Airspeed Trend shows the speed it will reach in the next … seconds
10
Missed Approach Gradients
2.5% AEO & LOVIS OEI
2.1% OEI
Wheel/Tire im High Speed Bereich (RTO)
Kein Grund für RTO
NAV LOG how often during flight
at least every hour and once per flight
(OMA 30 minutes)
High Speed Regime
> 80kts
TO Segments Gradients
End of first segment (G/U) —> min 2.4%
SID —> min 3.3%
KVS max TOW um … T erhöhen
5T
Immer zuerst mit actual weight rechnen und dann das Delta zu PTOW anschauen
Bei MAX ALT hat man welche climb rate
300fpm
One Engine Inop 1h flight time equals
375NM
New Instrument Approach Classification
Type A > 250ft (DH) —> NPA, APV, PA
Type B < 250ft (DH) —> PA
Commencement of Flight (New Definition)
ENG START
min BLOCK FUEL muss vorhanden sein
OFP TANKF
L
F
L: Load as priority
F: Fuel has priority (zuerst tanken)
Minimum Flight Altitudes
1000”
2000” in mountaineus area (from 6500” AGL)
MTCA
Minimum Terrain Clearance Altitude
On all airway segments
red italic font
SID/STAR: 5NM either side of centerline
Airways: 10NM either side of centerline
eRM:
high charts: lowest 10.100ft
low charts: lowest 3.100ft
MGA
Minimum Grid Altitude
Lowest safte altitude to be flown off track
Minimum=2000”
< 10.000” Purple
> 10.000” Red
MSA
Minimum Sector Altitude
1000” Obstacle Clearance
Sector of 25NM radius around defined point
MEA
Minimum Enroute Altitude
Black
NAVAID Coverage
Radar Coverage (ATC)
Category B Airports
Trigger CityLine Flyaway Manual checken
Green Dot Symbol
Green dot speed symbol
• Best lift to drag ratio speed
• Engine out speed
• Manoeuvering speed in clean configuration
VLS
Minimum Selectable Speed
Alpha Protection Speed
Speed at which angle-of-attack protection becomes active
Alpha Max Symbol
Speed corresponding to the maximum angle-of-attack
Target Speed
Taken from FCU input ~> selected speed ~> blue speed bug
Taken from FMGC ~> managed speed ~> magenta speed bug
Radio Altimeter readout below…
2500ft AGL
"M" indicates manual tuned NAVAID
Navaid symbol • VOR/DME
Navaid symbol • NDB
Altitude Alert Warning
Comparison between actual altitude and selected ALT on FCU
Triggered when deviation more than 250 ft
Number of Flaps
1 inner at each wing
1 outter at each wing
Slats
5 Slats at each wing
Aileron Droop
Downward deflection of ailerons when flaps extended
LGCIU
Landing Gear Control Interface Unit
Hashed one - active LGCIU
Non hashed one - standby LGCIU
Required Ceiling
If a particular ceiling is required by the state authority for a specific
approach this is indicated by the prefix ”C” to the numeric value.
In this case the given value must not be considered as MDH/DH but
as required ceiling and has to be accounted for in the flight planning.
Whenever a ceiling has to be observed, the MDH/DH is omitted by
intention. The difference between the state given ceiling value and
the MDA/DA does not necessarily correspond to the airport or THR
elevation.
Minimum Descent Height (MDH) / Decision Height (DH)
Where no specific ceiling is required, the mathematical difference
between the threshold or touchdown zone elevation and DA/MDA is
published as MDH or DH.
RVR bis zu welcher Sichtweite angegeben?
1,5km
Was ist ab einem CAT planungstechnisch relevant
Nur RVR
Approach Minima - Sichtwerte unter 800m
RVR oder Visibility müssen den vorgegebenen Werten entsprechen —> Keine Korrekturen erlaubt
Approach Minima - Alle Werte zwischen 800 bis 1,5
RVR - Ansonsten kann eine Rerpoted MV in eine Converted MV umgerechnet werden
Wenn jedoch eine RVR gemeldet ist, dann muss diese auch angewandt werden
Approach Mimima - Alle Werte über 1.5km
RMV muss in CMV umgerechnet werden (muss dann mindestens 1800 betragen)
Dimensions A320
Length 38m
Tail Height 12m
Wingspan 34m
MLG Width 7.6m
Minimum pavement width for 180° turn?
Theoretical 23m
Operational 30m
T.O. INHIBIT
Cancelled above 1500ft
LDG INHIBIT
Active below 800ft
Cancelled 80kts on ground
Level 1 Failure
E/WD (AMBER)
Level 2 Failure
MASTER CAUTION
Single Chime (SC)
Level 3 Failure
MASTER WARNING
Contineous Chime
EW/D (RED)
Cancel MASTER WARNINGS & MASTER CAUTIONS to…
Reset FWC
Seat belt signs come on at…
Slats extension in flight when set to AUTO
Cabin Altitude >11.300ft
NO SMOKING
FASTEN SEAT BELTS
EXIT SIGNS
Automatically ON
EMERGENCY EXIT LT (normal operation)
ARM
LT when Landing Gear retracted
RWY TURN OFF & NOSE LIGHTS
AUTOMATICALLY OFF
DC BUS 1
Batteries are charged via…
DC Battery BUS which is supplied by DC1
Emergency electrical supply
Static Inverter
Minimum 50% Battery Capacity
25.5 V
EMER GEN FAILURE 1+2 (Battery)
Battery 1 —> AC ESS & AC STAT INV BUS
Battery 2 —> DC ESS
Battery Capacity: Approx. 22 minutes
EMER GEN Supplies…
AC ESS BUS
ESS TR
DC ESS BUS
RAT powers which hydraulic system?
Blue
ECAM Handling Primary Failure is…
Boxed
GEN Output
0-100%
116V
400HZ
Battery Voltage
28V
Hydraulic System Colours
Green Blue Yellow
Green Hydraulic System Operates…
Flight Controls
Landing Gear
Normal Brake
Blue Hydraulic System
Yellow System
Cargo Door
Alternate and Parking Brake
Hydraulic System Pressure
3000 psi
Cold Soak
Temperature of liquid decreases
Hydraulic quantity shrinks
PTU opens when…
differential pressure between green and yellow is >500 psi
Flight controls are … controlled and … operated
electrically controlled
hydraulically operated
Rudder and THR also controlled mechanically
How many ailerons?
1 each side
How many spoilers?
5 each side
# of Flight Control Computers (FCT)
2 ELAC
3 SEC
2 FAC
Controll of the roll axis
1 Aileron
4 Spoilers (2-5)
Spoiler pair 1 not used for roll control
Using speed brake only spoilers… extend
2,3,4
Ground spoilers during brake or RTO
All 5 go up
Normal Law (5 protections)
3 Modes in Normal Law
Ground Mode
Flight Mode
Flare Mode
Attitude at 50ft memorized
< 30ft memorized value progressively reduced to 2° nose down
Positive pilot action required to flare the A/C
G-Load Limits (Flight Envelope)
+2.0 g to 0 g with slats extended
+2.5 g to -1 g in clean configuration
Max. Nose Down
15°
Max. Nose Up
30°
25° (CONF FULL)
Alpha Floor
A/THR Mode “Alpha-FLOOR”
Load Alleviation Function (LAF)
Active in condition of turbulence
Symmetrically upward movement of ailerons and spoilers 4 and 5
If 1 SFCC fails (speed of slats and ailerons)
Slats and Flaps operate at half speed
Engine Start (when does start valve close and IGN switches to OFF?)
N2 > 50%
Start Valve reopens after 30 sec if 2nd engine not started
Automatic Start Process (at which N2% happens what?)
16% N2 active igniter on
22% N2 fuel flow increases
How many FADEC channels?
2
When is a TA triggered?
CPA is ca. 40 sec away
ca. 15 sec warning time
When is a RA triggered?
CPA between 15-35 sec away
RA always require a crew response
TCAS MODE A
Range
Bearing
Non altitude reporting (NAR)
TAs only
TCAS MODE C
Altitude
Relative Altitude
TAs
RAs
TCAS MODE S (standard for commercial)
Closure speed
Air to air data link
Co-ordinated RAs
RA inhibited in climb below…
1100ft AGL in climb
1200ft AGL for descent type RAs
Non threat traffic (TCAS)
> 6 NM range or > +/- 1200ft vertical altitude
Oxygen Masks Cabin deploy…
automatically at cabin pressure altitude > 14000 ft
manually from the cockpit
Oxygen supply for cabin… and crew…
chemical generators for cabin supply
oxygen bottle for cockpit supply
portable oxygen system
LDG which hydraulic system
green
Nose wheel steering by which hydraulic system?
LDG brakes operated by which hydraulic systems?
green (normal) or yellow
LDG deactivated at… kts
> 260 kts
Triple Indicator
indicates yellow hydraulic pressure on left and right brakes
indicates ACCU PRESS from yellow hydraulic system
AUTO/BRK starts braking
LO: 4 sec after ground spoiler deployment
MED: 2 sec after ground spoiler deplyoment
MAX: not selectable in flight
Minimum OXY PRESSURE CKPT
1500 PSI
Tank capacity
ca. 18-19 t (depending on density)
Flight time
About 8 hours flighttime
Fuel filling (time)
full fueling 20 minutes
Fuel feed sequence
First CTR TK fuel is used to reduce wing load
Inner tank low limit
< 750 KG
windshield wipers can be used until… kts
230 kts
LAND MODE
LAND mode automatically engages when the LOC and the G/S modes are engaged, and the aircraft is below 400 feet RA. The FMA displays "LAND", indicating that LOC and G/S are locked. No action on the FCU will disengage LAND mode. Flare and ROLL OUT modes will successively engage
Stabilization Criteria
Landing Configeration
Speed
Adequate Power
Rate of Descent
Autopilot after T/O
100ft AGL and at least 5s after liftoff
Autopilot in approach with FINAL APP, V/S or FPA mode
250 ft AGL
ILS CAT 1 in FMA
160 ft AGL
EPR (Engine Pressure Ratio)
Difference between inlet and outlet pressure
TO/GA Thrust how long max?
5 min
10 min (engine failure)
Reduced TO Thrust =
FLEX
High Flap Setting reduces … and is more suitable for … obstacles
ASD … close in …
Low Flap Setting increases … and is more suitable for … obstacles
ASD … distant … due increased climb performance
N1 vibration is an indication for fan blade …
icing
AWO includes …
LV TAXI
LVTO
CAT II
CAT III
Aiming Point Markings … m
300m after THR
LVTO Values
< RVR 400m Low Visbility TO
RVR 125m Minimum for TO
200m for inexperienced F/O
RNP Approach requires… for onboard monitoring and alerting and an accuracy of …
GPS
0.3 or better
RNP accuracy Terminal Area… Enroute…
1
Deviation RNP Lateral & Vertical at Approach Preparation
1°
0.1°
V/DEV Range
+/- 200 ft
XTK Error in Final Approach (RNAV)
Discontinue if >0.3 NM
V/DEV error in Final Approach (RNAV)
Discontinue in case of deviation of 75 ft below the vertical path (3/4 dot)
Callout at 1/2 dot
Noise Abatement Departure Procedure (NADP) 1
1500 ft AGL Thrust Reduction Altitude
3000 ft AGL Acceleration Altitude
Noise Abatement Departure Procedure (NADP) 2
1000 ft AGL THRUST
1000 ft AGL ACCELERATION
Wann RWY THR in PROG Page
Non-Precision Approach
RA “CLIMB” (sec to react)
5 sec
RA “INCREASE CLIMB” “CLIMB NOW” (how many sec to react)
2.5 sec
X-TRK Limit (FINAL APP)
> 0,3 NM
Call-out bei 0,1 NM
Maximum Altitude Flaps/Slats Extended
20000 ft
MIN RAT SPEED
140 kts
L/G DN (DUAL HYD FAIL & EMER ELEC CONFIG)
DIRECT LAW
Bis dahin Trimmung via Elevator
Summaries (Emergencies)
Situation Assessment
Summaries
Approach Preparation
Arrival Briefing
Approach
AUTOPILOT at TAKEOFF
100 ft AGL and at least 5 sec after liftoff
AUTOPILOT ILS CAT 1
Fail Passive wird zu …
there is no significant out-of-trim condition or deviation of flight path or attitude - but the landing is not completed automatically
Fail Operational
An automatic landing system is fail-operational if, in the event of a failure, the approach, flare and landing can be completed by the remaining part of the automatic system
APU Battery Start (Alt.)
25000 ft
APU Bleed Air & Elec Power (Alt.)
Hydraulic power remains available … after the shut down of the related engine
30 sec
Darf man mit Flaps 3 selected unter F Speed sinken?
Ja
Benutzung von LAPA bei einem Abnormal
VLS Check
Thrust beim Takeoff bei Crosswind > 20 kt or Tailwind
50% —> 70% —> FLX/TOGA
Approach using FPA Guidance
For LOC ONLY (Press LOC pb-sw when …)
GO AROUND ALTITUDE set …
CONTINUE:
AP …
FD …
RWY TRACK …
FOR LOC ONLY press when:
Cleared for approach
On the intercept trajectory for the final approach course
LOC deviation is available
GO AROUND Altitude set when below go-around altitude to avoid unexpected altitude capture
CONTINUE when visual contact
AP OFF
FD OFF
RWY TRACK set
Approach using FINAL APP Guidance
APPR pb on FCU press …
FD
APPR pb on FCU press when:
Cleared for the approach
TO waypoint is FDP
GO AROUND ALTITUDE set when at the FDP
CONTINUE when visual reference
FD AS RQRD
Approach using LOC G/S Guidance
APPR pb on FCU …
APs …
GO AROUND ALTITUDE …
When intercepting from above set FCU ALTITUDE …
AP
APPR pb on FCU:
APs both on
GO AROUND ALTITUDE set
When intercepting from above set the FCU ALTITUDE above the A/C altitude
AP AS RQRD
ENGINE FAILURE after V1 (Pitch)
12,5°
Engine Failure on RF leg
Continue on RF if FMCG working and NAV ACCURACY HIGH
RA 1+2 Fault
APPR oder LOC noch funktional?
Was passiert bei Gear Down
LOC
Direct Law
A320 EO CAT III Single
50’ / 200m
DIRECT LAW (Vorbereitung approach)
Landing Distance Procedure Apply
FLAPS 3 only
Turbulence Penetration Speed
250 kts below FL 200
275 kts between FL 200 - 310
M 0.76 above FL 310
AUTOPILOT CIRCLING APPROACH
500 ft AGL
Approach Preparation Circling Approach
F-PLN: Enter instrument approach procedure
SECF-PLN: Copy active F-PLN and Revise the landing runway
Wind Limit for N/W Steering Fault
Crosswind < 15kts
ELEC FAULT/FAIL
Expanded Procedure für Einschränkungen
IR FAULT (SET SWITCH TO ATT)
Only if IR FAULT light is blinking
GUSTS bei LAPA
Nur normalen Werte
Maximum Crosswind for T/O and Landing
35 kt (gust included)
Maximum Tailwind for T/O
15 kt
Maximum Tailwind for Landing
10 kt
SOS Berechnung Wind
L&V (5kt Tailwind)
LAND or NO LAND WITH ENG FAIL ON FINAL
Below 1000 ft and stabel —> Land
Above 1000 ft only if ECAM ACTIONS COMPLETED before 1000 ft —> Land
Speed Brakes are inhibted …
CONFIG FULL
Thrust levers above MCT position
ALPHA FLOOR activation
AOA PROT
Elevator Fault
SEC 1 and SEC 3 both have faults
Colour Code Heading PERF PAGE
White
Green
Green -> Active Flight Phase (Activate APPR PHASE)
White -> Non active flight phase
How to disengage TOGA LK
Instinctive disconnect A/THR Push Buttons
Landing Gear & Nose Wheel Steering are exclusively operated by which hydraulic system
Turbulence penetration speeds
<20.000ft -> 250kts
>20.000ft -> 275kts/M.76
>FL310 -> M.76
RVSM Airspace
On ground
Inflight
RVSM Airspace: FL290-FL410
On ground prior RVSM: <75ft
Inflight prior RVSM: +-200ft
RVSM: +-150ft
A319/320 CONFIG SPEEDS
CONF 1: 230 kt
CONF 1+F: 215 kt
CONF 2: 200 kt
CONF 3: 185 kt
CONF FULL: 177 kt
Triple Click
Mode Reversion
Wann wird der Brake Fan gestartet?
5 min nach der Landung (low thrust setting), beim eindrehen ins Gate oder wenn Brake Temp >500 Grad
Last changed8 months ago
