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Qantas > A380 Limitations, Recalls and Memory Items > Flashcards

A380 Limitations, Recalls and Memory Items Flashcards

1
Q

Aircraft General / Flight Maneuvering Load Acceleration Limits

Clean configuration

A

-1 G to +2.5 G

LIM-AG-F_CTL | 31-MAR-06

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2
Q

Aircraft General / Flight Maneuvering Load Acceleration Limits

Other than clean configurations

A

0 G to +2 G

LIM-AG-F_CTL | 31-MAR-06

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3
Q

Aircraft General / Speeds

Maximum operating speed

VMO and MMO

A

340 kt / M O.89

LIM-AG-SPD | 15-MAY-07

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4
Q

Aircraft General / Operational Parameters / Environmental Envelope

Maximum operating altitude

A

43,100 ft

LIM-AG-OPS | 31-MAR-21

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5
Q

Aircraft General / Operational Parameters / Environmental Envelope

Maximum altitude for take-off and landing

A

10,000 ft

LIM-AG-OPS | 31-MAR-21

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6
Q

Aircraft General / Operational Parameters / Environmental Envelope

Maximum OAT at sea level

A

55 °C

LIM-AG-OPS | 31-MAR-21

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7
Q

Aircraft General / Operational Parameters / Environmental Envelope

Minimum TAT

A

-53 °C

LIM-AG-OPS | 31-MAR-21

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8
Q

Aircraft General / Airport Operations and Wind Limitations / Runway Limitations

Maximum runway slope

(mean)

A

±2 %

LIM-AG-OPS | 02-JAN-20

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9
Q

Aircraft General / Airport Operations and Wind Limitations / Runway Limitations

Minimum runway width

A

45 m

LIM-AG-OPS | 02-JAN-20

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10
Q

Aircraft General / Airport Operations and Wind Limitations

Maximum certified crosswind for take-off

(gust included)

A

35 kt

LIM-AG-OPS | 03-MAR-15

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11
Q

Aircraft General / Airport Operations and Wind Limitations

Maximum certified crosswind for landing

(gust included)

A

40 kt

LIM-AG-OPS | 03-MAR-15

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12
Q

Aircraft General / Airport Operations and Wind Limitations

Maximum tailwind at take-off

A

15 kt

LIM-AG-OPS | 05-SEP-13

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13
Q

Aircraft General / Airport Operations and Wind Limitations

Maximum tailwind at landing

Airport pressure altitude at, or below 8,000 ft

A

15 kt

LIM-AG-OPS | 05-SEP-13

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14
Q

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.

A

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.

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15
Q

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.

A

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.

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16
Q

Aircraft General / Speeds

Maximum cockpit window speed

Opening and Closing

A

Opening . . . 250 kt

Closing . . . 160 kt

LIM-AG-SPD | 14-FEB-07

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

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17
Q

Aircraft General / Speeds

Maximum flaps / slats speed

CONF 1

A

263 kt

LIM-AG-SPD | 14-NOV-06

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18
Q

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.

A

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.

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19
Q

Aircraft General / Speeds

Maximum flaps / slats speed

CONF 2

A

220 kt

LIM-AG-SPD | 14-NOV-06

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20
Q

Aircraft General / Speeds

Maximum flaps / slats speed

CONF 3

A

196 kt

LIM-AG-SPD | 14-NOV-06

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21
Q

Aircraft General / Speeds

Maximum flaps / slats speed

CONF FULL

A

182 kt

LIM-AG-SPD | 14-NOV-06

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22
Q

Aircraft General / Speeds

Maximum speed with the landing gear extended

VLE (and Mach)

A

250 kt / M O.55

LIM-AG-SPD | 01-AUG-08

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23
Q

Aircraft General / Speeds

Maximum speed with the landing gear operating

VLO (and Mach)

A

250 kt / M O.55

LIM-AG-SPD | 01-AUG-08

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24
Q

Aircraft General / Speeds

Maximum speed for landing gear gravity extension

VLE/VLO (and Mach)

A

220 kt / M O.48

LIM-AG-SPD | 01-AUG-08

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25
Q

Aircraft General / Speeds

Maximum tire ground speed

A

204 kt

LIM-AG-SPD | 13-MAY-08

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26
Q

Aircraft General / Speeds

Minimum control speed
(one-engine inoperative)

VMCL

A

120 kt

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27
Q

Aircraft General / Speeds

Minimum control speed
(two-engines inoperative)

VMCL-2

A

144 kt

LIM-AG-SPD | 02-OCT-06

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28
Q

Aircraft General / Speeds

Maximum windshield wipers operating speed

A

250 kt

LIM-AG-SPD | 14-FEB-07

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29
Q

Aircraft General / Weight and Centre of Gravity Limits

Maximum Taxi Weight

A

574,000 kg

LIM-AG-WGHT | 02-FEB-18

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30
Q

Aircraft General / Weight and Centre of Gravity Limits

Maximum Take-off Weight

MTOW

A

572,000 kg

LIM-AG-WGHT | 02-FEB-18

MTOW, MLW, and MZFW vary with the center of gravity.

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31
Q

Aircraft General / Weight and Centre of Gravity Limits

Maximum Landing Weight

MLW

A

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.

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32
Q

Aircraft General / Weight and Centre of Gravity Limits

Maximum Zero Fuel Weight

MZFW

A

366,000 kg

LIM-AG-WGHT | 02-FEB-18

MTOW, MLW, and MZFW vary with the center of gravity.

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33
Q

Aircraft General / Weight and Centre of Gravity Limits

Minimum Weight

A

270,000 kg

LIM-AG-WGHT | 02-FEB-18

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34
Q

Air BLEED/COND/PRESS/VENT / Air Conditioning with HP Ground Air Supply

Use of HP ground air supply when APU supplies bleed air

A

Do not use HP ground air supply, when APU supplies bleed air

LIM-AIR | 31-MAR-06

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35
Q

Air BLEED/COND/PRESS/VENT / Take-off Packs Off Prohibited

Take-off with both packs OFF

A

Take-off with both packs OFF is prohibited

LIM-AIR | 14-APR-22

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36
Q

Air BLEED/COND/PRESS/VENT / Cabin Pressure

Maximum positive differential pressure

A

9.65 psi

LIM-AIR | 27-SEP-22

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37
Q

Air BLEED/COND/PRESS/VENT / Cabin Pressure

Maximum negative differential pressure

A

-0.725 psi

LIM-AIR | 27-SEP-22

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38
Q

Procedures / Abnormal and Emergency Procedures / CABIN PRESS

CABIN PRESS warning is triggered if the cabin altitude is above ____ .

A

9,550 ft

PRO-ABN-CAB_PRESS | 25-MAR-09

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39
Q

Auto Flight System / General

Minimum height for use of autopilot after take-off

A

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.

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40
Q

Auto Flight System / General

Minimum height for use of autopilot during a
non-precision approach

A

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.

41
Q

Auto Flight System / General

Minimum height for use of autopilot during a
circling approach

A

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.

42
Q

Auto Flight System / General

Minimum height for use of autopilot during a
CAT I ILS approach

APPR1 displayed on the FMA

A

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.

43
Q

Auto Flight System / General

Minimum height for use of autopilot after
manual go-around

A

100 ft AGL

LIM-AFS-10 | 02-FEB-18

44
Q

Auto Flight System / General

Minimum height for use of autopilot during all other phases

A

500 ft AGL

LIM-AFS-10 | 02-FEB-18

45
Q

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

Maximum headwind for
auto land

GLS CAT I, ILS CAT II or ILS CAT III

A

38 kt

LIM-AFS-30 | 06-OCT-14

46
Q

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

A

15 kt

LIM-AFS-30 | 06-OCT-14

47
Q

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

Maximum crosswind for
auto land

GLS CAT I, ILS CAT II or ILS CAT III

A

30 kt

LIM-AFS-30 | 06-OCT-14

48
Q

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

Alert height

A

200 ft

LIM-AFS-30 | 07-OCT-18

49
Q

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.

A

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.

50
Q

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.

A

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.

51
Q

Auxiliary Power Unit / General

After ____ consecutive APU start attempts, the flight crew must wait ____ before a new start attempt.

A

3 … 60 min

LIM-APU | 10-APR-18

This 60 min period is to allow the APU starter to cool down.

52
Q

Auxiliary Power Unit / Operational Envelope

The APU can operate when the aircraft speed is below ____ .

(except in emergency configuration)

A

M 0.56

LIM-APU | 02-FEB-18

In the case of an all-engine failure, the APU can operate at any aircraft speed.

53
Q

Auxiliary Power Unit / Operational Envelope

Maximum pressure altitude for APU start

A

20,000 ft

LIM-APU | 02-FEB-18

54
Q

Auxiliary Power Unit / Operational Envelope

APU can supply electrical power, and bleed air, up to ____ ft pressure altitude.

A

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.

55
Q

Auxiliary Power Unit / Operational Envelope

Number of APU Generators that can operate in flight

A

1

LIM-APU | 02-FEB-18

56
Q

Communication / HF Communication

Use of HF communication during refuelling

A

During refuelling, HF communication should not be used

LIM-COM | 05-MAR-09

57
Q

Electrical / Electrical Outlets

Use of electrical outlets during take-off and landing

A

Do not use the electrical outlets during takeoff and landing.

LIM-ELEC | 31-MAR-06

58
Q

Engines / Thrust Setting/EGT Limits

Take-off and go-around
(all engines operative)

Time Limit and EGT Limit

A

Time Limit . . . 5 min

EGT Limit . . . 900 °C

LIM-ENG | 29-JUL-09

59
Q

Engines / Thrust Setting/EGT Limits

Take-off and go-around
(one engine inoperative)

Time Limit and EGT Limit

A

Time Limit . . . 10 min

EGT Limit . . . 900 °C

LIM-ENG | 29-JUL-09

60
Q

Engines / Thrust Setting/EGT Limits

Maximum Continuous Thrust (MCT)

EGT limit

A

850 °C

LIM-ENG | 29-JUL-09

61
Q

Engines / Thrust Setting/EGT Limits

Starting

On Ground and In Flight EGT limit

A

On Ground . . . 700 °C

In Flight . . . 850 °C

LIM-ENG | 29-JUL-09

62
Q

Engines / Oil

Minimum starting temperature

A

-40 °C

LIM-ENG | 07-JUL-20

63
Q

Engines / Oil

Minimum temperature prior to take-off

A

40 °C

LIM-ENG | 07-JUL-20

64
Q

Engines / Oil

Minimum quantity with
OAT < 0 °C

Flight Time below 14 h and at or above 14 h

A

13 qts minimum, or
6 qts + 0.5 qt/h for flight time at or above 14 h

LIM-ENG | 07-JUL-20

65
Q

Engines / Oil

Minimum quantity with
OAT ≥ 0 °C

Flight Time below 8 h and at or above 8 h

A

10 qts minimum, or
6 qts + 0.5 qt/h for flight time at or above 8 h

LIM-ENG | 07-JUL-20

66
Q

Engines / Starter

Maximum continuous starter operation

Multiple cycles and one cycle

A

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

67
Q

Engines / Starter

Wait ____ after the last cycle to allow the starter to cool

A

30 min

LIM-ENG | 05-JAN-21

68
Q

Engines / Starter

No running engagement of the starter when the ____ is above ____ .

On Ground and In Flight

A

On Ground . . . N3 … 10 %

In Flight . . . N3 … 30 %

LIM-ENG | 05-JAN-21

69
Q

Engines / Reverse Thrust

Maximum reverse should not be used below ____ kt.

A

70 kt

LIM-ENG | 10-SEP-07

Idle reverse is allowed down to aircraft stop.

70
Q

Engines / Reduced Thrust Takeoff

Reduced thrust take-off on contaminated runways

A

Takeoff at reduced thrust is not allowed on contaminated runways

LIM-ENG | 19-JAN-15

71
Q

Engines / Reduced Thrust Takeoff

FLEX temperature limits

Maximum and Minimum FLEX rating

A

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

72
Q

Fuel / Fuel Temperature

JET A fuel

Minimum fuel temperature

A

-40 °C

LIM-FUEL | 10-JAN-18

73
Q

Fuel / Fuel Temperature

JET A1 fuel

Minimum fuel temperature

A

-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.

74
Q

Fuel / Maximum Allowed Wing Fuel Imbalance

Feed Tanks 1 / Feed Tanks 4

Maximum allowed wing imbalance at take-off, in flight, and landing

A

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.

75
Q

Fuel / Maximum Allowed Wing Fuel Imbalance

Feed Tanks 2 / Feed Tanks 3

Maximum allowed wing imbalance at take-off, in flight, and landing

A

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.

76
Q

Fuel / Maximum Allowed Wing Fuel Imbalance

Left Inner Tank / Right Inner Tank

Maximum allowed wing imbalance at take-off, in flight, and landing

A

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.

77
Q

Fuel / Maximum Allowed Wing Fuel Imbalance

Left Mid Tank / Right Mid Tank

Maximum allowed wing imbalance at take-off, in flight, and landing

A

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.

78
Q

Fuel / Maximum Allowed Wing Fuel Imbalance

Left Outer Tank / Right Outer Tank

Maximum allowed wing imbalance at take-off, in flight, and landing

A

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.

79
Q

Landing Gear / Brake Temperature

Maximum brake temperature for take-off

A

300 °C

LIM-LG | 31-MAR-21

80
Q

Landing Gear / Maximum Altitude with the Landing Gear Extended

Maximum altitude at which the landing gear can be extended

A

21,000 ft

LIM-LG | 31-MAR-21

81
Q

Landing Gear / Taxi with Deflated Tires

Maximum taxi speed

A

3 kt

LIM-LG | 07-NOV-16

82
Q

Landing Gear / Taxi with Deflated Tires

Up to ____ tires can be deflated

A

9

LIM-LG | 07-NOV-16

83
Q

Landing Gear / Taxi with Deflated Tires

Maximum deflated tires per landing gear

Nose Landing Gear

A

1

LIM-LG | 07-NOV-16

84
Q

Landing Gear / Taxi with Deflated Tires

Maximum deflated tires per landing gear

Body Landing Gear (BLG)

A

2

LIM-LG | 07-NOV-16

Two deflated tires per BLG provided they are not on the same axle.

85
Q

Landing Gear / Taxi with Deflated Tires

Maximum deflated tires per landing gear

Wing Landing Gear (WLG)

A

2

LIM-LG | 07-NOV-16

Two deflated tires per WLG provided they are not on the same axle.

86
Q

Landing Gear / Taxi with Abnormal Wing or Body Landing Gear

Maximum taxi speed

A

5 kt

LIM-LG | 30-MAR-21

87
Q

Landing Gear / Taxi with Abnormal Wing or Body Landing Gear

Maximum NWS angle

A

50 °

LIM-LG | 30-MAR-21

88
Q

Landing Gear / Taxi with Abnormal Wing or Body Landing Gear

Maximum crosswind component for taxi

Wing Landing Gear (WLG) and Body Landing Gear (BLG

A

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.

89
Q

Navigation / On-board Airport Navigation System (OANS)

Use during take-off

PF display

A

Not authorized on PF display

LIM-NAV-10 | 23-DEC-20

90
Q

Navigation / On-board Airport Navigation System (OANS)

Use during roll-out after touchdown

PF and PM Display

A

PM Display . . . Authorized

PF Display . . . Authorized at taxi speed

LIM-NAV-10 | 23-DEC-20

91
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

LOSS OF BRAKING

A

“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)

92
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

EMER DESCENT

A

“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

93
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

STALL RECOVERY

A

“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.

94
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

STALL WARNING AT LIFTOFF

A

“STALL, TOGA 12.5 °”

PRO-ABN-MISC | 31-MAR-21

THRUST . . . . . . . . . . . . . . . . . . . . TOGA
PITCH ATTITUDE . . . . . . . . . . . . 12.5 °
BANK . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL

95
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

UNRELIABLE AIR SPEED INDICATION

A

“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

96
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

TAWS WARNING

A

“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.

97
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

TCAS CAUTION -
TRAFFIC ADVISORY

A

“TCAS, I HAVE CONTROL”

PRO-ABN-SURV | 31-MAR-21

Do not perform a maneuver based on a TA alone.

98
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

TCAS WARNING -
RESOLUTION ADVISORY

A

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

99
Q

Abnormal and Emergency Procedures / MEMORY ITEMS

WINDSHEAR WARNING -
REACTIVE WINDSHEAR

A

“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

Qantas (2 decks)

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