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Premier questions Flashcards

1
Q

Maximum Ramp Weight

A

14,900 LBS

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2
Q

Maximum Takeoff Weight

A

14,700 LBSMaximum takeoff weight may be additionally restricteddue to altitude, temperature, and field length.Takeoff weight is limited by most restrictive of:

  • Maximum certified takeoff weight
  • Maximum takeoff weight permitted by climb requirments
  • Takeoff field length
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3
Q

Maximum Landing Weight

A

14,000 LBSMaximum landing weight may be additionally restricteddue to altitude, temperature, and field length.Landing weight is limited by most restrictive of:

  • Maximum certified landing weight
  • Maximum landing weight permitted by climb requirments or brake energy limits
  • Landing distance
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4
Q

Maximum Zero Fuel Weight

A

11,000 LBS

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5
Q

Engine Model

A

Pratt and WhitneyJT15D-4B

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6
Q

Thrust Generated (per Engine)

A

2500 LBS

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7
Q

Engine Bypass Ratio

A

2.6 : 1

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8
Q

Maximum Fan N1

A

106.0 %

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9
Q

Maximum Turbine N2

A

97.0 %

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10
Q

Maximum Start ITT

A

700o C (2 sec.)

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11
Q

Maximum Continuous ITT

A

680o C

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12
Q

Idle ITT

A

580o C (typical)

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13
Q

Transient (acceleration) ITT

A

710o C

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14
Q

Maximum Temperature for Engine Start

A

ISA +39o C

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15
Q

Starter Limits

A

3 attempts in 30 minutes,with 30 seconds rest between

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16
Q

Battery Limits for Starting

A

3 starts per hour

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17
Q

Minimum Oil Pressure

A

35 PSI (idle)

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18
Q

Maximum Oil Pressure

A

85 PSIG

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19
Q

Minimum Oil Temperature

A

-40o C (starting and idle)

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20
Q

Maximum Oil Temperature

A

121o C

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21
Q

Minimum Fuel Temperature for Start

A

-23o C (Jet A)-54o C (Jet B)

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22
Q

Minimum Battery Voltage

A

24V DC

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23
Q

External Power Unit Limits

A

28V DC (no load) / Maximum 1000A output

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24
Q

Minimum Ambient OAT for Battery Start

A

-18o C

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25
Q

Maximum Generator Current

A

300A

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26
Q

Maximum Airport ElevationTake-Off and Landing

A

14,000 FT

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27
Q

Maximum Tailwind

28
Q

Demonstrated Crosswind

29
Q

Maximum Water / Slush Depth on Runway

30
Q

Maximum Tire Speed

31
Q

Minimum Ambient Temperature

32
Q

Maximum Ambient Temperature

A

ISA +39o C (takeoff and landing)

33
Q

Freon A/C

A

Must be off for start and above FL180

34
Q

Autopilot and Yaw Damper

A

Must be off for Take-Off and Landing

35
Q

Vertical Navigation

A

Must be off below 500 FT AGL

36
Q

Maximum Crosswind with Thrust Reversers

37
Q

Oil Tank

A

2.08 GAL1.21 USABLE

38
Q

Oxygen

A

22 / 60 / 64 CU FT623 / 1700 / 1812 CU LLocated in Tailcone

39
Q

Hydraulics

40
Q

Hydraulic Brake Reservoir

41
Q

Windshield Alcohol

42
Q

TKS Reservoir

A

7.1 / 7.5 / 8.6 GAL

43
Q

VMO - SL - 8,000 FT

44
Q

VMO - 8,000 FT - FL 29,315

45
Q

MMO above 29,315

46
Q

VFE - FULL/35o

47
Q

VFE-PART/20o

48
Q

VLE

A

172 KTS or VMO

49
Q

VLO

A

172 KTS or250 KTS (extend) / 200 KTS (retract)if SBS550-32-8 appliedIncreased maximum gear extended speed

50
Q

VSB (speed brakes)

A

No speed limit but,must be stowed by 50 FT AGL

51
Q

Maximum A/P operating speeds

A

VMO - 261 KTS or 276 KTS (altitude)or MMO - .721 M

52
Q

VMCA

53
Q

VMCG

54
Q

VA

A

145 KTS - 274 KTSDepending on weight and altitude SL - 145 - 194 20,000 FT - 146 - 206 5,000 FT - 145 - 196 25,000 FT - 148 - 23710,000 FT - 145 - 198 30,000 FT - 151 - 270 15,000 FT - 146 - 199 35,000 FT - 162 - 242

55
Q

Minumum Speed in Sustained Icing

56
Q

Pressure Diferential

57
Q

Typical Cruise Altitudes

A

FL 330 - FL 400

58
Q

Normal Cabin Pressure Differential Range

A

0.0 - 8.8 PSI

59
Q

Aborted Take-Off

A

If speed above 50 KTS,refer to AFM for turnaround time.

60
Q

Fuel Capacity

A

862 GAL5,875 LBS @ 6.82 LBS/GAL5,818 LBS @ 6.75 LBS/GAL (standard)5,750 LBS @ 6.67 LBS/GAL

61
Q

Maximum Fuel Imbalance

A

200 LBS (normal)600 LBS (emergency)

62
Q

Main gear tire pressure

A

120 +/-5 PSI

63
Q

Nose gear tire pressure

A

120 +/-5 PSI

64
Q

Jet A minimum temperature

65
Q

Minimum fuel level annunciated

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