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Falcon 20 F retrofit > Falcon 20 F retrofit limitations > Flashcards

Falcon 20 F retrofit limitations Flashcards

1
Q

Atmospheric temperature limits at FL 420?

A

-35 to -70

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2
Q

Nose wheels must be equipped with

A

chined tires

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3
Q

Takeoff and Landing altitude limitation

A

10,000ft

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4
Q

Minimum engine oil temperature for exceeding idle power?

A

30º C

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5
Q

Maximum landing gear extended speed Vle?

A

220 its

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6
Q

ITT maximum continuous?

A

968º

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7
Q

Maximum windshield wiper operating speed?

A

180 kts

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8
Q

Using landing gear emergency extension system will not restow the inner gear doors. The maximum operating speed in this condition is:

A

190 kts

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9
Q

External access baggage limit?

A

165 lbs

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10
Q

Hydraulic fluid approved?

A

MIL - 5606

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11
Q

731-5BR-2C Engine trust ratings?

A

Takeoff - 4750 lbs thrust

Max Continuous - 4634 lbs

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12
Q

Maximum landing gear operating speed Vlo?

A

190 kts

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13
Q

Wing anti-icing must not be used . . .

A
  1. With ram air temp in excess of 10ºC (50ºC)

2. On the ground except for a maintenance check.

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14
Q

Maximum speed for use of sliding pilot window?

A

160 its

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15
Q

Maximum speed with flaps at 25 degrees?

A

190 kts

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16
Q

Maximum operating altitude?

A

FL 420

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17
Q

MMO maximum?

A

Mach .865

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18
Q

For what type of flight activities is the airplane approved?

A
  1. Day and night VFR and IFR
  2. Extended overwater
  3. Icing Conditions
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19
Q

Minimum flight crew?

A

2

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20
Q

Maximum number of pax?

A

10

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21
Q

Flight maneuvering load acceleration limits flaps extended?

A

+2 - 0 g’s

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22
Q

Maximum N1?

A

Takeoff - 100%

Transient Max Allowable - 103% for 5 seconds.

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23
Q

Maximum landing weight?

A

28,880 lbs

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24
Q

ITT Maximum Take off temp?

A

978º and 996 with APR on

25
Q

Engine start during windmilling air start must reach 60% N2 in . . .

A

45 seconds max

26
Q

Engine oil pressure idle?

A

25 - 46 psi

27
Q

Pressure fueling should not exceed . . .

A

50 psi

28
Q

Atmospheric temperature limits at sea-level

A

-55 to 48ºC

29
Q

Engine oil temperature maximum limits?

A

140º C above 30,000 ft with an overshoot to 149 allowable for 2 minutes max.

30
Q

APS 85 Autopilot can be used en-route at the minimum height of?

A

1000 ft agl

31
Q

VMO maximum at FL200 ?

A

380 kts

32
Q

Engine oil pressure Take-off?

A

38 - to 46 psi

33
Q

Ground start from Light off to idle must be no more than _________ seconds.

A

60 seconds

34
Q

VMO maximum at sea-level?

A

350 kts

35
Q

Maximum N2?

A

100.8% continuous and 103% max overshoot for 5 seconds

36
Q

Tires must be qualified for a minimum ground speed of?

A

182 kts

37
Q

Flap Speed maximum 40 Degrees?

A

180 kts

38
Q

“OIL 1” or “OIL 2” will illuminate on warning panel if engine oil pressure falls below . . .?

A

25 psi

39
Q

Wing and Engine anti-icing must not be used with a ram air temperature in excess of . . .?

A

10º C

40
Q

Vmcg is defined as the minimum speed, whilst on the ground, that directional control can be maintained, using only aerodynamic controls, with one engine inoperative, and takeoff power applied on the other engine(s). What is this speed?

A

110.5 kts

41
Q

Engine synchronizer is not to be used . . .?

A

For takeoff, landing or missed approaches

42
Q

During ground start or starter assist air start the time from 10% N2 to light off should be no more than . . .

A

10 seconds

43
Q

Va -Full application of rudder or aileron controls, as well as maneuvers that involve angles-of-attack near the stall must be confined to speeds below

A

200 kts

44
Q

Airbrakes may not be extended below . . .

A

500 ft agl

45
Q

ITT Maximum for starting

A

978º C

46
Q

Maximum airbrake operating and extended speed?

A

No Limitations

47
Q

What is Va speed?

A

200 kts

48
Q

Flight maneuvering load acceleration limits with flaps retracted?

A

2.5 to -1 g’s

49
Q

VMCA is defined as the minimum speed, while in the air, at which directional control can be maintained with one engine inoperative and the operating engine at takeoff power. What is this speed?

A

105.5 kts

50
Q

Takeoff and Landing tailwind limit

A

10 kts

51
Q

Maximum cabin differential

A

8.5 psi

52
Q

Maximum Takeoff Weight

A

30,325 lbs

53
Q

APS-85 autopilot may be used for approaches down to a minimum height of . . .

A

100 ft provided the radar altimeter is operational, 150 ft if it is not.

54
Q

Minimum flight weight?

A

18,320 lbs

55
Q

Maximum ramp weight?

A

30,500 lbs

56
Q

Takeoff and Landing runway slope limit?

A

2%

57
Q

Maximum Speed at Flaps 10º?

A

190 kts

58
Q

Zero Fuel Weight?

A

22,500 lbs

59
Q 
Maximum Ramp weight \_\_\_\_\_\_\_\_
Maximum Takeoff weight \_\_\_\_\_\_\_\_\_\_
Maximum Landing weight \_\_\_\_\_\_\_\_\_\_\_
Zero Fuel weight \_\_\_\_\_\_\_\_\_\_\_\_
Minimum Flight weight \_\_\_\_\_\_\_\_\_\_\_
A 
Max Ramp - 30,500 lbs
Max Takeoff - 30,325 lbs
Max Landing - 28,820 lbs
Zero Fuel - 22,500 lbs
Minimum Flight - 18,320 lbs

Falcon 20 F retrofit (10 decks)

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