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E-145 MEMORY ITEMS > Memory Items > Flashcards

Memory Items Flashcards

Memorize Memory Items (92 cards)

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1
Q

02 MASK DONNING PROCEDURE

A 
HEADSET (REMOVE)
OXYGEN MASK (DON)
SMOKE GOGGLES if smoke present (ON)
REGULATOR if smoke/fumes present (EMER)
AFTER SMOKE PURGED (MASK 100%)
HEADSET (ON)
HOT MIC (OFF)
MASK MIC audio panel (MASK OUT)
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2
Q

SMOKE FIRE OR FUMES

A

OXYGEN MASKS - (DON 100%)
SMOKE GOGGLES - (DON)
CREW COMMUNICATION - (ESTABLISH)

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3
Q

SMOKE EVACUATION

A

OXYGEN MASKS - (DON 100%)
SMOKE GOGGLES - (DON)
CREW COMMUNICATION - (ESTABLISH)

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4
Q

BAGGAGE SMOKE

A

FIRE EXTG BAGG BUTTON (IF INSTALLED) -

PUSH IN

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5
Q

EFB FIRE CONCERNS

A

FLIGHT ATTENDANT - (EMER CALL)
GLOVES - DON
EFB AND MOUNT - RELEASE FROM WINDOW
EFB AND MOUNT - PURGE FROM COCKPIT

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6
Q

AILERON RUNAWAY/ROLL TRIM RUNAWAY

A

QUICK DISCONNECT BUTTON - PRESS AND HOLD

AILERON SHUTOFF SYS 1 AND 2 - PUSH OUT

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7
Q

AIRPLANE OVERSPEED

A

AIRSPEED - MAX VMO/MMO

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8
Q

EMERGENCY DESCENT

A 
CABIN CREW - NOTIFY
FSTN BELTS - ON
THRUST LEVERS - IDLE
SPEED BRAKE - OPEN
AIRSPEED MAX - 250 KIAS
LANDING GEAR - DOWN
DESCENT - INITIATE
ALTITUDE - MEA OR 10,000 FT, WHICHEVER IS HIGHER
ATC - NOTIFY
IF UNABLE TO ESTABLISH COMMS - SQUAWK 7700
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9
Q

JAMMED AILERON

A

AILERON DISCONNECTION HANDLE - PRESS AND PULL

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10
Q

JAMMED ELEVATOR

A

ELEVATOR DISCONNECTION HANDLE - PRESS AND PULL

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11
Q

PITCH TRIM RUNAWAY

A

QUICK DISCONNECT BUTTON - PRESS AND HOLD

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12
Q

RAPID CABIN DEPRESSURIZATION

A

CREW OXYGEN MASKS - DON

CREW COMMUNICATION - ESTABLISH

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13
Q

IF EMERGENCY DESCENT IS NECESSARY:

A 
CABIN CREW - NOTIFY
FSTN BELTS - ON
THRUST LEVERS - IDLE
SPEED BRAKE - OPEN
AIRSPEED MAX - 250 KIAS
LANDING GEAR - DOWN
DESCENT - INITIATE
ALTITUDE - MEA OR 10,000 FT, WHICHEVER IS HIGHER
ATC - NOTIFY
IF UNABLE TO ESTABLISH COMMS - SQUAWK 7700
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14
Q

ABNORMAL ENGINE START – TO ABORT START

A

ASSOCIATED THRUST LEVER - IDLE

ASSOCIATED START/STOP SELECTOR - STOP

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15
Q

RUDDER/YAW TRIM RUNAWAY

A

QUICK DISCONNECT BUTTON - PRESS AND HOLD

RUDDER SHUTOFF SYS 1 AND 2 - PUSH OUT

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16
Q

APU FIRE

A

APU FUEL SHUTOFF VALVE - PUSH IN

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17
Q

BATTERY OVERTEMPERATURE

A

AFFECTED BATTERY - OFF

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18
Q

ATTCS FAILURE

A

THRUST LEVERS - MAX

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19
Q

DUAL ENGINE FAILURE

A

AIRSPEED - MIN 260 KIAS

OXYGEN MASK - AS REQUIRED

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20
Q

ENGINE FIRE, SEVERE DAMAGE, OR SEPARATION

A

ASSOCIATED THRUST LEVER - IDLE
ASSOCIATED START/STOP SELECTOR - STOP
ASSOCIATED FIRE EXTINGUISHING HANDLE - PULL (DO NOT ROTATE)

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21
Q

INADVERTENT SPOILER OPEN

A

SPEED BRAKE - CLOSE

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22
Q

STEERING SYSTEM INOPERATIVE OR
UNCOMMANDED SWERVING ON THE GROUND
– TAKEOFF OR LANDING

A

STEERING HANDWHEEL - DO NOT USE

STEERING DISENGAGEMENT BUTTON - PRESS

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23
Q

STABILIZED APPROACH CRITERIA – NOT GRADED

A

• From 1,000 feet
above the TDZE
FINAL LANDING CONFIGURATION SELECTED
ON GLIDE PATH WITH A SUSTAINED DESCENT RATE OF 1200 FPM OR
LESS
ON CORRECT LATERAL TRACK
ABOVE IDLE THRUST WITH AIRSPEED TRENDING TOWARDS CALCULATED
APPROACH SPEED PER SOP
• From 500 feet
above the TDZE
ABOVE IDLE THRUST AT CALCULATED APPROACH SPEED PER SOP (-5
KNOTS TO +10 KNOTS)
A minimum height for Vap not less than ___1,000___ feet above TDZE for approaches in IMC.
A minimum height for Vap not less than ___500_____ feet above TDZE for approaches in VMC.
If conditions are not met: A MISSED APPROACH MUST BE EXECUTED

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24
Q

MAXIMUM RAMP WEIGHT

A

XR - 53,351 LBS

LR - 50,044 LBS

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25
MAXIMUM TAKEOFF WEIGHT
XR - 53,131 LBS | LR - 49,823 LBS
26
MAXIMUM LANDING WEIGHT
XR 44,092 LBS | LR 43,651 LBS
27
MAXIMUM ZERO FUEL WEIGHT
XR 40,785 LBS | LR 40,564 LBS
28
MINIMUM TOTAL AIR TEMPERATURE IN CRUISE | FLIGHT ABOVE 25,000 FT
-45 °C
29
NO MAINTENANCE ACTION IS REQUIRED IF | MOMENTARY DEVIATIONS OCCUR DOWN TO
-50°C
30
VLO FOR RETRACTION
200 KIAS
31
VLO FOR EXTENSION
250 KIAS
32
VLE
250 KIAS
33
VA
200 KIAS
34
MAXIMUM FLAP EXTENSION SPEEDS (XR)
9 – 250 KIAS 18 –200 KIAS 22 –180 KIAS 45 –160 KIAS
35
MAXIMUM FLAP EXTENSION SPEEDS ABOVE | 10,000 FT AND Y/D DISENGAGED (XR Only)
9 - 250 KIAS 18 - 200 KIAS 22 - 180 KIAS 45 - 145 KIAS
36
MAXIMUM FLAP EXTENSION SPEEDS (LR)
9 – 250 KIAS 18 – 200 KIAS 22 – 200 KIAS 45 – (and momentarily) 145 (160 momentarily) KIAS
37
MAXIMUM ALTITUDE FOR FLAP EXTENSION
20,000 FT
38
MAXIMUM TAKEOFF/LANDING TAILWIND
10 KTS
39
MAXIMUM USABLE FUEL QUANTITY PER WING TANK
5,717 LBS
40
UNUSABLE FUEL QUANTITY PER WING TANK
39 LBS
41
MAXIMUM USABLE FUEL QUANTITY IN VENTRAL | TANK (XR)
1863 LBS
42
UNUSABLE FUEL QUANTITY IN VENTRAL TANK | XR
21 LBS
43
UNUSABLE FUEL QUANTITY WITH ANY | ASSOCIATED ELECTRIC PUMP INOPERATIVE
365 LBS
44
MAXIMUM PERMITTED IMBALANCE BETWEEN TANKS
800 LBS
45
MINIMUM FUEL TANK TEMPERATURE
-40 °C
46
MAXIMUM FUEL TANK TEMPERATURE
52 °C
47
APU MINIMUM TEMPERATURE
-54 °C
48
APU MAXIMUM ALTITUDE FOR START
30,000 FT
49
APU MAXIMUM OPERATIONAL ALTITUDE
37,000 FT
50
APU MAXIMUM ROTOR SPEED
108%
51
APU MAXIMUM ROTOR SPEED FOR AUTO | SHUTDOWN
104%
52
APU MAXIMUM EGT FOR START
884 °C
53
APU MAXIMUM EGT CONTINUOUS
680 °C
54
APU EGT MAY BE EXCEEDED UP TO
717 °C FOR 5 MINUTES
55
MINIMUM BATTERY TEMPERATURE FOR APU | START
-20 °C
56
APU STARTER LIMITS
BETWEEN THREE CONSECUTIVE ATTEMPTS - 1 MINUTE OFF | BETWEEN 2 SETS OF 3 CONSECUTIVE ATTEMPTS 30 MINUTES OFF
57
ENGINE MODEL
XR - AE3007A1E | LR - AE3007A1P
58
N1 MAXIMUM
100%
59
N2 MAXIMUM
XR - 105% | LR 102.4%
60
ITT MAXIMUM FOR START
800 °C
61
ITT MAXIMUM IN TAKEOFF MODES
XR - 970 °C FOR 5 MIN XR – TEMPERATURES BETWEEN ___971__°C & __992___°C ARE TIME LIMITED TO __90____ SECONDS LR - 948 °C FOR 5 MIN
62
ITT MAXIMUM CONTINUOUS
XR - 935 °C | LR - 901 °C
63
OIL PRESSURE BELOW 88% N2
MIN- 34 MAX- 110
64
OIL PRESSURE AT OR ABOVE 88% N2 (XR)
MIN- 48 MAX- 110
65
OIL PRESSURE AT OR ABOVE 88% N2 (LR)
MIN- 50 MAX- 110
66
MINIMUM OIL TEMPERATURE
21 °C
67
MAXIMUM OIL TEMPERATURE
126 °C
68
MAXIMUM VIBRATION
HP- 1.1 LP- 1.8
69
TAKEOFF THRUST MODES FOR TAKEOFF
XR (3 MODES) - E T/O, T/O, ALT T/O-1 | LR (2 MODES) - T/O, ALT T/O-1
70
ENGINE STARTER LIMITS – GROUND STARTING OR DRY MOTORING -OR THE FOLLOWING CYCLE LIMITS
UP TO 5 MINUTES ON, 5 MINUTES OFF
71
ENGINE STARTER LIMITS – GROUND | FIRST TO FOURTH CYCLES
1 MINUTE ON, 1 MINUTE OFF
72
ENGINE STARTER LIMITS – GROUND | FOLLOWING CYCLES
1 MINUTE ON, 5 MINUTES OFF
73
ENGINE STARTER LIMITS – IN FLIGHT | MAXIMUM CONTINOUS OPERATION TIME
5 MINUTES ON
74
ENGINE WARM UP – COLD ENGINE
4 MIN
75
ENGINE WARM UP – WARM ENGINE
2 MIN
76
ENGINE COOL DOWN
2 MIN
77
MAXIMUM TEMPERATURE FOR ANTI-ICING OPERATIONS
10 °C
78
MINIMUM TEMPERATURE FOR MANUAL ANTIICING OPERATION
-40 °C
79
HOLDING CONFIGURATION | (GEAR, FLAPS, SPEED
GEAR UP, FLAPS UP, MIN 200 KIAS
80
MAXIMUM AIRSPEED FOR WINDSHIELD WIPER | OPERATION
170 KIAS
81
MAXIMUM LOAD ON MAIN GENERATOR
400 A
82
MAXIMUM LOAD ON APU GENERATOR | UP TO FL300
400 A
83
MAXIMUM LOAD ON APU GENERATOR | ABOVE FL300
300A
84
MAXIMUM BATTERY TEMPERATURE
70 °C
85
MAXIMUM DIFFERENTIAL PRESSURE
7.8 PSI
86
MAXIMUM DIFFERENTIAL OVERPRESSURE
8.1 PSI
87
MAXIMUM DIFFERENTIAL NEGATIVE PRESSURE
-0.3 PSI
88
AUTOPILOT MINIMUM ENGAGEMENT HEIGHT | AFTER TAKEOFF
500 FT
89
AUTOPILOT MINIMUM DECISION ALTITUDE | DURING ILS APPROACH
200 FT
90
AUTOPILOT MINIMUM USE HEIGHT | XR
160 FT
91
AUTOPILOT MINIMUM USE HEIGHT | LR
200 FT
92
AUTOPILOT MALFUNCTION ALTITUDE LOSS
CRUISE 80 FT MANEUVER 40 FT ILS APPROACH 35 FT

E-145 MEMORY ITEMS (1 decks)

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