A380 Limitations, Recalls and Memory Items Flashcards
Aircraft General / Flight Maneuvering Load Acceleration Limits
Clean configuration
-1 G to +2.5 G
LIM-AG-F_CTL | 31-MAR-06
Aircraft General / Flight Maneuvering Load Acceleration Limits
Other than clean configurations
0 G to +2 G
LIM-AG-F_CTL | 31-MAR-06
Aircraft General / Speeds
Maximum operating speed
VMO and MMO
340 kt / M O.89
LIM-AG-SPD | 15-MAY-07
Aircraft General / Operational Parameters / Environmental Envelope
Maximum operating altitude
43,100 ft
LIM-AG-OPS | 31-MAR-21
Aircraft General / Operational Parameters / Environmental Envelope
Maximum altitude for take-off and landing
10,000 ft
LIM-AG-OPS | 31-MAR-21
Aircraft General / Operational Parameters / Environmental Envelope
Maximum OAT at sea level
55 °C
LIM-AG-OPS | 31-MAR-21
Aircraft General / Operational Parameters / Environmental Envelope
Minimum TAT
-53 °C
LIM-AG-OPS | 31-MAR-21
Aircraft General / Airport Operations and Wind Limitations / Runway Limitations
Maximum runway slope
(mean)
±2 %
LIM-AG-OPS | 02-JAN-20
Aircraft General / Airport Operations and Wind Limitations / Runway Limitations
Minimum runway width
45 m
LIM-AG-OPS | 02-JAN-20
Aircraft General / Airport Operations and Wind Limitations
Maximum certified crosswind for take-off
(gust included)
35 kt
LIM-AG-OPS | 03-MAR-15
Aircraft General / Airport Operations and Wind Limitations
Maximum certified crosswind for landing
(gust included)
40 kt
LIM-AG-OPS | 03-MAR-15
Aircraft General / Airport Operations and Wind Limitations
Maximum tailwind at take-off
15 kt
LIM-AG-OPS | 05-SEP-13
Aircraft General / Airport Operations and Wind Limitations
Maximum tailwind at landing
Airport pressure altitude at, or below 8,000 ft
15 kt
LIM-AG-OPS | 05-SEP-13
Aircraft General / Airport Operations and Wind Limitations
Maximum wind for cabin door operation is ____ kt
Maximum wind is ____ kt, if the aircraft nose is oriented into the wind.
The cabin door must be closed before the wind reaches ____ kt.
40 kt
LIM-AG-OPS | 06-OCT-14
Maximum wind is 50 kt, if the aircraft nose is oriented into the wind.
The cabin door must be closed before the wind reaches 60 kt.
Aircraft General / Airport Operations and Wind Limitations
Maximum wind for cargo door operation is ____ kt
Maximum wind is ____ kt, if the aircraft nose is oriented into the wind, or if the door is on the leeward side.
The cargo door must be closed before the wind reaches ____ kt.
40 kt
LIM-AG-OPS | 06-OCT-14
Maximum wind is 50 kt, if the aircraft nose is oriented into the wind, or if the door is on the leeward side.
The cargo door must be closed before the wind reaches 60 kt.
Aircraft General / Speeds
Maximum cockpit window speed
Opening and Closing
Opening . . . 250 kt
Closing . . . 160 kt
LIM-AG-SPD | 14-FEB-07
Opening the cockpit window is not possible with the packs ON.
Aircraft General / Speeds
Maximum flaps / slats speed
CONF 1
263 kt
LIM-AG-SPD | 14-NOV-06
Aircraft General / Speeds
Maximum flaps / slats speed
CONF 1+F
In CONF 1+F, when the aircraft reaches a speed of ____ kt, the ARS automatically retracts the flaps to CONF 1.
222 kt
LIM-AG-SPD | 14-NOV-06
In CONF 1+F, when the aircraft reaches a speed of 212 kt, the ARS automatically retracts the flaps to CONF 1.
Aircraft General / Speeds
Maximum flaps / slats speed
CONF 2
220 kt
LIM-AG-SPD | 14-NOV-06
Aircraft General / Speeds
Maximum flaps / slats speed
CONF 3
196 kt
LIM-AG-SPD | 14-NOV-06
Aircraft General / Speeds
Maximum flaps / slats speed
CONF FULL
182 kt
LIM-AG-SPD | 14-NOV-06
Aircraft General / Speeds
Maximum speed with the landing gear extended
VLE (and Mach)
250 kt / M O.55
LIM-AG-SPD | 01-AUG-08
Aircraft General / Speeds
Maximum speed with the landing gear operating
VLO (and Mach)
250 kt / M O.55
LIM-AG-SPD | 01-AUG-08
Aircraft General / Speeds
Maximum speed for landing gear gravity extension
VLE/VLO (and Mach)
220 kt / M O.48
LIM-AG-SPD | 01-AUG-08
Aircraft General / Speeds
Maximum tire ground speed
204 kt
LIM-AG-SPD | 13-MAY-08
Aircraft General / Speeds
Minimum control speed
(one-engine inoperative)
VMCL
120 kt
Aircraft General / Speeds
Minimum control speed
(two-engines inoperative)
VMCL-2
144 kt
LIM-AG-SPD | 02-OCT-06
Aircraft General / Speeds
Maximum windshield wipers operating speed
250 kt
LIM-AG-SPD | 14-FEB-07
Aircraft General / Weight and Centre of Gravity Limits
Maximum Taxi Weight
574,000 kg
LIM-AG-WGHT | 02-FEB-18
Aircraft General / Weight and Centre of Gravity Limits
Maximum Take-off Weight
MTOW
572,000 kg
LIM-AG-WGHT | 02-FEB-18
MTOW, MLW, and MZFW vary with the center of gravity.
Aircraft General / Weight and Centre of Gravity Limits
Maximum Landing Weight
MLW
391,000 kg
LIM-AG-WGHT | 02-FEB-18
MTOW, MLW, and MZFW vary with the center of gravity.
In exceptional conditions (in-flight turnback or diversion), an immediate landing at a weight above maximum landing weight is permitted, provided that the flight crew follows the overweight landing procedure.
Aircraft General / Weight and Centre of Gravity Limits
Maximum Zero Fuel Weight
MZFW
366,000 kg
LIM-AG-WGHT | 02-FEB-18
MTOW, MLW, and MZFW vary with the center of gravity.
Aircraft General / Weight and Centre of Gravity Limits
Minimum Weight
270,000 kg
LIM-AG-WGHT | 02-FEB-18
Air BLEED/COND/PRESS/VENT / Air Conditioning with HP Ground Air Supply
Use of HP ground air supply when APU supplies bleed air
Do not use HP ground air supply, when APU supplies bleed air
LIM-AIR | 31-MAR-06
Air BLEED/COND/PRESS/VENT / Take-off Packs Off Prohibited
Take-off with both packs OFF
Take-off with both packs OFF is prohibited
LIM-AIR | 14-APR-22
Air BLEED/COND/PRESS/VENT / Cabin Pressure
Maximum positive differential pressure
9.65 psi
LIM-AIR | 27-SEP-22
Air BLEED/COND/PRESS/VENT / Cabin Pressure
Maximum negative differential pressure
-0.725 psi
LIM-AIR | 27-SEP-22
Procedures / Abnormal and Emergency Procedures / CABIN PRESS
CABIN PRESS warning is triggered if the cabin altitude is above ____ .
9,550 ft
PRO-ABN-CAB_PRESS | 25-MAR-09
Auto Flight System / General
Minimum height for use of autopilot after take-off
100 ft AGL and at least 5 s after liftoff
LIM-AFS-10 | 02-FEB-18
An internal PRIM logic prevents the autopilot from engaging during 5 s after liftoff.
Auto Flight System / General
Minimum height for use of autopilot during a
non-precision approach
200 ft AGL
LIM-AFS-10 | 02-FEB-18
The AP or FD in OP DES or DES mode can be used in approach.
However, its use is only permitted if the AFS CP selected altitude is set to, or above, the higher of:
- MDA/MDH, or
- 500 ft AGL.
Auto Flight System / General
Minimum height for use of autopilot during a
circling approach
200 ft AGL
LIM-AFS-10 | 02-FEB-18
The AP or FD in OP DES or DES mode can be used in approach.
However, its use is only permitted if the AFS CP selected altitude is set to, or above, the higher of:
- MDA/MDH, or
- 500 ft AGL.
Auto Flight System / General
Minimum height for use of autopilot during a
CAT I ILS approach
APPR1 displayed on the FMA
160 ft AGL
LIM-AFS-10 | 02-FEB-18
The AP or FD in OP DES or DES mode can be used in approach.
However, its use is only permitted if the AFS CP selected altitude is set to, or above, the higher of:
- MDA/MDH, or
- 500 ft AGL.
Auto Flight System / General
Minimum height for use of autopilot after
manual go-around
100 ft AGL
LIM-AFS-10 | 02-FEB-18
Auto Flight System / General
Minimum height for use of autopilot during all other phases
500 ft AGL
LIM-AFS-10 | 02-FEB-18
Auto Flight System / Automatic Approach, Landing, and Roll-Out
Maximum headwind for
auto land
GLS CAT I, ILS CAT II or ILS CAT III
38 kt
LIM-AFS-30 | 06-OCT-14
Auto Flight System / Automatic Approach, Landing, and Roll-Out
Maximum tailwind for
auto land at, or below 8,000 ft
GLS CAT I, ILS CAT II or ILS CAT III
15 kt
LIM-AFS-30 | 06-OCT-14
Auto Flight System / Automatic Approach, Landing, and Roll-Out
Maximum crosswind for
auto land
GLS CAT I, ILS CAT II or ILS CAT III
30 kt
LIM-AFS-30 | 06-OCT-14
Auto Flight System / Automatic Approach, Landing, and Roll-Out
Alert height
200 ft
LIM-AFS-30 | 07-OCT-18
Auxiliary Power Unit / General
During the APU start, the flight crew must wait ____ after setting the APU MASTER pb-sw to ON, before setting the APU START pb to ON.
5 s
LIM-APU | 10-APR-18
These 5 s correspond to the time the ECB needs to power up when the APU MASTER pushbutton-switch is set to ON.
Auxiliary Power Unit / General
In the case of an aborted APU start or APU shutdown, the flight crew must wait ____ before a new start attempt.
60 s
LIM-APU | 10-APR-18
This 60 s period is due to the ECB inhibition logic after an aborted APU start or APU shutdown.
Auxiliary Power Unit / General
After ____ consecutive APU start attempts, the flight crew must wait ____ before a new start attempt.
3 … 60 min
LIM-APU | 10-APR-18
This 60 min period is to allow the APU starter to cool down.
Auxiliary Power Unit / Operational Envelope
The APU can operate when the aircraft speed is below ____ .
(except in emergency configuration)
M 0.56
LIM-APU | 02-FEB-18
In the case of an all-engine failure, the APU can operate at any aircraft speed.
Auxiliary Power Unit / Operational Envelope
Maximum pressure altitude for APU start
20,000 ft
LIM-APU | 02-FEB-18
Auxiliary Power Unit / Operational Envelope
APU can supply electrical power, and bleed air, up to ____ ft pressure altitude.
22,500 ft
LIM-APU | 02-FEB-18
APU bleed air can be supplied provided the aircraft airspeed is below M 0.56.
Use of APU bleed air for wing anti-ice is not permitted.
Auxiliary Power Unit / Operational Envelope
Number of APU Generators that can operate in flight
1
LIM-APU | 02-FEB-18
Communication / HF Communication
Use of HF communication during refuelling
During refuelling, HF communication should not be used
LIM-COM | 05-MAR-09
Electrical / Electrical Outlets
Use of electrical outlets during take-off and landing
Do not use the electrical outlets during takeoff and landing.
LIM-ELEC | 31-MAR-06
Engines / Thrust Setting/EGT Limits
Take-off and go-around
(all engines operative)
Time Limit and EGT Limit
Time Limit . . . 5 min
EGT Limit . . . 900 °C
LIM-ENG | 29-JUL-09
Engines / Thrust Setting/EGT Limits
Take-off and go-around
(one engine inoperative)
Time Limit and EGT Limit
Time Limit . . . 10 min
EGT Limit . . . 900 °C
LIM-ENG | 29-JUL-09
Engines / Thrust Setting/EGT Limits
Maximum Continuous Thrust (MCT)
EGT limit
850 °C
LIM-ENG | 29-JUL-09
Engines / Thrust Setting/EGT Limits
Starting
On Ground and In Flight EGT limit
On Ground . . . 700 °C
In Flight . . . 850 °C
LIM-ENG | 29-JUL-09
Engines / Oil
Minimum starting temperature
-40 °C
LIM-ENG | 07-JUL-20
Engines / Oil
Minimum temperature prior to take-off
40 °C
LIM-ENG | 07-JUL-20
Engines / Oil
Minimum quantity with
OAT < 0 °C
Flight Time below 14 h and at or above 14 h
13 qts minimum, or
6 qts + 0.5 qt/h for flight time at or above 14 h
LIM-ENG | 07-JUL-20
Engines / Oil
Minimum quantity with
OAT ≥ 0 °C
Flight Time below 8 h and at or above 8 h
10 qts minimum, or
6 qts + 0.5 qt/h for flight time at or above 8 h
LIM-ENG | 07-JUL-20
Engines / Starter
Maximum continuous starter operation
Multiple cycles and one cycle
Either:
- Two consecutive cycles of 2 min duration maximum, plus one additional cycle of 1 min, with a run down to zero N3 between each cycle, or
- One 5 min cycle.
LIM-ENG | 05-JAN-21
Engines / Starter
Wait ____ after the last cycle to allow the starter to cool
30 min
LIM-ENG | 05-JAN-21
Engines / Starter
No running engagement of the starter when the ____ is above ____ .
On Ground and In Flight
On Ground . . . N3 … 10 %
In Flight . . . N3 … 30 %
LIM-ENG | 05-JAN-21
Engines / Reverse Thrust
Maximum reverse should not be used below ____ kt.
70 kt
LIM-ENG | 10-SEP-07
Idle reverse is allowed down to aircraft stop.
Engines / Reduced Thrust Takeoff
Reduced thrust take-off on contaminated runways
Takeoff at reduced thrust is not allowed on contaminated runways
LIM-ENG | 19-JAN-15
Engines / Reduced Thrust Takeoff
FLEX temperature limits
Maximum and Minimum FLEX rating
The FLEX temperature must not be:
- Higher than ISA + 60 °C, or
- Lower than the flat rating temperature or actual OAT
LIM-ENG | 19-JAN-15
Fuel / Fuel Temperature
JET A fuel
Minimum fuel temperature
-40 °C
LIM-FUEL | 10-JAN-18
Fuel / Fuel Temperature
JET A1 fuel
Minimum fuel temperature
-47 °C
LIM-FUEL | 10-JAN-18
If any of the two previous flights were from the USA (where Jet A fuel is uplifted), the fuel freeze point for the next sector must be considered to be -40 °C.
Fuel / Maximum Allowed Wing Fuel Imbalance
Feed Tanks 1 / Feed Tanks 4
Maximum allowed wing imbalance at take-off, in flight, and landing
3,000 kg
LIM-FUEL | 28-SEP-12
In abnormal conditions (i.e. fuel system failures) the above-mentioned maximum fuel imbalance values may be exceeded without significantly affecting the aircraft handling qualities. The aircraft remains fully controllable in all phases of the flight.
Fuel / Maximum Allowed Wing Fuel Imbalance
Feed Tanks 2 / Feed Tanks 3
Maximum allowed wing imbalance at take-off, in flight, and landing
3,000 kg
LIM-FUEL | 28-SEP-12
In abnormal conditions (i.e. fuel system failures) the above-mentioned maximum fuel imbalance values may be exceeded without significantly affecting the aircraft handling qualities. The aircraft remains fully controllable in all phases of the flight.
Fuel / Maximum Allowed Wing Fuel Imbalance
Left Inner Tank / Right Inner Tank
Maximum allowed wing imbalance at take-off, in flight, and landing
3,000 kg
LIM-FUEL | 28-SEP-12
In abnormal conditions (i.e. fuel system failures) the above-mentioned maximum fuel imbalance values may be exceeded without significantly affecting the aircraft handling qualities. The aircraft remains fully controllable in all phases of the flight.
Fuel / Maximum Allowed Wing Fuel Imbalance
Left Mid Tank / Right Mid Tank
Maximum allowed wing imbalance at take-off, in flight, and landing
2,500 kg
LIM-FUEL | 28-SEP-12
In abnormal conditions (i.e. fuel system failures) the above-mentioned maximum fuel imbalance values may be exceeded without significantly affecting the aircraft handling qualities. The aircraft remains fully controllable in all phases of the flight.
Fuel / Maximum Allowed Wing Fuel Imbalance
Left Outer Tank / Right Outer Tank
Maximum allowed wing imbalance at take-off, in flight, and landing
1,200 kg
LIM-FUEL | 28-SEP-12
In abnormal conditions (i.e. fuel system failures) the above-mentioned maximum fuel imbalance values may be exceeded without significantly affecting the aircraft handling qualities. The aircraft remains fully controllable in all phases of the flight.
Landing Gear / Brake Temperature
Maximum brake temperature for take-off
300 °C
LIM-LG | 31-MAR-21
Landing Gear / Maximum Altitude with the Landing Gear Extended
Maximum altitude at which the landing gear can be extended
21,000 ft
LIM-LG | 31-MAR-21
Landing Gear / Taxi with Deflated Tires
Maximum taxi speed
3 kt
LIM-LG | 07-NOV-16
Landing Gear / Taxi with Deflated Tires
Up to ____ tires can be deflated
9
LIM-LG | 07-NOV-16
Landing Gear / Taxi with Deflated Tires
Maximum deflated tires per landing gear
Nose Landing Gear
1
LIM-LG | 07-NOV-16
Landing Gear / Taxi with Deflated Tires
Maximum deflated tires per landing gear
Body Landing Gear (BLG)
2
LIM-LG | 07-NOV-16
Two deflated tires per BLG provided they are not on the same axle.
Landing Gear / Taxi with Deflated Tires
Maximum deflated tires per landing gear
Wing Landing Gear (WLG)
2
LIM-LG | 07-NOV-16
Two deflated tires per WLG provided they are not on the same axle.
Landing Gear / Taxi with Abnormal Wing or Body Landing Gear
Maximum taxi speed
5 kt
LIM-LG | 30-MAR-21
Landing Gear / Taxi with Abnormal Wing or Body Landing Gear
Maximum NWS angle
50 °
LIM-LG | 30-MAR-21
Landing Gear / Taxi with Abnormal Wing or Body Landing Gear
Maximum crosswind component for taxi
Wing Landing Gear (WLG) and Body Landing Gear (BLG
WLG . . . 40 kt
BLG . . . 35 kt
LIM-LG | 30-MAR-21
For taxi with one abnormal WLG, the maximum recommended crosswind for landing is applicable.
Navigation / On-board Airport Navigation System (OANS)
Use during take-off
PF display
Not authorized on PF display
LIM-NAV-10 | 23-DEC-20
Navigation / On-board Airport Navigation System (OANS)
Use during roll-out after touchdown
PF and PM Display
PM Display . . . Authorized
PF Display . . . Authorized at taxi speed
LIM-NAV-10 | 23-DEC-20
Abnormal and Emergency Procedures / MEMORY ITEMS
LOSS OF BRAKING
“LOSS OF BRAKING”
PRO-ABN-BRAKES | 31-MAR-21
● IF NO BRAKING:
REV . . . . . . . . . . . . . . . . . . . . . . MAX (PF)
BRAKE PEDALS . . . . . . . . . . . . RELEASE (PF)
A-SKID OFF . . . . . . . . . . . . . . . ORDER (PF)
A-SKID . . . . . . . . . . . . . . . . . . . OFF (PM)
BRAKE PEDALS . . . . . . . . . . . . PRESS (PF)
● IF STILL NO BRAKING:
PARK BRK . . . . . . . . . . . . . . ON (PF)
Abnormal and Emergency Procedures / MEMORY ITEMS
EMER DESCENT
“EMERGENCY DESCENT”
PRO-ABN-MISC | 31-MAR-21
CREW OXY MASKS . . . . . . . . . . . . . . . USE
SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . ON
EMER DESCENT . . . . . . . . . . . . . . . . . INITIATE
● IF A/THR IS NOT ACTIVE:
ALL THR LEVERS . . . . . . . . . . . . . . . IDLE
SPEED BRAKE LEVER . . . . . . . . . . . . . FULL
Abnormal and Emergency Procedures / MEMORY ITEMS
STALL RECOVERY
“STALL, I HAVE CONTROL”
PRO-ABN-MISC | 31-MAR-21
NOSE DOWN PITCH . . APPLY
BANK . . . . . . . . . . . . . . WINGS LEVEL
● WHEN OUT OF STALL (NO LONGER STALL
INDICATIONS):
THRUST . . . . . . . . . . INCREASE SMOOTHLY
SPEEDBRAKES . . . . CHECK RETRACTED
FLIGHT PATH . . . . . RECOVER SMOOTHLY
● IF IN CLEAN CONFIGURATION AND
BELOW 20,000 FT:
FLAP 1 . . . . . . . . . SELECT
Note: if a risk of ground contact exists, once clearly out of stall (no longer stall indications), establish smoothly a positive climb gradient.
Abnormal and Emergency Procedures / MEMORY ITEMS
STALL WARNING AT LIFTOFF
“STALL, TOGA 12.5 °”
PRO-ABN-MISC | 31-MAR-21
THRUST . . . . . . . . . . . . . . . . . . . . TOGA
PITCH ATTITUDE . . . . . . . . . . . . 12.5 °
BANK . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL
Abnormal and Emergency Procedures / MEMORY ITEMS
UNRELIABLE AIR SPEED INDICATION
“UNRELIABLE SPEED”
PRO-ABN-NAV | 31-MAR-21
● IF SAFE CONDUCT OF FLIGHT IMPACTED:
AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
◼︎ BEFORE THRUST REDUCTION:
ALL THR LEVERS . . . . . . . . . . . . . . . . . TOGA
PITCH TARGET . . . . . . . . . . . . . . . . . . . 12.5 °
◼︎ AFTER THRUST REDUCTION:
● IF DERATED CLIMB ENGAGED:
ALL THR LEVERS . . . . . . . . . . . . . . . MCT
ALL THR LEVERS . . . . . . . . . . . . . . . . . CLB
PITCH TARGET . . . . . . . . . . (see below)
| < 10,000 ft | 10,000-25,000 ft | > 25,000 ft |
| 12.5 ° | 10 ° | 5 ° |
● IF THE FLAPS LEVER IS SET TO FULL:
FLAPS . . . . . . . . . . . . . . . . . . . . CONF 3
FLAPS & L/G . . . . . . . . MAINTAIN CONF
SPEED BRAKES . . . . . . CHECK RETRACTED
Abnormal and Emergency Procedures / MEMORY ITEMS
TAWS WARNING
“PULL UP TOGA”
PRO-ABN-SURV | 31-MAR-21
● IF THE TAWS TRIGGERS ONE OF THE PULL UP ALERTS:
AP . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
PITCH . . . . . . . . . . . . . . . . . . . . . . . PULL UP
THR LEVERS . . . . . . . . . . . . . . . . . . . . . TOGA
SPEED BRAKE LEVER . . . . . . . . CHECK RETRACTED
BANK . . . . . . . . . . . . . . WINGS LEVEL or ADJUST
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.
Abnormal and Emergency Procedures / MEMORY ITEMS
TCAS CAUTION -
TRAFFIC ADVISORY
“TCAS, I HAVE CONTROL”
PRO-ABN-SURV | 31-MAR-21
Do not perform a maneuver based on a TA alone.
Abnormal and Emergency Procedures / MEMORY ITEMS
TCAS WARNING -
RESOLUTION ADVISORY
PRO-ABN-SURV | 31-MAR-21
ALL RA, EXCEPT ANY CLIMB RA DURING APPROACH IN CONF 3 OR FULL:
- AP (if engaged) . . . OFF
- FDs . . . OFF
Respond promptly and smoothly
- VERTICAL SPEED . . . ADJUST OR MAINTAIN
ANY CLIMB RA DURING APPROACH IN CONF 3 OR FULL:
- GO-AROUND . . . PERFORM
- VERTICAL SPEED . . . MONITOR
Respect stall, GPWS or windshear warnings.
ATC . . . NOTIFY
WHEN “CLEAR OF CONFLICT” AURAL ALERT SOUNDS:
- ATC . . . NOTIFY
- LATERAL AND VERTICAL GUIDANCE . . . ADJUST
- AP/FD . . . AS REQD
Abnormal and Emergency Procedures / MEMORY ITEMS
WINDSHEAR WARNING -
REACTIVE WINDSHEAR
“WINDSHEAR TOGA”
PRO-ABN-SURV | 31-MAR-21
◼︎ ON GROUND, AT TAKE-OFF:
● BEFORE V1:
If there are significant variations in
airspeed, and in airspeed trend below the
indicated V1, reject the take-off.
● AFTER V1:
THR LEVERS . . . TOGA
REACHING Vr . . . ROTATE NORMALLY
SRS ORDERS . . . FOLLOW
◼︎ WHEN AIRBORNE, DURING INITIAL
CLIMB, OR AT LANDING:
THR LEVERS . . . . . . . . . . . . . . . TOGA
AP (if engaged) . . . . . . . . . . . . . KEEP ON
SRS ORDERS . . . . . . . . . . . . . . FOLLOW
- DO NOT CHANGE CONFIGURATION
(SLATS/FLAPS, GEAR) UNTIL OUT OF
WINDSHEAR
- CAREFULLY MONITOR FLIGHT PATH AND
SPEED
- RECOVER SMOOTHLY TO CLIMB, WHEN
OUT OF WINDSHEAR