Limitations Flashcards

1
Q

Aircraft Length

A

103’ 11” (104’)

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2
Q

Aircraft Width

A

93’ 11” (94’)

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3
Q

Aircraft Height

A

32’ 4” (33’)

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4
Q

Max Passengers

A

76 (12 First, 64 Coach)

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5
Q

Cargo Compartment - FWD

A

3,306 lbs

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6
Q

Cargo Compartment - AFT

A

2,535 lbs

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7
Q

Minimum Crew

A

Left Seat Pilot and Right Seat Pilot

Captain and First Officer

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8
Q

Aircraft Operations

A
  • Day and Night
  • VFR and IFR
  • Icing Conditions
  • CAT I and CAT II
  • RVSM
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9
Q

Max Cabin Differential Overpressure

A

8.7 psi

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10
Q

Max Cabin Differential Pressure

Above FL370

A

8.3 psi

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11
Q

Max Cabin Differential Pressure

At or Below FL370

A

7.8 psi

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12
Q

Max Cabin Differential Negative Pressure

A

-0.5 psi

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13
Q

Max Cabin Differential for Takeoff and Landing

A

0.2 psi

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14
Q

Max Altitude Depressurized

A

10,000’ or MEA whichever is higher

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15
Q

Mmo (Above FL280)

A

0.82

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16
Q

Vmo (Above 10,000’ to FL280)

A

320 KIAS

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17
Q

Vmo (Below 10,000’)

A

250 KIAS (FAA Regulatory Speed, Structural Speed Limit is 300 KIAS)

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18
Q

Va

A

240 KIAS

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19
Q

Vle

A

250 KIAS

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20
Q

Vlo

A

250 KIAS

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21
Q

Vlr

A

250 KIAS

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22
Q

Vfe1

A

230 KIAS

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23
Q

Vfe2

A

215 KIAS

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24
Q

Vfe3

A

200 KIAS

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25
Q

Vfe4

A

180 KIAS

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26
Q

Vfe5

A

180 KIAS

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27
Q

VfeFull

A

165 KIAS

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28
Q

Max Turbulent Airspeed

Below 10,000’

A

250 KIAS

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29
Q

Max Turbulent Airspeed

10,000’ and Above

A

270 KIAS or .76 Mach

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30
Q

Max Crosswind for takeoff (Dry/Wet)

A

35 kts Dry, 30 kts Wet

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31
Q

Max Crosswinds for Landing

A
Poor: 8kts
Medium to Poor: 12kts
Medium: 15kts
Good to Medium: 20kts
Good: 31kts
38kts
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32
Q

Max Tailwind

A

10 kts

33
Q

Max DV Window Operation

A

160 KIAS

34
Q

Max Tire Speed

A

195 KIAS

35
Q

Max Windshield Wiper Speed

A

250 KIAS

36
Q

Max Operating Altitude

A

41,000’

37
Q

Max Altitude with Flaps Extended

A

20,000’

38
Q

Max Takeoff and Landing Elevation

A

8,000’

39
Q

Min Takeoff and Landing Elevation

A

-1,000’

40
Q

Min/Max Takeoff and Landing

Temperature (SAT)

A

-40 degrees C / 52 degrees C

41
Q

APU name

A

Sundstrand APS 2300

42
Q

APU Starting limits

A

1st and 2nd Start Attempt - START/ON then 60 sec. OFF

3rd Start Attempt - START/ON then 5 min. OFF

43
Q

APU Min Operation Temp

A

-54 degrees C

44
Q

APU Max Operation Temp

A

ISA +35 degrees C

45
Q

APU EGT (Start)

A

1032 degrees C

46
Q

APU EGT (Continuous)

A

717 degrees C

Note: No time limit in amber on the ground/inflight from 662C to 717C

47
Q

APU Max Operation Altitude

Electrical

A

33,000’

48
Q

APU Max Start Altitude

A

30,000’

49
Q

APU Max Operation Altitude

Eng. Start Assist

A

21,000’

50
Q

APU Max Operation Altitude

ECS Bleed

A

15,000’

51
Q

APU Max Rotor Speed

A

108%

52
Q

Autopilot Min Engagement Alt

A

Above 400’

53
Q

Autopilot Min Engaged Alt

A

Above 50’

54
Q

Engine name

A

GE CF34-8E5

55
Q

Engine max N1

A

100%

56
Q

Engine max N2

A

100%

57
Q

Engine Max Start ITT

A

815 degrees C

58
Q

Engine Max Normal T/O ITT

A

965C (2 min) / 949C (3 min) [Total - 5 min]

59
Q

Engine Max T/O and G/A ITT

A

1006C (2 min) / 990C (3 min) [Total - 5min]

60
Q

Engine Min/Max Oil Pressure

A

25 psi / 95 psi

61
Q

Engine Continuous Oil Temp

A

155 degrees C

62
Q

Engine Transient Oil Temp

A

163 degrees C (15 min limit)

63
Q

Engine Thrust: T/O-1 / OEI ATTCS

A

T/O-1 = 13,000 lbs / OEI ATTCS = 14,200 lbs

64
Q

Engine Thrust: T/O-2 / OEI ATTCS

A

T/O-2 = 11,800 lbs / OEI ATTCS = 13,000 lbs

65
Q

Fuel types

A
  • Brazilian - QAV1
  • ASTM - Jet A or A1
  • American - JP8
66
Q

Max Fuel Capacity

A

20,934 lbs (10,467 lbs per tank)

67
Q

Max Useable Fuel Quantity

A

20,784 lbs (10,392 lbs per tank)

68
Q

Unusable Fuel Quantity

A

150 lbs (75 lbs per tank)

69
Q

Maximum Fuel Imbalance

A

800 lbs

70
Q

Minimum Fuel Tank Temp

A

-40 degrees C

71
Q

Crossfeed Operation

A

Crossfeed Knob must be OFF for Takeoff and Landing

72
Q

Starter Limits (Dry Motor)

A

1st - Max 90 sec, 5 min cooldown
2nd to 5th - Max 30 sec, 5 min cooldown
(After 5 seq dry motors, 15 min cooldown)

73
Q

Starter Limits (Normal)

A

1st and 2nd - 90/120sec (Grd/Flt), 10 sec Cool-down

3rd to 5th, 90/120sec (Grd/Flt), 5 min Cool-down

74
Q

Taxi and Ramp Weight

A

85,800

75
Q

Takeoff Weight (MTOW)

A

85,500

76
Q

Landing Weight (MLW)

A

74,900

77
Q

Zero Fuel Weight (MZFW)

A

69,800

78
Q

Maximum allowable in-flight difference between Captain and FO altimiters for RVSM

A

200ft

79
Q

Max reverse thrust is not permitted below __ KIAS during normal operations

A

60