A320 MEMORY ITEMS
EMERGENCY DESCENT
PF PM
Crew O2 Masks Use Crew O2 Masks Use
COM Verify ESTABLISH (INT RMP) COM Verify (INT RMP)
Signs On
DESCENSO DE EMERGENCIA
Descent Initiate
ALT TURN AND PULL
HDG TURN AND PULL
SPEED PULL
FMA ANNOUNCE
If A/Thrst not active IDLE
SPEED BREAK FULL
Engine mode Sel IGN
ATC Notify
XPNDR 7700
ECAM ACTIONS
14000ft Cabina Nivelada
*25000ft 20min, 14000ft 30min
Stall
PF
STALL I HAVE CONTROL
Nose down pitch control, apply
Bank wings level
When out of the stall, no longer stall, indications
Thrust increase smoothly as needed
SPD BRK check retracted
Flight path recover smoothly
If below 20 000ft Flaps 1
At Lift Off:
Stall, TOGA 15
Thrst levers TOGA
Pitch 15º
Bank Wings Level
Engine Failure in Cruise
DO NOT DECELERATE BELOW GREEN DOT
STANDARD STRATEGY OBSTACLE STRATEGY
MCT Thr MCT
A/THR OFF A/THR OFF
HDG Turn and Pull HDG Turn and Pull
ALT Prog Page MCDU EOLRC ALT PERF Page MCDU (Drift Down)
ATC Notify ATC Notify
SPD 300kts and Pull SPD GREEN DOT and Pull
ALT Set and Pull ALT Set and Pull
ECAM OEB ACTIONS
When V/S below 500ft/min When cleared of Obstacles, return to
V/S 500flt/min Pull STD strategy.
A/THR ON
When Reaching EO LRC
SPD Manage
If Engine Failure occurs below EO FL
A/THR keep on
A320 MEMORY ITEMS
LOSS OF BREAKING Unreliable Speed Indication
PF PM PF
LOSS OF BRAKING UNRELIABLE SPEED
Reversrs Full A/P OFF
Brake pedals release A/THR OFF
Anti Skid Off (Order) Anti Skid off F/D OFF
Brake pedals press (1000psi max) If:
If still no braking Below Thrt Red alt and Below 10000ft
Prk Brk use Short and Succesive apps Above Thrt Red alt and Below 10000ft
Above Thrt Red alt and Above 10000ft
If:
In Conf 1,2 or 3
In conf full
Speed Break retracted
L/G Up
TCAS GPWS
PF PF
TCAS I HAVE CONTROL Pull Up TOGA
AP Off A/P Off
FD Off Pitch Full Up
Follow VS Orders THR Levers TOGA
SPD BRK check retracted
Bank Wings Level or adjust
WINDSHEAR Do not change Conf until out of obstacle
PF
WINDSHEAR TOGA Terrain Cautions
THRS LEVERS TOGA Night IMC
Rotate A/P Off
SRS orders Follow Pitch Full Up
If no FD 17,5 THR Levers TOGA
SPD BRK check retracted
If Airborne Bank Wings Level or adjust
TOGA Daylight VMC
If AP on keep on Flight Path Adjust
SRS Follow
Sink Rate Caution
Above 1000ft IMC or Above 500ft VMC
Do not change Conf until out of W/S Flight Path Adjust
Below 1000ft IMC or Below 500ft VMC
If Before V1: Delay Take Off Go Around Consider
Dont Sink Caution
Flight Path Adjust
Too Low Gear/Flaps
Go Around Perform
GlideSlope Caution
Above 1000ft IMC or Above 500ft VMC
Flight Path Adjust
When App requieres deliberate below GS
G/S Mode Off
Below 1000ft IMC or Below 500ft VMC
Go Around Consider
ndication
15º TOGA
10º CLB
5º CLB
Mantain
Flaps 3
WEIGHT CEO NEO 319 APU
Max Taxi Weight 77400 79400 75900 Rotor Limit
Max TO Weight 77000 79000 75500 Max EGT BLW 25000ft
Max LDG Weight 66000 67400 62500 Max EGT ABV 25000ft
Maz Zero Fuel Weight 62500 64300 58500 Max EGT 5 sec Sht Dwn
Minimun Weight 37230 40600 35400 Max EGT Inm Sht Dwn
CEO NEO 319 Max EGT APU Running
RLW BOGOTA 64000 67400 59500
SHARKLETS 66000 61800 OIL TEMPERATURE
Max Continuous
DO NOT SET ALL IRS TO HC-CJV Max Transient 15`
OFF WHEN IN FLAPS HC-CJW CEO
Minimun Starting Temp
ONE TO AVOID RTLU HC-CRU Minimum TO Temp
DAMAGE
HC-CSF OIL QUANTITY
Minimum Quantity
ENGINE VIBRATION CEO NEO
N1 +o=6 NA
N2 +o = 4.3 NA
FUEL TEMPERATURE
NARROW RWY Dispatch Not Allwd Diversion 45mt RWY MIN
NWS Inop Rudder Jam MAX
One BRK or more INOP Rudder pedal Jam
Yaw Dumper Sys Fault
RTL Sys Fault
NWS Loos
Double BSCU fault
Double LGCIU Fault
SEVERE TURBULENCE CEO NEO 319
FL 330-390 0.76 0.76 0.76
FL 200-310 275 280 280
FL 050-150 250 260 255
CATEGORIA CAT II CAT III FP CAT III FO
100 FT 50 FT 100 FT (AH)
Taxi SPD 10 Kts RVR 300 Mts RVR 175 mts 20 FT W/DH
T-OFF 150 Mts RVR RVR 75 Mts WO/DH
ENGINE OUT CAT II & III FPasive Approved in conf Full, and EOPRO completed
before reaching 1000ft in approach
WIND CEO NEO
HD 30 30
TL 10 10
CW 20 20 (15 AT RLLOUT OEI)
CEO NEO APU BLEED CEO NEO
107% 107% As Engine Start 20000 20000
900 1090 AC and Cond Single Pack 20000 22500
982 1120 AC and Cond dual Pack 15000 15000
682
700-742 THRUST EGT LIMITS CEO NEO
675 TOGA ALL ENGINES 5` 950 1060
TOGA ONE ENGINE 10` 950 1060
CEO NEO MCT 915 1025
140 140 STARTING GRD 725 750
155 155 STARTING IN FLGHT 725 875
-40 -40
-10 19 SHAFT SPEEDS CEO NEO
CEO NEO N1 104% 101%
10.6 or N2 105% 116.50%
9,5 + Cons 8,9 + Cons
(0,5 x hr) (0,45 x hr) STARTER CEO NEO
3 AUTOM ATTEMPTS 1 CICLO 1 CICLO
CEO NEO SUCCESIVE CICLES COOL 20 SEGUNDOS 60 SEGUNDOS
-36 -36 4 CICLOS COOL 15 MIN 15 MIN
54 55 NOT RUN IF N2 ABV 20% 63%
RNP AR APPROACH
TOP HAT Identify IAF DESCEND
Identify IF
Flight Plan
Identify FDP (º)
Check not "Too Steep path" displayed after FDP
IAF
RMP Set extraction: VOR y Curso
Deselect Navaids Data Page RAD NAV
Set Radio Navs TO FDP
FDP
SET RWY OR FDP
PROG
SET RNP VALUE
Insert destination conditions PERF
CHECK FUEL ESCALA LAT/DEV
EOPRO, OTHER APP, ALT RWY SEC F/PLAN
ARRIVAL BRIEFING MANAGEMENT OF DEGRADED NAVIGATION
Final app not engage
GPS Primary Lost both ND'sçDual AP Failure if RNP BLW 0.3
Loss of GPWS TERRAIN if ofstacles GO AROUND
NAV ALT Discrepancies
In case of deviation 75ft below or abv vertical path (3/4 dot)
NAV ACC DOWNGRADE Both FMGS
NAV FM/GPS Position Disagree
FMS1-2 POS Difference EXTRACTION
Dual Loss of FMGC or FINAL APP MODE
EXTRACTION
Terrain Inconsistencies
GPS Primary on both ND`s
GPS 1+2 BOTH IN NAV
TERRAIN ON ND
BARO REF/ALTIMETER CHECK
AP/FD FLUJO PFD
L/DEV CHECK DISPLAYED
ARM APP
FINAL APP CHCK ENGAGED
GO AROUND ALT SET
FLIGHT PARAMETERS MONITOR
CHECK ALTITUDE CROSSINGS FAF
1 RNP = 1 DOT
1/2 DOT = CALL OUT LAT/DEV
GO AROUND SEGUN APP RNP
DEPARTURE CHANGE PF PM
Final T/Off Performance data Final T/Off Performance data
FMS Take off Data Revise
FMS Take off Data Crosscheck
EFB MCDU GD Compare
Flaps Lever As Appropiate
F-Plan (SID, Trans) Check
Initial Climb and SPEX Limit
Re Briefing Re Briefing
Departure Change CH-List Departure Change CH-List
CRUISE PF PM
TCAS (ALL / BELOW)
ECAM MEMO ECAM MEMO
SD PAGES SD PAGES
FLIGHT PROGRESS FLIGHT PROGRESS
MCDU PROG MCDU FPLAN
STEP FLIGHT LEVEL STEP FLIGHT LEVEL
NAV ACC NAV ACC
RADAR
OXYGEN MASKS OXYGEN MASKS
RVSM PROCEDURES EQUIPMENT PF PM
2 ADR`S + 2 DMC'S RVSM Procedures Request aboveXPNDR
1 TRANSPONDER FL 270 PFD (2)
1 AP FMA
1 FCU CHANNEL AP 1 or 2
2 PFD CRZ FL
1 FWC ALT STD/Crosscheck
200 Ft Tolerance (MO)
ECAM STATUS
RVSM DEVIATIONS EAST (0-179) LEFT Descend 300ft
+ o = 5Nm RIGHT Climb 300ft
WEST (180-359) LEFT Climb 300ft
+ o = 5Nm RIGHT Descend 300ft
AFTER TAKE OFF (AVION LIMPIO) PM
APU Bleed Off
APU Master Off
Engine Mode Selector as RQRD
TCAS (TA/RA)
ANTI ICE as RQRD
Wing ANTI ICE AS RQRD
10000ft PM
Exterior lights (LDG OFF)
Signs OFF THEN ON
ARPT (EFIS)
AFTER 10000ft OFP
WX
WINDS
ETP or DD/DP
SEC F/PLN
GO AROUND NEAR THE GROUND PF PM
GO AROUND ATTITUDE
TOGA
Rotate Flight Parameters Monitor
GO AROUND GO AROUND FLAPS (ABV 100FT) Flaps retract One Step
FMA Check announce
POSITIVE CLIMB
Gear Up L/D Up
erance (MO)
VISUAL PATTERN Line Up V1 CUT ENG FAIL
Set Circuit ALT FCU FLY, NAVIGATE COMMUNICATE
Pre SLT RWY HDG PF PM
After Lift Off Gear Up
Pull HDG Consider TOGA No Read and Do actions
SPD, ATHR Pitch 12.5 then follow FD until 400ft AGL
Flaps 1 Beta Target
Pull Speed Consider AP Activate Secondary F/Plan
Set DownWind HDG Above 400 Ft.
After Bank ECAM ACTIONS
Activate APPR Phase EO ACC ALT
Manage SPD STOP ECAM
FD Off Push to Level Off
Bird ON Clean up the A/C
Set DownWind track At G/D Speed
APP Check List ALT Pull
Set DIR TO RWY Radial In THR Lever MCT
AP Off as requiered
Check Time Abeam THRSHL Secure the Engine Before EO ACC ALT
Flaps One No Damage: Master Off
Flaps two (10 sec before turn) Damage: Agent 1 DISCH
3 Sec before Turn Set RWY Track Fire: Agent 2 DISCH
Básico
Initiate descend (YOYO) GS FROM ABV CLEARED TO LOC ARM LOC
Gear Down CLEARED FOR ILS ARM APP
Flaps Three FCU ALT SET ABV
Flaps Full V/S (-1500/-2000 FT/MIN)
Landing Check List CHECK G/S IS ARMED
G/S STAR
G/S 1000ft Stabilized
EVACUACION CAPT FO
Parking Brake Set
ATC (VHF1) Notify
When A/C is stopped
Tripulación en sus estaciones
Delta P (Used) Check at Zero
Delta P Not Used
Cab PR Mode Manual
V/S CTL Full Up
All ENG Masters OFF
All FIRE pb (ENG & APU) PUSH
All Agents AS RQRD
If Evacuation Require
Evac Initiate (EVACUAR, EVACUAR, EVACUAR)
EMER EVAC COMMAND ON, ATC ADVISE
If Evacuation NOT Require
Cabin Crew and Pax NOTIFY (Situación Controlada)
FO: Termina lista de chequeo, asiste en 1L posterior aleja pax de AC
CAPT: Ultimo en abandonar la nave
ECAM 1 Memory Items or OEB Immediate Actions Crosscheck ENG Master Levers
2 OEB IR Mode Selector
3 ECAM All guarded Controls
4 QRH Cockpit Circuit Brakers
PF indicates Thrust Lever
STATUS PF STOP ECAM PM Confirms
Consider: PF Operates requiered Lever
1 Any normal Check lists
2 System Reset
3 Any additional Procedures
PF CONTINUE ECAM
PM ECAM ACTIONS COMPLETED
USE OF SUMMARIES
A) ASSESMENT 1 Ecam Actions
2 Status (Ecam Actions Completed) E
3 Cruise Summary P
4 Fuel Consuption (Fuel Penalty Factors) A
5 Landing Performance
B) APP PREPARATION 6 Status Page
7 Summaries (APP, LDG, GA) B
8 MCDU (TOP HAT)
C) APP BRIEFING 9 Using Summaries B
10 STATUS
D) APPROACH 11 Refer to APP Summary Q
12 Check STS and All APP Procedures completed
F FACTS
O OPTIONS
R RISKS
D DECISIONS
E EXECUTION
C CHECK
COMM CP T Type of Emergency
E Evacuation
S Signal
T Time
TaskSharing PM Indicates related control
PF Confirms
PM Operates requiered control
ADVISORIES C Cab PRESS
ADV ON ECAM A APU
E Electric
E ENGINE
F FUEL
O OXIGEN
cam Actions Completed
lan
dvise
uild the APP
rief the APP
RH
HYDRAULIC S
BLUE FAULT YELLOW FAULT
Reservoir Low Level - 2.4 LT Reservoir Low Level
Reservoir Overheats + o = 93C - o = 88C Reservoir Overheats
Reservoir Low air Pressure - o = 22 PSI + o = 30 PSI Reservoir Low air Pressure
Elec Pump Low Pressure - o = 1450 PSI + o = 1750 PSI Elec Pump Low Pressure
Elec Pump Overheat Elec Pump Overheat
Low Eng Pump Pressure
HYDRAULIC SYSTEM FAULTS
GREEN FAULT PTU
- 3.5 Lt Reservoir Low Level - 3.5 LT
+ o = 93C - o = 88C Reservoir Overheats + o = 93C - o = 88C
- o = 22 PSI + o = 25 PSI Reservoir Low air Pressure - o = 22 PSI + o = 25 PSI
- o = 1450 PSI + o = 1750 PSI Low Eng Pump Pressure - o = 1750 PSI + o = 2200 PSI
- o = 1750 PSI + o = 2200 PSI
FAULT
G or Y reservoir Overheats
G or Y reservoir Low air Pressure
G or Y reservoir Low fluid level
