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Premier questions Flashcards

(65 cards)

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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
Maximum Generator Current
300A
26
Maximum Airport ElevationTake-Off and Landing
14,000 FT
27
Maximum Tailwind
10 KTS
28
Demonstrated Crosswind
29 KTS
29
Maximum Water / Slush Depth on Runway
0.5 IN
30
Maximum Tire Speed
165 KTS
31
Minimum Ambient Temperature
-54o C
32
Maximum Ambient Temperature
ISA +39o C (takeoff and landing)
33
Freon A/C
Must be off for start and above FL180
34
Autopilot and Yaw Damper
Must be off for Take-Off and Landing
35
Vertical Navigation
Must be off below 500 FT AGL
36
Maximum Crosswind with Thrust Reversers
25 KTS
37
Oil Tank
2.08 GAL1.21 USABLE
38
Oxygen
22 / 60 / 64 CU FT623 / 1700 / 1812 CU LLocated in Tailcone
39
Hydraulics
.65 GAL
40
Hydraulic Brake Reservoir
.25 GAL
41
Windshield Alcohol
.5 GAL
42
TKS Reservoir
7.1 / 7.5 / 8.6 GAL
43
VMO - SL - 8,000 FT
261 KTS
44
VMO - 8,000 FT - FL 29,315
276 KTS
45
MMO above 29,315
.721 M
46
VFE - FULL/35o
172 KTS
47
VFE-PART/20o
200 KTS
48
VLE
172 KTS or VMO
49
VLO
172 KTS or250 KTS (extend) / 200 KTS (retract)if SBS550-32-8 appliedIncreased maximum gear extended speed
50
VSB (speed brakes)
No speed limit but,must be stowed by 50 FT AGL
51
Maximum A/P operating speeds
VMO - 261 KTS or 276 KTS (altitude)or MMO - .721 M
52
VMCA
83 KTS
53
VMCG
73 KTS
54
VA
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
Minumum Speed in Sustained Icing
160 KTS
56
Pressure Diferential
8.5 PSI
57
Typical Cruise Altitudes
FL 330 - FL 400
58
Normal Cabin Pressure Differential Range
0.0 - 8.8 PSI
59
Aborted Take-Off
If speed above 50 KTS,refer to AFM for turnaround time.
60
Fuel Capacity
862 GAL5,875 LBS @ 6.82 LBS/GAL5,818 LBS @ 6.75 LBS/GAL (standard)5,750 LBS @ 6.67 LBS/GAL
61
Maximum Fuel Imbalance
200 LBS (normal)600 LBS (emergency)
62
Main gear tire pressure
120 +/-5 PSI
63
Nose gear tire pressure
120 +/-5 PSI
64
Jet A minimum temperature
-23oC
65
Minimum fuel level annunciated
185 LBS

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