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Limitations > EMB145 > Flashcards

EMB145 Flashcards

1
Q

Operational ceiling

A

37.000 FT

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2
Q

FLAPS X-R BELOW 10.000FT

FLAPS 9

A

250 KIAS

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3
Q

FLAPS X-R BELOW 10.000 FT

FLAPS 18

A

200 KIAS

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4
Q

FLAPS X-R BELOW 10.000 FT

FLAPS 22

A

200 KIAS

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5
Q

FLAPS X-R BELOW 10.000 FT

FLAPS 45

A

160 KIAS

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6
Q

FLAPS X-R ABOVE 10.000 FT AND YD OFF

FLAPS 9

A

250 KIAS

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7
Q

FLAPS X-R ABOVE 10.000 FT AND YD OFF

FLAPS 18

A

200 KIAS

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8
Q

FLAPS X-R ABOVE 10.000 FT AND YD OFF

FLAPS 22

A

180 KIAS

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9
Q

FLAPS X-R ABOVE 10.000 FT AND YD OFF

FLAPS 45

A

145 KIAS

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10
Q

FLAPS LR

FLAPS 9

A

250 KIAS

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11
Q

FLAPS LR

FLAPS 22

A

200 KIAS

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12
Q

FLAPS LR

FLAPS 45

A

145 KIAS

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13
Q

MAXIMUM AFT CARGO WEIGHT LR/X-R

A

2646 LBS

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14
Q

MAX BATTERY TEMPERATURE

A

70 C

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15
Q

MAX LOAD APU GENERATOR BELOW

A

30.000 FT IS 400 AMPS

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16
Q

MAX LOAD APU GENERATOR ABOVE

A

30.000 FT IS 300 AMPS

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17
Q

MAX LOAD MAIN GENERATOR

A

400 AMPS

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18
Q

ENGINE COOL DOWN TIME

A

AT LEAST 1 MINUTE AT IDLE THRUST OR TAXI THRUST

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19
Q

TO INCREASE N2 ABOVE 83% THE ENGINE OIL TEMPERATURE MUST BE MINIMUM AT

( CAN INCREASE N2 ABOVE 83% IF )

A

40C

IF THE OIL TEMPERATURE IS BELOW 40C BUT THE ENGINES HAVE BEEN RUNNING FOR AT LEAST 8 MINUTES, IT CAN INCREASE N2 ABOVE 83%

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20
Q

ENGINE WARN UP TIME AFTER ENGINE IS SHUT DOWN LESS THAN 90 MINUTES

A

2 MINUTES

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21
Q

ENGINE WARN UP TIME AFTER ENGINE IS SHUT DOWN MORE THAN 90 MINUTES

A

4 MINUTES

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22
Q

MAX ALTITUDE TO EXTEND FLAPS

A

20.000 FT

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23
Q

MAX AIRSPEED AFTER TAKE OFF DURING CLIMB WITHOUT RE-TRIMMING

A

160 KIAS

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24
Q

MAX RECOMMENDED CROSS WIND WITH RUNWAY DRY

A

30 KIAS

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25
Q

MAX RECOMMENDED CROSSWIND WITH RUNWAY WET

A

30 KIAS

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26
Q

MAX USABLE FUEL QUANTITY EACH TANK -

LR

A

5717 ( 844.9 US GALLONS ) LBS EACH TANK

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27
Q

MAX USABLE FUEL QUANTITY EACH TANK -

X-RAYS

A

MAIN TANKS: 5717 LBS ( 844.9 US GALLONS )

VENTRAL: 1863 LBS ( 275.3 US GALLONS )

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28
Q

APU MAX OPERATING ALTITUDE

A

37.000 FT

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29
Q

POWER PLANT MAX VIBRATION

LP SPOOL

HP SPOLL

NOTES:

A

LP SPOOL = 1.8 IPS ( INCHES PER SECOND )

HP SPOOL = 1.1 IPS ( INCHES PER SECOND )

IT CAN BE IN THE AMBER RANGE BELOW 2.5 IPS FOR 5 MINUTES DURING T/O AND G/A PHASES AND 10 SECONDS FOR ALL OTHER FLIGHT PHASES

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30
Q

HOW DO YOU KNOW THAT THE BATTERIES ARE FULLY CHARGED?

A

THE BATTERIES DOES NOT CHARGE FROM THE GPU

THE APU MUST BE RUNNING FOR AT LEAST 30 MINUTES, DESELECT THE APU GENERATOR AND CHECK IF THE BATTERY VOLTAGE DOES NOT DROP BELOW 24 V

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31
Q

FUEL TEMPERATURE

MIN

MAX

A

MIN FUEL TEMPERATURE = - 54 C

MAX FUEL TEMPERATURE = + 52 C

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32
Q

MAX ALTITUDE TO START THE APU

A

30.000 FT

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33
Q

OIL TEMPERATURE

MIN

MAX

A

MIN OIL TEMPERATURE = 21 C IT CAN BE AS LOW AS -40C FOR LUBRIFICATION OIL ESPECIFIED BY…

MAX OIL TEMPERATURE = 126 C

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34
Q

OIL PRESSURE BELOW 88% N2

MIN

MAX

A

MIN = 34 PSI

MAX = 110 PSI

MAX CAN EXCEED DURING ENGINE START IF OIL TEMPERATURE IS BELOW 21C, ENGINE MUST REMAIN AT IDLE UNTILL OIL PRESSURE IS BELOW 110 PSI

MAX CAN EXCEED FOR UP TO 5 MINUTES
111 - 115 = 5 MINUTES
116 - 155 = 2 MINUTES

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35
Q

OIL PRESSURE ABOVE 88% N2
MIN
MAX

A 
MIN = 50 PSI 
MAX 110 PSI 
MIN CAN BE IN THE ABNORMAL RANGE FROM 34 - 50 PSI DURING T/O AND G/A PHASES
MAX CAN BE EXCEED UP TO 5 MINUTES
111-115 = 5 MINUTES
116 - 155 = 2 MINUTES
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36
Q

APU STARTER LIMITS
COOLING PERIOD BETWEEN EACH STARTING ATTEMPT
BETWEEN 3 CONSECUTIVE ATTEMPTS

A

1 MINUTE OFF

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37
Q

APU STARTER LIMITS
COOLING PERIOD BETWEEN EACH STARTING ATTEMPT
BETWEEN 2 SERIES OF 3 CONSECUTIVE ATTEMPTS

A

30 MINUTES OFF

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38
Q

MAX RAMP WEIGHT

LR

A

48722 LBS

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39
Q

ENGINE STARTER LIMITS
ON THE GROUND
STARTING OR DRY MOTORING

A

UP TO 5 MINUTES ON / 5 MINUTES OFF

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40
Q

ENGINE STARTER LIMITS
ON THE GROUND
FIRST TO FOURTH CYCLES

A

1 MINUTE ON / 1 MINUTE OFF

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41
Q

ENGINE STARTER LIMITS
ON THE GROUND
FOLLOWING CYCLES

A

1 MINUTE ON / 5 MINUTES OFF

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42
Q

ENGINE STARTER LIMITS IN FLIGHT

A

MAX CONTINUOUS OPERATION IS 5 MINUTES ON

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43
Q

ATTCS MUST BE OPERATIVE FOR

A

ALT T/O 1 MODE

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44
Q

MAX RECOMMENDED CROSSWIND ON RUNWAY COMPACT SNOW

A

25 KIAS

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45
Q

MAX RECOMMENDED CROSSWIND ON RUNWAY WITH STANDING WATER OR SLUSH

A

20 KIAS

46
Q

MAX RECOMMENDED CROSSWIND ON RUNWAY WITH ICE ( NO MELTING )

A

10 KIAS

47
Q

ITT MAX CONTINUOUS

A

901 C

48
Q

ICING CONDITIONS

MAX TEMPERATURE FOR ANTI ICE OPERATION

A

+10C

49
Q

T/O THRUST IS LIMITED TO

A

5 MINUTES

50
Q

ICING CONDITIONS

MINIMUM TEMPERATURE FOR MANUAL ANTI ICE OPERATION

A

-40 C

51
Q

ITT MAX FOR T/O MODES ( ALT T/O1 MODE AND T/O )

A

948 C

52
Q

ICING CONDITIONS

HOLDING CONFIGURATION

A 
AIRSPEED = MINIMUM 200 KIAS 
FLAPS = UP 
GEAR = UP
53
Q

ITT MAX FOR START

A

800 C

54
Q

POWER PLANT

N2 MAX

A

102.4%

55
Q

MAX T/O WEIGHT

LR

A

48501 LBS

56
Q

MAX TAIL WIND FOR LANDING AND T/O

A

10 KNOTS

57
Q

POWER PLANT

N1 MAX

A

100%

58
Q

AUTO PILOT CAT I LIMITATION

A

MINIMUM ALTITUDE COUPLED TO ILS = 200 FT

SINGLE ENGINE GO - AROUND IS PROHIBITED

59
Q

MAX ZERO FUEL WEIGHT

A

39462 LBS

60
Q

DIRECT VISION WINDOW

MAX SPEED TO REMOVE

A

140 KNOTS

61
Q

MAX OPERATING TEMPERATURE

A

ISA + 35 C

62
Q

WINDSHIELD WIPERS

MAX SPEED TO OPERATE

A

170 KIAS

63
Q

TAT LIMITATION IS

A

ABOVE 25.000 FT IS LIMITED TO ISA - 45 C

TAT = TOTAL AIR TEMPERATURE USED IN THE AIR 
SAT = SATURATED AIR TEMPERATURE USED ON THE GROUND
64
Q

MAX SPEED PENETRATION TURBULENT AIR AT OR BELOW 10.000 FT

A

200 KIAS

65
Q

MAX ALTITUDE CEILING

A

37.000 FT

66
Q

LAND GEAR RETRACTION ( VLO )

A

200 KIAS

67
Q

ICING CONDITIONS

SINGLE ENGINE OR SINGLE BLEED MAX ALTITUDE

A

15.000 FT

68
Q

OPERATIONAL ENVELOPE PRESSURE ALTITUDE FOR LR AND X-R

AIRPORT ELEVATIONS

A 
LR = -1.000 FT TO 8.000 FT 
X.R = -1.000 FT TO 10.000 FT
69
Q

WHEN OPERATING WITH APU BLEED SUPPLYING PACK 1 ( ENG 1 BLEED CLOSED ) AND ENG 2 BLEED SUPPLYING PACK 2 ( CROSSBLEED CLOSED ), MAX OPERATING ALTITUDE IS

A

37.000 FT

70
Q

MAX OPERATING ALTITUDE WHEN 1 BLEED OR 1 PACK IS CLOSED IS:

A

25.000 FT

71
Q

MAX SPEED TO PENETRATE TURBULENT AIR ABOVE 10.000 FT

A

250 KIAS OR M.63 WHICHEVER IS LOWER

72
Q

MEMORY ITENS

JAMMED AILERON

A

AILERON DISCONNECT PULL

73
Q

LANDING GEAR EXTENSION ( VLO )

A

250 KIAS

74
Q

MEMORY ITENS 18

AILERON / ROLL TRIM RUNWAY

A

QUICH DISCONNECT BUTTON PRESS AND HOLD

AILERON SYSTM 1 AND 2 OFF

75
Q

MEMORY ITENS 18

INADVERTENT SPOILER OPENING IN FLIGHT

A

SPEED BRAKE CLOSE

76
Q

UNUSABLE FUEL QUANTITY EACH TANK

LR

A

39 LBS

77
Q

MEMORY ITENS 18

RAPID CABIN DEPRESSURIZATION

A

CREW OXYGEN MASK —- DON
CREW COMMUNICATION—— STABLISH
EMERGENCY DESCENT —— AS REQUIRED

78
Q

MEMORY ITENS 18

EMERGENCY DESCENT

A 
CABIN CREW —— NOTIFY 
FASTEN BELTS —— ON
THRUST LEVER —— IDLE 
SPEED BRAKE —— OPEN
AIRSPEED ——- 250 KIAS 
L/G ——- DOWN 
ALTITUDE—— MEA OR 10.000 FT WHICHEVER IS HIGHER
79
Q

MEMORY ITENS 18

ABNORMAL ENGINE START

A

TO ABORT START:
ASSOCIATED THRUST LEVER —- IDLE
START/STOP SELECTOR —— STOP

80
Q

MEMORY ITENS 18

RUDDER/YAW TRIM RUNWAY

A

QUICK DISCONNECT BUTTON —- PRESS

RUDDER SYSTEMS 1 AND 2 OFF

81
Q

MEMORY ITENS 18

STEERING SYSTEM INOPERATIVE OR UNCOMMANDED SWERVING ON GROUND

A

STEERING HAND WHEEL —— DO NOT USE

STEERING DISENGAGEMENT BUTTON —— PRESS

82
Q

DURING POWER UP INITIALIZATION THE AIRCRAFT …

A

CAN NOT BE MOVED

83
Q

MAX DIFFERENTIAL PRESSURE

A

7.8 PSI

84
Q

LANDING GEAR EXTENDED

A

250 KIAS

85
Q

MANEUVERING SPEED VA

A

200 KIAS

86
Q

VMO/MMO

A

0 - 8.000 = LR: 250 KIAS X.R=300 KIAS

  1. 000 - 26.000 = 320 KIAS LR AND X.R
  2. 000 - 37.000 = LR: M.78 AND X.R:M.80
87
Q

MAX DIFFERENTIAL OVERPRESSURE

A

8.1 PSI

88
Q

MEMORY ITENS 18

JAMMED ELEVATOR

A

ELEVATOR DISCONNECT—— PULL

89
Q

MEMORY ITENS 18

PITCH TRIM RUNWAY

A

QUICK DISCONNECT BUTTON —- PRESS AND HOLD

90
Q

MEMORY ITENS 18

DUAL ENGINE FAILURE

A 
AIRSPEED —— MINIMUM 260 KIAS 
OXYGEN MASK ( IF REQUIRED )—- DON
91
Q

MAX DIFFERENTIAL NEGATIVE PRESSURE

A

-O.3 PSI

92
Q

MAX LANDING WEIGHT

LR

A

42.549 LBS

93
Q

OXYGEN REQUIRED FOR 2 CREW MEMBERS

A

1.100 PSI ( WILL PROVIDE 2 HOURS OF OXYGEN)

94
Q

MEMORY ITENS 18

ATTCS FAILURE

A

THRUST LEVER—— MAX

95
Q

OXYGEN REQUIRED FOR 2 CREW MEMBERS AND 1 OBSERVER

A

1.500 PSI ( PROVIDE 2 HOURS OF OXYGEN)

96
Q

MAX CARGO WEIGHT WITHOUT HORIZONTAL RESTRAINING NET

A

2.182 LBS

97
Q

AUTO PILOT CAT II LIMITATIONS

A

MINIMUM ALTITUDE COUPLED TO ILS = 50 FT

DECISION HEIGHT = 100 FT

98
Q

UNUSABLE FUEL WITH 1 ELETRIC FUEL PUMP INOPERATIVE

A

365 LBS

99
Q

MEMORY ITENS 18

APU FIRE

A

APU FUEL SHUT OFF VALVE —- CLOSE

100
Q

MEMORY ITENS 18

BAGGAGE COMPARTMENT SMOKE

A

EAICAS WARNING “ BAGG SMOKE “ —— VERIFY

BAGGAGE FIRE EXTINGUISHING BUTTON —— PRESS

101
Q

MINIMUM ALTITUDE TO ENGAGE THE AUTO PILOT AFTER T/O OR G/A

A

500 FT

102
Q

ALTITUDE ( ELEVATION 0 )

MAX DIFFERENCE ALLOWED BETWEEN CA AND FO ALTIMETERS

A

50 FT

103
Q

ALTITUDE ( ELEVATION 0 )

MAX DIFFERENCE ALLOWED BETWEEN CA AND FO ALTIMETERS TO STAND BY ALTIMETERS

A

150 FT

104
Q

MEMORY ITENS 18

SMOKE FIRE,FUMES/SMOKE EVACUATION

A

CREW OXYGEN MASK —- DON,100%
SMOKE GOGGLES —— DON
CREW COMMUNICATION—- STABLISH

105
Q

INTEGRATED STAND BY INSTRUMENT SYSTEM
ISIS
MAX DURATION ON BATTERY POWER

A

40 MINUTES

106
Q

MEMORY ITENS 18

BATTERY OVERTEMPERATURE

A

ASSOCIATED BATTERY —- OFF

107
Q

MEMORY ITENS 18

WINDSHEAR PREVENTION / RECOVERY

A

THRUST LEVER —- MAX

GO AROUND BUTTON —- PRESS

108
Q

INTEGRATED STAND-BY INSTRUMENT SYSTEM
ISIS
MAX DURATION ON BATTERY POWER IS …. AND CAN BE EXTENDED TO….

A

MAX BATTERY POWER 40 MINUTES

CAN BE EXTENDED TO 45 MINUTES IF PITOT 3 SENSOR HEATING BUTTON IS TURNED OFF WHEN NOT OPERATING IN ICING CONDITIONS

109
Q

CAT II RESTRICTIONS

7

A 
MAX TAIL WIND = 1O KTS 
MAX HEADWIND= 25 KYS
MAX CROSSWIND = 10 KTS
MINIMUM RVR = 1.200 
AP = ENGAGED 
FD = COUPLED TO CAPTAIN SIDE 
SINGLE ENGINE APPROACH = PROHIBITED
110
Q

MEMORY ITENS 18

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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