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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
Q

During all starts do not exceed___% N1 for __ minutes after start, or until all indications are in the normal range. Whichever is longer

A

75%

2 min

25
Q

Operate engines at or near idle for __ minutes prior to shutdown

A

2

26
Q

Maximum oil pressure for takeoff

A

45 psi

27
Q

Continuous ignition must be used when….

A

Refer to POH chapter 3

28
Q

Starter cranking limits (ground only)

A

START. MAX TIME ON. FOLLOWED BY
1. 90 sec 10 sec
2. 90 sec. 10 sec
3+. 90 sec. 5 min

29
Q

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

A

30

30

No Limitations - TOGA thrust may be applied before brakes released

30
Q

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:

A

Apply maximum of 75% N1 before brake release, then TOGA thrust

31
Q

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:

A

Apply maximum of idle/taxi thrust before brake release, then TOGA thrust

32
Q

Maximum fuel imbalance from the right to left wing for takeoff

A

300 pounds

33
Q

Maximum fuel imbalance for all phases of flight except takeoff

A

800 pounds

34
Q

Maximum total fuel for pressure refueling

A

19,594

35
Q

Takeoff with an excess of ___ pounds in the center tank is not permitted unless each wing tank is above ____

A

4,400 pounds

36
Q

APU starter motor duty cycle is limited to not more than __ starts/start attempts in _____ with a __ minute delay between cranking attempts

A

3

1 hour

2

37
Q

Maximum altitude for APU bleed air extraction

A

25,000 pounds

38
Q

With the APU door not closed or the door position unknown:

The airplane must be limited to:

A

220 KIAS or the APU must remain in operation

39
Q

VFE/VFO FLAPS 1

A

230

40
Q

VFE/VFO FLAPS 8

A

230

41
Q

VFE/VFO FLAPS 20

A

220

42
Q

VFE/VFO FLAPS 30

A

185

43
Q

VFE/VFO FLAPS 45

A

170

44
Q

Gear speeds:

Extension
Down and locked retraction

A

220

220

200

45
Q

Maximum airspeed for windshield wiper operation

A

220

46
Q

Maximum turbulence penetration speed

A

280 KIAS / .75 Maxh whichever is lower

47
Q

CRJ-701

Maximum altitude for single pack operation

A

31,000 feet

48
Q

CRJ-900

Maximum altitude for single pack operation

A

25,000 feet

CRJ-700/900 (1 decks)

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