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Mesa Airlines Training > EJET - Limitations (2024 PC) > Flashcards

EJET - Limitations (2024 PC) Flashcards

1
Q

MAX RAMP WEIGHT (LR)

A

85,870 lbs

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2
Q

MAX TAKEOFF WEIGHT (LR)

A

85,517 lbs

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3
Q

MAX LANDING WEIGHT (LR)

A

74,957 lbs

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4
Q

Max Zero Fuel Weight (LR)

A

69,886 lbs

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5
Q

FWD Baggage Compartment Max Load?

A

3,306 lbs

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6
Q

AFT Baggage Compartment Max Load

A

2,535 lbs

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7
Q

Max Operating Altitude?

A

41,000 feet

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8
Q

Max Operating Speed 8,000-10,000 feet

A

300-320 knots (increases linearly)

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9
Q

Max Altitude for Takeoff, Landing, Ground Start

A

10,000 feet

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10
Q

Landing below ____ degrees C, may not takeoff again until further maintenance inspection

A
  • 40 degrees C (SAT)
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11
Q

Minimum Takeoff and Landing Altitude

A

-1,000 feet

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12
Q

Minimum Ambient Temperature for Operation

A

-54 degrees C (SAT)

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13
Q

Max Ambient Temperature for Takeoff and Landing

A

52 degrees C

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14
Q

Maximum Altitude for Flap Extension

A

20,000 feet

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15
Q

Max Landing Gear Extension Speed (Vlo - extend)

A

250 knots

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16
Q

Max Landing Gear Retraction Speed (Vlo-retract)?

A

250 knots

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17
Q

Max Landing Gear Extended Speed (Vle)

A

250 knots

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18
Q

Maximum Speed to Open the Direct Vision Window?

A

160 knots

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19
Q

Max Operating Speed?

A

Vmo/Mmo

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20
Q

Max Operating Speed up to 8,000 feet?

A

300 knots

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21
Q

Max Operating Speed from 10,000 feet to FL 290?

A

320 knots (Vmo)

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22
Q

Max Operating Speed FL 290-410?

A

0.82 mach (Mmo)

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23
Q

Max Operating Mach?

A

Mmo (0.82 mach)

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24
Q

What is Vfe-1?

A

230 knots

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25
Q

What is Vfe-2?

A

215 knots

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26
Q

What is Vfe-3?

A

200 knots

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27
Q

What is Vfe-4?

A

180 knots

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28
Q

What is Vfe-5?

A

180 knots

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29
Q

What is Vfe-Full?

A

165 knots

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30
Q

Maximum tire ground speed?

A

195 knots

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31
Q

Maximum Takeoff and Landing Tailwind

A

10 knots

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32
Q

Maximum Recommended Takeoff Crosswind - DRY RUNWAY

A

38 knots

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33
Q

Maximum Recommended Takeoff Crosswind - WET RUNWAY?

A

31 knots

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34
Q

Maximum Recommended Takeoff Crosswind for - COMPACTED SNOW

A

20 knots

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35
Q

Maximum recommended takeoff crosswind for - STANDING WATER/SLUSH/WET SNOW/DRY SNOW?

A

18 knots

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36
Q

Maximum recommended takeoff crosswind for - ICE (including WET ICE)?

A

12 knots

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37
Q

Maximum recommended crosswind for static takeoff?

A

25 knots

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38
Q

Maximum recommended takeoff crosswind per Mesa Airlines, Inc?

A

28 knots

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39
Q

What is the maximum recommended crosswind for landing - DRY RUNWAY

A

38 knots

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40
Q

What is the maximum recommended crosswind for landing with code 5/5/5 - GOOD

A

31 knots

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41
Q

What is the maximum recommended crosswind for landing with code 4/4/4

A

20 knots

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42
Q

What is the maximum recommended crosswind for landing with 3/3/3 - MEDIUM

A

15 knots

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43
Q

What is the maximum recommended crosswind for landing with code 2/2/2

A

12 knots

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44
Q

What is the maximum recommended crosswind speed for landing with code 1/1/1

A

8 knots

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45
Q

What is the maximum crosswind speed for landing witch code 0/0/0 - braking action nil

A

No operations allowed

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46
Q

Flap maneuvering load acceleration limits for flaps up/flaps down

A

Flaps up = -1.0 g to 2.5 g

Flaps down = 0.0 g to 2.0 g

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47
Q

Max runway slope

48
Q

What is the approved runway surface type

49
Q

Max Fuel Capacity

A

20,935 lbs

10,392.5 lbs per tank or 1,535.5 gallons

50
Q

Unusable Fuel Quantity Per Tank

A

75 lbs (11 gallons)

51
Q

Maximum permitted fuel imbalance between tanks?

A

794 lbs (rounded to nearest 800 lbs)

52
Q

Minimum fuel tank temperature

A

-37 degrees C

53
Q

Limitation on takeoff and cross feed operation

54
Q

What is the make and model of the E-175 APU

A

Sundstrand APS 2300

55
Q

Min temperature for APU start

A

-54 degrees C

56
Q

Max Altitude for APU Start (inflight)

A

30,000 feet

57
Q

Max Altitude for APU Operation?

A

33,000 feet

58
Q

Max Altitude for APU (electrical load), if used for electrics?

A

33,000 feet

59
Q

Max Altitude for APU Operation if used for bleed air?

A

15,000 feet

60
Q

Max Altitude for APU when used to assist for engine starting?

A

21,000 feet

61
Q

Max rotor speed of the APU?

62
Q

Max continuous EGT for APU?

A

717 degrees C

63
Q

Max EGT for APU start?

A

1,032 degrees C

64
Q

APU Starter Cooling Period

Attempts 1,2
Attempts 3

A

Attempts 1, 2
1 min ON, 1 min OFF

Attempts 3
1 min ON, 5 min OFF

65
Q

Max N1 with brakes applied?

66
Q

What kind of engine does the E175 have?

A

General Electric CF34-8E5

67
Q

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

A

10 minutes

68
Q

What is the Max N1 Speed?

69
Q

What is the minimum N2 speed?

70
Q

What is the maximum N2 speed?

71
Q

What is the max ITT for engine start (engine start limitation)?

A

815 degrees C (limited to 10 minutes)

72
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

73
Q

Max continuous ITT?

A

960 degrees C

74
Q

Minimum Oil Pressure

75
Q

What is maximum oil pressure?

76
Q

Maximum continuous engine oil temperature?

A

155 degrees C

77
Q

What is the maximum engine oil transient temperature?

A

163 degrees C (above 155 degrees, limited to 15 minutes)

78
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 period

79
Q

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

Attempt 1
Attempt 3-5

A

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

Attempt 3-5
90 Seconds ON, 5 minutes OFF

IN-FLIGHT BOTH are 120 seconds ON

80
Q

Flex Limitations

A
  1. Flex reduction must not exceed 25% of the full takeoff thrust
  2. FLEX is prohibited on contaminated runways
  3. ATTC (Automatic Takeoff Thrust Control System) must be ON for both takeoffs and landings.
81
Q

Maximum Differential Pressure

82
Q

Maximum Differential Overpressure?

83
Q

Maximum Differential Negative Pressure?

84
Q

Maximum Differential Pressure for Takeoff and Landing?

85
Q

Max Altitude for Single Pack Operations?

A

31,000 feet

86
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 feet AFE

2.) When operating on ramps, taxiways, runways when surface snow, ice, standing water or slush may get into the engine nacelles or freeze on the engine nacelles and probes

A

5 degrees C, ALL

87
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

88
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

89
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

90
Q

Maximum airspeed for windshield wiper operations?

91
Q

Autopilot minimum engagement height (Takeoff)

A

1,000 feet AGL

92
Q

Autopilot Minimum Use Height (Coupled ILS approach)

A

50 feet AGL

93
Q

When is TAS, TAT, SAT information valid?

A

Only above 60 knots

94
Q

What is the limitation pertaining to transmitting with VHF 1?

A

Standby magnetic compass indication is not valid

95
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)

96
Q

Max latitude for stationary alignment

A

78.25 degrees North to 78.25 degrees South

97
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

98
Q

CAT II approach and landing must be performed with flaps___

99
Q

CAT II demonstrated headwind

100
Q

CAT II demonstrated tailwind

101
Q

CAT II demonstrated crosswind

102
Q

What is the max difference for routes in degrees between published charts and FMS?

103
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 the approach procedure

104
Q

What equipment is required for RVSM? (Oral Question)

A

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

105
Q

Max airspeed for RAT operation?

106
Q

Brake temperature limitation for takeoff…

A

Amber, do not takeoff with brake temps in amber

107
Q

Max Turbulent Airspeed

A

Below 10,000 feet: 250 knots

Above 10,000 feet: 270 knots/.76 Mach whichever is slower

108
Q

What is the height of the E-175?

109
Q

What is the length of the E-175?

110
Q

What is the distance you need to make a 180 degree turn in E-175?

111
Q

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

A

11 degrees

112
Q

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

A

10 degrees

113
Q

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

114
Q

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

A

12 degrees

115
Q

What is the wingspan for the E-175?

A

93’11”

Mesa Airlines Training (26 decks)

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