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STUDY > Limitations > Flashcards

Limitations Flashcards

1
Q

Vne

A

BW = 205 KIAS / 218 KTAS
SW = 230 KIAS
198 KIAS (Seavue)

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2
Q

Va

A

BW = 144 KIAS (3.5 kts/500 lb decrease)

SW = 158 KIAS (4.5 kts/500 lb decrease)

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3
Q

Vfe

A

BW = CL 0.6 + 4 KIAS

SW = 134 KIAS

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4
Q

Vlo

A

135 KIAS

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5
Q

Vle

A

BW = 150 KIAS

SW = 160 KIAS

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6
Q

Maximum Wind Limitations:

Total Wind Takeoff/Landing
Gust Factor
Crosswind
Tailwind

A

30 kts
20 kts
BW = 17 kts, SW = 20 kts
10 kts

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7
Q

Maximum Ramp Weight

A

BW = 12,500 lbs

SW = 10,500 lbs

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8
Q

Maximum Landing Weight

A

BW = 10,500 lbs

SW = 8,500 lbs

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9
Q

Maximum Fuel Weight

A

BW = 6,074 lbs

SW = 3,800 lbs

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10
Q

Maximum Recommended AOA operating Range

A

-6 degrees to +10 degrees

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11
Q

KU Band pitch operating range
KU Band roll operating range

A

+/- 10 degrees
+/- 20 degrees

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12
Q

SAS Limitations Pitch
SAS Limitations Roll

A

+/-25 degrees
+/- 40 degrees

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13
Q

Max Torque (900 HP)

A

108% Maximum (DEEC Mode)

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14
Q

Max RPM

A

105.5% for 30 seconds (normal)

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15
Q

Max EGT

A

770 C (1 second during start)
730 C (CBP)
675 C (during flight)

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16
Q

Min Oil Temp at Start
Min Oil Temp
Caution Oil Temp
Max Oil Temp

A

-40 C
56 C
116 C
119 C

17
Q

Min Oil Pressure
Max Oil Pressure

A

44 psi
126 psi

18
Q

Min Fuel Feed Pressure
Max Fuel Feed Pressure

A

16 psi
60 psi

19
Q

Min Interstage Fuel Pressure
Max Interstage Fuel Pressure

A

20 psi
85 psi

20
Q

Min Fuel Temperature
Max Fuel Temperature

A

-30 C
+55 C

21
Q

Minimum Runway Length

A

6,000 ft

22
Q

Lockout/ Lost Link Logic

A

50 kts

23
Q

Min Fuel

A

400 lbs

24
Q

Emergency Fuel

A

250 lbs

25
Q

Fuel Burn Planning

A

200 lbs/hr

26
Q

VITs:
Software Version
Temps/Volts
Payload Data
Op/Emergency Mission
GPS P Code
Fuel

A

0
8/9
11
17/18
23
48

27
Q

MTS Limits

A

-54 C (on for 10 min prior to below -40 C)

28
Q

LTM Eye Safe Range

A

324 meters

29
Q

How far should personnel be away from aircraft if Ku TX RF is enabled?

A

70 feet due to radiation hazard (use strobes as a warning signal)

30
Q

What is the ASM definition of a stable approach?

A

Within 1 NM of threshold to 200’ HAT:
Airspeed = Vref +15/-10 KIAS
No full-scale deflection of GLS

Within 200’ HAT:
Airspeed = Vref +10/-5 KIAS
No full-scale deflection of GLS

31
Q

Taxi Speed Limits

Smooth Surface
Smooth Surface (>10,000lbs)
Irregular Surface

A

Smooth Surface = 20 kts
Smooth Surface (>10,000lbs) = 10 kts
Irregular Surface= 5 kts

32
Q

Taxi Turn Limits

Normal, symmetrical load
Asymmetrical load or >10,000 lbs

A

Normal, symmetrical load = 8 kts
Asymmetrical load or >10,000 lbs = 5 kts

33
Q

Enhanced Taxi Speed Limits

A

Centerline = 15 kts
Heading = 10 kts

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