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CRJ-700/900 > Limitations > Flashcards

Limitations Flashcards

0
Q

CRJ-701

Maximum takeoff weight

A

75,000

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1
Q

CRJ-701

Maximum taxi and ramp weight

A

75,250

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2
Q

CRJ-701

Maximum landing weight

A

67,000

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3
Q

CRJ-701

Maximum Zero Fuel Weight

A

62,300

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4
Q

CRJ-701

Maximum Operating Altitude

A

41,000 feet

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5
Q

CRJ-900

Maximum taxi and ramp weight

A

85,000

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6
Q

CRJ-900

Maximum takeoff weight

A

84,500

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7
Q

CRJ-900

Maximum landing weight

A

75,100

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8
Q

CRJ-900

Maximum zero fuel weight

A

70,750

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9
Q

CRJ-900

Maximum operating altitude

A

41,000 feet

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10
Q

Definition of Cowl-Anti Icing conditions

A

Refer to chapter 3 POH

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11
Q

When must Cowl Anti-Ice be ON

A

Refer to chapter 3 POH

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12
Q

Definition of Wing Anti-Ice icing conditions

A

Refer to chapter 3 POH

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13
Q

When must Wing Anti-Ice be ON

A

Refer to chapter 3 POH

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14
Q

Maximum tailwind for takeoff and landing

A

10 knots

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15
Q

Maximum 90 degree crosswind for takeoff and landing

A

27 knots

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16
Q

Maximum 90 crosswind for landing from a CAT II approach

A

15 knots

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17
Q

Maximum headwind for landing from a CAT II approach

A

17 knots

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18
Q

CRJ-701

Maximum weight in the forward cargo compartment

A

1,000 pounds

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19
Q

CRJ-701

Maximum weight in the aft cargo compartment

A

3,300 pounds

20
Q

CRJ-900

Maximum weight in the aft cargo compartment

A

3,740 pounds

21
Q

CRJ-900

Maximum weight in the forward cargo compartment

A

1,700 pounds

22
Q

EICAS Limit Markings

A

RED - maximum operating range

AMBER - caution range

GREEN - Normal operating range

23
Q

Maximum ITT for advancement of thrust levers from SHUTOFF to IDLE

A

120 C (??)

24
During all starts do not exceed___% N1 for __ minutes after start, or until all indications are in the normal range. Whichever is longer
75% 2 min
25
Operate engines at or near idle for __ minutes prior to shutdown
2
26
Maximum oil pressure for takeoff
45 psi
27
Continuous ignition must be used when....
Refer to POH chapter 3
28
Starter cranking limits (ground only)
START. MAX TIME ON. FOLLOWED BY 1. 90 sec 10 sec 2. 90 sec. 10 sec 3+. 90 sec. 5 min
29
What is the limitation associated with the following statement Within ___ degrees on either direction of the airplane nose -no wind speed limit OR greater than ____ degrees in either direction of the airplane nose with less than 5 knots
30 30 No Limitations - TOGA thrust may be applied before brakes released
30
What is the limitation associated with the following statement Wind direction __ degrees in either direction of the airplane nose and wind speed between __ and __ knots:
Apply maximum of 75% N1 before brake release, then TOGA thrust
31
What is the limitation associated with the following statement Wind direction greater than __ in either direction of the airplane nose and wind speed greater than __ knots:
Apply maximum of idle/taxi thrust before brake release, then TOGA thrust
32
Maximum fuel imbalance from the right to left wing for takeoff
300 pounds
33
Maximum fuel imbalance for all phases of flight except takeoff
800 pounds
34
Maximum total fuel for pressure refueling
19,594
35
Takeoff with an excess of ___ pounds in the center tank is not permitted unless each wing tank is above ____
4,400 pounds
36
APU starter motor duty cycle is limited to not more than __ starts/start attempts in _____ with a __ minute delay between cranking attempts
3 1 hour 2
37
Maximum altitude for APU bleed air extraction
25,000 pounds
38
With the APU door not closed or the door position unknown: The airplane must be limited to:
220 KIAS or the APU must remain in operation
39
VFE/VFO FLAPS 1
230
40
VFE/VFO FLAPS 8
230
41
VFE/VFO FLAPS 20
220
42
VFE/VFO FLAPS 30
185
43
VFE/VFO FLAPS 45
170
44
Gear speeds: Extension Down and locked retraction
220 220 200
45
Maximum airspeed for windshield wiper operation
220
46
Maximum turbulence penetration speed
280 KIAS / .75 Maxh whichever is lower
47
CRJ-701 Maximum altitude for single pack operation
31,000 feet
48
CRJ-900 Maximum altitude for single pack operation
25,000 feet

CRJ-700/900 (1 decks)

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