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EDV Systems > All Limitations > Flashcards

All Limitations Flashcards

1
Q

Super Cooled Large Droplet Icing (SLD) Limitation:

A

Continued operation in areas where SLD conditions exist is prohibited.

SLD icing conditions indicated by ice accretion on flight compartment side windows.

Wing anti ice must be ON
Cowl anti ice must be ON
Leave icing conditions when side window icing occurs.

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2
Q

Maximum runway slopes approved for takeoff/landing:

A

2% up or down

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3
Q

Max Ramp Weight (MRW) 700/900?

A

700 = 75,250
900 = 85,000

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4
Q

Max Takeoff Weight (MTOW) 700/900?

A

700 = 75,000
900 = 84,500

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5
Q

Max Landing Weight (MLW) 700/900?

A

700 = 67,000
900 = 75,100

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6
Q

What approach Category is the CRJ 700? 900?

A

CRJ 700 = C
CRJ 900 = D

Under some CRJ 900 reduced landing reference speed operations Category C may be used.

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7
Q

Maximum Zero Fuel Weight (MZFW) 700/900?

A

700 = 62,300
900 = 70,750

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8
Q

Minimum Flight Weight (Min Flight Weight) 700/900?

A

700 = 42,000
900 = 45,000

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9
Q

Max tailwind component for takeoff and landing? 700/900?

A

10 kt for both

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10
Q

Maximum crosswind component for takeoff on a dry runway 700/900?

A

700 = 28
900 = 35

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11
Q

Maximum crosswind component for landing on a dry runway 700/900?

A

700 = 30
900 = 32

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12
Q

Maximum crosswind for takeoff and landing on wet runway?

A

27

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13
Q

Maximum crosswind for takeoff and landing on a runway with RCC (Runway Condition Code) of 3?

A

20

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14
Q

Maximum crosswind for takeoff and landing on a runway with RCC (Runway Condition Code) of 2 or 1?

A

15

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15
Q

Maximum crosswind for takeoff and landing on a dry runway with a crewmember on high minimum status?

PIC:____
SIC:____

A

PIC 25
SIC 15

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16
Q

When is a Flex Thrust Takeoff Prohibited? (4 things)

A
  1. If wing and/or cowl anti-icing bleeds in use
  2. Runway contaminated (all except wet rwy)
    • Can be used on wet rwy with wet performance data in use
  3. Windshear/downdrafts forecasted
  4. Anti-skid system inop
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17
Q

Maximum cruise mach # in RVSM airspace for 700? 900?

A

700 = .83 mach
900 = .82 mach

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18
Q

Maximum airport pressure altitude for takeoff/landing

A

8,000 ft

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19
Q

Maximum operating altitude?

A

41,000 FT

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20
Q

Flight Deck Door

A
  1. Must be kept closed at all times ecept to allow entrance/exit in accordance with FOM/CFM
  2. If opened must use challenge/response and locking verification
  3. If required remember leaves, another crew member must be present to ensure not locked out of flight deck
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21
Q

CRJ 700/900 Flap limits

A

1* = 230 both
8* = 230 both
20* = 220 CRJ 900 / 230 CRJ 700
30* = 185 both
45* = 170 both

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22
Q

Landing Gear Speeds

A

Gear down = below 220
Down and locked = below 220
Gear up = below 200

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23
Q

Turbulence Penetration speed

A

280 or .75 Mach

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24
Q

Max windshield wiper speed

A

250 knots

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25
Q

Tire speed CRJ 700/900

A

700 = 182
900 = 195

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26
Q

Max ambient air temp for operation

A

ISA + 35* C

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27
Q

Minimum ambient air temp for operation

A

-40C/F

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28
Q

How far from suitable airport if cargo is carried?

A

60 minutes

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29
Q

Taxi lights must be switched off if airplane is stationary in excess of __ minutes.

A

10

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30
Q

Autopilot operations with a glide path that exceeds ___ degrees are prohibited.

A

3.5

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31
Q

Minimum autopilot operation altitudes

A

Normal = 600ft AGL
Non precision = 400 AGL
Precision = 80 AGL
Precision OEI = 110 AGL

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32
Q

RVSM Autopilot limitation

A

Same ADC and transponder source must coupled to autopilot

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33
Q

Setting DA/MDA when not even increment (example 236’ AGL)

A

Next 10’ increment (240’)

34
Q

When must cowl anti ice be on on the ground?

A

OAT 10* C + visible moisture

Or

10* C + ramp/taxiway/runway contamination present

35
Q

If cowl anti ice and continuous ignition are both required which must be turned on first?

A

Cowl anti ice

36
Q

When must cowl anti ice be on in flight?

A

10*C + visible moisture unless SAT is -40 or below

Or

Icing conditions (listed above) / ICE annunciation

37
Q

When must wing anti ice be on during ground operations?

A

5*C + visible moisture

Or

5*C + runway contamination

38
Q

When can you turn on wing anti ice on the ground if type 2-4 fluids are applied?

A

Just prior to thrust increase for takeoff

39
Q

When must wing anti ice be used in flight?

A

10*C + visible moisture unless SAT is -40 or below: Icing conditions and speed is less than 230 knots

Or

ICE annunciation

40
Q

Do not hold in icing conditions with _____

A

Flaps and slats extended

41
Q

Wing/cowl anti ice selection is prohibited with _____

A

The APU as a bleed source in manual mode

42
Q

Airplane Cold Soak first flight of the day steps:

A

When below -30*C(-22F) for more than 8 hours:

  1. Motor engines for 60 seconds and verify fan rotation before starting.
  2. Thrust reversers actuated until cycle is 2 seconds or less
43
Q

Continuous ignition must be used when:

A
  1. Takeoff landing on contaminated RWY
  2. Flight through moderate/heavy rain
  3. Flight through moderate/heavy turbulence
  4. Vicinity of thunderstorms
44
Q

Reduced thrust takeoff must not be used when:

A
  1. Wing or cowl anti ice in use
  2. Contaminated rwy (except wet)
  3. Wind shear/downdrafts forecast
  4. Anti skid Inop
45
Q

Max speed for ADG deployment?

A

Vmo /vmmo

46
Q

Min temp for starting APU on ground

A

-40C/F

47
Q

APU starter attempts?

A

3 in one hour, two minute delay between starts

48
Q

Cargo load limitations:
AFT:
CRJ-900 FWD:
CRJ-700 FWD:

A

AFT: 3,650
FWD 900: 1,700
FWD 700: 1,000

49
Q

Turbulence Penetration speed:

A

280 Kts or .75 mach whichever is lower

50
Q

Max speed if windshield wiper has failed:

A

250kts

51
Q

Pressurization maximum relief different pressure:

A

8.7 PSI

52
Q

Pressurization maximum negative differential pressure:

A

-.5 PSI

53
Q

During taxi and takeoff the differential pressure must not exceed:

A

.1 PSI

54
Q

During initial landing (at touchdown) the maximum differential pressure must not exceed:

A

1.0 PSI

55
Q

CRJ-900 Maximum altitude for single pack operations with MORE than 82 cabin occupants including flight attendants:

A

25,000’

56
Q

CRJ-900 Maximum altitude for single pack operations with LESS than 82 cabin occupants including flight attendants:

A

31,000’

57
Q

CRJ-700 Maximum altitude for single pack operation:

A

31,000’

58
Q

The airplane must be completely depressurized prior to to:

A

opening any of the doors.

59
Q

To preclude possible crew and/or passenger ear damage, use of EMER DEPRESS switch above ______ feet is prohibited.

A

15,000’

60
Q

Main and APU Generator maximum load limitation (in kVA)

A

40 for each main generator and 40 for APU

61
Q

In flight the maximum permissible continuous load on each TRU is ____.

A

120 amps

62
Q

Maximum permissible time for ground operations with DC power is ____

A

5 minutes for CRT display cooling reasons.

63
Q

Maximum permissible fuel imbalance between the contents of the main left tank and main right tank are:

A

During takeoff: 300 lbs
All other phases: 800 lbs

64
Q

Takeoff with a fuel load in excess of ____ lbs in the center tank is not permitted unless each wing tank is above ____ lbs.

A

500
4,400

65
Q

Minimum fuel for a go around is ____ per wing assuming a maximum airplane climb attitude of __ degrees nose up.

A

600 lbs
10 degrees

66
Q

Takeoff with engine fuel temperature indications below __ degrees is prohibited

A

5 degrees C or 41 F

67
Q

Powered cross flow and gravity cross flow must be off ____

A

For takeoff

68
Q

APU Bleed air extraction is not permitted above:

A

25,000’

69
Q

Engine must remain ___ until oil pressure reaches normal operating range

A

Idle

70
Q

During all starts, do not exceed ___ N1 for ___ minutes after start or until all operating indications are in the normal range, whichever is longer.

A

75% N1
2 minutes

71
Q

Starter must not be used if indicated N2 RPM exceeds:

A

45%

72
Q

Engine START GROUND limitations:
Start 1&2 |Max time on: _____ | Followed by: _____ cool down
Start 3 through 5|Max time on: _____ | Followed by: _____ cool down

A

|Max time on: 90 seconds | Followed by: 10 seconds cool down
|Max time on: 90 seconds | Followed by: 5 minutes cool down

73
Q

Engine Start Or Motoring IN FLIGHT limitations:
Start 1&2 |Max time on: _____ | Followed by: _____ cool down
Start 2 through 5|Max time on: _____ | Followed by: _____ cool down

A

|Max time on: 120 seconds | Followed by: 10 seconds cool down
|Max time on: 60 seconds | Followed by: 5 minutes cool down

74
Q

Engine MOTORING GROUND limitations:
Start 1&2 |Max time on: _____ | Followed by: _____ cool down
Start 2 through 5|Max time on: _____ | Followed by: _____ cool down

A

|Max time on: 90 seconds | Followed by: 5 minutes cool down
|Max time on: 30 seconds | Followed by: 5 minutes cool down

75
Q

At initiation of thrust lever movement from SHUT OFF to IDLE (2 temps):

A
  1. ITT must be 120 degrees C or less for all ground starts
  2. ITT must be 90 degrees C or less for all air starts
76
Q

During landing maximum reverse thrust is prohibited below ___ Kts and reverse idle should be achieved by __ kts.

A

75
60

77
Q

Do not attempt a ___ after deployment of the thrust reversers.

A

Go around.

78
Q

Flight spoilers must not be extended in flights below an altitude of ____ AGL (company).

A

1,000’

79
Q

Flight with slats/flaps extended at altitudes above ____ is prohibited.

A

15,000’

80
Q

To ensure adequate maneuvering, flight spoilers must not be extended in flight at airspeeds below ____ for the current weight/flap configuration.

A

VREF + 10

81
Q

Both stall protection system switches must remain on for:

A

All phases of flight.

EDV Systems (21 decks)

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