Limitations Flashcards

1
Q

Kinds of Operation

A

-Day and Night
-VFR
-IFR
-Icing
-CAT I & II
-RVSM
-Extended Overwater(When EOW Equipped)

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2
Q

ERJ-170 (STD) Max Weights

A

Taxi and Ramp:79.6
Takeoff(MTOW):79.3
Landing(MLW):72.3
Zero Fuel:65.2

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3
Q

ERJ170(LR) Max Weights

A

Taxi and Ramp:82.4
Takeoff(MTOW):82
Landing(MLW):72.3
Zero Fuel:65.2

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4
Q

ERJ175 Max Weights

A

Taxi and Ramp:85.8
Takeoff(MTOW):85.5
Landing(MLW):75
Zero Fuel:69.8

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5
Q

Max Headwind (CAT II Approach)

A

25 knots

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6
Q

Max Crosswind for Landing Vis < 4000 or 3/4

A

15 Knots

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7
Q

Maximum Takeoff and Landing Tailwind

A

10 Knots

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8
Q

Max Operating Altitude

A

41,000 ft

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9
Q

Max Altitude with Flaps/Slats Extended

A

20,000 ft

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10
Q

Max Takeoff and Landing Altitude

A

10,000 ft

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11
Q

Max and Minimum Static Air Temp(SAT) for Takeoff, Landing and Ground Start

A

Max:54 degrees Celsius
Min:-40 degrees Celsius

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12
Q

Max Takeoff Crosswind for RWYCC

A

6:35 Knots
5:30 Knots
4:20 Knots
3:15 Knots
2:12 Knots
1:8 Knots
0:Prohibited

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13
Q

Max Landing Crosswind for RWYCC

A

6:38 Knots
5:31 Knots
4:20 Knots
3:15 Knots
2:12 Knots
1:8 Knots
0:Prohibited

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14
Q

MMO (Maximum operating Mach number)

A

.82 Mach

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15
Q

Vmo (Maximum Operating Airspeed)

A

320 Knots

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16
Q

Turbulent Airspeed (Below 10k)

A

250 KIAS

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17
Q

Turbulent Airspeed (At or Above 10k)

A

270 KIAS or .76 Mach (Whichever is lower)

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18
Q

Tire Limit Ground Speed

A

195 Knots

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19
Q

Maximum airspeed for windshield wiper operation

A

250 KIAS

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20
Q

Max Airspeed to open direct vision window

21
Q

Vlo (Max gear extension/retraction speed)
Vle (Max gear extended speed)

22
Q

Vfe (Max Flap Operating Speeds)

A

KIAS
1:230
2:215
3:200
4:180
5:180
Full:165

23
Q

Approved Fuel

A

JET A & JET A1

24
Q

Fuel Density

A

6.77 LBS per Gallon

25
Minimum Fuel Tank Temperature
-37 Degrees Celsius
26
Maximum Fuel Imbalance
794 Lbs
27
Fuel Capacity
Max Usable:10,392lbs per tank Unusable Fuel:75lbs per tank
28
Max altitude for single pack Air Conditioning
31,000 ft
29
Brake cooling limitation
Do not takeoff with Amber brake temperature indicators
30
Autopilot Limitations
-Do not takeoff or go-around -Do not activate until 400ft AGL -During landing turn off autopilot 50ft AGL
31
Engine
General Electric CF34-8E5 -High Bypass Dual Rotor Turbofan
32
Engine Limitation Colors
Maximum and Minimum Limitations:Red Caution Range:Amber Normal Operating Range:Green
33
Oil Temp Limits
Continuous:155 Degrees Celsius Transient:163 Degrees Celsius(above 155 limited up to 15 minutes)
34
Oil Pressure Limits
Min:25psi Max:95psi
35
Engine Rpm Limits
N1 Min: N/a N1 Max:99.5% N2 Min:58.5% N2 Max:99.4%
36
Starter Time Limits
-Start 1st and 2nd Max 90 Seconds ON(ground) followed by 10 seconds off -Start 3rd through 5th Max 120 Seconds ON(in flight) followed by 5 minutes off
37
Starter Dry Motoring Time Limits
-Start 1st Max 90 Seconds ON followed by 5 minutes off -Start 2nd through 5th Max 30 seconds ON followed by 5 minutes off (After 5 sequential motorings needs 15 minute cool down)
38
Thrust Reverse
-Ground Use Only -Power back is prohibited -After landing below 60kts reduce max thrust not permitted, below 60kts set to idle
39
APU Starter Time Limits
-Start 1st and 2nd APU Master control on followed by 60 seconds off -Start 3rd cycle APU Master control on followed by 5 minutes off
40
APU Operational Limits (Starting)
-Temp Max: ISA +39 Degrees C -Temp Min: -54 Degrees C -Altitude: 30,000 ft
41
APU Operational Limits (Altitude for Operation 30k)
-Max Altitude for Electrical AC Power:33,000ft -Max Altitude for Bleed Air to Power AC:15,000ft -Max Altitude for Bleed Air to Assist Engine Start:21,000ft
42
Minimum #2 Battery Temp for APU Starting
-20 Degrees Celsius
43
Maximum RVSM Altitude Different between CA & FO
180ft
44
Pressurization Max Pressure Differential
8.4 PSI
45
Pressurization Maximum Differential Overpressure
8.8 PSI
46
Maximum Negative Differential Pressure
-0.5 PSI
47
Pressurization Maximum Differential Pressure for Takeoff and Landing
0.2 PSI
48
Max Power for Takeoff
14,200 Lbs of Thrust
49
Normal Power For Takeoff (TO-1)
13,000 Lbs of Thrust