EMB145 Flashcards
(110 cards)
1
Q
Operational ceiling
A
37.000 FT
2
Q
FLAPS X-R BELOW 10.000FT
FLAPS 9
A
250 KIAS
3
Q
FLAPS X-R BELOW 10.000 FT
FLAPS 18
A
200 KIAS
4
Q
FLAPS X-R BELOW 10.000 FT
FLAPS 22
A
200 KIAS
5
Q
FLAPS X-R BELOW 10.000 FT
FLAPS 45
A
160 KIAS
6
Q
FLAPS X-R ABOVE 10.000 FT AND YD OFF
FLAPS 9
A
250 KIAS
7
Q
FLAPS X-R ABOVE 10.000 FT AND YD OFF
FLAPS 18
A
200 KIAS
8
Q
FLAPS X-R ABOVE 10.000 FT AND YD OFF
FLAPS 22
A
180 KIAS
9
Q
FLAPS X-R ABOVE 10.000 FT AND YD OFF
FLAPS 45
A
145 KIAS
10
Q
FLAPS LR
FLAPS 9
A
250 KIAS
11
Q
FLAPS LR
FLAPS 22
A
200 KIAS
12
Q
FLAPS LR
FLAPS 45
A
145 KIAS
13
Q
MAXIMUM AFT CARGO WEIGHT LR/X-R
A
2646 LBS
14
Q
MAX BATTERY TEMPERATURE
A
70 C
15
Q
MAX LOAD APU GENERATOR BELOW
A
30.000 FT IS 400 AMPS
16
Q
MAX LOAD APU GENERATOR ABOVE
A
30.000 FT IS 300 AMPS
17
Q
MAX LOAD MAIN GENERATOR
A
400 AMPS
18
Q
ENGINE COOL DOWN TIME
A
AT LEAST 1 MINUTE AT IDLE THRUST OR TAXI THRUST
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%
20
Q
ENGINE WARN UP TIME AFTER ENGINE IS SHUT DOWN LESS THAN 90 MINUTES
A
2 MINUTES
21
Q
ENGINE WARN UP TIME AFTER ENGINE IS SHUT DOWN MORE THAN 90 MINUTES
A
4 MINUTES
22
Q
MAX ALTITUDE TO EXTEND FLAPS
A
20.000 FT
23
Q
MAX AIRSPEED AFTER TAKE OFF DURING CLIMB WITHOUT RE-TRIMMING
A
160 KIAS
24
Q
MAX RECOMMENDED CROSS WIND WITH RUNWAY DRY
A
30 KIAS
25
MAX RECOMMENDED CROSSWIND WITH RUNWAY WET
30 KIAS
26
MAX USABLE FUEL QUANTITY EACH TANK -
LR
5717 ( 844.9 US GALLONS ) LBS EACH TANK
27
MAX USABLE FUEL QUANTITY EACH TANK -
X-RAYS
MAIN TANKS: 5717 LBS ( 844.9 US GALLONS )
| VENTRAL: 1863 LBS ( 275.3 US GALLONS )
28
APU MAX OPERATING ALTITUDE
37.000 FT
29
POWER PLANT MAX VIBRATION
LP SPOOL
HP SPOLL
NOTES:
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
30
HOW DO YOU KNOW THAT THE BATTERIES ARE FULLY CHARGED?
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
31
FUEL TEMPERATURE
MIN
MAX
MIN FUEL TEMPERATURE = - 54 C
MAX FUEL TEMPERATURE = + 52 C
32
MAX ALTITUDE TO START THE APU
30.000 FT
33
OIL TEMPERATURE
MIN
MAX
MIN OIL TEMPERATURE = 21 C IT CAN BE AS LOW AS -40C FOR LUBRIFICATION OIL ESPECIFIED BY...
MAX OIL TEMPERATURE = 126 C
34
OIL PRESSURE BELOW 88% N2
MIN
MAX
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
35
OIL PRESSURE ABOVE 88% N2
MIN
MAX
```
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
```
36
APU STARTER LIMITS
COOLING PERIOD BETWEEN EACH STARTING ATTEMPT
BETWEEN 3 CONSECUTIVE ATTEMPTS
1 MINUTE OFF
37
APU STARTER LIMITS
COOLING PERIOD BETWEEN EACH STARTING ATTEMPT
BETWEEN 2 SERIES OF 3 CONSECUTIVE ATTEMPTS
30 MINUTES OFF
38
MAX RAMP WEIGHT
LR
48722 LBS
39
ENGINE STARTER LIMITS
ON THE GROUND
STARTING OR DRY MOTORING
UP TO 5 MINUTES ON / 5 MINUTES OFF
40
ENGINE STARTER LIMITS
ON THE GROUND
FIRST TO FOURTH CYCLES
1 MINUTE ON / 1 MINUTE OFF
41
ENGINE STARTER LIMITS
ON THE GROUND
FOLLOWING CYCLES
1 MINUTE ON / 5 MINUTES OFF
42
ENGINE STARTER LIMITS IN FLIGHT
MAX CONTINUOUS OPERATION IS 5 MINUTES ON
43
ATTCS MUST BE OPERATIVE FOR
ALT T/O 1 MODE
44
MAX RECOMMENDED CROSSWIND ON RUNWAY COMPACT SNOW
25 KIAS
45
MAX RECOMMENDED CROSSWIND ON RUNWAY WITH STANDING WATER OR SLUSH
20 KIAS
46
MAX RECOMMENDED CROSSWIND ON RUNWAY WITH ICE ( NO MELTING )
10 KIAS
47
ITT MAX CONTINUOUS
901 C
48
ICING CONDITIONS
| MAX TEMPERATURE FOR ANTI ICE OPERATION
+10C
49
T/O THRUST IS LIMITED TO
5 MINUTES
50
ICING CONDITIONS
| MINIMUM TEMPERATURE FOR MANUAL ANTI ICE OPERATION
-40 C
51
ITT MAX FOR T/O MODES ( ALT T/O1 MODE AND T/O )
948 C
52
ICING CONDITIONS
| HOLDING CONFIGURATION
```
AIRSPEED = MINIMUM 200 KIAS
FLAPS = UP
GEAR = UP
```
53
ITT MAX FOR START
800 C
54
POWER PLANT
| N2 MAX
102.4%
55
MAX T/O WEIGHT
LR
48501 LBS
56
MAX TAIL WIND FOR LANDING AND T/O
10 KNOTS
57
POWER PLANT
| N1 MAX
100%
58
AUTO PILOT CAT I LIMITATION
MINIMUM ALTITUDE COUPLED TO ILS = 200 FT
| SINGLE ENGINE GO - AROUND IS PROHIBITED
59
MAX ZERO FUEL WEIGHT
39462 LBS
60
DIRECT VISION WINDOW
| MAX SPEED TO REMOVE
140 KNOTS
61
MAX OPERATING TEMPERATURE
ISA + 35 C
62
WINDSHIELD WIPERS
| MAX SPEED TO OPERATE
170 KIAS
63
TAT LIMITATION IS
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
MAX SPEED PENETRATION TURBULENT AIR AT OR BELOW 10.000 FT
200 KIAS
65
MAX ALTITUDE CEILING
37.000 FT
66
LAND GEAR RETRACTION ( VLO )
200 KIAS
67
ICING CONDITIONS
| SINGLE ENGINE OR SINGLE BLEED MAX ALTITUDE
15.000 FT
68
OPERATIONAL ENVELOPE PRESSURE ALTITUDE FOR LR AND X-R
| AIRPORT ELEVATIONS
```
LR = -1.000 FT TO 8.000 FT
X.R = -1.000 FT TO 10.000 FT
```
69
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
37.000 FT
70
MAX OPERATING ALTITUDE WHEN 1 BLEED OR 1 PACK IS CLOSED IS:
25.000 FT
71
MAX SPEED TO PENETRATE TURBULENT AIR ABOVE 10.000 FT
250 KIAS OR M.63 WHICHEVER IS LOWER
72
MEMORY ITENS
| JAMMED AILERON
AILERON DISCONNECT PULL
73
LANDING GEAR EXTENSION ( VLO )
250 KIAS
74
MEMORY ITENS 18
| AILERON / ROLL TRIM RUNWAY
QUICH DISCONNECT BUTTON PRESS AND HOLD
| AILERON SYSTM 1 AND 2 OFF
75
MEMORY ITENS 18
| INADVERTENT SPOILER OPENING IN FLIGHT
SPEED BRAKE CLOSE
76
UNUSABLE FUEL QUANTITY EACH TANK
| LR
39 LBS
77
MEMORY ITENS 18
| RAPID CABIN DEPRESSURIZATION
CREW OXYGEN MASK —- DON
CREW COMMUNICATION—— STABLISH
EMERGENCY DESCENT —— AS REQUIRED
78
MEMORY ITENS 18
| EMERGENCY DESCENT
```
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
MEMORY ITENS 18
| ABNORMAL ENGINE START
TO ABORT START:
ASSOCIATED THRUST LEVER —- IDLE
START/STOP SELECTOR —— STOP
80
MEMORY ITENS 18
| RUDDER/YAW TRIM RUNWAY
QUICK DISCONNECT BUTTON —- PRESS
| RUDDER SYSTEMS 1 AND 2 OFF
81
MEMORY ITENS 18
| STEERING SYSTEM INOPERATIVE OR UNCOMMANDED SWERVING ON GROUND
STEERING HAND WHEEL —— DO NOT USE
| STEERING DISENGAGEMENT BUTTON —— PRESS
82
DURING POWER UP INITIALIZATION THE AIRCRAFT ...
CAN NOT BE MOVED
83
MAX DIFFERENTIAL PRESSURE
7.8 PSI
84
LANDING GEAR EXTENDED
250 KIAS
85
MANEUVERING SPEED VA
200 KIAS
86
VMO/MMO
0 - 8.000 = LR: 250 KIAS X.R=300 KIAS
10. 000 - 26.000 = 320 KIAS LR AND X.R
26. 000 - 37.000 = LR: M.78 AND X.R:M.80
87
MAX DIFFERENTIAL OVERPRESSURE
8.1 PSI
88
MEMORY ITENS 18
| JAMMED ELEVATOR
ELEVATOR DISCONNECT—— PULL
89
MEMORY ITENS 18
| PITCH TRIM RUNWAY
QUICK DISCONNECT BUTTON —- PRESS AND HOLD
90
MEMORY ITENS 18
| DUAL ENGINE FAILURE
```
AIRSPEED —— MINIMUM 260 KIAS
OXYGEN MASK ( IF REQUIRED )—- DON
```
91
MAX DIFFERENTIAL NEGATIVE PRESSURE
-O.3 PSI
92
MAX LANDING WEIGHT
| LR
42.549 LBS
93
OXYGEN REQUIRED FOR 2 CREW MEMBERS
1.100 PSI ( WILL PROVIDE 2 HOURS OF OXYGEN)
94
MEMORY ITENS 18
| ATTCS FAILURE
THRUST LEVER—— MAX
95
OXYGEN REQUIRED FOR 2 CREW MEMBERS AND 1 OBSERVER
1.500 PSI ( PROVIDE 2 HOURS OF OXYGEN)
96
MAX CARGO WEIGHT WITHOUT HORIZONTAL RESTRAINING NET
2.182 LBS
97
AUTO PILOT CAT II LIMITATIONS
MINIMUM ALTITUDE COUPLED TO ILS = 50 FT
| DECISION HEIGHT = 100 FT
98
UNUSABLE FUEL WITH 1 ELETRIC FUEL PUMP INOPERATIVE
365 LBS
99
MEMORY ITENS 18
| APU FIRE
APU FUEL SHUT OFF VALVE —- CLOSE
100
MEMORY ITENS 18
| BAGGAGE COMPARTMENT SMOKE
EAICAS WARNING “ BAGG SMOKE “ —— VERIFY
| BAGGAGE FIRE EXTINGUISHING BUTTON —— PRESS
101
MINIMUM ALTITUDE TO ENGAGE THE AUTO PILOT AFTER T/O OR G/A
500 FT
102
ALTITUDE ( ELEVATION 0 )
| MAX DIFFERENCE ALLOWED BETWEEN CA AND FO ALTIMETERS
50 FT
103
ALTITUDE ( ELEVATION 0 )
| MAX DIFFERENCE ALLOWED BETWEEN CA AND FO ALTIMETERS TO STAND BY ALTIMETERS
150 FT
104
MEMORY ITENS 18
| SMOKE FIRE,FUMES/SMOKE EVACUATION
CREW OXYGEN MASK —- DON,100%
SMOKE GOGGLES —— DON
CREW COMMUNICATION—- STABLISH
105
INTEGRATED STAND BY INSTRUMENT SYSTEM
ISIS
MAX DURATION ON BATTERY POWER
40 MINUTES
106
MEMORY ITENS 18
| BATTERY OVERTEMPERATURE
ASSOCIATED BATTERY —- OFF
107
MEMORY ITENS 18
| WINDSHEAR PREVENTION / RECOVERY
THRUST LEVER —- MAX
| GO AROUND BUTTON —- PRESS
108
INTEGRATED STAND-BY INSTRUMENT SYSTEM
ISIS
MAX DURATION ON BATTERY POWER IS .... AND CAN BE EXTENDED TO....
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
CAT II RESTRICTIONS
| 7
```
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
MEMORY ITENS 18
| ENGINE FIRE, SEVERE DAMAGE OR SEPARATION
ASSOCIATED THRUST LEVER —- IDLE
ASSOCIATED START / STOP SELECTOR ——. STOP
ASSOCIATED FIRE EXTINGUISHING HANDLE —— PULL ( DO NOT ROTATE )
