOVERY
AS SOON AS ANY STALL INDICATION (COULD BE AURAL WARNING, “STALL STALL” RED MESSAGE ON PFD, BUFFET…) IS RECOGNIZED, APPLY THE IMMEDIATE ACTIONS:
NOSE DOWN PITCH CONTROL…..APPLY
-THIS WILL REDUCE ANGLE OF ATTACK
NOTE: IN CASE OF LACK OF PITCH DOWN AUTHORITY, REDUCING THRUST MAY BE NECESSARY.
BANK…..WINGS LEVEL
^WHEN OUT OF THE STALL (NO LONGER STALL INDICATIONS):
THRUST…..INCREASE SMOOTHLY AS NEEDED
NOTE: IN CASE OF ONE ENGINE INOPERATIVE, PROGRESSIVELY COMPENSATE THE THRUST ASYMMETRY WITH RUDDER.
SPEEDBRAKES…..CHECK RETRACTED
FLIGHT PATH…..RECOVER SMOOTHLY
**^IF IN CLEAN CONFIGURATION AND BELOW 20,000 FEET:** FLAP1…..SELECT NOTE: IF A RISK OF GROUND CONTACT EXISTS, ONCE CLEARLY OUT OF STALL (NO LONGER STALL INDICATIONS), ESTABLISH SMOOTHLY A POSITIVE CLIMB GRADIENT.
STALL WARNING AT LIFTOFF
IF STALL WARNINGS TRIGGER AT LIFTOFF, APPLY THE FOLLOWING IMMEDIATE ACTIONS:
THRUST…..TOGA
AT THE SAME TIME:
PITCH ATTITUDE…..15 DEGREES
BANK…..WINGS LEVEL
WINDSHEAR WARNING - REACTIVE WINDSHEAR
IF WINDSHEAR IS DETECTED, BOTH PFDS DISPLAY A WINDSHEAR MESSGE. AN ASSOCIATED AURAL WINDSHEAR ALERT SOUNDS THREE TIMES.
IF THE FLIGHT CREW DETECTS WINDSHEAR, APPLY THE FOLLOWING RECOVERY TECHNIQUE:
^AT TAKEOFF:
**^IF BEFORE V1:** IF THERE ARE SIGNIFICANT VARIATIONS IN AIRSPEED, AND IN AIRSPEED TREND BELOW THE INDICATED V1, REJECT THE TAKEOFF. -IF WINDSHEAR OCCURS DURING THE TAKEOFF ROLL, THE AIRCRAFT MAY REACH V1 LATER (OR SOONER) THAN EXPECTED. THE FLIGHT CREW SHOULD ENSURE THAT THERE IS SUFFICIENT RUNWAY REMAINING TO STOP THE AIRCRAFT, IF NECESSARY. **^IF AFTER V1:** THR LEVERS…..TOGA REACHING VR…..ROTATE SRS ORDERS…..FOLLOW -IF NECESSARY THE FLIGHT CREW MAY PULL THE SIDESTICK FULLY BACK. NOTE: IF THE FD BARS ARE NOT DISPLAYED, MOVE TOWARD AN INITIAL PITCH OF 17.5 DEGREES. THEN, IF NECESSARY, TO PREVENT A LOSS IN ALTITUDE, INCREASE THE PITCH ATTITUDE.
^AIRBORNE, INITIAL CLIMB OR LANDING:
THR LEVERS AT TOGA…..SET OR CONFIRM
AP (IF ENGAGED)…..KEEP ON
SRS ORDERS…..FOLLOW
-IF NECESSARY, THE FLIGHT CREW MAY PULL THE SIDESTICK FULLY BACK.
NOTE:
- AUTOPILOT DISENGAGES IF THE ANGLE OF ATTACK VALUE GOES ABOVE A PROT.
- IF THE FD BARS ARE NOT DISPLAYED, MOVE TOWARD AN INITIAL PITCH ATTITUDE OF 17.5 DEGREES. THEN, IF NECESSARY, TO PREVENT A LOSS IN ALTITUDE, INCREASE THE PITCH ATTITUDE.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR.
CLOSELY MONITOR FLIGHT PATH AND SPEED.
RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR.
