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Canadair CRJ200 (none) > Basic Limitations > Flashcards

Basic Limitations Flashcards

1
Q

Maximum Ramp Weight

A

53,250 lbs

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2
Q

Maximum Takeoff Weight

A

53,000 lbs

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3
Q

Maximum Landing Weight

A

47,000 lbs

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4
Q

Maximum Zero Fuel Weight

A

44,000 lbs

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5
Q

Maximum Temp for takeoff and landing

A

ISA +35C

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6
Q

Minimum Temp for takeoff and landing

A

-40C

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7
Q

Maximum takeoff landing altitude

A

10,000

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8
Q

Maximum runway slope

A

+2%

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9
Q

Maximum tailwind

A

10 kts

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10
Q

Maximum operating altitude

A

FL 410

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11
Q

Maximum load in the cargo compartment

A

3,500 lbs

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12
Q

Must be with ____ min of suitable airport with cargo hold in use.

A

45 min

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13
Q

Minimum time between an rejected takeoff (RTO) and subsequent takeoff.

A

15 min

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14
Q

Maximum BTMS temperature for takeoff.

A

06

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15
Q

Load factor limit flaps up

A

-1.0 to +2.5 Gs

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16
Q

Load factor limit flaps down

A

0.0 to +2.0 Gs

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17
Q

Minimum oxygen psi for dispatch

A

1410 psi

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18
Q

VLE

A

250

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19
Q

VLO

A

250

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20
Q

VLO (retract)

A

200

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21
Q

VFE (8)

A

215

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22
Q

VFE (20)

A

215

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23
Q

VFE (30)

A

185

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24
Q

VFE (45)

A

170

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25
Q

Maximum wiper speed

A

220

26
Q

Maximum tire speed

A

182

27
Q

Turbulence penetration speed

A

280 or 0.75M (whichever is lower)

28
Q

Maximum ADG deployment speed

A

VMO or MMO

29
Q

Stabilizer/Mach trim inop speed

A

250 or 0.70M

30
Q

Maximum number of passengers on stairs

A

4

31
Q

Maximum time lights on when stationary

A

10 min

32
Q

Minimum altitude for AP engagement

A

600 ft AGL

33
Q

Minimum altitude for AP (precision approach)

A

80 ft AGL or not less than 50 ft below DA

34
Q

Minimum altitude for NP (non precision approach)

A

400 ft AGL or 50 ft below MDA whichever is higher

35
Q

Maximum L/R fuel tank quantity

A

4,760 lbs

36
Q

Maximum C (center) fuel tank quantity

A

4,998 lbs

37
Q

Cannot take off with less than 500 lbs in center tank unless

A

Each wing tank has more than 4,400 lbs

38
Q

Approved fuel

A

Jet A

39
Q

Minimum fuel quantity for a go around

A

450 lbs a side

40
Q

Minimum fuel feed takeoff temp

A

+5C

41
Q

Minimum bulk fuel temp

A

-40C

42
Q

Maximum fuel imbalance

A

800 lbs

43
Q

Cross flows (powered and gravity) must be ____ for takeoff.

A

OFF

44
Q

Maximum ITT (APR Not Op.) ____ (first 2 minutes) ____ (next 3 minutes)

A

900C, 884C

45
Q

Maximum ITT (APR Op.) ____ (first 2 minutes) ____ (next 3 minutes)

A

928C, 900C

46
Q

MCT max ITT

A

900C

47
Q

Maximum N1%

A

98.6%

48
Q

Maximum N2% to introduce fuel

A

20.0%

49
Q

Maximum ITT during start

A

900C

50
Q

Maximum N1% and N2% for takeoff

A

96.2%, 98.3%

51
Q

Maximum N1% and N2% for APR takeoff

A

98.6%, 99.4%

52
Q

Engines must be running for a minimum of ____ prior to takeoff.

A

2 min

53
Q

Engines must be at idle for a minimum of ____ prior to shutdown.

A

2 min

54
Q

Engine start cycle limits

A

1 minute ON, 10 sec OFF
1 minute ON, 10 sec OFF
1 minute ON, 5 min OFF

55
Q

Maximum ITT for engine start on the ground

A

less than or equal to 120C

56
Q

Maximum ITT for in-flight engine start

A

less than or equal to 90C

57
Q

Maximum N2% to engage starter

A

Starter not to be used if greater than 55% N2

58
Q

Dry motoring limits

A

90 sec ON, 5 min OFF

30 sec ON, 5 min OFF

59
Q

Continuous ignition must be used

A 
Takeoff/landing on contaminated runway
Takeoff with crosswind greater than 10 kts
Moderate or greater rain
Moderate or greater turbulence
Flight in vicinity of thunderstorms
60
Q

Thrust reverser limitations on takeoff

A

No go arounds after thrust reverser deployment

Takeoff with any abnormal thrust reverser annunciator is prohibited

Canadair CRJ200 (none) (3 decks)

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