ERJ-175 Limitations Flashcards

1
Q

Emergency Fuel

A
  • EMERGENCY fuel - 1,500 LB
  • Landing with less than 30 mins of fuel
  • Emergency fuel provides 30 minutes of fuel endurance based upon 1,500 ft AFE / Green Dot / Clean.
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2
Q

Minimum fuel

A
  • Minimum fuel - 2,250

- Minimum fuel provides 45 minutes of fuel endurance based upon 1,500 ft AFE / Green Dot / Clean.

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3
Q

How do you know when you have low fuel?

A

The fuel indicators turn amber when fuel in the respective tank drops below 1,320 lb (2,640 lb total).

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4
Q

Battery minimum voltage

A

22.5 V

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5
Q

Minimum oil pressure for start

A

25 psi

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6
Q

Max fuel compactly

A

20,935 lbs

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7
Q

Max fuel imbalance

A
794 lbs 
(It is permissible to takeoff with a “fuel imbalance” annunciation as long as it doesn’t exceed 794 lbs
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8
Q

Min fuel tank temp

A

Minus 37 degrees Celsius

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9
Q

Fuel cross feed for takeoff?

A

Fuel crossfeed must be selected OFF during takeoff and landing.

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10
Q

APU Start Temperature operational limits

A

-54 degrees Celsius

ISA +35 degrees

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11
Q

APU Start Altitude Operational Limits

A

30,000’

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12
Q

Planned reserve fuel

A

Calculated at 45 mins at 15,000 ‘ and a cruise speed of 250 kias
E175 - 2,450 lbs

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13
Q

Planned Hold Fuel

A

Calculated at planned landing weight and 10,000’ above the destination airport

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14
Q

Engine start attempts limitations

A

Start 1&2: 90 seconds on, 10 seconds off
Start 3-5: 90 seconds ON, 5 minutes OFF
Increase start attempt time to 120 seconds if in flight

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15
Q

Electrical systems: Integrated drive generators

A

An IDG consists of the integration of a constant speed drive and an AC generator to supply constant frequency AC power to the aircraft.
They are engine driven and directly connected to the engine output via a set of gear boxes

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16
Q

Max takeoff weight (MTOW)

A

175LL - 85,098 lbs

175LR - 85,517 lbs

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17
Q

Max Landing weight

A

Both 74,957 lbs

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18
Q

Max ramp Weight

A

175 LL - 85, 450 lbs

175 LR - 85,870 lbs

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19
Q

Max zero fuel weight

A

175 LL - 69,467 lbs

175LR - 69,886 lbs

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20
Q

Wing span

A

93’11”

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21
Q

A/C length

A

103’11”

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22
Q

Tail height

A

32’4”

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23
Q

Max operating Altitude

A

FL410

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24
Q

Max altitude to takeoff and land

25
Max temperature takeoff and land
ISA +35 degrees (+52C)
26
Max single PACK ops
31,000’
27
Vmo SL to 8000’
300 kts
28
Vmo 10,000 to Mach transition
320 kts
29
Mmo
.82 Mach
30
Va
240 kts
31
Gear operation speed
250 kts
32
Vtire
195 kts
33
V RAT Deploy max
Vmo/Mmo
34
Vmin (To provide electrical power)
130 kts
35
Vb below 10,000
(Turbulence penetration speed) | 250 kts
36
Vb 10,000 and above
270 kts / .76 m whichever is lower
37
Vwiper speed max
250 kts
38
Vwindow
160 kts
39
Max wind recommended dry runway
38 kts
40
Max xwind recommended wet runway
31 kts
41
Max xwind recommended compacted snow
20 kts
42
Max recommended xwind With Standing Water/Slush/Wet Snow/Dry Snow
18 kts
43
Max recommended xwind with ice
12 kts
44
Max altitude with flaps/slats extended
20,000’
45
Enroute operations with flaps
Prohibited
46
Minimum spoiler speed
180 kts
47
Cat 2 approach flap setting
Mandatory flaps 5
48
Landing flaps full GA
Go around flaps 4
49
Landing flaps 5 GA
Go Around flaps 2
50
APU Max operating altitude
33,000’
51
MAX APU use for engine starting
21,000’
52
Max APU use for air conditioning/pressurization
15,000’
53
Max APU operating Altitude:
33,000 ft
54
Max APU use for engine starting:
21,000 ft
55
MAx APU use for air conditioning/pressurization:
15,000 ft
56
Max forward and aft cargo limits?
Forward 3306 lbs | Aft 2535 lbs
57
Maximum Taxi speeds
30 Straight/dry 10 Turns Dry 10 Straight/wet or contaminated 5 Turns wet or contaminated
58
Required RVSM equipment and requirements:
- Overshoot or undershoot must notify ATC by 200’ - Vertical Speed less than 1500 ‘ per minute - XPDR - Either primary ALtimeter System - Altitude alerting and capture system - Autopilot