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Falcon 50EX Limitations > Falcon 50EX Limitations > Flashcards

Falcon 50EX Limitations Flashcards

1
Q

Baggage Limit

A

2,205 lbs and floor loading limit of 123 lbs / sqft.

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2
Q

Maximum Passengers

A
  • Depending on accommodation, within the limit of 19 passengers maximum authorized by the emergency exits
  • Max pax for flight above 45,000ft = 12
  • The loading manual provides approved interiors accommodating 10 passengers using the third crew member seat.
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3
Q

Max Ramp Weight

A

40,780 lbs.

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4
Q

Max Takeoff Weight

A

40,780 lbs.

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5
Q

Max Landing Weight

A

35,715 lbs

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6
Q

Max Zero Fuel Weight

A

25,570 lbs

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7
Q

Minimum Flight Weight

A

18,959 lbs

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8
Q

Vfe Slats Extended

A

200 KIAS

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9
Q

Ffe Slats Extended+Flaps 20

A

190 KIAS

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10
Q

Vfe Slats Extended+Flaps 48

A

175 KIAS

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11
Q

Max Altitude for Slats or Flaps Extended

A

20,000 ft

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12
Q

Max Landing Gear Extended Speed (Vle/Mle)

A

220 KIAS / 0.75 M

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13
Q

Max Landing Gear Operating Speed (Vlo/Mlo)

A

190 KIAS / 0.70 M

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14
Q

Minimum Control Speed (Vmca)

A

82.5 KCAS

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15
Q

Max Operating Speed (Vmo/Mmo)

A
  • 350 KIAS @ sea level, increasing linearly to 370 KIAS at 10,000 ft.
  • 370 KIAS from 10,000 ft. to 24,000 ft.
  • Mmo - 0.86 M above 24,000 ft.
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16
Q

Maneuvering Speed (Va)

A

210 KIAS CAUTION: Full application of rudder and aileron controls, as well as maneuvers that involve (AOA) near the stall, must be confined to speeds below Va. Rapidly alternating large rudder applications in combination with large sideslip may result in structural failure at any speed.

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17
Q

Max Airport Pressure Altitude

A

-1,000 ft. through +14,000 ft.

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18
Q

Max Tailwind

A

10 Kts

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19
Q

Max Tire Ground Speed

A

180 Kts

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20
Q

Maneuvering Flight Load Factors?

A

Flaps Up……….+2.6 to -1
Flaps Down……….+2 to Zero
Note: These load factors limit the angle of band permitted in turns and limit the severity of pull-up maneuvers.

21
Q

Max Operating Altitude

A

49,000 ft.

22
Q

Min autopilot use height after takeoff?

A

1,000 ft.

23
Q

Min autopilot use hight in cruise?

A

1,000 ft.

24
Q

Min autopilot use height for non-precision approach?

A

160 ft.

25
Q

Min autopilot use height for precision approach?

A

80 ft.

26
Q

Note: The autopilot must not be engaged for takeoff or landing.
Takeoff is not permitted with the yaw damper not centered.

A

Note: The autopilot must not be engaged for takeoff or landing.
Takeoff is not permitted with the yaw damper not centered.

27
Q

The autopilot can be disengaged by any one of the following?

A
  1. Depressing the pilot or copilot control disengage button.
  2. Selecting the DISENGAGED position of the AP controller lever.
  3. Depressing either control wheel GO-AROUND pushbutton.
  4. Depressing either pitch trim button.
  5. Activating the TAILPLANE EMERG switch.
28
Q

Max Generator Output

A

Transient ( 1 min max) = 350 A
Up to 39,000 ft. = 300 A
Above 39,000 ft. = 250 A

29
Q

Max DC Voltage

A

32 VDC

30
Q

Battery Temperature:

A 
Amber Light (warm) at or above.....120*F
Red Light (hot) at or above.....150*F
On A/C with SB F50-295 or M2245:
Red Light (hot) at or above.....160*F
31
Q

Max Pressure Differential

A

9.5 psi (pressure relief setting)

32
Q

Airbrakes

A

Extension of the air brakes within 500 ft. from the round is not permitted.

33
Q

Max Slats Extended Speed

A

270 KIAS (With AUTO SLATS Light On)

34
Q

Fuel Anti-Icing Additives

A

Anti-icing additive, conforming to MIL- I -27686D/E (JP-4/JP-8) or MIL- I -85470 (JP-5) specifications or equivalent at a concentration not in excess of 0.15% by volume.

35
Q

Approved Hydraulic Fluid

A

Hydraulic fluids approved for use must conform to MIL-H-5606 specification (NATO codes H515 or H520)

36
Q

(Hydraulics) Max Altitude for Standby Pump Operation

A

45,000 ft.

37
Q

Engine Anti-Ice Limitations

A

The engine anti-ice system must not be used with TAT in excess of +10C (50F)

38
Q

Wing Anti-Ice Limitations

A

The wing anti-ice system must not be used with TAT in excess of +10C (50F)

39
Q

Minimum Oxigen Pressure

A

Below 10,000 without passengers = 650 psi

Minimum Two Crew with 10 or Fewer Passengers to FL 410 = 700 psi

40
Q

APU Speed Limitation

A

Max rated = 100%
Max allowed = 107%
Note: The APU must be operated on the ground only

41
Q

APU Exhaust Gas Temperature Limit

A

Maximum rated = 680C (1,255F)

Maximum allowed = 732C (1,350F)

42
Q

APU Max Generator Output

A

300 A

43
Q

Powerplant Manufacturer / Model

A

Honeywell / TFE731-40

44
Q

Max Engine Rotor Speeds N1 and N2

A

Takeoff - Max continuous 100.1% N1….101% N2
Transient 10 sec max. allowable = 100.6%…..102.5% N2
100% N1 = 21,000 RPM and 100% N2 = 31,173 RPM

45
Q

Min/Max Oil Pressure: T/O, Climb, Max Continuous Power

A

Minimum 65 PSI

Maximum 80 PSI

45
Q

Min/Max Oil Pressure: IDLE

A

Minimum 50 psi

Maximum 80 psi

45
Q

Max Transient Oil Pressure

A

100 psi

46
Q

Max oil pressure:

A 
SL to 30,000 - 127c
Above 30,000 - 140c
Transient all altitudes -149c < 2min
Min oil temp to exceed idle power - 30c
Min oil temp = -40c

Falcon 50EX Limitations (1 decks)

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