LIMITATIONS Flashcards
LEARN FCOM LIMITATIONS
WHAT SHOULD YOU PERFORM IF A FUEL SPILL OCCURS?
A NORMAL APU SHUTDOWN
MAX ALTITUDE FOR AIR CON AND PRESSURISATION ON APU ONLY (DUAL PACKS OPS ON APU)
15,000 FEET
MAX ALTITUDE FOR AIR CON AND PRESSURIZATION ON APU (SINGLE PACK OPS ON APU) - MOST CONSERVATIVE ON FLEET
20,000 FEET
MAX ALT FOR START ASSIST WITH APU
20,000 FEET
WHAT IS THE WAIT TIME AFTER 3 CONSECUTIVE START ATTEMPTS OF APU
60 MINUTES
MIN ALT FOR AUTOPILOT ENGAGEMENT
AFTER MANUAL GO-AROUND
100 FEET AGL
MIN ALT FOR AUTOPILOT ENGAGEMENT
ALL OTHER PHASES (321)
900 FEET AGL
MIN ALT FOR AUTOPILOT ENGAGEMENT
ALL OTHER PHASES (320)
500 FEET AGL
MIN ALT FOR AUTOPILOT ENGAGEMENT
AFTER TAKE OFF (HEIGHT AND TIME)
100 FEET AGL OR 5 SECONDS AFTER LIFT OFF
MIN ALT FOR AUTOPILOT WITH
ILS CAT 1 DISPLAYED
160 FEET RAD ALT
MIN ALT FOR AUTOPILOT IN NPA/APV USING
FINAL APP, V/S, FPA
250 FEET AGL
TOGA THRUST LIMIT TIME SINGLE ENGINE
CEO/NEO
10 MINUTES
MAXIMUM REVERSE SHOULD NOT BE USED BELOW
70 KNOTS
THE ENGINE IS ABLE TO START IN CROSSWIND UP TO HOW MUCH
35 KNOTS
COOLING PERIOD REQUIRED AFTER THREE FAILED START CYCLES (CEO)
(ONE CYCLE IS ONE FAILED START ATTEMPT, COMPARED TO NEO WHERE ONE CYCLE IS THREE ATTEMPTS)
30 MINUTES
COOLING PERIOD REQUIRED AFTER 5 MINUTES OF CONTINUOUS CRANK (CEO)
30 MINUTES
FOR GROUND STARTS (AUTO OR MAN) A ____ SECOND PAUSE IS REQUIRED BETWEEN SUCCESSIVE CYCLES (CEO) (NB. WE ARE PROBABLY GOING TO CALL MOC ANYWAY PRIOR TO TRYING AGAIN)
15 SECONDS
THE STARTER MUST NOT BE RUN ABOVE WHAT N2 ON GROUND / IN FLIGHT (CEO)
10% / 18%
COOLING PERIOD REQUIRED AFTER THREE FAILED START CYCLES (NEO)
(ONE CYCLE = THREE ATTEMPTS)
15 MINUTES
COOLING PERIOD REQUIRED AFTER 5 MINUTES OF CONTINUOUS CRANK (NEO)
15 MINUTES
FOR GROUND STARTS A ____ SECOND PAUSE IS REQUIRED BETWEEN SUCCESSIVE CYCLES (NEO)
35 SECONDS
THE STARTED MUST NOT BE RUN ABOVE WHAT N2
NEO
20 %
MAX OPERATING ALTITUDE WITH SLATS/FLAPS EXTENDED
20,000 FEET
A320 CEO
INNER FUEL TANKS MAX ASYMMETRY (OUTER TANKS BALANCED WITH ONE FULL)
500 KG
A320 CEO
OUTER FUEL TANKS MAX ASYMMETRY (INNER TANKS BALANCED)
370 KG
A320/1 NEO
FUEL TANKS MAX ASYMMETRY (HEAVIER TANK FULL)
400 KG
WHEN IS ICE ACCRETION CONSIDERED SEVERE
WHEN ACCUMULATION REACHES 5MM THICKNESS ON THE AIRFRAME
MAX G LOADING CLEAN
+2.5G / -1.0G
MAX G LOADING NOT CLEAN
0.0G / +2.0G
CARGO DOOR MAX WIND
40 KNOTS
CARGO DOOR MAX WIND IF ON LEEWARD SIDE OR NOSE INTO WIND
50 KNOTS
COCKPIT WINDOW OPEN MAX SPEED
200 KNOTS
MAX TAXI SPEED IN TURN IF ABOVE 76,000KG
20 KNOTS
MAX COMPANY CROSSWIND LIMIT
DRY
DAMP/WET UP TO 3MM
SLUSH/DRY OR WET SNOW/FROST UP TO 3MM
35KT
30KT
25KT
MAX DEMONSTRATED CROSSWIND (T/O OR LDG)
38 KNOTS INCL GUSTS
A320 MAX LANDING WEIGHT
66,000KG
A321 MAX LANDING WEIGHT
79,200KG
VLO (RETRACTION)
MAX SPEED LANDING GEAR RETRACTION
220 KNOTS / M 0.54
MAX TAILWIND FOR T/O AND LANDING
15 KNOTS
MAX WIND SPEED FOR PASSENGER DOOR OPERATION
65 KNOTS
CAN WE DO SPECIAL AUTHORISATION ILS
NOT PERMITTED
THE FWD AND AFT CARGO DOORS MUST BE CLOSED BEFORE WHAT WIND SPEED
65 KNOTS
MAXIMUM WINDOW WIPERS OPERATING SPEED
230 KNOTS
WITH PASSENGERS ON BOARD, DON’T EXCEED ____ MINUTES WITHOUT AIR CON SUPPLY
20 MINUTES
SEVERE TURB PENETRATION SPEED (CEO)
RECHECK THIS ANSWER
DEFINE ICING CONDITIONS
OAT/TAT <= +10DEG TO SAT -40DEG
WITH VISIBLE MOISTURE
LANDING CALC REQUIRED FOR ALL RUNWAYS LESS THAN _____M
2000M
VLE
MAX SPEED WITH GEAR EXTENDED
280KT / M0.67
VLO (EXTEND)
MAX SPEED FOR EXTENSION
250KTS / M0.60
MAXIMUM TIRE SPEED
195KTS
VMCA
114KIAS
MAX SPEED @ -2000’
WE CAN USE APU BLEED AIR AND AIR FROM HP START UNIT AT THE SAME TIME FOR STARTING
TRUE / FALSE
FALSE
YOU CAN GET SHUDDER IN THE NON RETURN VALVE
MAX POSITIVE DIFFERENTIAL PRESSURE
9.0 PSI (+/- 0.1 PSI)
MAX NEGATIVE DIFFERENTIAL PRESSURE
-1.0 PSI
SAFTEY VALVE RELIEF SETTING
8.6 PSI (+/- 0.1 PSI)
LP AIR CONDITIONING UNIT AND PACKS MUST BE USED AT THE SAME TIME WHEN ON THE GROUND.
TRUE / FALSE
FALSE.
PACKS MUST BE OFF WHEN USING LP GROUND AIR TO PREVENT ADVERSE AFFECTS ON THE AIR CON SYSTEM.
MIN ALT FOR AUTOPILOT CIRCLING APPROACH CAT C/D
500’ CAT C
600’ CAT D
RESTRICTIONS WITH USING OP DES / DES IN APPROACH WITH AP ENGAGED
FCU MUST BE SET TO HIGHER OF MDA/MDH OR 500’ AGL
MAX SLOPE
+/- 2%
MINIMAL RUNWAY WIDTH
A320 / A321
30M
SELECT WHICH CONFIG FOR TAILWIND LANDINGS GREATER THAN 10KTS?
FLAPS FULL
VMO/MMO
WHAT ABOUT IN ALTERNATE LAW?
350/M0.82
REDUCES TO 320KT IN ALT LAW
VMCL
MIN CONTROL SPEED FOR LANDING
HIGHEST ON FLEET
116KIAS
REQUIRED RNP VALUES FOR…
ENROUTE
TERMINAL
APPROACH
AP ON
- 0 E
- 5 T
- 3 A
MIN DH CAT 2 DUAL
100’ RADIO
MIN DH CAT 3 SINGLE
50’ RADIO
CAT 3 DUAL ALERT HEIGHT
100’ RADIO
MAX TOGA TIME TWO ENG
5 MINS
ENGINE WARM UP TIME REQD
2MINS FOR SOME A/C TO COMPLETE CENTRE TANK PUMP TEST
5MINS IF AOG>2HOURS TO REDUCE THERMAL SHOCK
MINIMUM OIL PRESSURE
65PSI (MOST LIMITING)
MINIMUM OIL TEMP BEFORE T/O
50 DEG
MIN OIL REQD ON PM ECAM CHECK BEFORE WALK-AROUND CEO/NEO
11QT PLUS 0.3Q PER INTENDED FLIGHT HOUR NEXT SECTOR
14QT FOR NEO
MIN FUEL TEMP JET A1
-43 DEG
MAX BRAKE TEMP FOR T/O
WHAT ABOUT WITH FANS ON?
300DEG
150DEG
MAX TAXI SPEED WITH MAX ONE TIRE PER GEAR DEFLATED (NOT DAMAGED)
WHAT ABOUT TWO?
7KTS
3KTS
IF ITS DAMAGED YOU MUST ASK FOR AN INSPECTION PRIOR TO VACATING RWY.
A320
MLG WIDTH
WINGSPAN
LENGTH
- 6m
- 1m (NS) / 35.8 (S)
- 57m
A321
MLG Width
Wingspan
Length
- 59m
- 8m
- 51m
MAX OPERATING ALT
39,800’
SEVER TURBULENCE PENETRATION SPEED
A321
RECHECK
FUEL SAVINGS FROM
TOD
3000’
TOD - 1040kg
3000’ - 550kg
MIN SPEED WITH ICE ACCRETION
CONF 1,2,3
CONF FULL
WAI INOP
VLs + 10kts
VLs + 5kts
VLs + 10kts or GREEN DOT
ADD PILOT INCREMENT AS SPEED COMES BACK DURING THE FLARE