Memory Items Flashcards

Question

“RECOVERY” RECOVERY

Answer 1

Technique to return the aircraft to a normal state after a TCAS RA/UPSET/GPWS/STALL/WINDSHEAR ESCAPE AUTOPILOT ON FLCH Engage BUG UP Set Flaps Up Maneuvering speed CLEAN UP Retract Flaps on Schedule

Answer 2

◦ Disengage A/P ◦ Disconnect A/T If Req’d ◦ Smoothly adjust pitch to satisfy TA ◦ Fly planned lateral path

Answer 3

◦ Thrust - Maximum ◦ Disengage A/P ◦ Disconnect A/T If Req’d Flaps 20 ◦ Positive Rate: Gear Up ◦ Pitch Smoothly adjust to satisfy TA ◦ Fly planned lateral path

Answer 4

"FIREWALL" ◦ Disengage A/P ◦ Disconnect A/T ◦ Maximum Thrust aggressively ◦ Roll Wings level & ◦ Pitch up to 20 NU ◦ Pitch limit if necessary ◦ Retract Speedbrakes

Answer 5

“STALL” AP AT DISC ◦ Pitch nose down to exit stall ◦ May need to decrease Thrust ◦ Roll wings level ◦ Increase Thrust smoothly ◦ Check/Retract Speekbrakes ◦ Maintain existing Gear/Flaps ◦ If clean during T/O; Flaps 1

Answer 6

"WINDSHEAR TOGA" ◦ Disconnect A/P ◦ Push TOGA ◦ Disconnect A/T ◦ Maximum Thrust aggressively ◦ Rolls Wings level & Pitch to 15*NU ◦ Follow TO/GA ◦ Retract Speedbrakes

Answer 7

"WINDSHEAR TOGA" ◦ Push TOGA ◦ Verify TOGA ◦ Verify Thrust advances GA ◦ Monitor system performance ◦ Retract Speedbrakes

Answer 8

Disengage A/P and disconnect A/T Nose down as much as full – TRIM Reduce Thrust Roll for nose down Recover: Roll wings level at horizon Check airspeed and adjust thrust Establish pitch attitude

Answer 9

Disengage A/P and disconnect A/T Recover from stall if necessary Roll in shortest direction to wings level Recover: Adjust pitch – TRIM Adjust thrust and drag

Answer 10

N1-0 N2-0 High vibe

Answer 11

NORMAL SECONDARY DIRECT

Answer 12

PRIMARY SECONDARY ALTERNATE

Answer 13

2 MINS EMERGENCY STATIONS X2 30 SEC BRACE FOR LANDING X2 REMAIN SEATED X2

Answer 14

Deplane immediately and leave your personal belongings.

Answer 15

THRUST REDUCTION 1500 ACC HEIGHT 3000

Answer 16

THRUST REDUCTION 1000 ACC HEIGHT 1000

Answer 17

3’ OR COLDER 40% 5 SECONDS 60 MINS EVERY 50-55% with high vibes bring vines to 4 units or less

Answer 18

When the primary ice detection system is not being used or is inoperative, icing conditions may exist in flight when displayed TAT is less than or equal to 15°C. In flight, when displayed TAT is greater than 10°C but less than or equal to 15°C and visible moisture is present, engine and wing anti-ice must be selected ON except activation may be delayed until 2500 ft AGL for take-off.

Answer 19

Icing conditions also exist when the OAT on the ground and for take-off is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals).

Answer 20

Ground Operation in Icing Conditions During ground operations (including taxi-in and taxi-out) in icing conditions when the OAT is 3°C or below, the engine must be run up to a minimum of 40% N1 for at least 5 sec duration at intervals no greater than 60 min. If high engine vibration indications occur, a run-up to 50% N1 may be done. Engine anti-ice must be selected ON during all ground operations when icing conditions exist or are anticipated, except when the temperature is below -40°C OAT. Do not use engine anti-ice if OAT (on the ground) exceeds 10°C.

Answer 21

LNAV/HDG ALTITUDE DRILL?

Answer 22

• activation of the master caution system • system failure(s) • unusual noise or vibration • tire failure • abnormally slow acceleration • take-off configuration warning • fire or fire warning • engine failure • predictive windshear warning • the airplane is unsafe or unable to

Answer 23

• fire or fire warning • engine failure • predictive windshear warning • the airplane is unsafe or unable to fly

Answer 24

When both of the following exist, do an engine run-up to minimize ice build-up: • OAT is 3°C or below • visible moisture present (fog with visibility of one statute mile [1600 m] or less, rain, snow, sleet, ice crystals, and so on) Run-up to a minimum of 40% N1 for at least 5 sec duration at intervals no greater than 60 min. If high engine vibration indications occur, a run-up to 50% N1 may be done. If take-off is not completed within 120 min total taxi time, manually de-ice the engines before take-off

Answer 25

CAUTION: Avoid prolonged operation in moderate to severe icing conditions. If moderate to severe icing conditions are encountered: Note: Operation in icing conditions may result in engine vibration indications above the normal operating range during ice shedding. During flight in moderate to severe icing conditions for prolonged periods with N1 settings at or below 70%, or when fan icing is suspected due to high engine vibration, the fan blades must be cleared of any ice. Do the following procedure every 15 min on both engines, one engine at a time: Reduce thrust toward idle then increase to a minimum of 70% N1 for 10 to 30 sec.

Memory Items Flashcards

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