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Mesa Airlines Training > EJET - Limitations (AQP) > Flashcards

EJET - Limitations (AQP) 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

Max Ramp Weight (LL)

A

85,450 lbs

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6
Q

Max Takeoff Weight (LL)

A

85,098 lbs

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7
Q

Max Landing Weight (LL)

A

74,957 lbs

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8
Q

Max Zero Fuel Weight (LL)

A

69,467 lbs

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9
Q

FWD Baggage Compartment Max Load?

A

3,306 lbs

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10
Q

AFT Baggage Compartment Max Load?

A

2,535 lbs

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11
Q

Max Operating Altitude?

A

41,000 feet

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12
Q

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

A

300-320 knots (increases linearly)

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13
Q

Max Altitude for Takeoff, Landing, Ground start?

A

10,000 feet

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14
Q

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

A
  • 40 degrees C (SAT)
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15
Q

Minimum Takeoff and Landing Altitude

A

-1,000 feet

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16
Q

Min Ambient temperature for operation

A
  • 54 degrees C (SAT)
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17
Q

Max Ambient temperature for takeoff and landing

A

52 degrees C

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18
Q

Maximum Altitude for Flap Extension

A

20,000 feet

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19
Q

Max Landing Gear retraction speed (Vlo - retract)

A

250 kts

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20
Q

Max Landing Gear extension speed (Vlo - extension)?

A

250 kts

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21
Q

Max Landing Gear extended speed (Vle)

A

250 kts

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22
Q

Maximum speed to open the direct vision window?

A

160 kts

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23
Q

Max Operating Speed

A

Vmo/Mmo

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24
Q

Max Operating Speed up to 8,000 feet?

A

300 knots

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25
Q

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

A

320 knots (Vmo)

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26
Q

Max Operating Speed FL 290-410?

A

0.82 mach (Mmo)

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27
Q

Max Operating mach?

A

Mmo (0.82 mach)

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28
Q

What is Vfe - 1?

A

230 kts

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29
Q

What is Vfe - 2?

A

215 knots

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30
Q

What is Vfe - 3?

A

200 Knots

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31
Q

What is Vfe - 4?

A

180 Knots

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32
Q

What is Vfe - 5?

A

180 Knots

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33
Q

What if Vfe - FULL?

A

165 Knots

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34
Q

Maximum Tire Ground Speed?

A

195 knots

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35
Q

Maximum Takeoff and Landing Tailwind?

A

10 knots

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36
Q

Maximum recommended takeoff crosswind for - DRY RUNWAY?

A

38 Knots

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37
Q

Maximum recommended takeoff crosswind for - WET RUNWAY?

A

31 Knots

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38
Q

Maximum recommended takeoff crosswind for - COMPACTED SNOW?

A

20 Knots

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39
Q

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

A

18 knots

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40
Q

Maximum recommended takeoff crosswind with ICE (including WET ICE)?

A

12 knots

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41
Q

Max recommended crosswind for static takeoff?

A

25 knots

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42
Q

What is the maximum recommended crosswind landing for DRY runway?

A

38 knots

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43
Q

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

A

31 knots

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44
Q

What is the maximum recommended crosswind landing speed for condition 4/4/4 - compacted snow?

A

20 knots

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45
Q

What is the maximum recommended crosswind speed for landing with code 3/3/3 - wet runway?

A

15 knots

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46
Q

What is the maximum recommended crosswind speed for landing with code 2/2/2 - wet/slush more than 1/8th inch depth?

A

12 knots

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47
Q

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

A

8 knots

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48
Q

What is the maximum recommended crosswind for landing with code 0/0/0 braking action NIL?

A

No operations allowed

49
Q

Flap maneuvering load acceleration limits for flaps up/flaps down

A

Flaps Up = -1.0g to 2.5g

Flaps Down = 0.0g to 2.0g

50
Q

Max runway slope

A

+/- 2%

51
Q

What is the approved runway surface type?

A

Paved

52
Q

Max Fuel Capacity?

A

20,935 lbs

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

53
Q

Unusable Fuel Quantity per tank?

A

75 lbs (11 gallons)

54
Q

Maximum permitted fuel imbalance between tanks?

A

794 lbs (roundest to nearest 800 lbs)

55
Q

Minimum Fuel Tank Temperature

A

-37 degrees C

56
Q

Limitation on takeoff and cross feed operation

“Crossfeed Operations must be ___ for takeoff and landing”

A

OFF

57
Q

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

A

Sundstrand APS 2300

58
Q

Min Temperature for APU start?

A

-54 degrees C

59
Q

Max altitude for APU START (in-flight)?

A

30,000 feet

60
Q

Max altitude for APU Operation?

A

33,000 feet

61
Q

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

A

33,000 feet

62
Q

Max altitude for APU operation if used for Bleed Air?

A

15,000 feet

63
Q

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

A

21,000 feet

64
Q

Max Rotor Speed of the APU?

A

108%

65
Q

Max Continuous EGT for APU?

A

717 degrees C

66
Q

Max EGT for APU Start?

A

1,032 degrees C

67
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

68
Q

Max N1 with brakes applied?

A

60%

69
Q

What kind of engine does the E175 have?

A

General Electric CF34-8E5

70
Q

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

A

10 minutes

71
Q

What is the max N1 speed?

A

99.5%

72
Q

What is the Minimum N2 speed?

A

58.5%

73
Q

What is the maximum N2 speed?

A

99.4%

74
Q

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

A

815 degrees C (limited to 10 minutes)

75
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

76
Q

Max continuous ITT

A

960 degrees C

77
Q

Minimum Oil Pressure?

A

25 PSI

78
Q

What is maximum oil pressure?

A

95 PSI

79
Q

Maximum Continuous Engine Oil Temperature?

A

155 degrees C

80
Q

What is the Maximum Engine Oil Transient Temperature?

A

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

81
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

82
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

83
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 both takeoffs and landings
84
Q

Maximum Differential Pressure?

A

8.4 PSI

85
Q

Maximum Differential Overpressure?

A

8.8 PSI

86
Q

Maximum Differential Negative Pressure

A
  • 0.5 PSI
87
Q

Maximum Differential Pressure for Takeoff and Landing?

A

0.2 PSI

88
Q

Max Altitude for Single Pack Operations?

A

31,000 feet

89
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

90
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 or freeze on the engine nacelles and probes
A

5 degrees C, ALL

91
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

92
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

93
Q

Maximum Airspeed for Windshield Wiper Operation?

A

253 Knots

94
Q

Autopilot Minimum Engagement Height (Takeoff)

PER MESA CFM

A

1,000 feet AGL

95
Q

Autopilot Minimum Use Height (Coupled ILS Approach)

A

50 feet AGL

96
Q

When is TAS, TAT, SAT information valid?

A

Only above 60 Knots

97
Q

What is the limitation pertaining to transmitting with VHF 1?

A

Standby magnetic compass indication is not valid

98
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)

99
Q

Max Latitude for stationary alignment

A

78.25 degrees North to 78.25 degrees South

100
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
101
Q

CAT II approach and landing must be performed with flaps ___

A

5

102
Q

CAT II demonstrated headwind?

A

25 knots

103
Q

CAT II demonstrated tailwind

A

10 knots

104
Q

CAT II demonstrated crosswind

A

12 knots

105
Q

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

A

Up to 3 degrees is acceptable

106
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

107
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)

108
Q

Max airspeed for RAT Operation?

A

Vmo/Mmo

109
Q

Brake temperature limitation for takeoff…

Do not takeoff with brake temperatures in ____

A

Amber, do not takeoff with brake temps in amber

110
Q

Max Turbulent Airspeed

A

Below 10,000 feet: 250 Knots

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

111
Q

What is the height of the E175?

A

32’4”

112
Q

What is the length of the E175?

A

103’11”

113
Q

What is the wingspan of the E175?

A

93’ 11”

114
Q

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

A

59’ 2”

115
Q

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

A

11 degrees

116
Q

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

A

10 degrees

117
Q

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

A

N/A

118
Q

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

A

12 degrees

Mesa Airlines Training (26 decks)

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