A380 Limitations, Recalls and Memory Items

Question 1

Aircraft General / Flight Maneuvering Load Acceleration Limits

Clean configuration

Answer 1

-1 G to +2.5 G

LIM-AG-F_CTL | 31-MAR-06

Question 2

Aircraft General / Flight Maneuvering Load Acceleration Limits

Other than clean configurations

Answer 2

0 G to +2 G

LIM-AG-F_CTL | 31-MAR-06

Question 3

Aircraft General / Speeds

Maximum operating speed

VMO and MMO

Answer 3

340 kt / M O.89

LIM-AG-SPD | 15-MAY-07

Question 4

Aircraft General / Operational Parameters / Environmental Envelope

Maximum operating altitude

Answer 4

43,100 ft

LIM-AG-OPS | 31-MAR-21

Question 5

Aircraft General / Operational Parameters / Environmental Envelope

Maximum altitude for take-off and landing

Answer 5

10,000 ft

LIM-AG-OPS | 31-MAR-21

Question 6

Aircraft General / Operational Parameters / Environmental Envelope

Maximum OAT at sea level

Answer 6

55 °C

LIM-AG-OPS | 31-MAR-21

Question 7

Aircraft General / Operational Parameters / Environmental Envelope

Minimum TAT

Answer 7

-53 °C

LIM-AG-OPS | 31-MAR-21

Question 8

Aircraft General / Airport Operations and Wind Limitations / Runway Limitations

Maximum runway slope

(mean)

Answer 8

±2 %

LIM-AG-OPS | 02-JAN-20

Question 9

Aircraft General / Airport Operations and Wind Limitations / Runway Limitations

Minimum runway width

Answer 9

45 m

LIM-AG-OPS | 02-JAN-20

Question 10

Aircraft General / Airport Operations and Wind Limitations

Maximum certified crosswind for take-off

(gust included)

Answer 10

35 kt

LIM-AG-OPS | 03-MAR-15

Question 11

Aircraft General / Airport Operations and Wind Limitations

Maximum certified crosswind for landing

(gust included)

Answer 11

40 kt

LIM-AG-OPS | 03-MAR-15

Question 12

Aircraft General / Airport Operations and Wind Limitations

Maximum tailwind at take-off

Answer 12

15 kt

LIM-AG-OPS | 05-SEP-13

Question 13

Aircraft General / Airport Operations and Wind Limitations

Maximum tailwind at landing

Airport pressure altitude at, or below 8,000 ft

Answer 13

15 kt

LIM-AG-OPS | 05-SEP-13

Question 14

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.

Answer 14

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.

Question 15

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.

Answer 15

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.

Question 16

Aircraft General / Speeds

Maximum cockpit window speed

Opening and Closing

Answer 16

Opening . . . 250 kt

Closing . . . 160 kt

LIM-AG-SPD | 14-FEB-07

Opening the cockpit window is not possible with the packs ON.

Question 17

Aircraft General / Speeds

Maximum flaps / slats speed

CONF 1

Answer 17

263 kt

LIM-AG-SPD | 14-NOV-06

Question 18

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.

Answer 18

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.

Question 19

Aircraft General / Speeds

Maximum flaps / slats speed

CONF 2

Answer 19

220 kt

LIM-AG-SPD | 14-NOV-06

Question 20

Aircraft General / Speeds

Maximum flaps / slats speed

CONF 3

Answer 20

196 kt

LIM-AG-SPD | 14-NOV-06

Question 21

Aircraft General / Speeds

Maximum flaps / slats speed

CONF FULL

Answer 21

182 kt

LIM-AG-SPD | 14-NOV-06

Question 22

Aircraft General / Speeds

Maximum speed with the landing gear extended

VLE (and Mach)

Answer 22

250 kt / M O.55

LIM-AG-SPD | 01-AUG-08

Question 23

Aircraft General / Speeds

Maximum speed with the landing gear operating

VLO (and Mach)

Answer 23

250 kt / M O.55

LIM-AG-SPD | 01-AUG-08

Question 24

Aircraft General / Speeds

Maximum speed for landing gear gravity extension

VLE/VLO (and Mach)

Answer 24

220 kt / M O.48

LIM-AG-SPD | 01-AUG-08

Question 25

# Aircraft General / Speeds Maximum tire ground speed

Answer 25

**204 kt** | LIM-AG-SPD | 13-MAY-08

Question 26

# Aircraft General / Speeds Minimum control speed (one-engine inoperative) | VMCL

Answer 26

**120 kt**

Question 27

# Aircraft General / Speeds Minimum control speed (two-engines inoperative) | VMCL-2

Answer 27

**144 kt** | LIM-AG-SPD | 02-OCT-06

Question 28

# Aircraft General / Speeds Maximum windshield wipers operating speed

Answer 28

**250 kt** | LIM-AG-SPD | 14-FEB-07

Question 29

# Aircraft General / Weight and Centre of Gravity Limits Maximum Taxi Weight

Answer 29

**574,000 kg** | LIM-AG-WGHT | 02-FEB-18

Question 30

# Aircraft General / Weight and Centre of Gravity Limits Maximum Take-off Weight | MTOW

Answer 30

**572,000 kg** | LIM-AG-WGHT | 02-FEB-18 ## Footnote MTOW, MLW, and MZFW vary with the center of gravity.

Question 31

# Aircraft General / Weight and Centre of Gravity Limits Maximum Landing Weight | MLW

Answer 31

**391,000 kg** | LIM-AG-WGHT | 02-FEB-18 ## Footnote 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.

Question 32

# Aircraft General / Weight and Centre of Gravity Limits Maximum Zero Fuel Weight | MZFW

Answer 32

**366,000 kg** | LIM-AG-WGHT | 02-FEB-18 ## Footnote MTOW, MLW, and MZFW vary with the center of gravity.

Question 33

# Aircraft General / Weight and Centre of Gravity Limits Minimum Weight

Answer 33

**270,000 kg** | LIM-AG-WGHT | 02-FEB-18

Question 34

# Air BLEED/COND/PRESS/VENT / Air Conditioning with HP Ground Air Supply Use of HP ground air supply when APU supplies bleed air

Answer 34

**Do not use** HP ground air supply, when APU supplies bleed air | LIM-AIR | 31-MAR-06

Question 35

# Air BLEED/COND/PRESS/VENT / Take-off Packs Off Prohibited Take-off with both packs OFF

Answer 35

Take-off with both packs OFF is **prohibited** | LIM-AIR | 14-APR-22

Question 36

# Air BLEED/COND/PRESS/VENT / Cabin Pressure Maximum positive differential pressure

Answer 36

**9.65 psi** | LIM-AIR | 27-SEP-22

Question 37

# Air BLEED/COND/PRESS/VENT / Cabin Pressure Maximum negative differential pressure

Answer 37

**-0.725 psi** | LIM-AIR | 27-SEP-22

Question 38

# Procedures / Abnormal and Emergency Procedures / CABIN PRESS CABIN PRESS warning is triggered if the cabin altitude is above ____ .

Answer 38

**9,550 ft** | PRO-ABN-CAB_PRESS | 25-MAR-09

Question 39

# Auto Flight System / General Minimum height for use of autopilot after take-off

Answer 39

**100 ft** AGL and at least **5 s** after liftoff | LIM-AFS-10 | 02-FEB-18 ## Footnote An internal PRIM logic prevents the autopilot from engaging during **5 s** after liftoff.

Question 40

# Auto Flight System / General Minimum height for use of autopilot during a non-precision approach

Answer 40

**200 ft** AGL | LIM-AFS-10 | 02-FEB-18 ## Footnote 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.

Question 41

# Auto Flight System / General Minimum height for use of autopilot during a circling approach

Answer 41

**200 ft** AGL | LIM-AFS-10 | 02-FEB-18 ## Footnote 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.

Question 42

# Auto Flight System / General Minimum height for use of autopilot during a CAT I ILS approach | APPR1 displayed on the FMA

Answer 42

**160 ft** AGL | LIM-AFS-10 | 02-FEB-18 ## Footnote 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.

Question 43

# Auto Flight System / General Minimum height for use of autopilot after manual go-around

Answer 43

**100 ft** AGL | LIM-AFS-10 | 02-FEB-18

Question 44

# Auto Flight System / General Minimum height for use of autopilot during all other phases

Answer 44

**500 ft** AGL | LIM-AFS-10 | 02-FEB-18

Question 45

# Auto Flight System / Automatic Approach, Landing, and Roll-Out Maximum headwind for auto land | GLS CAT I, ILS CAT II or ILS CAT III

Answer 45

**38 kt** | LIM-AFS-30 | 06-OCT-14

Question 46

# 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

Answer 46

**15 kt** | LIM-AFS-30 | 06-OCT-14

Question 47

# Auto Flight System / Automatic Approach, Landing, and Roll-Out Maximum crosswind for auto land | GLS CAT I, ILS CAT II or ILS CAT III

Answer 47

**30 kt** | LIM-AFS-30 | 06-OCT-14

Question 48

# Auto Flight System / Automatic Approach, Landing, and Roll-Out Alert height

Answer 48

**200 ft** | LIM-AFS-30 | 07-OCT-18

Question 49

# 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.

Answer 49

**5 s** | LIM-APU | 10-APR-18 ## Footnote These 5 s correspond to the time the ECB needs to power up when the APU MASTER pushbutton-switch is set to ON.

Question 50

# 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.

Answer 50

**60 s** | LIM-APU | 10-APR-18 ## Footnote This 60 s period is due to the ECB inhibition logic after an aborted APU start or APU shutdown.

Question 51

# Auxiliary Power Unit / General After ____ consecutive APU start attempts, the flight crew must wait ____ before a new start attempt.

Answer 51

**3** ... **60 min** | LIM-APU | 10-APR-18 ## Footnote This 60 min period is to allow the APU starter to cool down.

Question 52

# Auxiliary Power Unit / Operational Envelope The APU can operate when the aircraft speed is below ____ . | (except in emergency configuration)

Answer 52

**M 0.56** | LIM-APU | 02-FEB-18 ## Footnote In the case of an all-engine failure, the APU can operate at any aircraft speed.

Question 53

# Auxiliary Power Unit / Operational Envelope Maximum pressure altitude for APU start

Answer 53

**20,000 ft** | LIM-APU | 02-FEB-18

Question 54

# Auxiliary Power Unit / Operational Envelope APU can supply electrical power, and bleed air, up to ____ ft pressure altitude.

Answer 54

**22,500 ft** | LIM-APU | 02-FEB-18 ## Footnote 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.

Question 55

# Auxiliary Power Unit / Operational Envelope Number of APU Generators that can operate in flight

Answer 55

**1** | LIM-APU | 02-FEB-18

Question 56

# Communication / HF Communication Use of HF communication during refuelling

Answer 56

During refuelling, HF communication **should not be used** | LIM-COM | 05-MAR-09

Question 57

# Electrical / Electrical Outlets Use of electrical outlets during take-off and landing

Answer 57

**Do not use** the electrical outlets during takeoff and landing. | LIM-ELEC | 31-MAR-06

Question 58

# Engines / Thrust Setting/EGT Limits Take-off and go-around (all engines operative) | Time Limit **and** EGT Limit

Answer 58

Time Limit . . . **5 min** EGT Limit . . . **900 °C** | LIM-ENG | 29-JUL-09

Question 59

# Engines / Thrust Setting/EGT Limits Take-off and go-around (one engine inoperative) | Time Limit **and** EGT Limit

Answer 59

Time Limit . . . **10 min** EGT Limit . . . **900 °C** | LIM-ENG | 29-JUL-09

Question 60

# Engines / Thrust Setting/EGT Limits Maximum Continuous Thrust (MCT) | EGT limit

Answer 60

**850 °C** | LIM-ENG | 29-JUL-09

Question 61

# Engines / Thrust Setting/EGT Limits Starting | On Ground **and** In Flight EGT limit

Answer 61

On Ground . . . **700 °C** In Flight . . . **850 °C** | LIM-ENG | 29-JUL-09

Question 62

# Engines / Oil Minimum starting temperature

Answer 62

**-40 °C** | LIM-ENG | 07-JUL-20

Question 63

# Engines / Oil Minimum temperature prior to take-off

Answer 63

**40 °C** | LIM-ENG | 07-JUL-20

Question 64

# Engines / Oil Minimum quantity with OAT < 0 °C | Flight Time below 14 h **and** at or above 14 h

Answer 64

**13 qts** minimum, or **6 qts + 0.5 qt/h** for flight time at or above 14 h | LIM-ENG | 07-JUL-20

Question 65

# Engines / Oil Minimum quantity with OAT ≥ 0 °C | Flight Time below 8 h **and** at or above 8 h

Answer 65

**10 qts** minimum, or **6 qts + 0.5 qt/h** for flight time at or above 8 h | LIM-ENG | 07-JUL-20

Question 66

# Engines / Starter Maximum continuous starter operation | Multiple cycles **and** one cycle

Answer 66

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

Question 67

# Engines / Starter Wait ____ after the last cycle to allow the starter to cool

Answer 67

**30 min** | LIM-ENG | 05-JAN-21

Question 68

# Engines / Starter No running engagement of the starter when the ____ is above ____ . | On Ground **and** In Flight

Answer 68

On Ground . . . **N3** … **10 %** In Flight . . . **N3** … **30 %** | LIM-ENG | 05-JAN-21

Question 69

# Engines / Reverse Thrust Maximum reverse should not be used below ____ kt.

Answer 69

**70 kt** | LIM-ENG | 10-SEP-07 ## Footnote Idle reverse is allowed down to aircraft stop.

Question 70

# Engines / Reduced Thrust Takeoff Reduced thrust take-off on contaminated runways

Answer 70

Takeoff at reduced thrust is **not allowed** on contaminated runways | LIM-ENG | 19-JAN-15

Question 71

# Engines / Reduced Thrust Takeoff FLEX temperature limits | Maximum **and** Minimum FLEX rating

Answer 71

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

Question 72

# Fuel / Fuel Temperature JET A fuel | Minimum fuel temperature

Answer 72

**-40 °C** | LIM-FUEL | 10-JAN-18

Question 73

# Fuel / Fuel Temperature JET A1 fuel | Minimum fuel temperature

Answer 73

**-47 °C** | LIM-FUEL | 10-JAN-18 ## Footnote 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.

Question 74

# Fuel / Maximum Allowed Wing Fuel Imbalance Feed Tanks 1 / Feed Tanks 4 | Maximum allowed wing imbalance at take-off, in flight, and landing

Answer 74

**3,000 kg** | LIM-FUEL | 28-SEP-12 ## Footnote 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.

Question 75

# Fuel / Maximum Allowed Wing Fuel Imbalance Feed Tanks 2 / Feed Tanks 3 | Maximum allowed wing imbalance at take-off, in flight, and landing

Answer 75

**3,000 kg** | LIM-FUEL | 28-SEP-12 ## Footnote 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.

Question 76

# Fuel / Maximum Allowed Wing Fuel Imbalance Left Inner Tank / Right Inner Tank | Maximum allowed wing imbalance at take-off, in flight, and landing

Answer 76

**3,000 kg** | LIM-FUEL | 28-SEP-12 ## Footnote 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.

Question 77

# Fuel / Maximum Allowed Wing Fuel Imbalance Left Mid Tank / Right Mid Tank | Maximum allowed wing imbalance at take-off, in flight, and landing

Answer 77

**2,500 kg** | LIM-FUEL | 28-SEP-12 ## Footnote 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.

Question 78

# Fuel / Maximum Allowed Wing Fuel Imbalance Left Outer Tank / Right Outer Tank | Maximum allowed wing imbalance at take-off, in flight, and landing

Answer 78

**1,200 kg** | LIM-FUEL | 28-SEP-12 ## Footnote 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.

Question 79

# Landing Gear / Brake Temperature Maximum brake temperature for take-off

Answer 79

**300 °C** | LIM-LG | 31-MAR-21

Question 80

# Landing Gear / Maximum Altitude with the Landing Gear Extended Maximum altitude at which the landing gear can be extended

Answer 80

**21,000 ft** | LIM-LG | 31-MAR-21

Question 81

# Landing Gear / Taxi with Deflated Tires Maximum taxi speed

Answer 81

**3 kt** | LIM-LG | 07-NOV-16

Question 82

# Landing Gear / Taxi with Deflated Tires Up to ____ tires can be deflated

Answer 82

**9** | LIM-LG | 07-NOV-16

Question 83

# Landing Gear / Taxi with Deflated Tires Maximum deflated tires per landing gear | Nose Landing Gear

Answer 83

**1** | LIM-LG | 07-NOV-16

Question 84

# Landing Gear / Taxi with Deflated Tires Maximum deflated tires per landing gear | Body Landing Gear (BLG)

Answer 84

**2** | LIM-LG | 07-NOV-16 ## Footnote Two deflated tires per BLG provided they are not on the same axle.

Question 85

# Landing Gear / Taxi with Deflated Tires Maximum deflated tires per landing gear | Wing Landing Gear (WLG)

Answer 85

**2** | LIM-LG | 07-NOV-16 ## Footnote Two deflated tires per WLG provided they are not on the same axle.

Question 86

# Landing Gear / Taxi with Abnormal Wing or Body Landing Gear Maximum taxi speed

Answer 86

**5 kt** | LIM-LG | 30-MAR-21

Question 87

# Landing Gear / Taxi with Abnormal Wing or Body Landing Gear Maximum NWS angle

Answer 87

**50 °** | LIM-LG | 30-MAR-21

Question 88

# Landing Gear / Taxi with Abnormal Wing or Body Landing Gear Maximum crosswind component for taxi | Wing Landing Gear (WLG) **and** Body Landing Gear (BLG

Answer 88

WLG . . . **40 kt** BLG . . . **35 kt** | LIM-LG | 30-MAR-21 ## Footnote For taxi with one abnormal WLG, the maximum recommended crosswind for landing is applicable.

Question 89

# Navigation / On-board Airport Navigation System (OANS) Use during take-off | PF display

Answer 89

**Not authorized** on PF display | LIM-NAV-10 | 23-DEC-20

Question 90

# Navigation / On-board Airport Navigation System (OANS) Use during roll-out after touchdown | PF **and** PM Display

Answer 90

PM Display . . . **Authorized** PF Display . . . **Authorized at taxi speed** | LIM-NAV-10 | 23-DEC-20

Question 91

# Abnormal and Emergency Procedures / MEMORY ITEMS LOSS OF BRAKING

Answer 91

"LOSS OF BRAKING" | PRO-ABN-BRAKES | 31-MAR-21 ## Footnote **● 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)

Question 92

# Abnormal and Emergency Procedures / MEMORY ITEMS EMER DESCENT

Answer 92

"EMERGENCY DESCENT" | PRO-ABN-MISC | 31-MAR-21 ## Footnote CREW OXY MASKS . . . . . . . . . . . . . . . USE SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . ON EMER DESCENT . . . . . . . . . . . . . . . . . INITIATE **● IF A/THR IS NOT ACTIVE:** ALL THR LEVERS . . . . . . . . . . . . . . . IDLE SPEED BRAKE LEVER . . . . . . . . . . . . . FULL

Question 93

# Abnormal and Emergency Procedures / MEMORY ITEMS STALL RECOVERY

Answer 93

"STALL, I HAVE CONTROL" | PRO-ABN-MISC | 31-MAR-21 ## Footnote 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.*

Question 94

# Abnormal and Emergency Procedures / MEMORY ITEMS STALL WARNING AT LIFTOFF

Answer 94

"STALL, TOGA 12.5 °" | PRO-ABN-MISC | 31-MAR-21 ## Footnote THRUST . . . . . . . . . . . . . . . . . . . . TOGA PITCH ATTITUDE . . . . . . . . . . . . 12.5 ° BANK . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL

Question 95

# Abnormal and Emergency Procedures / MEMORY ITEMS UNRELIABLE AIR SPEED INDICATION

Answer 95

"UNRELIABLE SPEED" | PRO-ABN-NAV | 31-MAR-21 ## Footnote **● 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

Question 96

# Abnormal and Emergency Procedures / MEMORY ITEMS TAWS WARNING

Answer 96

"PULL UP TOGA" | PRO-ABN-SURV | 31-MAR-21 ## Footnote **● 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.

Question 97

# Abnormal and Emergency Procedures / MEMORY ITEMS TCAS CAUTION - TRAFFIC ADVISORY

Answer 97

"TCAS, I HAVE CONTROL" | PRO-ABN-SURV | 31-MAR-21 ## Footnote Do not perform a maneuver based on a TA alone.

Question 98

# Abnormal and Emergency Procedures / MEMORY ITEMS TCAS WARNING - RESOLUTION ADVISORY

Answer 98

| PRO-ABN-SURV | 31-MAR-21 ## Footnote **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

Question 99

# Abnormal and Emergency Procedures / MEMORY ITEMS WINDSHEAR WARNING - REACTIVE WINDSHEAR

Answer 99

"WINDSHEAR TOGA" | PRO-ABN-SURV | 31-MAR-21 ## Footnote **◼︎ 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