EJet Limits Flashcards

1
Q

Maximum Ramp Weight (MRW)

A

85,870

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2
Q

Maximum Takeoff Weight (MTOW)

A

85,517

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3
Q

Maximum Landing Weight (MLW)

A

74,957

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4
Q

Maximum Zero Fuel Weight (MZFW)

A

69,886

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5
Q

Max Operating Airspeed

A

VMO

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6
Q

Max Operating Mach Number

A

MMO (.82M)

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7
Q

Maximum Airspeed for RAT Operation

A

VMO/MMO

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8
Q

Turbulent Airspeed: Below 10,000 feet

A

250 KIAS

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9
Q

Turbulent Airspeed: At or Above 10,000 feet

A

270 KIAS/.76M

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10
Q

Maximum Tire Limit Ground Speed

A

195 Knots

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11
Q

Maximum Windshield Wiper Operation Speed

A

253 KIAS

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12
Q

Maximum Gear Speed: Extension (VLOE)

A

250 KIAS

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13
Q

Maximum Gear Speed: Extended (VLE)

A

250 KIAS

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14
Q

Maximum Gear Speed: Retraction (VLOR)

A

250 KIAS

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15
Q

Minimum Flight Crew

A

Pilot and Copilot

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16
Q

Max Takeoff and Landing Tailwind Component

A

10 knots

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17
Q

Max Runway Slope

A

+/-2%

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18
Q

Runway Surface Type

A

Paved

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19
Q

Flap Maneuvering Load Acceleration Limits:Flaps Up

A

-1.0 G to +2.5 G

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20
Q

Flap Maneuvering Load Acceleration Limits:Flaps Down (1, 2, 3, 4, 5, and FULL)

A

-0.0 G to +2.0 G

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21
Q

Max Operating Altitude

A

41,000 feet

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22
Q

Max Takeoff and Landing Altitude

A

8,000 feet

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23
Q

Min Takeoff and Landing Altitude

A

-1,000 feet

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24
Q

Max Ambient Air Temperature for Takeoff and Landing

A

52°C

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25
Q

Max Flap Extension Altitude

A

20,000 feet

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26
Q

Maximum latitude for stationary alignment

A

78.25°N to 78.25°S

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27
Q

Min Ambient Temperature Approved for Takeoff

A

-40°C (SAT)

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28
Q

Min Ambient Temperature for Operation

A

-54°C (SAT)

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29
Q

Flaps Operating Speed: Flaps 1

A

230 KIAS

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30
Q

Flaps Operating Speed: Flaps 2

A

215 KIAS

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31
Q

Flaps Operating Speed: Flaps 3

A

200 KIAS

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32
Q

Flaps Operating Speed: Flaps 4

A

180 KIAS

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33
Q

Flaps Operating Speed: Flaps 5

A

180 KIAS

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34
Q

Flaps Operating Speed: Flaps Full

A

165 KIAS

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35
Q

Up to 8,000 feet

A

300 KIAS

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36
Q

Max speed 8,000 to 10,000 feet

A

300 to 320 KIAS (Increases Linearly)

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37
Q

Max speed 10,000 feet to FL290

A

320 KIAS (VMO)

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38
Q

Max speed FL290 to FL410

A

.82M (MMO)

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39
Q

Max Fuel Capacity (Total)

A

20,935 lb. (10392.5 lb. or 1535.5 US Gal per tank)

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40
Q

Unusable Quantity per Tank

A

75 lbs. / 11 US Gal per tank

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41
Q

Maximum Fuel Imbalance

A

794 lb.

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42
Q

Minimum Fuel Tank Temperature

A

-37°C

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43
Q

Max Differential Pressure

A

8.4

44
Q

Max Differential Overpressure

A

8.8 psi

45
Q

Max Differential Negative Pressure

A

-0.5 psi

46
Q

Max Differential Pressure for Takeoff and Landing

A

0.2 psi

47
Q

Max altitude for single pack operation

A

Flight Level 310

48
Q

Engine Name

A

General Electric CF34-8E5 (A-10/S-2)

49
Q

Engine Limits: N1

A

[-] to [99.5%]

50
Q

Engine Limits: N2

A

[58.5%] to [99.4%]

51
Q

Engine Limits: ITT (Start)

A

[-] to [815℃]

52
Q

Engine Limits: ITT (Max T/O & Go Around) {Notes 1 & 2}

A

[-] to [990℃ (Time limited to 10 min.) (Can be exceeded up to 1006℃ during the first 2 min.]

53
Q

Engine Limits: ITT (Max Continuous)

A

[-] to [960℃]

54
Q

Engine Limits: OIL PRESSURE

A

[25 psi] to [95 psi]

55
Q

Engine Limits: OIL TEMPERATURE: (Continuous)

A

[-] to [155℃]

56
Q

Engine Limits: OIL TEMPERATURE: (Transient) {Note 3}

A

[-] to [163℃ (Transient operation above 155℃ limited to 15 min.)]

57
Q

Red on EICAS

A

Max & Min Limitations

58
Q

Amber on EICAS

A

Caution Range

59
Q

Green on EICAS

A

Normal Operating Range

60
Q

NOTE: For FLEX - reduction must not exceed: ___ of the ___ ____ ____

A

25% of the full takeoff thrust

61
Q

NOTE: FLEX is prohibited: on _____ _____

A

on contaminated runways

62
Q

NOTE: ATTCS must be ____ for all T/O and landings

A

ON

63
Q

Engine Starter Duty Cycle: Attempts 1 & 2 GROUND

A

90 Sec ON / 10 sec OFF

64
Q

Engine Starter Duty Cycle: Attempts 1 & 2 AIR

A

120 Sec ON / 10 sec OFF

65
Q

Engine Starter Duty Cycle: Attempts 3, 4 & 5 GROUND

A

90 Sec ON / 10 sec OFF

66
Q

Engine Starter Duty Cycle: Attempts 3, 4 & 5 AIR

A

120 Sec ON / 5 min OFF

67
Q

Dry Motoring Duty Cycle Limits: Attempt 1

A

90 Sec ON / 5 min OFF

68
Q

Dry Motoring Duty Cycle Limits: Attempts 2, 3, 4, & 5

A

30 Sec ON / 5 min OFF (After 5 sequential motorings, cycle may be epeated following a 15 min cool down)

69
Q

APU Started Duty Cycle: Attempts 1 & 2

A

1 min ON / 1 min OFF

70
Q

APU Started Duty Cycle: Attempt 3

A

1 min ON / 5 min OFF

71
Q

APU Type?

A

Hamilton Sundstrand APS 2300

72
Q

Min START Temp & ALT

A

[-54℃] & [-]

73
Q

Max START Temp & ALT

A

[APU temp matches the Airplane Operational Envelope temp] & [30,000 ft]

74
Q

Min Operational Temp

A

APU temp matches the Airplane Operational Envelope temp

75
Q

Max Operational Temp

A

APU temp matches the Airplane Operational Envelope temp

76
Q

Min Operational ALT

A

[-]

77
Q

Max Operational ALT

A

33,000 ft

78
Q

Min Operational ELE GEN

A

[-]

79
Q

Max Operational ELE GEN

A

33,000 ft

80
Q

Min Operational BLEED

A

[-]

81
Q

Max Operational BLEED

A

15,000 ft

82
Q

Min Operational TO ASSIST ENGINE START

A

[-]

83
Q

Max Operational TO ASSIST ENGINE START

A

21,000 ft

84
Q

Min ROTOR SPEED

A

[-]

85
Q

Max ROTOR SPEED

A

108%

86
Q

MAX EGT NOTES

A

[In-flight, there is no automatic shutdown if EGT exceeds the limits.] [There is no time limitation for operating the APU on ground or in flight in the amber range between662°C and 717°C.]

87
Q

Min EGT: START AND CONTINUOUS

A

[-] to [1032℃]

88
Q

Max EGT: START AND CONTINUOUS

A

[-] to [717℃]

89
Q

TAS, TAT, SAT valid above…

A

…60 KIAS

90
Q

Standby Mag Comp NOT VALID while transmitting on…

A

…VHF #1

91
Q

Min A/P useage (T/O)?

A

400’ AGL per Flight Manual & 1000’ AGL per Mesa

92
Q

Min approach height (Coupled ILS)

A

50’ AGL

93
Q

X-feed MUST be OFF…

A

…during T/O and Landing

94
Q

If brake temp is in the AMBER

A

…DO NOT T/O

95
Q

Icing conditions

A

ground OAT or inflight TAT is 10℃ or below with visible moisture

96
Q

Max FWD Cargo Weight

A

3,306 lbs.

97
Q

Max AFT Cargo Weight

A

2,535 lbs.

98
Q

Dimensions: Nose to Tail

A

103’11’

99
Q

Dimensions: Wing tip to Wing tip

A

93’11’

100
Q

Dimensions: Height of Tail

A

32’4”

101
Q

Trun Radius

A

59’2”

102
Q

Max x-wind Limit: DRY

A

38 knots

103
Q

Max x-wind Limit: WET

A

31 knots

104
Q

Max x-wind Limit: compact SNOW

A

20 knots

105
Q

Max x-wind Limit: standing water / SLUSH

A

18 knots

106
Q

Max x-wind Limit: wet ICE

A

12 knots

107
Q

Max x-wind Limit: Static T/O

A

25 knots