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Ultra Memory Items > Limitations > Flashcards

Limitations Flashcards

1
Q

Minimum Crew:

A
  • Pilot and Copilot
  • The Pilot Must Have A CE-500 Type Rating And Meet The Requirements Of FAR 61.58
  • The Copilot Shall Possess A Multi-engine Rating, An Instrument Rating For Flight Above Or Into IMC And Meet The Requirements Of FAR 61.55
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2
Q

Baggage Limits:

A

Aft Cabin Storage Compartment: 600 LBS
Tailcone Baggage Compartment:500 LBS
Nose Baggage Compartment: 350 LBS

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3
Q

Passenger Seat Position:

A

For Takeoff and Landings, the following apply:

  • Seat Must Be Fully Upright And Outboard
  • Passenger Seat Belts And Shoulder Harnesses Must Be Fastened
  • The Seat Just Aft Of The Emergency Exist Must Be In Most Aft Position
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4
Q

Maximum Taxi and Ramp Weight:

A

16,500 Pounds

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5
Q

Maximum Takeoff Weight:

A

16,300 Pounds

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6
Q

Maximum Landing Weight:

A

15,200 Pounds

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7
Q

What is the Maximum Zero Fuel Weight:

A

12,200 Pounds

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8
Q

Maximum Flaps Extended (VFE ) for:

A 
Full Flaps (35°) : 173 KIAS
Partial Flaps (7° or 15°): 200 KIAS
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9
Q

Maximum Landing Gear Extended Speed (VLE):

A

292 KIAS

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10
Q 
Maximum Landing Gear
Operating Speed (VLO):
A 
Extending = 250 KIAS
Retracting = 200 KIAS
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11
Q

VMCA (Minimum Control - Air):

A

85 KIAS

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12
Q

VMCG (Minimum Control - Ground):

A

86 KIAS

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13
Q

Maximum VMO Below 8,000 Feet:

A

261 KIAS

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14
Q

Maximum VMO Between 8,000 and 28,907 Feet:

A

292 KIAS

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15
Q

Maximum MMO (Above 28,907 Feet):

A

0.755M Indicated

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16
Q

Maximum Speedbrake Extension (VSB):

A

NO LIMIT

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17
Q

Maximum Autopilot Operation (Speed):

A

292 KIAS or 0.755M

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18
Q

Maximum Airport Pressure Altitude for Takeoff and Landing:

A

14,000 Feet

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19
Q

Maximum Air Temperature Approved for Takeoff and Landing:

A

ISA + 39°C

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20
Q

Maximum Crosswind - Demonstrated:

A

20 KTS

21
Q

Maximum Tailwind Component:

A

10 KTS

22
Q

Maximum Tire Ground Speed

A

165 KTS

23
Q

Maximum Water/Slush on the Runway:

A

0.5 Inch

24
Q

Vertical Navigation (VNAV) System Must be OFF Below:

A

500 Feet AGL

25
Q

Minimum Airspeed for Sustained Flight in Icing Conditions (Except for Approach and Landing):

A

160 KIAS

26
Q

Maximum Calibrated Operating Altitude:

A

45,000 Feet

27
Q

Generator Load in Flight

A

300 Amps

28
Q

Maximum Load Factor in Flight for Flaps UP

A

-1.44 to +3.6G at 16,300 LBS

29
Q

Maximum Load Factor in Flight for Flaps 7° to 35°

A

-0.0 to +2.0G at 16,300 LBS

30
Q

Maximum Load Factor for Landing, Flaps 15° to 35°

A

+3.5G at 15,200 LBS

31
Q

Minimum Altitude for Autopilot Use:

A
  • 1,000 ft AGL – Enroute
  • 300 ft AGL - Non-Precision Approach
  • 180 ft AGL - Approaches
    The autopilot and yaw-damper must be off for takeoff and landing.
32
Q

Which Standby Instruments Must be

Functioning for Takeoff?

A
  • ATT
  • ALT/ASI
  • HSI
    A Satisfactory Preflight Test Must be Accomplished on the Standby Gyro System
33
Q

Generator Load ground

A

125 Amps at 46% N2

225 Amps at 52% N2

34
Q

Battery Limitations for Engine Starts

A
  • Three Engines Starts per Hour
  • Three Generator-Assisted, Cross-Starts Equal One Battery Start
  • GPU Start Does NOT Count as a Battery Cycle
35
Q

STARTER Limitations for Engine Starts

A

With Battery as Starter Power Source:
- Three Engine Starts per 30 Minutes with a 30- Second Rest Period Between Cycles
With GPU or Generator-Assisted, Cross-Start:
- TWO Engine Starts per 30 Minutes with 30- Second Rest Period Between Cycles

36
Q

What are the Voltage considerations when

using GPU for engine starts?

A

Use of GPU with a voltage in excess of 28V DC or current in excess of 1,000 amps may damage the starter.

37
Q

Maximum Pressure Differential

A

8.9 psid, +0.1 or -0.1 psid

38
Q

The Stall Warning System:

A

Must be Verified Operational for Takeoff per the Preflight Test in the AFM

39
Q

What Are the Maximum Asymmetric Fuel Weights for Normal and Emergency Conditions?

A
  • Normal: 200 lbs

- Emergency: 600 lbs

40
Q

Pitot/Static Heat Permissible Operating Time

A

Limit Ground Operations of Pitot/Static Heat to 2 MINUTES to Preclude Damage to the Pitot/Static Tubes and the Angleof-Attack Probe

41
Q

When Must All Anti-Ice Systems Be Turned On?

A

Operating in Visible Moisture and When TAT/RAT is Below +10Flight Idle 52(min) 580

42
Q

Continuous Use of the Supplemental Oxygen System is Prohibited Above the Following CABIN Altitudes:

A
  • Carrying Passengers - 25,000 ft

- Crew Only - 40,000 ft EROS

43
Q

Reverse Thrust Must be Reduced to Idle Reverse by Which Speed

A

60 KIAS

44
Q

Maximum Reverse Thrust is Limited to:

A

Fan Speed

  • 86% for Ambient Temperatures Above -18°C
  • 79% for Ambient Temperatures Below -18°C
45
Q

Additional Thrust Reverser Limitations

A
  • Must be Verified Operational Per Preflight Test
  • Prohibited During Touch and Go Landings
  • Prohibited on Sod or Gravel Runways
  • Max. Deployment Time is 15 Minutes in Any One-Hour Period
46
Q

Powerplant Operating Limits

JT15D-5D Engines

A

N1 N2 ITT Time
Takeoff 100.0 97.0 720°C 5 Min
Start – – 550°C 700°C

47
Q

APPROACH AND LANDING IN ICING CONDITIONS

A

When any residual ice is present or can be expected during approach and landing, engine anti-ice must be on to maintain adequate stall warning margin.

48
Q

Minimum oil temperature for starting

A

-40°C

49
Q

Thrust Reverser Depoyment

A

The nosewheel must be in firm contact with the ground prior to deploying thrust reversers

Ultra Memory Items (3 decks)

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