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Mesa Airlines Training > EJET Limitations (Pre-Class) > Flashcards

EJET Limitations (Pre-Class) Flashcards

1
Q

Max Altitude for APU (Electrical Load), if used for electrics?

A

33,000 feet

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2
Q

Landing below ___ degrees C, may not takeoff again without further maintenance inspection

A
  • 40 degrees C (SAT)
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3
Q

Flaps full speed

A

165 knots

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4
Q

What is the time limit for takeoff thrust on the CF34-8E5 engines

A

10 minutes

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5
Q

Max Differential Pressure for Takeoff and Landing

A

0.2 PSI

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6
Q

Maximum airspeed for RAT operation

A

VMO/MMO

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7
Q

Brake Temperature limitation for Takeoff…

Do Not Takeoff with ____

A

Brake Temperatures in the Amber

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8
Q

Max crosswind recommended for takeoff on a standing water/slush/wet snow/dry snow runway?

A

18 knots

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9
Q

Engine Starter Duty Cycle Limits, Ground vs. In-flight?

  • Attempt 1 and 2*
  • Attempt 3-5*
A

Attempts 1-2:
90 Seconds ON, 10 Seconds OFF

Attempts 3-5:
90 Seconds ON, 5 Minutes OFF

IN FLIGHT both are 120 Seconds on

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10
Q

FLEX limitations

A
  1. ) FLEX reduction must not exceed 25% of the full takeoff thrust
  2. ) FLEX is prohibited on contaminated runways
  3. ) ATTCS (Automatic Takeoff Thrust Control System) must be ON for all takeoffs and landings
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11
Q

Autopilot Minimum Use Height (Coupled ILS Approach)

A

50 feet AGL

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12
Q

Flaps 1 speed?

A

230 knots

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13
Q

Max N2

A

99.4%

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14
Q

Max Fuel Capacity

A

20,935 lbs

Per tank
10,392.5 lbs per tank or 1,535.5 gallons

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15
Q

Max Continuous Engine Oil Temperature

A

155 degrees C

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16
Q

Max Altitude for APU OPERATION?

A

33,000 feet

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17
Q

What is the max N1 speed

A

99.5%

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18
Q

Maximum N1 with brakes applied?

A

60%

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19
Q

Max crosswind allowed for static takeoff?

A

25 knots

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20
Q

Max Operating Speed, up to 8,000 feet?

A

300 knots

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21
Q

Max Runway Slope

A

+/- 2%

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22
Q

Flap Maneuvering Load Acceleration Limits Flaps Up/ Flaps Down

A
  • 1.0 g to 2.5 G

0. 0 g to 2.0 g

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23
Q

Max altitude for APU operation when used for bleed air?

A

15,000 feet

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24
Q

Dry Motoring Duty Cycle Limits

  • Attempt 1*
  • Attempt 2-5*
A

Attempt 1:
90 Seconds ON, 5 Minutes OFF

Attempt 2-5:
30 Seconds ON, 5 Minutes OFF

NOTE After 5 sequential motorings, cycle may be repeated following a 15 minute cool down

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25
Q

Max Operating Speed, 10,000 - FL 290?

A

320 knots (VMO)

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26
Q

Maximum Zero Fuel Weight (MZFW) for E-175 LR

A

69,886 lbs

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27
Q

Engine Limitation Temp for Start?

A

815 degrees C (limited to 10 minutes)

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28
Q

Max Altitude for Takeoff, Landing and Ground Start?

A

10,000 feet

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29
Q

Max takeoff and go around ITT

A

990 degrees C
(Can be exceeded up to 1,006 degrees C for 2 minutes)

*Time limited to 5 minutes with all engines operative, 10 minutes with single engine

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30
Q

Unusable quantity per tank

A

75 lbs per tank

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31
Q

Flaps 2 speed?

A

215 knots

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32
Q

Max crosswind recommended for takeoff on a compacted snow runway?

A

20 knots

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33
Q

What is the AFT BAGGAGE weight capacity?

A

2,535 lbs

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34
Q

Maximum Gear Speed?

Extension (VLOE)
Extended (VLE)
Retraction (VLOR)

A

250 knots

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35
Q

Max Differential Overpressure

A

8.8 PSI

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36
Q

Max continuous ITT

A

960 degrees C

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37
Q

Max Operating Speed, 8,000-10,000 feet?

A

300-320 knots (increases linearly)

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38
Q

What is the limitation pertaining to LOC BACK Course approaches?

A

LOC back course approaches are not authorized with use of the IESS (Integrated Electronic Standby System)

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39
Q

What kind of engines does the E175 have

A

General Electrics CF34-8E5

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40
Q

Max Continuous EGT for APU

A

717 degrees C

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41
Q

Maximum Tire Limit Ground Speed

A

195 knots

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42
Q

Temperature Compensation Baro-Nav operation

A
  1. ) must be coordinated with ATC

2. ) must be used for operation outside the temperature limits published on approach procedure

43
Q

Autopilot Minimum Engagement Height (Takeoff)

Per Mesa CFM

A

1,000 feet AGL

44
Q

Max turbulent airspeed

A

Below 10,000 feet - 250 knots

At or Above 10,000 - 270 KIAS/.76M

45
Q

Maximum speed to open the direct vision window?

A

160 knots

46
Q

Max Takeoff and Landing Tailwind Component

A

10 knots

47
Q

Minimum N2

A

58.5%

48
Q

Max Oil Pressure

A

95 PSI

49
Q

Max Latitude for stationary alignment

A

78.25 degrees N to 78.25 Degrees south

50
Q

Max Operating Speed, FL 290-410?

A

0.82 Mach (MMO)

51
Q

Limitation on takeoff and cross feed operations

“Crossfeed Operations must be ____ for takeoff and landing

A

Off

52
Q

Max altitude for APU operation when used to assist for engine starting?

A

21,000 feet

53
Q

Max altitude for APU START (In-Flight)?

A

30,000 feet

54
Q

Min Temperature for APU start?

A

-54 degrees C

55
Q

Max Ambient Air Temperature for Takeoff and Landing

A

52 degrees C

56
Q

Max Flap Extension Altitude

A

20,000 feet

57
Q

Maximum Takeoff Weight (MTOW) for E-175 LR

A

85,517 lbs

58
Q

Flaps 4 speed

A

180 knots

59
Q

Maximum Windshield Wiper Operational Speed

A

253 knots

60
Q

Max EGT for APU start

A

1,032 degrees C

61
Q

On ground between ____ and ____ the TO DATA SET MENU on the MCDU must be set to ___ when:

  1. ) If there is a possibility when encountering visible moisture up to 1,700 AFE
  2. ) When operating on ramps, taxiways, runways where surface snow, ice standing water or slush may get into the engine nacelles ingested or freeze on engines nacelles and probes
A

5 degrees C and 10 degrees C,

ENG

62
Q

Maximum Ramp Weight (MRW) for E-175 LR

A

85,870 lbs

63
Q

Min Ambient temperature for operation

A
  • 54 degrees C (SAT)
64
Q

Max Differential Negative Overpressure

A

-0.5 PSI

65
Q

Max Differential Pressure

A

8.4 PSI

66
Q

Definition of Icing Conditions?

A

When on the ground or for Takeoff the temperature (OAT) is 10 degrees C, or Inflight TAT is 10 degrees C or lower
With visible moisture present with visibility of less than 1 mile

67
Q

Max crosswind recommended for takeoff on a dry runway?

A

38 knots

68
Q

Max operating Mach

A

MMO (.82M)

69
Q

Max crosswind recommended for takeoff on a runway with ice (including wet ice)?

A

12 knots

70
Q

APU Starter Cooling Period

  • Attempt 1, 2*
  • Attempt 3*
A

Attempt 1, 2
1 min ON, 1 Min OFF

Attempt 3
1 min ON, 5 min OFF

71
Q

Max Altitude for Single Pack Operation

A

Flight Level 310

31,000 feet

72
Q

Max rotor speed of the APU

A

108%

73
Q

Maximum Fuel Imbalance

A

794 lbs (rounded to nearest 800 lbs)

74
Q

Maximum Landing Weight (MLW) for E-175 LR

A

74,957 lbs

75
Q

Max Operating Altitude

A

41,000 feet

76
Q

Min Oil Pressure

A

25 PSI

77
Q

What is the FWD baggage weight capacity?

A

3,306 lbs

78
Q

Max Transient engine oil temperature

A

163 degrees C

Transient operation above 155 degrees C limited to 15 minutes

79
Q

Flaps 5 speed

A

180 knots

80
Q

Minimum Takeoff and Landing Altitude

A

-1,000 feet

81
Q

Max crosswind recommended for takeoff on a wet runway?

A

31 knots

82
Q

Minimum Fuel Tank Temperature

A

-37 degrees C

83
Q

Flaps 3 speed

A

200 knots

84
Q

On ground when OAT is below ____ the TO DATA SET MENU on the MCDU must be set to ___ when:

  1. ) If there is a possibility when encountering visible moisture up to 1,700 AFE
  2. ) When operating on ramps, taxiways, runways where surface snow, ice standing water or slush may get into the engine nacelles ingested or freeze on engines nacelles and probes
A

5 degrees C, ALL

85
Q

Engine/Wing Anti-Ice system operates automatically in ice encounters when the ___ selector is in the ___ position

If either one or both ice detectors fail crew must select the ___ selector to the ___ position

A

MODE, AUTO

MODE, ON

86
Q

CAT II approach and landing must be performed with flaps ___

A

5

87
Q

Max ramp weight for E-175 LL?

A

85,450 lbs

88
Q

Max Takeoff Weight (MTOW) for E-175 LL ?

A

85,098 lbs

89
Q

What is the max landing weight (MLW) of the E-175 LL?

A

74,957 lbs

90
Q

What is the max zero fuel weight (MZFW) of the E-175 LL?

A

69,467 lbs

91
Q

What is the cooling period after each start attempt?

  • Attempt 1 and 2*
  • Attempt 3*
A

Attempt 1 and 2 = 1 min OFF

Attempt 3 = 5 min OFF

92
Q

On ground below ____ the TO DATA SET MENU on the MCDU must be set to ___ when:

  1. ) If there is a possibility when encountering visible moisture up to 1,700 AFE
  2. ) When operating on ramps, taxiways, runways where surface snow, ice standing water or slush may get into the engine nacelles ingested or freeze on engines nacelles and probes
A

5 degrees C

ALL

93
Q

In flight, if one or both ice detectors fail, the crew must do what…?

A

The crew must select the MODE selector to ON:

  • When icing conditions exist or anticipated below 10 degrees C (TAT) with visible moisture
94
Q

What is the height of the E175?

A

32’4”

95
Q

What is the length of the E175?

A

103’11”

96
Q

What is the wingspan of the E175?

A

93’11”

97
Q

What is the distance you need to make a 180 degree turn in the E175?

A

52’9”

98
Q

With FD inoperative what pitch angle would you use for flaps 1?

A

11 degrees

99
Q

With FD inoperative what pitch angle would you use for flaps 2?

A

10 degrees

100
Q

With FD inoperative what pitch angle would you use for flaps 3?

A

N//A

101
Q

With FD inoperative what pitch angle would you use for flaps 4?

A

12 degrees

102
Q

What equipment is required for RVSM? (Oral question)

A

Autopilot
Altitude Alerting System
Altitude Reporting transponder (x1, must be operational)
Air Data Computers (x2, both must be operational)

103
Q

What kind of APU does the E175 have?

A

APU is a Sunstrand APS 2300

Mesa Airlines Training (26 decks)

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