Limitations Flashcards

(54 cards)

1
Q

Maximum Ramp and Taxi Weight:

A

Maximum Ramp and Taxi Weight: 85,000 lbs

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2
Q

Maximum T/O Weight:

A

Maximum T/O Weight: 84,500 lbs

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3
Q

Maximum Landing Weight:

A

Maximum Landing Weight: 75,100lbs

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4
Q

Maximum Zero Fuel Weight:

A

Maximum Zero Fuel Weight: 70,750 lbs

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5
Q

Minimum Flight Weight:

A

Minimum Flight Weight: 45,000 lbs

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6
Q

Maximum Cargo Weight:
Forward Cargo
NG

A

1700 lbs for both

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7
Q

How much time must the flight be within if cargo is carried in either compartment?

A

60 min

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8
Q

Turbulence Penetration Speed:

A

280 kts or M.75

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9
Q

Maximum Relief Differential Pressure (Delta P):

A

8.7 PSI

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10
Q

Maximum Negative Differential Pressure (Delta P):

A

-0.5 PSI

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11
Q

Max Diff. Pressure for Taxi, T/O and Ldg:

A

0.1 PSI

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12
Q

Maximum altitude for single PACK operation with 82 cabin occupants or less:

A

31,000 ft

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13
Q

Maximum altitude for single PACK operation with 83 cabin occupants or more:

A

25,000 ft

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14
Q

Autopilot engagement is prohibited…

A

Below 600 ft AGL

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15
Q

Autopilot engagement is prohibited at what altitude for visual and NPA?

A

400 ft AGL

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16
Q

Autopilot engagement is prohibited at what altitude for PA?

A

80 ft AGL

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17
Q

Autopilot engagement is prohibited at what altitude for 1 engine inop PA?

A

110 ft AGL

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18
Q

Autopilot engagement is prohibited at what altitude for APV approaches (CRG 900 NG)?

A

80 ft AGL

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19
Q

Autopilot engagement is prohibited at what altitude for 1 engine inop APV approaches (CRJ 900 NG)?

A

110 ft AGL

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20
Q

In the CRJ 900 NG what equipment mus tbe on board for RNAV approaches to LPV Minima?

A

1 FMS, 1 GPS & 2 PFD’s

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21
Q

AC Generator Altitude Range:

A

0 - 41,000 ft

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22
Q

AC Main Generator Load Limitation:

23
Q

AC APU Generator Load Limitation:

24
Q

Maximum Continous Load on each TRU:

25
Maximum Permissible Time with DC Power Only:
5 Min (Display Cooling)
26
Maximum speed for ADG Deployment:
Vmo/Mmo
27
Maximum Altitude for Slat/Flap Operation:
15,000 ft
28
Flap Operating Speeds (F1 - F45): Flaps 1 Flaps 8 Flaps 20 Flaps 30 Flaps 45
Flaps 1 - 230 KIAS **Same speeds for Vfe** Flaps 8 - 230 KIAS Flaps 20 - 220 KIAS Flaps 30 - 185 KIAS Flaps 45 - 170 KIAS
29
Minimum Altitude for Spoiler Use:
300 ft AGL
30
Fuel Quantities: Left/Right Main Tanks Center Tank Total
Left/Right Main Tanks: 7942 lbs Center Tank: 4610 lbs Total: 19594 lbs
31
Max Fuel Imbalance Between Main Tanks - T/O:
300 lbs
32
Max Fuel Imbalance Between Main Tanks - All Phases of Flight:
800 lbs
33
Minimum Fuel for a Go-Around in Each Main Tank:
600 lbs
34
Hydraulic System Pressure Range (Normal):
2800-3200 PSI
35
Hydraulic System Quantity Range (Normal):
45% - 85%
36
Maximum Operating Speed of the Windshield Wiper:
250 KIAS
37
What Temperature do COWLS need to be on?
10 Degrees or below and visible moisture, contaminated RWY or any Precipitation
38
What Temperature does Wing Anti ice need to be on?
5 Degrees or below and visible moisture, contaminated RWY or any Precipitation
39
Landing Gear Operating Speed: Extension Down and Locked Retraction
Extension: 220 KIAS Down and Locked: 220 KIAS Retraction: 200 KIAS
40
Minimum Brake Cooling Time:
15 min
41
Engine Start Cranking Time on Ground:
90 Sec
42
Engine Start Cranking Time in Air:
2 min the first time then 1 min
43
ITT Start Temperatures: Ground Air
Ground - 120 or less Air - 90 or less
44
Oil Pressure: Idle T/O MCT
Idle - 25 PSI T/O - 45 PSI MCT - 95 PSI
45
APU Operating Altitude:
41,000 ft
46
APU Max Starting Altitude:
37,000 ft
47
Maximum Pressure Altitude for T/O and Ldg (NG):
8,000 ft (10,000 ft)
48
Minimum Temperature for T/O and Ldg:
-40 C
49
Maximum Operating Speed
335 KIAS or M.82
50
Minimum Hydraulic Quanities for all Systems 1, 2 and 3
1 - 34% 2 - 29% 3 - 31 %
51
N2% at Idle
55-65
52
N1% at Idle
20-25
53
Maximum APU Bleed Altitude
25,000 ft
54
Maximum Main Engine Start Using APU
21,000 ft