Lim Flashcards
1
Q
Autopilot minimum Engagment Height
A
400 ft
2
Q
Minimum Use Height (MUH) Autopilot
Cruise and Descent
A
1000 ft
3
Q
Minimum Use Height (MUH)
Approach
A
50ft
4
Q
Maximum differential pressure
A
8.4 psi
5
Q
Maximum differential negative pressure
A
-0.5 psi
6
Q
Maximum differential overpressure
A
8.8psi
7
Q
Maximum differential pressure Take-off and Landing
A
0.2 psi
8
Q
Engine Starter Limits
(GROUND and IN FLIGHT)
A
1) GROUND START- (90s 10s) (90s 10s)
(90s 5min) (90s 5min) (90s 5min)
2) IN FLIGHT START- (120s 10s)
(120s 10s) (120s 5min) (120s 5min) (120s 5min)
9
Q
Engine Starter
DRY MOTORING DUTY CYCLE LIMITS
A
(90s 5min) (30s 5 min) (30s 5min) (30s 5min) (30s 5min) (30s 5min)
After 5 sequential motoring 15min
10
Q
ENGINE
MAX GROUND START ITT
A
740 C
11
Q
ENGINE
MAX IN-FLIGHT START ITT
A
875 C
12
Q
ENGINE
MAX CONTINUOUS ITT
A
960 C
13
Q
ENG MAX OIL TEMPERATURE
A
155 C
14
Q
Max Cabin Diff. Press up to 37000 ft
A
7.8 psi
15
Q
Max Cabin Diff. Pressure above 37000 ft
A
8.4 psi
16
Q
Max Tire Speed
A
195 KTS
17
Q
APU ALTITUDE START LIMIT
A
30000 ft
18
Q
APU ELECTRICAL GEN MAX ALTITUDE LIMIT
A
33000 ft
19
Q
APU BLEED MAX OPERATIONAL ALTITUDE
A
15000 ft
20
Q
APU MAX ALTITUDE ENGINE START
A
21000ft
21
Q
APU MAX ROTOR SPEED
A
108%
22
Q
APU EGT START LIMIT
A
1032 C
23
Q
APU EGT CONTINUOUS LIMIT
A
717 C
24
Q
ENG MIN OIL PRESSURE
A
25psi (During starts with oil temperature below -22C the minimum oil pressure is 5 psi, time limited to 2 min.)
25
VMO below 8000ft
300KT
26
10000ft
320KTS
27
Mmo
0.82 mach
28
Flaps 1
230 Kts
29
Flaps 2
215 KTS
30
FLAPS 3
200 KTS
31
FLAP 4
180KTS
32
FLAP 5
180 KTS
33
FLAP FULL
165 KTS
34
FLAPS UP LOAD FACTOR LIMIT
-1.0 g 2.5g
35
FLAPS DOWN LOAD FACTOR LIMIT
0.0 g / 2.0 g
36
Max Operating Altitude
41000 ft
37
VLO EXTENSION
265 KTS
38
VLE
265 KTS
39
VLO Retraction
235KTS
40
Maximum Fuel (both Wings)
13192 kg
41
Unusable Fuel (per wing tank )
46 kg
42
Maximum Flap Extended Altitude
20000 ft
43
MZFW (Maximum Zero Fuel Weight)
42500kg. EMB 195
40800kg. EMB 190
44
MLW (Maximum Landing Weight)
45000kg E195
43000kg E190
45
Max Speed Direct Vision Window
160 KIAS
46
Runway Limits
Runway
Slope from -2% to +2%
Surface PAVED
47
Windshield Wiper Speed Limitation
253 KIAS
48
ENG MAX N1 and N2 indication
100%
49
ENG Minimum N2
59.3%
50
Max Permitted Fuel Imbalance Tanks
360 kg
51
APU STARTER LIMITS (cooling period)
Cooling period after each starting attempt
(1st and 2nd) 60s OFF
(3rd attempt) 5 min OFF
52
MAX CONTAMINANT DEPTH TAKE-OFF
25.4mm
53
MRW (Max Ramp Weight)
50950 kg E195
50460 kg E190
54
MTOW (Max. Take-off Weight)
50790 kg EMB 195
50300 kg EMB 190
55
Temperature Limitation ANTI-ICE System
NO TEMPERATURE LIMITATION FOR ANTI-ICE SYSTEM
56
ON GROUND
The TO DATASET MENU ON MCDU must be set to ENG when?
(ICE AND RAIN PROTECTION)
1) OAT is within 5-10 C. ( 5 compreso )
2)If there is any possibility of encountering visible moisture up to 1700ft AFE
3)When operating on ramp,taxiways,or runways where surface snow, ice, standing water, or slush may be ingested by the engine, nacelles, or engine sensor probes
57
ON GROUND
The TO DATASET MENU on the MCDU must be set to ALL when?
(ICE AND RAIN PROTECTION)
1)OAT is below 5 C
2) If there is any possibility of encountering visible moisture up to 1700 ft AFE
3) 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, nacelle, or engine sensor probes.
58
ICE AND RAIN PROTECTION
IN FLIGHT
The engine and wing anti-ice systems operate automatically, in case of ice encounter when the Ice Protection Mode Knob is in the AUTO position.
If either one or both ice detectors are failed, the Crew must set the Mode Selector to ON when icing conditions exists or are anticipated below 10 C TAT with visible moisture.
59
CROSSFEED OPERATION
CROSSFEED Selector Knob must be set OFF during take-off and landings
60
MINIMUM CREW
2 pilots
61
Minimum Equipments Required for CAT II APPROACHES
(Demonstrated to meet airworthiness requirements)
- 2 IRS (Inertial Reference Systems)
- 2 FDs (Flight Director Systems)
- 2 PFDs (Primary flight Displays)
- 1 Windshield Wiper
- 2 VOR/ILS NAV System
- 1 VHF/COMM System
- 1 RA (Radio Altimeter)
- 1 EGPWS (Ground Proximity Warning System)
- 2 ADS (Air Data Systems)
- 1 Autopilot System Channel
NOTE: Manual FD (Flight Director) CAT II ILS Approaches are prohibited.
62
CAT II APPROACH AND LANDINGS FLAPS LIMITATION
CAT II approach and landing must be performed with flaps 5.
63
FLIGHT CONTROLS CAT II LIMITATION
CAT II is prohibited with the SPOILER FAULT EICAS message displayed.
64
DEMONSTRATED WIND COMPONENTS CAT II
Headwind 37 KTS
Tailwind 15 KTS
Crosswind 16KTS
( values not to be considered limiting)
65
RVSM MINIMUM EQUIPMENT REQUIRED
During RVSM operation it is necessary that the following equipment and instruments be in proper operating condition.
- 2 RVSM Compliant ADs (Air Data Systems)
- 1 Autopilot with Altitude Hold Mode operative
- 1 Altitude Alerter
- 1 Transponder
66
Max take-off and landing tailwind component
15 KT
67
FUEL TEMPERATURE LIMIT
JET A / F35= -37 C
JET A1 / JP-8 / QAV-1 / F-34 / F-35= -44
68
Maximum latitude for stationary Alignment
78.25 gradi
69
MAX XWIND DRY
(Take-off)
38 KTS
70
MAX XWIND WET
(Take-off)
31 KT
71
MAX XWIND SNOW
(Take-off)
20 KT
72
MAX XWIND SLUSH/WET SNOW
(Take-off)
18 KTS
73
MAX XWIND WITH ICE
(Take-off)
12KT
74
MAX TAILWIND (take-off and landing)
15 KTS
75
AUTOLAND MAX TAILWIND & XWIND
15 KTS & 15KTS
76
Max Airport Altitude for the AUTOLAND
7340 ft
77
AIRPLANE SERVICE CEALING
41000ft
78
TAKE-OFF,LANDING AND GROUND OPERATION ENVELOPE LIMIT
-1000
79
MAX TEMP FL 410
-21.5
80
Lenght EMB 195
38.67
81
Height Embraer 195
10,55
82
Wingspan EMB 195
28,72
83
TAILSPAN EMBRAER 195
12.08 m
84
WHEELBASE width
5.94
85
AUTOLAND MAX HEADWIND
25 KTS
86
MAX TAKE-OFF AND LANDING TEMPERATURE AND GROUND TEMP
( 0 FT )
+50
87
MIN TAKE-OFF AND LANDING TEMPERATURE
( 0 ft )
-40 C
(In the event of a landing below -40,the airplane may not take-off without further maintenence inspection)
88
Operational envelope limit MAX TEMP
FROM 0 to 36000 (more or less)
ISA + 35
89
ANTI-ICE AUTOMATIC NORMAL OPERATION ENGAGEMENT HEIGHT
1700 FT AFE
90
ENGINE MAX TAKE-OFF AND GO AROUND ITT
983 C. (Above 5.5 C for 2 sec, 4.4 C for 5 sec, 3.6 C for 15 sec, 2.4 C 30 sec)
91
MAGNETIC CUT-OUT REGIONS (IRS)
North 73.125 < X < 82
West 80 < X < 130
North > 82
West/East 0 < x < 180
South 60 < x < 82
East 120 < x < 160
South > 82
East/West 0 < x < 180
92
Runway slope for AUTOLAND
Min -1%
Max +1%
93
Min BATT 2 APU temperature for engine start
-20 C
94
Minimum OIL temperature engine for cold Ops
-22 C and minimum oil pressure of 25 psi can be lowered to 5 psi
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