Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

JSX Training Pack > Operating Limitations > Flashcards

Operating Limitations Flashcards

1
Q

Max Zero Fuel Weight (MZFW) - E135

A

35,274 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max Ramp Weight (MRW) - E135

A

44,312 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max Takeoff Weight (MTOW) - E135

A

44,092 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Max Landing Weight (MLW) - E135

A

40,785 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Max Zero Fuel Weight (MZFW) - E145

A

40,564 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Max Ramp Weight (MRW) - E145

A

50,044 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Max Takeoff Weight (MTOW) - E145

A

49,823 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Max Landing Weight (MLW) - E145

A

43,651 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Takeoff/Landing Minimum Altitude

A

-1000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Takeoff/Landing Maximum Altitude

A

8,000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Maximum Operating Altitude

A

37,000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Mmo

A

Mach .78

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Vmo

A

250 KIAS to 8000’ / 320 KIAS above 10,000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Vlo for Extension

A

250 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Vlo for Retraction

A

200 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Vle

A

250 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Va

A

200 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Turbulent Air Penetration Below 10,000’

A

200 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Turbulent Air Penetration Above 10,000’

A

250 KIAS / .63M whichever is lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Vfe - Flaps 9

A

250 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Vfe - Flaps 18/22

A

200 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Vfe - Flaps 45

A

145 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Maximum Altitude for Flap Extension

A

20,000’

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Max A/S for Windshield Wiper Operation

A

170 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Max A/S After Takeoff/During Climb Without Trimming

A

160 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Max Recommended A/S to Remove DV Windows

A

140 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

Max Crosswind Dry/Wet Runway

A

30 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

Max Takeoff/Landing Tailwind Component

A

10 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

Maximum Load on Main Generator

A

400 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

Maximum Load on APU Generator up to 30,000’

A

400 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Maximum Load on APU Generator above 30,000’

A

300 A

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

Maximum Battery Temperature

A

70° C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

Usable Wing Fuel Per Tank

A

5,717 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

Unusable Fuel Per Tank

A

39 LBS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

Unusable Quantity Per Fuel Tank (Elec Pump INOP)

A

365 LBS

36
Q

Maximum Imbalance Between Wing Tanks

A

800 LBS

37
Q

Min Fuel Tank Temp

A

-40° C

38
Q

Max Fuel Tank Temp

A

52° C

39
Q

Min Fuel Temp @ FCOC Without Icing Inhibitor

A

4° C

40
Q

Maximum Altitude for Start

A

30,000’

41
Q

Max Operating Altitude

A

37,000’

42
Q

Maximum Rotor Speed

A

108%

43
Q

Rotor Speed for Automatic Shutdown

A

104%

44
Q

Maximum EGT for Start

A

884° C

45
Q

Maximum Continous EGT

A

680° C

46
Q

Maximum Continous EGT for 5 Min Max

A

717° C

47
Q

Minimum Battery Temperature for Start

A

-20° C

48
Q

Cooling Period Between First Three Start Attempts

A

1 min off

49
Q

Cooling Period Between Two Series of Three Start Attempts

A

30 Mins off

50
Q

Maximum N1

A

100%

51
Q

Maximum N2 (Steady State)

A

102.4%

52
Q

Max ITT for Start

A

800° C

53
Q

Max ITT Takeoff (5 Min Max)

A

948° C

54
Q

Max Continous ITT

A

901° C

55
Q

Min Oil Press Below 88% N2

A

34 PSI

56
Q

Min Oil Pressure Above 88% N2

A

50 PSI

57
Q

Max Oil Press (Steady State Temp >21° C)

A

95 PSI

58
Q

Max Oil Press (Transient 5 Min)

A

110 PSI

59
Q

Min Oil Temp for N2 Above 83%

A

40° C

60
Q

Min Oil Temp for Starting

A

-40° C

61
Q

Min Oil Temp Cont Ops

A

21° C

62
Q

Max Oil Temp Cont Ops

A

126° C

63
Q

Min/Max Fuel Temp

A

-40/+52° C

64
Q

Eng Dry Motoring Ops

A

5 min on / 5 min off

65
Q

Eng Start Limits (1st - 4th Cycles)

A

1 min on / 1 min off

66
Q

Eng Start Limits (5th Cycle)

A

1 min on / 5 min off

67
Q

Eng Warm-Up

A

4 min for cold eng / 2 min for warm eng

68
Q

Engine is considered cold if shutdown for more than

A

90 mins

69
Q

Min Oil Temp to Increase N2 Above 83%

A

40° C / or run eng for 8 mins / or static runup to 88% N2 and ensure oil pressure is equal or less than 83 PSI

70
Q

Cold Weather Ops Restriction

A

Idle RPM max until press < 95 PSI

71
Q

Eng Cool Down

A

1 min @ idle/taxi speed before shutdown

72
Q

Maximum Differential Pressure

A

7.8 PSI

73
Q

Maximum Differential Overpressure

A

8.1 PSI

74
Q

Maximum Differential Negative Pressure

A

-0.3 PSI

75
Q

Maximum Temp for Anti-Icing Operations

A

10° C

76
Q

Minimum Temp for Manual Anti-Icing Operation

A

-40° C

77
Q

Single Engine or Single Bleed Max Altitude in Icing Conditions

A

15,000’

78
Q

Holding in Icing Conditions

A

Landing gear-up / Flaps up / Min airspeed 200 KIAS

79
Q

Icing Conditions

A

10° C or less and visible moisture

80
Q

APU Bleed as Pneumatic Source for Anti-Icing System

A

Do not use

81
Q

Maximum Airspeed for Windshield Wiper Operation

A

170 KIAS

82
Q

Min Engagement Height After Takeoff

A

500’

83
Q

Autopilot Coupled Approaches Approved Down to

A

200’

84
Q

Descent Below MDA on Non-Precision Approach with A/P Engaged

A

Prohibited

85
Q

Single Engine Go-Around With Autopilot Engaged

A

Prohibited

JSX Training Pack (11 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions