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Jetstar B787 Limitations Nov 2021 > Nov 2021 Limitations > Flashcards

Nov 2021 Limitations Flashcards

Repetition

1
Q

Maximum Takeoff and Landing Tailwind Component

A

15kts

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2
Q

HF radio

A 
# Do not operate HF radios when refueling. 
# Avoid weather radar operation in a hangar.
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3
Q

Maximum crosswind for takeoff and landing

A

Takeoff. 35kts

Landing. 33kts

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4
Q

Severe turbulent air penetration speed (in severe turbulence)

A

• 290 KIAS below 25,000 feet • 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet.

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5
Q

Maximum taxi weight

A

228 383kgs

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6
Q

Maximum Takeoff weight

A

227 930kgs

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7
Q

Maximum landing weight

A

172 365kgs

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8
Q

Maximum zero fuel weight

A

161 025kgs

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9
Q

Autopilot/Flight Director System

A 
# The autopilot must not be engaged below a min engage altitude of 200ft AGL after TO. 
# Autoland capability may only be used for operations into runways at or below 8400 feet airport field elevation. 
# Without LAND 2 or 3 annunciated, the AP must be disengaged below 100 feet AGL.
# With LAND 2 or LAND 3 annunciated and GS angles greater than 3.25 degrees, the AP must be disengaged below 100 feet AGL.
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10
Q

Low Visibility (HUD) Takeoff

A 
# Headwind 25 knots 
# Tailwind 15 knots 
# Crosswind 20 knots
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11
Q

Automatic Landing

A 
# Headwind 25 knots 
# Tailwind 15 knots 
# Crosswind 25 knots 
# The maximum glideslope angle is 3.25 degrees. 
# The minimum glideslope angle is 2.5 degrees.
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12
Q

FLCH on approach

A

Do not use FLCH on final approach below 1,000 feet AFE.

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13
Q

Minimum oil temperature for start

A

Oil temperature must be greater than - 40° C for engine start.

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14
Q

Reverse thrust

A 
# Intentional selection of reverse thrust in flight is prohibited. 
# Backing the airplane with use of reverse thrust is prohibited.
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15
Q

Control input

A

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.

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16
Q

[] CABIN ALTITUDE

A 
• EITHER CREW MEMBER
 ~ “OXYGEN MASKS ON”
• BOTH CREW MEMBERS
~ ESTABLISH COMMS
IS CABIN ALTITUDE IS CONTROLLABLE – YES or NO?
• IF CABIN ALTITUDE IS UNCONTROLLABLE
~ PM…PASS OXYGEN – ON
• PF
~ SET LOWER ALTITUDE on MCP and CLOSES THE THRUST LEVERS 
• PM
~ “PASSENGER OXYGEN SWITCH ON”
• PM
~ CABIN PA… ”ATTENTION CABIN CREW EMERGENCY DESCENT”
• PF
~ EXTEND SPEEDBRAKES and DESCEND as REQUIRED at REQUIRED SPEED
• PM
~ MONITOR PF ACTIONS
~ DECLARE EMERGENCY
~ REQUEST AREA QNH
~ SQK 7700
~ CHECK LSALT or MORA/MEA
~ TURN EXTERIOR LIGHTS ON
~ COMPLETE CAB ALT CHECKLIST
• PF
~ ADJUST LEVEL OFF ALTITUDE
• PM
~ “CABIN ALTITUDE NON NORMAL CHECKLIST”
• PF
~ ACCOMPLISH CABIN ALTITUDE CHECKLIST
17
Q

ABORTED ENGINE START

A

ON THE GROUND
• FUEL CONTROL switch (affected side)
~ OFF

18
Q

DUAL ENGINE FAIL/STALL

A 
BOTH ENGINES BELOW IDLE
• FUEL CONTROL switches (both)
~ CUTOFF then RUN (Cutoff for 1 second)
• RAM AIR TURBINE switch
~ PUSH and HOLD (for 1 second)
(set airspeed above 270kts)
19
Q

[]ENGINE AUTOSTART L, R

A

N THE AIR
• FUEL CONTROL switch (affected side)
~ CONFIRM… CUTOFF

20
Q

[] ENGINE LIMIT EXCEED or SURGE L, R

A 
• A/T ARM switch (affected side)
~ CONFIRM… OFF
• THRUST LEVER (affected side)
~ CONFIRM… RETARD until MESSAGE BLANKS or the THRUST 
LEVER is at IDLE
21
Q

ENGINE SVR DAMAGE/SEP L, R

A 
• A/T ARM switch (affected side)
v CONFIRM… OFF
• THRUST LEVER (affected side)
~ CONFIRM… IDLE
• FUEL CONTROL switch (affected side)
~ CONFIRM… CUTOFF
• ENGINE FIRE switch (affected side)
v CONFIRM… PULL
22
Q

[] FIRE ENGINE L, R

A 
• A/T ARM switch (affected side)
~ CONFIRM… OFF
• THRUST LEVER (affected side)
~ CONFIRM… IDLE
• FUEL CONTROL switch (affected side)
~ CONFIRM… CUTOFF
• ENGINE FIRE switch (affected side)
~ CONFIRM… PULL
• IF THE FIRE ENG MESSAGE stays SHOWN:
~ ENGINE FIRE switch (affected side)
> ROTATE TO STOP AND HOLD FOR 1 SECOND
• IF AFTER 30 SECONDS, THE FIRE ENG MESSAGE stays SHOWN:
~ ENGINE FIRE switch (affected side)
> ROTATE TO THE OTHER STOP AND HOLD FOR 1 SECOND
23
Q

STABILIZER

A

• STAB CUTOUT switches
~ CUTOUT
• DO NOT EXCEED CURRENT AIRSPEED

24
Q

[] AIRSPEED UNRELIABLE

A 
• AUTOPILOT DISCONNECT switch
~ PUSH
• A/T ARM switch (both)
~ OFF
• F/D switches (both)
~ OFF
• SET THE FOLLOWING GEAR UP,PITCH ATTITUDE and THRUST:
~ FLAPS EXTENDED 10° and 85% N1
~ FLAPS UP 4° and 70%
25
Q

SMOKE, FIRE or FUMES

A

• ALL PILOTS DON OXYGEN MASKS

26
Q

VOLCANIC ASH ENCOUNTER – ENGINE FLAMEOUT

A 
• PERFORM A DESCENDING 180° TURN
• FUEL CONTROL switches (both)
~ CUTOFF then RUN (Cutoff for 1 second)
• RAM AIR TURBINE switch
~ PUSH and HOLD (for 1 second)
27
Q

APPROACH TO STALL or STALL RECOVERY

A

• SMOOTHLY APPLY NOSE DOWN TO REDUCE ANGLE of ATTACK (Bank angle may be required to
reduce G loading, and THRUST to IDLE to assist with PITCH DOWN)
• ROLL WINGS LEVEL
• ADVANCE THRUST LEVERS ( If required)
• RETRACT SPEED BRAKES
• DURING LIFTOFF, if FLAPS are UP call “FLAPS 1”
• CHECK AIRSPEED, PITCH and THRUST
• RESUME NORMAL FLIGHT PATH
• RE-ENGAGE AUTOPILOT and AUTOTHRUST

28
Q

REJECTED TAKEOFF

A 
• PRIOR TO 80 KNOTS BE STOP MINDED
• ABOVE 80 KNOTS STOP for the following:
~ FIRE or FIRE WARNING
~ ENGINE FAILURE
~ WINDSHEAR
~ AIRCRAFT UNSAFE
• CAPTAIN ANNOUNCES “STOP”
• ONCE STOPPED:
~ PARK BRAKE SET
~ “ALL PASSENGERS REMAIN SEATED and AWAIT FURTHER INSTRUCTIONS”
~ REQUEST EMERGENCY SERVICES (if required), and ADVISE ATC of POSTION
~ CARRYOUT REQUIRED CHECKLISTS
~ EVACUATION REQUIRED
> CARRYOUT EVACUATION CHECKLISTS…
~ RETURN TO GATE
> CHECK AIRCRAFT SYSTEMS
> CHECK BRAKE TEMPS
> CHECK and ADVISE CABIN STATUS
> REQUEST ATC CLEARANCE
29
Q

EGPWS

A
  • AUTOPILOT DISCONNECT
  • AUTOTHROTTLES DISCONNECT
  • MAXIUMUM THRUST APPLY AGGRESSIVELY
  • ROLL WINGS LEVEL
  • PITCH UP 20°
  • SPEEDBRAKES RETRACT
30
Q

TCAS

A 
• CLEAN CONFIGURATION
~ AUTOPILOT DISCONNECT
~ AUTOTHROTTLE DISCONNECT
~ FLY THE BOX
~ MAINTAIN AIRSPEED
• LANDING CONFIGURATION
~ AUTOPILOT DISCONNECT
~ AUTOTHROTTLE DISCONNECT
~ MAXIUMUM THRUST APPLY AGGRESSIVELY
~ CALL “FLAPS 20”
~ FLY THE BOX
~ MAINTAIN AIRSPEED
~ POSITIVE RATE “GEAR UP”
31
Q

JET UPSET RECOVERY - Nose High

A 
• NOSE HIGH
~ AUTOPILOT DISCONNECT
~ AUTOTHROTTLE DISCONNECT
~ NOSE DOWN ELEVATOR
> REDUCED THRUST and BANK ANGLE maybe required to achieve NOSE DOWN
~ APPROACHING HORIZON
> ROLL WINGS LEVEL
> CHECK AIRSPEED, THRUST and PITCH
32
Q

JET UPSET RECOVERY - Nose Low

A 
• NOSE LOW
~ AUTOPILOT DISCONNECT
~ AUTOTHROTTLE DISCONNECT
~ ROLL WINGS LEVEL
~ NOSE UP ELEVATOR
~ CHECK AIRSPEED, THRUST, PITCH and DRAG as required
33
Q

WINDSHEAR

A 
• PRIOR TO V1 REJECT
• PREDICTIVE or REACTIVE WINDSHEAR 
~ SIMULTANEOUSLY 
> AUTOPILOT DISCONNECT
> TOGA switches PUSH
> MAXIUMUM THRUST APPLY AGGRESSIVLEY
> AUTOTHROTTLES DISCONNECT
~ WINGS ROLL LEVEL 
~ PITCH 15° UP
~ SPEEDBRAKES RETRACT
FLT DIR W/SHEAR GUIDANCE FOLLOW
34
Q

FIRE ENGINE TAILPIPE L, R

A 
• PM BEACON ON
• FUEL CONTROL switch (affected side)
~ CONFIRM… CUTOFF
• ENGINE FIRE switch (affected side)
~ VERIFY IN
• START SELECTOR (affected side)
~ START
• PM – ADVISE ATC and GROUND SERVICES

Jetstar B787 Limitations Nov 2021 (1 decks)

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