Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

Embraer E175 AFM Manufacturer > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Takeoff 175

A

37,500 Kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max Landing

A

34,000 Kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max Ramp Weight MRW

A

37,660 kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Max Zero Fuel Weight MZFW

A

31,700 kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Max 90 degree crosswind for CAT II

A

12 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Max 90 degree crosswind component (STEADY) - Takeoff RCC 6

A

38 Kt DRY RWY

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Max 90 degree crosswind component (STEADY) Takeoff wet RCC 3

A

15 Kt WET RWY

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Max takeoff and landing tailwind component including CAT II

A

10 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

XFEED Switch must be set to

A

OFF for takeoff and landing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Max Turbulent airspeed at or above 10,000 ft

A

270 Kt/.76 M

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Max windshield wiper operation speed

A

253 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Max gear extension speed VLO

A

250 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Max gear retraction speed VLO

A

250 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Max gear extended speed VLE

A

250 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Max speed flap position 1

A

230 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Max speed flap position 2

A

215 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Max speed flap position 3

A

200 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Max speed flap position 4 and 5

A

180 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Max speed flap position FULL

A

165 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

AP Precision approach CAT II

A

50 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

AP Minimum Engagement Height

A

400 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

AP Minimum Engagement Height cruise and descent

A

1000 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

AP Minimum Use Height Approach

A

50 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

ENGINE STARTER DUTY CYCLE (E1)

A

1st and 2nd attempt - 90 seconds ON (ground) / 10 seconds off

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

ENGINE STARTER DUTY CYCLE (E1) in flight

A

120 seconds ON (in flight)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Definition of Icing Conditions

A

Icing conditions may exist whenever the Outside Air Temperature
(OAT) on the ground or for takeoff, or Total Air Temperature (TAT)
inflight, is 10°C or below and visible moisture in any form is present
(such as clouds, fog with visibility of one mile or less, rain, snow, sleet,
and ice crystals).

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

The XFEED Selector must be set to

A

OFF during takeoff and landing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

Do not takeoff with brake temperature indicators in

A

the amber range

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

Maximum altitude with flaps/slats extended is

A

20,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

For E1 / E2 airplanes, after the engine has started, operate at or near idle for at least

A

two (2) minutes before selecting high thrust. Taxi time at or near idle can be included in the warm-up period.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

For E1 airplanes, following high thrust operation the engine will be operated at or near idle for

A

two (2) minutes before shutdown to thermally stabilize the engine’s hot section. Taxi time at or near idle can be included in this period

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

In the event that a limitation in this manual disagrees with the AFM limitation, the AFM will prevail. In the event that a placard or instrument marking disagrees with the limitations shown in this manual,

A

the more restrictive limitation will prevail.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

Max Headwind (for CAT II and LVO)

A

25 Kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

RUNWAY SLOPE Max (up hill, down hill)

A

+2.0%, -2.0%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

Min fuel temperature

A
  • 37°C
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

Max fuel imbalance left/right

A

360 kg

37
Q

ALTITUDES Max operating

A

41,000 ft

38
Q

ALTITUDES Max takeoff and landing

A

10,000 ft

39
Q

ALTITUDES Max flap extension

A

20,000 ft

40
Q

TEMPERATURES Max ambient for takeoff and landing

A

52°C

41
Q

TEMPERATURES Min ambient approved for takeoff

A

-54°C

42
Q

Max altitude for single pack operation

A

31,000 ft

43
Q

Max differential pressure

A

8.4 psi

44
Q

Max negative differential pressure

A

-0.5 psi

45
Q

Max differential pressure for takeoff & landing

A

0.2 psi

46
Q

LIMIT MANEUVERING LOAD FACTORS Flaps up

A

-1.0 to +2.5 G

47
Q

LIMIT MANEUVERING LOAD FACTORS Flaps down (1, 2, 3, 4, 5 and full)

A

0.0 to +2.0 G

48
Q

Max N1 and N2

A

99,5% 99,4%

49
Q

Max ITT During engine start

A

815°C

50
Q

Max ITT normal Takeoff and Go-Around

A

965ºC First 2 minutes of the total 5 minutes
limit

51
Q

Max ITT Normal Takeoff and Go Around emaining 3 minutes of the total
5 minutes limit

A

949ºC

52
Q

Max ITT Takeoff and Go-Around first 2 min / remaining 3 min of total 5 min

A

1006°C / 990 °C - Time limited to 5 min

53
Q

Max Continuous ITT

A

960°C

54
Q

Min Oil Pressure

A

25 psi

55
Q

Max Oil Temperature

A

95°C

56
Q

ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt- 90 seconds ON (ground) / 120 seconds ON (in flight)

A

5 minutes off

57
Q

Dry-Motoring Cycle 1st attempt / 2 through to 5

A

90 seconds ON / 30 seconds ON / 5 minutes off (After five sequential motorings, cycle may be repeated
following a 15-minute cool-down period)

58
Q

ENGINE STARTER DUTY CYCLE Maximum time

A

90/ 120 seconds ON (ground/in flight) / 10 sec off

59
Q

APU Starter Duty Cycle 1st and 2nd attempt

A

60 seconds off

60
Q

APU Starter Duty Cycle 3rd

A

5 minutes off

61
Q

APU - Min/ Max temperature for operations

A

-54°C / 52°C

62
Q

APU Max altitude for Start

A

30,000 ft

63
Q

APU Max altitude for electrical supply E1

A

33,000 ft

64
Q

APU Max altitude for bleed supply

A

15,000 ft

65
Q

APU Max altitude to assist engine start E1

A

21,000 ft

66
Q

APU Max rotor speed

A

108%

67
Q

APU Max EGT start.

A

1032°C

68
Q

APU Max EGT Continuous

A

717°C

69
Q

Maximum operating airspeed

A

VMO

70
Q

Maximum operating mach number

A

.82 (MMO)

71
Q

Maximum airspeed for RAT operation

A

VMO/MMO

72
Q

Turbulent air penetration speed (below 10,000 ft.)

A

250 KIAS

73
Q

Tire limit ground speed

A

195 Kt

74
Q

Low visibility - — Max Headwind

A

25 Kt .

75
Q

The takeoff weight (weight at brake release or at start of takeoff run) is
the lowest between MTOW and the following weights:

A

− Maximum takeoff weight as calculated using the approved
software, and as limited by field length, climb and brake energy.
− Maximum takeoff weight, as limited by enroute, and landing
operating requirements

76
Q

The landing weight is the lowest among MLW and the following
weights calculated using the approved software:

A

− Maximum approach and landing weight as limited by altitude,
temperature and climb gradient.

77
Q

Maximum fuel capacity is

A

11709 l (9496 kg).

78
Q

Maximum usable quantity per tank

A

5812.5 l (4714 kg)

79
Q

Unusable quantity per tank

A

42 l (34 kg)

80
Q

Max oil temperature continuous

A

155°C

81
Q

Max oil temperature transient

A

163°C

82
Q

Engine max STARTING DUTY CYCLE time 3rd to 5th

A

90 Seconds (On ground)
120 seconds (In-flight) / 5 min off

83
Q

For ground starts, the maximum cumulative starter run time
per start attempt is

A

90 seconds (motoring plus start time)

84
Q

For in-flight starts, the maximum cumulative starter run time
per start attempt is

A

120 seconds (motoring plus start time)

85
Q

Maximum differential overpressure

A

8.8 psi

86
Q

Due to engine compressor stall possibility, static takeoff is not
recommended with crosswind component greater than

A

25 kt

87
Q

Max headwind CAT II

A

25kt

88
Q

FMS - pilots must compare any procedures/route retrieved from the
FMS database with those published on the charts. Differences
between the charts and the FMS information up to

A

3 degrees are
acceptable.

Embraer E175 AFM Manufacturer (4 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions