Limitations Flashcards

(51 cards)

0
Q

Minimum engine fuel temperature limit for t/o

A

5 C @ engine inlet

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1
Q

Jet A minimum temperature for bulk fuel t/o limit

A

-30 C

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2
Q

Minimum fuel for go around

A

600 lbs

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3
Q

Pressure refueling

Left
Right
Center
Total

A

Left-7,492
Right-7,492
Center-4,610
Total-19,594

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4
Q

Gravity total

A

14,810 lbs

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5
Q

Max fuel imbalance between main tanks

A

300 lbs @ t/o, 800 lbs @ other phases

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6
Q

Engine starter cranking limits (flight)

Attempt 1
&
Attempt 2-5

A

Attempt 1- 120 sec on, 10 sec off

Attempt 2-5- 60 sec on, 5 min off

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7
Q

Engine starter cranking limits (ground)

Attempt 1 and 2
Attempt 3-5

A

Attempt 1-2- 90 sec on, 10 sec off

Attempt 3-5- 90 sec on, 5 min off

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8
Q

Continuous ignition must be used…

A
  1. T/o & landing on contaminated runway
  2. Moderate or heavier rain
  3. Moderate or heavier turbulence
  4. Vicinity of thunderstorms
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9
Q

Minimum oil pressure minimum steady state

A

25 psi

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10
Q

Minimum oil temp for start

A

-40 C

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11
Q

Minimum temperature for t/o

A

ISA-40 C

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12
Q

Max temperature for t/o and landing

A

ISA+35 C

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13
Q

Max operating altitude

A

41,000 ft

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14
Q

Max cargo belly weight

A

850 lbs

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15
Q

Max cargo FWD weight

A

850 lbs

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16
Q

Mac cargo AFT weight

A

4,375 lbs

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17
Q

Minimum flight weight

A

45,000 lbs

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18
Q

Max zero fuel weight

A

70,000 lbs

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19
Q

Max landing weight

A

73,500 lbs

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20
Q

Max t/o weight

21
Q

Max ramp weight

22
Q

APU max operating altitude

23
Q

APU minimum battery voltage for start

24
APU minimum temp cold soaked start
-40 C
25
Mixing of certain fuel types is permitted?
True
26
Max cruise Mach # in RVSM
.82m
27
RVSM required equipment
1 autopilot 1 altitude alerting system 2 transponders 2 air data computers
28
When must reverse thrust be reduced to idle
60 kts
29
Autopilot altitude restrictions...
80 ft precision 110ft single-engine precision 400 ft non-precision/visual
30
Max single pack operating altitude
25,000 ft
31
Max negative differential pressure
-.5 psi
32
Max differential pressure
8.7 psi
33
Max windshield wiper speed
250 kts
34
Max crj 700 crosswind component
27 kts dry | 15 kts slippery
35
Max crj 900 crosswind component
22 kts dry | 15 kts slippery
36
Max gear retract speed
200 kts
37
Max gear operating speed
220 kts
38
Max gear extend speed
220 kts
39
Max turbulence speed
280 kts | .75m
40
Flap 45
170 kts
41
Flap 30
185 kts
42
Flap 20
220 kts
43
Flap 1-8
230 kts
44
Max tailwind component
10 kts
45
Max runway slope
+/- 2*
46
In flight icing procedure
Cowl anti ice on in icing conditions or ICE is annunciation by the ice detector system. Wing anti ice must be on when annunciated by the ice detection system or in icing conditions and IAS is less than 230 kts.
47
Ground icing procedure
Cowl anti ice on in icing conditions or when OAT 10 C or less and operating on runways and taxiways with snow ice slush or standing water. Wing anti ice on OAT less than 5 C or below and visible moisture is present (1 mile visibility or less) and OAT is 5 C or below and runway is contaminated.
48
APU max altitude to use bleed air for engine start
25,000 ft
49
APU max altitude for bleed air use
25,000 ft
50
APU max starting altitude
37,000 ft