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Mesa EJET > Limitations > Flashcards

Limitations Flashcards

1
Q

E175 Types of Operations

A

IFR
VFR
CAT I, CAT II
Icing Conditions

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2
Q

Max Ramp Weight (MRW)

A

85,870 lbs.

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3
Q

Max T/O Weight (MTOW)

A

85,517 lbs.

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4
Q

Max Landing Weight (MLW)

A

74,957 lbs.

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5
Q

Max Zero Fuel Weight (MZFW)

A

69,886 lbs.

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6
Q

Minimum Flight Crew

A

2 (Pilot, Co-Pilot)

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7
Q

Max Tailwind T/O and Landing

A

10 knots

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8
Q

Max Runway Slope

A

+/- 2%

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9
Q

Runway Surface Type

A

Paved

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10
Q

Flap Maneuvering Load

Accelerations Limits - Flaps Up

A

-1.0 G to +2.5 G

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11
Q

Flap Maneuvering Load

Accelerations Limits - Flaps Down (1,2,3,4,5, Full)

A

0.0 G to +2.0 G

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12
Q

Max Operating Altitude

A

41,000 ft.

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13
Q

Max T/O and Landing Altitude

A

8,000 ft.

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14
Q

Min T/O and Landing Altitude

A

-1,000 ft.

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15
Q

Max Ambient Air Temp for T/O and Landing

A

52 C

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16
Q

Max Flap Extension Altitude

A

20,000 ft.

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17
Q

Max Latitude for Stationary Alignment

A

78.25 N to 78.25 S

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18
Q

Min Ambient Temp approved for T/O

A

-40 C (SAT)

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19
Q

Min Ambient Temp for Operation

A

-54 C (SAT)

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20
Q

Max Operating Mach Number (MMO)

A

.82 M

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21
Q

Max Operating Airspeed (VMO)

A

320 KIAS (VMO)

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22
Q

Max Airspeed for RAT Operation

A

VMO / MMO

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23
Q

Turbulent Airspeed

-Below 10,000 ft.

A

250 KIAS

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24
Q

Turbulent Airspeed

-At or above 10,000 ft.

A

270 KIAS / .76 M

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25
Q

Max Tire Limit Ground speed

A

195 knots

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26
Q

Max Windshield Wiper Operation

A

253 KIAS

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27
Q

Max Gear Speed

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

250 KIAS

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28
Q

Flaps 1 (Max Speed)

A

230 KIAS

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29
Q

Flaps 2 (Max Speed)

A

215 KIAS

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30
Q

Flaps 3 (Max Speed)

A

200 KIAS

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31
Q

Flaps 4 (Max Speed)

A

180 KIAS

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32
Q

Flaps 5 (Max Speed)

A

180 KIAS

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33
Q

Flaps Full (Max Speed)

A

165 KIAS

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34
Q

Max Operating Speed

-Up to 8,000 ft.

A

300 KIAS

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35
Q

Max Operating Speed

-8,000 to 10,000 ft.

A

300 to 320 KIAS (Increases Linearly)

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36
Q

Max Operating Speed

-10,000 ft to FL290

A

320 KIAS (VMO)

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37
Q

Max Operating Speed

-FL290 to FL410

A

.82 M (MMO)

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38
Q

Icing Conditions

A

Whenever the Outside Air Temperature (OAT) on ground and for T/O, or Total Air Temperature (TAT) inflight, is 10 degrees celsius or below and visible moisture in any form is present.

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39
Q

Max Fuel Capacity

A

20,935 lbs.

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40
Q

Max Fuel Capacity per Tank

A

10,392.5 lbs. (1535.5 US gallons)

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41
Q

Unusable Quantity per tank

A

75 lbs. (11 US gallons)

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42
Q

Max Fuel Imbalance

A

794 lbs.

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43
Q

Min Fuel Tank Temperature

A

-40 C

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44
Q

Crossfeed Operations

A

Must be OFF for T/O and Landing

45
Q

Pressurization

-Max Diff Pressure up to 37,000 ft.

A

7.80 psi

46
Q

Pressurization

-Max Diff Pressure above 37,000 ft.

A

8.34 psi

47
Q

Pressurization

-Max Diff Overpressure

A

8.77 psi

48
Q

Pressurization

-Max Diff Negative Pressure

A

-0.5 psi

49
Q

Pressurization

-Max Diff Pressure for T/O and Landing

A

0.2 psi

50
Q

Max Altitude for Single Pack Operation

A

FL310

51
Q

Brake Temp in Amber

A

Do not T/O

52
Q

Thrust Reversers

A
  • Ground Use Only
  • Not Authorized During Taxi
  • Do Not Attempt Go-around After Deployment
  • Power-back is Prohibited
  • Full Stop Landings Only
  • MIN REV Thrust with the Translating Cowl Open below 60 KIAS
  • Idle Thrust with Translating Cowl closed at 30 KIAS
53
Q

Auto Pilot

-Engagement Height for T/O

A

1,000 ft. AGL (Mesa CFM)

400 ft. AGL (AFM)

54
Q

Auto Pilot

-Min Use Height (Coupled ILS Approach)

A

50 ft. AGL

55
Q

Max N1

A

99.5%

56
Q

Min N2

A

58.5%

57
Q

Max N2

A

99.4%

58
Q

Max ITT for Start

A

815 C

59
Q

Max ITT for T/O and Go-around

A 
990 C (limited to 10 minutes)
-Can be exceeded up to 1006 C during first 2 minutes
60
Q

Max Cont. ITT

A

960 C

61
Q

Min Oil Pressure

A

25 psi

62
Q

Max Oil Pressure

A

95 psi

63
Q

Max Cont. Oil Temp

A

155 C

64
Q

Max Transient Oil Temp

A

163 C

Transient operation above 155 C limited to 15 min.

65
Q

EICAS Markings

-Red

A

Max and Min Limitations

66
Q

EICAS Markings

-Amber

A

Caution Range

67
Q

EICAS Markings

-Green

A

Normal Operating Range

68
Q

FLEX T/O Thrust

A

Reduction must not exceed 25% of Full T/O Thrust

69
Q

FLEX Thrust Prohibited On?

A

Contaminated Runways

70
Q

ATTCS must be ON for?

A

All T/O and Landings

71
Q

Engine Start Duty Cycle Limits

-Ground

A 
90 sec ON, 10 sec OFF
90 sec ON, 10 sec OFF
90 sec ON, 5 min OFF
90 sec ON, 5 min OFF
90 sec ON, 5 min OFF
72
Q

Engine Start Duty Cycle Limits

-Flight

A 
120 sec ON, 10 sec OFF
120 sec ON, 10 sec OFF
120 sec ON, 5 min OFF
120 sec ON, 5 min OFF
120 sec ON, 5 min OFF
73
Q

Dry Motoring Duty Cycle Limits

A 
90 sec ON, 5 min OFF
30 sec ON, 5 min OFF
30 sec ON, 5 min OFF
30 sec ON, 5 min OFF
30 sec ON, 5 min OFF

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

74
Q

APU

-Starter Duty Cycle

A

1 min ON, 1 min OFF
1 min ON, 1 min OFF
1 min ON, 5 min OFF

75
Q

APU

-Min Start Temp

A

-54 C

76
Q

APU

-Max Start Temp

A

APU temp matches Airplane Operational Envelope temp

77
Q

APU

-Max Start Altitude

A

30,000 ft.

78
Q

APU

-Temp Min and Max Operation

A

APU temp matches Airplane Operational Envelope

79
Q

APU

-Max Operation Altitude

A

33,000 ft.

80
Q

APU

-Max Electrical Gen

A

33,000 ft.

81
Q

APU

-Max Bleed

A

15,000 ft.

82
Q

APU

-Max Assist Engine Start

A

21,000 ft.

83
Q

APU

-Max Rotor Speed

A

108%

84
Q

APU

-Max EGT Start

A

1032 C

85
Q

APU

-Max Cont. EGT

A

717 C

86
Q

APU

-EGT

A

No automatic shutdown if EGT exceeds limits

No time limitation for operating the APU on ground or in flight in the Amber range between 662 C and 717 C

87
Q

TAS, TAT and SAT valid above

A

60 KIAS

88
Q

Standby Magnetic Compass not valid

A

while transmitting on VHF #1

89
Q

Baro mins must be use for all

A

CAT I approaches

90
Q

LOC Back course approaches using IESS is

A

Not authorized

91
Q

Pilots are authorized to deviate from their current ATC clearance

A

To the extent necessary to comply with an RA (Resolution Advisory)

92
Q

Is there an auto shutdown for the APU in flight if the EGT exceeds limits?

A

No

93
Q

Max Crosswind

-Dry Runway

A

38 knots

94
Q

Max Crosswind

-Wet Runway

A

31 knots

95
Q

Max Crosswind

-Compact Snow

A

20 knots

96
Q

Max Crosswind

-Standing Water or Slush

A

18 knots

97
Q

Max Crosswind

-Wet Ice or CAT II

A

12 knots

98
Q

Max Crosswind

-Static T/O

A

25 knots

99
Q

Max Speed for Operating DV Window

A

160 knots

100
Q

Aircraft Height

A

32’ 3”

101
Q

Aircraft Wingspan

A

93’ 11”

102
Q

Aircraft Length

A

103’ 11”

103
Q

Max Turn

-Nose Wheel Steering

A

76 degrees

104
Q

Max Turn

-Rudder

A

7 degrees

105
Q

Min Runway Width

A

59’ 2”

106
Q

AFT Cargo Capacity

A

2534 lbs.

107
Q

FWD Cargo Capacity

A

3306 lbs.

Heated and Ventilated

108
Q

Cabin Height

A

6’ 7”

109
Q

Cargo Height

A

3’ 1”

Mesa EJET (10 decks)

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