Limitations Flashcards

0
Q

Starter Limitations

Battery Limitations

A

Starter - 3/30min with a 90sec rest between.

Battery - 3/60min

  • X gen starts = 1/3 batt start
  • EXT Pwr = 0 batt starts
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1
Q
Max Ramp Weight?
Max Takeoff Weight?
Max Landing Weight?
Max Zero Fuel Weight?
Max Tailcone Baggage Weight?
A

XL. XLS
RAMP. 20,200#’s. 20,400#’s
T/O. 20,000#’s. 20,200#’s
Landing. 18,700#’s. 18,700#’s
ZERO fuel. 15,000#’s. 15,100#’s
Bagg. 700#’s. 700#’s

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2
Q

Max fuel imbalance

A

Normal - 400lbs
Emergency - 800lbs
Note - tank to tank transfer rate is aprox 700-900pph with engines shut down. (DC pump only, no motive flow valve with engines shutdown)
With eng operating, transfer rate depends on engine demands.

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3
Q

Speed limitations
Vmo (26,515’?
Vfe F7-15?
Vfe F35?

A
260kts
305kts
.75M
200kts
175kts
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4
Q

Speed limitations
Vle - Max Gear Extended speed?
Vle - Max Gear Extending Speed?
Vle - Max Gear Retracting Speed?

A

Max Gear Extended 250kts
Max Gear Extending 250kts
Max Gear Retracting 200kts

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5
Q

Min indicated airspeed in sustained icing (except approach and landing)?

A

160kts

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6
Q

Speedbrake limitations

Max speed for operation?

A

No limit

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7
Q

Autopilot limitations
Max Speed?
Min altitude for use enroute?
Min altitude for use on Non-Precision approach?
Min altitude for use on precision approach?

A

305KIAS or M.75
1000’ AGL
300’ AGL
180’ AGL

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8
Q

Max Operating Altitude?
Max Altitude for takeoff and landing?
Max Operating Altitude with up to 3 vortex generators?

A

FL 450
14,000’
FL 410

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9
Q

Max Generator Loads
Ground?
Airborne?

A

200A

300A

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10
Q

External power limitations
DC Volts?
DC Amps?

A

28VDC

800-1000A

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11
Q
APU Limitations
Max Starting Altitude?
Max Operating Altitude?
Max Generator Amps - Ground?
Max Generator Amps - Airborne?
Starter Cycles?
A
20,000'
30,000'
200A
300A
3/30mins with 90sec rest between
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12
Q

Cabin Pressurization
Normal?
Press Relief Valve?
Gauge Redline?

A
  1. 0-9.6PSI
  2. 5PSI
  3. 7PSI
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13
Q

Thrust Reverser Limitations
Max Deploy Time?
Max Thrust Reverse Power?
Landing Roll Idle Detent by?

A

3min/10min period
75% of takeoff thrust
60KIAS

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14
Q

Tail De-Ice Boots Limitations
Min Temp below 150kts?
Min Temp above 150kts?

A
  • 40C

- 35C

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15
Q

Anti-skid requirments

A

MUST be operational for takeoff and landing

16
Q
Takeoff and Landing Limitations
Max altitude?
Max Tailwind Component?
Max ambient temp?
Max tire ground speed?
LAV doors?
Autopilot & Yaw Damp?
A
14,000'
10kts
ISA+39C
165kts
Open for takeoff and landing
OFF for takeoff and landing
17
Q

Fuel Boost pumps on when?

A

Low fuel lights illuminate, or at 400lbs or less

18
Q

Max time for pitot/static on during ground operations?

A

2mins