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Airbus Sim FFS #5 > Engine Failures > Flashcards

Engine Failures Flashcards

0
Q

When is an engine considered damaged?

A

High vibration prior to flame out

Loud noise or explosion

Repeated and uncontrollable engine stalls

Abnormal engine indications: n1 or n2 ~ 0%

DO not relight

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1
Q

Engine Failure At V1

A 
Announce "Engine Failure"
Fly the aircraft.....rudder
GEAR UP
TOGA ....or (FLEX until green dot speed)
PITCH  ...................12.5 degrees
Beta Target.............TRIM with rudder
Navigate.................LAND ASAP
Above 400 feet.......ECAM ACTIONS
EO ACC ALT............V/S....,push to level off
CLEAN up a/c.........F speed flaps 1 / S speed flaps 0
Green dot speed.....OPN CLB....
MCT..........................SET
FMGS....prepare and brief approach
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2
Q

What are the EO ACC ALT procedures?

A

Order “Stop ECAM” before EO ACC ALT
V/S knob………………………..PUSH
FMA
CLEAN UP the aircraft…….F=FLAPS 1, S=FLAPS 0
ALT SELECTOR KNOB……PULL at green dot
THR LEVERS………………….MCT
FMA

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3
Q

When is an engine considered secured?

A

ENG MASTER OFF….for an engine failure without damage

AGENT 1 DISCH …for an engine failure with damage

Fire extinguished or AGENT 2…DISCH for an engine fire

Do not exceed the MAX EO ACC ALT (LPC NG or RTOW charts)

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4
Q

What are the ECAM actions?

A

ECAM PROCEDURE

SYSTEM DISPLAY

STATUS. (Before reading status…NORMAL C/L & computer resets)

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5
Q

What is the APPROACH PREPARATION ?

A

ANNOUNCE “you have controls”

FMS……PREPARE

APPR BRIEFING….PERFORM. (Standard briefing +status+ QRH)
Consider overweight landing)

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6
Q

ENGINE FAILURE AT CRUISE?

A 
FLY the Aircraft
LAND ASAP
THRUST LEVERS......MCT
A/THR........................OFF ( in order to freeze MCT)
ECAM ACTIONS
Do not decelerate below green dot!
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7
Q

What is the standard strategy for Engine Out Descent?

A

Mach.78 or 300kt……….SET AND PULL

EO LRC CEILING ALT….SET AND PULL
(On PROG page: REC MAX = EO LRC Ceiling)

FMA

V/S -500FT/MIN…..SET AND PULL (when <500ft/min

A/THR…………………ON
FMA

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8
Q

ALL ENGINE FLAME OUT / ENG DUAL FAILURE - fuel remaining?

A 
LAND ASAP
EMER ELEC PWR......MAN ON
THR LEVERS..............IDLE
FAC 1..........................OFF then ON
ENG MODE SEL.........IGN

OPTIUM RELIGHT SPEED……300 knots (2nm/1000’ glide rate)
PITCH….(about - 3.5 degrees for 60T or 132K
ATC 1 only….Landing strategy
IF NO RELIGHT after 30 seconds…..ENG MASTERS…off 30s…on
CREW OXY…ON
APU…start if able below FL 250

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9
Q

DUAL HYD FAILURE: G SYS LO PR?

A

NO IMMEDIATE ACTIONS REQUIRES; however,

ECAM ACTIONS ASAP

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10
Q

DUAL HYD FAILURE: HYD G+Y SYS LO PR?

A

FLY the A/C: LOSS OF AP + ALTN LAW

Flaps are lost with GY failure

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11
Q

When does the RAT (RAM AIR TURBINE) automatically extend?

A

All engines fail

Loss of AC BUS 1 and AC BUS 2

With RAT extended, the fuel consumption increases by 1%.

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12
Q

What is the EMERGENCY EVACUATION?

A

Aircraft parking brake…………….STOP/ON
ATC (VHF1)……………………………NOTIFY
Cabin Crew……………………………ALERT
^P………CHECK 0, if not, MODE SEL on MAN, V/S CTL FULL UP
ENG MASTERS………………………OFF
FIRE PUSHBUTTONS (ALL)……..PUSH
AGENTS (ENG and APU)………….AS REQUIRED

EVAC……………………………………..initiate if required
CABIN CREW and PAX……………Notify

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13
Q

What are some causes of UNRELIABLE AIRSPEED indications?

A

Water (heavy rain)
Severe Icing
Loss of heating
Probes damaged or plastic not removed from covers

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14
Q

How can you display the a/c altitude if you don’t trust it and you have an unreliable airspeed indication?

A

GPS altitude is displayed on the DATa page (difsrip)

L3 button GPS Monitor

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15
Q

AUTOMATIC EXTENSION OF GROUND SPOILERS happens ?

A

Wheel speed >72 knots

Ground spoilers are armed

All thrust levers are retarded to IDLE

16
Q

AUTOMATIC BRAKING ACTIVATION ( MAX or RTOW mode) when?

A

AUTOBRAKING is commanded by the ground spoilers extension but they won’t happen if the RTO is initiated below 72 Knots.

17
Q

When should you REJECT the takeoff?

A

Below 100 knots: any ECAM WARNING/CAUTION

Between 100 knots and V1:
Fire warning or severe damage
Sudden loss of engine thrust
Aircraft will not fly safely
Any RED ECAM Warning
Any amber ECAM caution of the ENG system or F/CTL
18
Q

What are the RTO actions from the PF?

A 
CALL...................."STOP"
All thrust levers.....IDLE
Reverse thrust......MAX AVAILABLE
Aircraft stopped: 
REVERSE...............STOWED
PARKING BRAKE...APPLY
PA Call...................."Attention crew! At stations
Announce ..............ECAM ACTIONS
19
Q

What are the RTO actions from the PNF?

A 
Reverse............check/announce
Deceleration.....check/announce
Any audio..........cancel
ATC....................inform
EMERGENCY EVAC PROCEDURE.....locate
ECAM actions.........initiate
20
Q

What is the EMERGENCY EVAC preparation?

A

PF: Announce……….”STOP ECAM”

Announce…………….”emergency evacuation procedure

PNF: ECAM ACTIONS………STOP

EMER EVAC PROC…………..READ and DO

21
Q

What is the EMER EVAC DECISION ?

A

PA call……..”EVACUATE”

EMER EVAC COMMAND……ON

22
Q

What happens when you lose 2 Radio Altimeters (NAV 1+2 FAULT)?

A

No AUTO CALLOUT
The G/S mode and the APPR mode can’t be engaged
The LOC is available but the AP/FD must be monitored
The GS signal is properly received
The status will change to DIRECT LAW with the LG down.

23
Q

What is the approach prep for both RA failed (NAV RA 1+2 FAULT).

A

Plan for an ILS
Don’t engage ILS APPR

LOC armed or RAW data
Use Track-FPA (Bird)

CONFIG 3
GEAR not down warning is triggered from FLAP 3 position

APPROACH speed: Vref + 10
NO AUTO CALLOUT during the flare

24
Q

ELEC EMER CONFIG is powered by what?

A

When Aircraft is in flight (>100k) RAT extends automatically and powers the BLUE system which drives the EMER GEN.

ELEC EMER CONFIG is caused by a loss of all AC buses, loss of all engines, loss of all generators, or a combo of failures.

25
Q

How is a GO Around conducted?

A

THRUST levers……TOGO
ROTATION…….Pitch 15 degrees…or 12.5 SE and then follow SRS
ANNOUNCE…..”GO Around Flaps”. …raise one notch
FMA…announce
Gear up……after positive climb
Auto pilot….ON
@ LVR CLB….THRUST to CL Detent.
F speed….flaps 1
S speed….flaps 0
“After T/O Climb check list….down to the line

26
Q

Windshear procedures?

A

CALLOUT…… “Windshear / TOGA”
SET ………,,…….TOGA
SRS……………….follow commands
Config…………….don’t change

27
Q

EGPWS memory items

A 
"PULL UP TOGA"
Full back stick and maintain
Thrust levers to TOGA
Check speed brakes retracted
Wings level
28
Q

Windshear recovery technique?

A 
"Windshear TOGA"
Set TOGA
Follow SRS command bar
Don't change the configuration 
AP can be used if engaged
Recover smoothly to a normal climb
29
Q

Stall recovery

A

Nose down pitch control…..apply
Bank…..wings level

Out of stall….THRUST…increase smoothly
Speed brakes……check retracted
Flight path….recover smoothly

30
Q

TCAS alert?

A

Announce…“TCAS, I HAVE CONTROL”
ND….adjust range

RA alert
ANNOUNCE….”AP OFF”….”FD’s OFF

Clear of conflict
Announce "FD's ON"
Announce "manage speed or set speed"
NAV or HDG manage or select
AP.....ON
31
Q

RTO procedures

A

CALL……STOP
Thrust levers……IDLE
Reverse thrust….MAX Available

Reverse stowed after a/c is stopped
Parking brake set….apply

PA “ATTENTION CREW! AT STATIONS”
ECAM actions

32
Q

Emergency descent procedures?

A

ALT……turn and pull………………………PNF…..ENG MODE SEL…IGN
HDG….turn off airways and pull……..PNF……ATC……NOTIFY
SPEED….pull………………………………..PNF…..ATC XPDR…consider
FMA….read
Speed brake…..full…….. PNF….PAX OXY MASK…..man on
Second loop
ALT FL 100………set
HDG………………..set
SPD/MACH……..press or VMO if no damage suspected

33
Q

Unreliable speed indication/ADR check

A

AP/FD……………………OFF
A/THR……………………OFF
PITCH/ THRUST…….15 deg TOGA. (Below THRST RED ALT)
…….10 deg CLB…..(above THRST RED ALT)
FLAPS CONF 0,1,2,3……MAINTAIN current CONFIG
FLAPS FULL…………select Config 3 and maintain
Speed brakes………..check retracted
LG………………………..UP
@MSA…..LVL off to trouble shoot
GOUGE setting……8.5 / 58% N1

34
Q

Loss of braking

A 
REV...............................MAX
BRAKE PEDALS...........RELEASE
A/SKID & NWS STG.....OFF
BRAKE PEDALS............PRESS
MAX BRAKE PRess.......1000 psi

If still no braking……short and successive applications

Airbus Sim FFS #5 (1 decks)

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