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
Engine start during windmilling air start must reach 60% N2 in . . .
45 seconds max
26
Engine oil pressure idle?
25 - 46 psi
27
Pressure fueling should not exceed . . .
50 psi
28
Atmospheric temperature limits at sea-level
-55 to 48ºC
29
Engine oil temperature maximum limits?
140º C above 30,000 ft with an overshoot to 149 allowable for 2 minutes max.
30
APS 85 Autopilot can be used en-route at the minimum height of?
1000 ft agl
31
VMO maximum at FL200 ?
380 kts
32
Engine oil pressure Take-off?
38 - to 46 psi
33
Ground start from Light off to idle must be no more than _________ seconds.
60 seconds
34
VMO maximum at sea-level?
350 kts
35
Maximum N2?
100.8% continuous and 103% max overshoot for 5 seconds
36
Tires must be qualified for a minimum ground speed of?
182 kts
37
Flap Speed maximum 40 Degrees?
180 kts
38
"OIL 1" or "OIL 2" will illuminate on warning panel if engine oil pressure falls below . . .?
25 psi
39
Wing and Engine anti-icing must not be used with a ram air temperature in excess of . . .?
10º C
40
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?
110.5 kts
41
Engine synchronizer is not to be used . . .?
For takeoff, landing or missed approaches
42
During ground start or starter assist air start the time from 10% N2 to light off should be no more than . . .
10 seconds
43
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
200 kts
44
Airbrakes may not be extended below . . .
500 ft agl
45
ITT Maximum for starting
978º C
46
Maximum airbrake operating and extended speed?
No Limitations
47
What is Va speed?
200 kts
48
Flight maneuvering load acceleration limits with flaps retracted?
2.5 to -1 g's
49
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?
105.5 kts
50
Takeoff and Landing tailwind limit
10 kts
51
Maximum cabin differential
8.5 psi
52
Maximum Takeoff Weight
30,325 lbs
53
APS-85 autopilot may be used for approaches down to a minimum height of . . .
100 ft provided the radar altimeter is operational, 150 ft if it is not.
54
Minimum flight weight?
18,320 lbs
55
Maximum ramp weight?
30,500 lbs
56
Takeoff and Landing runway slope limit?
2%
57
Maximum Speed at Flaps 10º?
190 kts
58
Zero Fuel Weight?
22,500 lbs
59
``` Maximum Ramp weight ________ Maximum Takeoff weight __________ Maximum Landing weight ___________ Zero Fuel weight ____________ Minimum Flight weight ___________ ```
``` 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 ```