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PSA > Limitations > Flashcards

Limitations Flashcards

1
Q

Max 90 degree xwind for T/O and LNDG

A

27kts

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2
Q

Minimum flight crew

A

One Captain and one First Officer

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3
Q

Max 90 degree xwind for reduced landing minima (RVR below 2400) to RWY without TDZ lights and or CL lights, including RWY with installed but inop TDZ lights and or CL lights

A

15kts

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4
Q

Max 90 degree crosswind for landing from a CAT II Approach

A

15kts

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5
Q

Max headwind for landing CAT II Approach

A

17kts

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6
Q

Max slope for T/O and LNDG

A

+2% uphill

-2% downhill

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7
Q

Max Tailwind

A

10kts

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8
Q

Max operating Alt (200)

A

36,000

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9
Q

Max pressure Alt for T/O and LNDG

A

8,000

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10
Q

Max ambient temp for T/O and LNDG

A

ISA +35 degrees C

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11
Q

Minimum ambient temp approved for T/O

A

-40 degrees C

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12
Q

Maneuvering Limit Load Factors

A

Flaps Retracted -1.0 to +2.5

Flaps Extended 0.0 to +2.0

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13
Q

Flap Operating Speeds

Max speed at which it is safe to extend the flaps

A

Flaps 0-8 200 KIAS
Flaps 8-20 200 KIAS
Flaps 20-30 185 KIAS
Flaps 30-45 170 KIAS

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14
Q

When must Cowl anti-ice be on

A

Cowl anti- ice must be on for all ground and flight operations when icing conditions exist, except when the inflight SAT is -40 C or below, or ICE is annunciated by the ice detection system.

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15
Q

Wing anti-ice must be ON

A

for all takeoff and flight operations when ICE is annunciated by the ice detection system or when icing conditions exist and the airspeed is less than 230 KIAS except when the inflight SAT is -40˚ C or below.

Wing anti ice must be on for the final two minutes prior to takeoff during all ground operations 5˚ C or below unless type IV anti-ice fluid has been applied

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16
Q

During all starts do not exceed______N1 for______mins.after start, or until all operating indications are in normal operating range, whichever is longer

A

75% N1

2 mins.

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17
Q

Engine to engine N2 split at ground idle power should not be greater than ____% N2.
If N2 is___% or less with OAT of__ degrees C or warmer, do not accelerate above idle

A

2%
57%
-20

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18
Q

Engine Start Temp

A

900 Degrees C

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19
Q

Continuous engine ignition must be used during the following:

A

T/O and landing on contaminated runway
Takeoff with high crosswind component of 15kts or more
Flight through moderate or heavier intensity rain
Flight through moderate or heavier intensity turbulence
Flight in the vicinity of thunderstorm

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20
Q

Max taxi and ramp weight (200)

A

53,250

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21
Q

Max takeoff weight (200)

A

53,000

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22
Q

Max landing weight (200)

A

47,000

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23
Q

Max zero fuel weight (200)

A

44,000

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24
Q

If cargo is being carried flight must be within____mins of suitable airport

A

45 mins.

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25
Q

Max weight in cargo compartment

A

3,500lbs

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26
Q

Max airspeed for turbulence penetration is_____

A

280KIAS or Mach .75 whichever is lower

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27
Q

Landing Gear Speeds

A

Extension 220KIAS
Down and locked 220KIAS
Retraction 200KIAS

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28
Q

Max airspeed for windshield wiper operation

A

220KIAS

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29
Q

Max airspeeds for windshield wiper operation failed in the non-parked position

A

220KIAS

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30
Q

Max cruising Mach in RVSM Airspace

A

.82 Mach

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31
Q

Tire limit ground speed

A

182 Knots

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32
Q

Flaps extended speeds

Max speeds at which the aircraft may be flown with the flaps extended

A 
(200, 700 and 900)
Flaps 1 230KIAS (700, 900)
Flaps 8 230KIAS
Flaps 20 220KIAS
Flaps 30 185KIAS
Flaps 45 170KIAS
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33
Q

Engine Starter Cranking Limits Max time on:

A

Start Max time on followed by
1 1 min. 10 secs. OFF
2 1 min. 10 secs. OFF
3 or > 1 min. 5 mins. OFF

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34
Q

The starter must not be engaged if indicated N2 RPM exceeds_____%.

A

55%

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35
Q

Max permissible fuel imbalance between the left and right wing tanks for

A

Takeoff 800Lbs

All phases of flight 800Lbs

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36
Q

Pressure Refueling (200)

A

Left tank 4,760lbs
Right tank 4,760lbs
Center tank 4,998lbs
Total 14,518lbs

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37
Q

Takeoff with a fuel load imbalance in excess of ____lbs. in the center tank is not permitted unless each wing tank is above_____lbs

A

500lbs

4,400lbs

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38
Q

APU Starter Limits (on Battery power)

A

Start Max time on Followed by
1 30 secs 2 mins OFF
2 30 secs 20 mins OFF
3 30 secs 2 mins OFF
4 30 secs 40 mins OFF

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39
Q

APU Starter Limits (DC ground power)

A

Start Max time on Followed by
1 15 secs 2 mins OFF
2 15 secs 20 mins OFF
3 15 secs 2 mins OFF
4 15 secs 40 mins OFF

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40
Q

APU Max starting altitude

A

30,000

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41
Q

APU Max operating altitude

A

36,000

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42
Q

Bleed air retraction from the APU is not permitted above (200)

A

15,000

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43
Q

If both engines are to be started using the APU bleed air, the operating engines thrust may not exceed____N2%?

A

70% N2

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44
Q

Airspeed for APU door open or unknown?

A

300KIAS or APU must remain on

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45
Q

Use of SPEED MODE (DES or IAS), flight director or autopilot coupled, during Approach is?

A

Prohibited

46
Q

Minimum height use of the autopilot is?

A

Take off 600 feet AGL
Non-precision Approach 400 feet AGL
Precision approach 80 feet AGL

47
Q

RVSM Required Equipment

A

Autopilot must be operational
Altitude Alerting System must be operational
Altitude Reporting Transponder (2) One must be operational
Air Data Computer (2) Both must be operational

48
Q

To protect the CRT displays, the max time on for ground operations with DC power is?

A

5 Minutes

49
Q

Enroute use of Slat/Flaps is?

A

Prohibited

50
Q

Max altitude with Slat/Flaps extended is?

A

15,000

51
Q

Minimum altitude for flight spoiler deployment is?

A

1,000 AGL

52
Q

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the recommended approach speed plus____KIAS

A

17KIAS

53
Q

During landing, application of thrust revers above___% N1 is not permitted at airspeeds below ___KIAS Below __KIAS thrust reverse must be reduced to____, not above___%N1.

A

60% N1
75KIAS
60KIAS
Idle
30% N1

54
Q

The taxi lights must be switched OFF whenever the airplane is stationary in excess of___mins.

A

10 Minutes

55
Q

Minimum brake cooling time is__mins. and all BTMS indicators must be___ and not____.

A

15 Minutes
Green
Increasing

56
Q

COWL Anti-Ice icing conditions exist when:

A

OAT10 C (Ground)or TAT10 degrees C (inflight) or below; AND
*visible moisture is present (such as clouds, rain, mist fog, sleet, snow or ice crystals) in flight,
OR
below 400’ AGL for ground operations
OR
*when operating on surfaces that are wet or contaminated

57
Q

Wing-Anti-Ice icing conditions exist when:

A

OAT (takeoff) is 5 C or below or TAT (inflight) is 10 C or below AND
*visible moisture is present (such as clouds, rain, mist fog, sleet, snow or ice crystals) in flight, OR below 400’ AGL for takeoff
OR
*when runway is wet or contaminated

58
Q

Flying in supercooled large droplet icing

A
  • Prohibited
  • Wing and cowl icing systems must be on
  • Leave icing conditions immediately when side window icing occurs
59
Q

Do not hold in icing conditions with ___and/or____extended.

A

Slats and/or flaps

60
Q

T/O is______with frost, ice, snow or slush adhering to any critical areas (wing, upper fuselage, horizontal stabilizer, control surfaces and engine inlets.)

A

Prohibited
*T/O is permitted with frost adhering to the upper surface of the fuselage if it is possible to distinguish surface features
Max 1/8” layer of frost on underside of wing that is caused by cold soak fuel

61
Q

Single Engine Taxi is____ when ramps or taxiways are contaminated with snow, slush or ice OR during icing
conditions.

A

prohibited

62
Q

In addition to a visual check, a tactile check of the wing leading edge, wing forward upper surface and wing rear upper surface
is required during the External Walkaround inspection to determine that the wing is free from frost, ice, snow or slush when:

A
  • The OAT is 5°C or less, or
  • The wing fuel temperature is 0°C or less, or
  • The atmospheric conditions have been conducive to frost formation.
  • Frost or ice may continue to adhere to wing surface for some time even at outside air temperatures above 5°C
63
Q

The engine limit display markings on EICAS

A

Red- Maximum and minimum limitations
Amber- Caution range
Green- Normal operating range

64
Q

Operate engines at or near idle for__ minutes prior to shutdown.

A

2 minutes

65
Q

Taxi time at a stabilized___% N2 or below may be credited towards the two-minute cool down period.

A

80%

66
Q

CRJ 200 has two______engines.

A

CF 34-3B1 Engine

67
Q

N1% normal range

A

0 to 98.5%

68
Q

ITT °C Maximum

A

900 C

69
Q

N2% RPM normal range (green)

A

0 to 99.2%

70
Q

Engine must remain at _____ until oil pressure reaches________.

A

IDLE

Normal operating range

71
Q

ITT must be below______before attempting to air start engine

A

90 C

72
Q

ITT must be below______before attempting to GROUND start engine

A

120 C

73
Q

Before the first flight of the day when the airplane has been cold-soaked at an ambient temp of_____C or below for more than_____hrs. Then engine and thrust reversers must

A
  • -30 C for 8 hours
  • Eng must be motored for 60 sec and fan rotation verified before an eng start is initiated.
  • Thrust reverses must be actuated until deploy and stode cycles are 2 sec or less on (700) and 5 secs. on (200)
74
Q

Minimum oil temp. for engine start (200/700)

A

-40 C

75
Q

Normal takeoff power and maximum power (2 engines) is limited to___ minutes.

A

5 mins.

76
Q

Oil pressures (above IDLE) between___and___psi require oil temperature monitoring.

A

25 and 45 psi

77
Q

Steady-state idle oil pressure.

A

25 psi minimum

78
Q

Takeoff Power minimum oil pressure.

A

45 psi minimum

79
Q

Maximum Continuous oil pressure

A

115 psi maximum

80
Q

dry-motoring cycle (with thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts. (Start times on and off)

A

Start Maximum Time ON Followed By:
1 attempt 90 Seconds 5 Minutes OFF
2 and Subsequent attempt 30 Seconds 5 Minutes OFF

81
Q

Takeoff with any thrust reverser lights ON, icons, or EICAS messages displayed is______.

A

Prohibited

82
Q

The minimum fuel quantity for go-around per wing tank (with the airplane level) and assuming a maximum airplane climb attitude of 10° nose up:

A

(200) 450 lbs.

83
Q

Powered crossflow and gravity crossflow must be____for takeoff.

A

OFF

84
Q

Takeoff with engine fuel temperature indications below 5°C (41°F) is_____.

A

prohibited

85
Q

Max APU RPM

A

107%RPM

86
Q

During single-engine operations, APU bleed air extraction for an engine start is not____.

A

permitted

87
Q

During double-engine failure conditions, APU bleed air extraction for engine starts is_____.
However, APU bleed air extraction is limited to_____ft. and below.

A

permitted

13,000’

88
Q

APU EGT °C normal operating range

A

0 to 712

89
Q

APU RPM % normal operating range

A

0 to 100

90
Q

Maximum relief differential pressure:

A

8.7 psi.

91
Q

Maximum negative differential pressure:

A

-0.5 psi.

92
Q

Max differential pressure for taxi, takeoff, and landing:

A

0.1 psi.

93
Q

Maximum altitude for single pack operation

A

25,000 ft.

94
Q

Low Pressure Air must be____ prior to the Main Cabin Door being closed and secure.

A

OFF

95
Q

The airplane must be completely _____prior to opening any of the airplane doors.

A

depressurized

96
Q

To preclude possible crew and/or passenger ear damage, use of the EMER DEPRESS switch above____feet is prohibited.

A

15,000 feet

97
Q

The bleed air 10th-stage valves must be____for takeoff and landing if the anti-ice systems have been selected___. (200) only

A

closed

ON

98
Q

Individual AC generators (main/APU) loading must not exceed the following values: (200)

A

0 to 35,000 ft.
Main Generator (each) 30 KVA
APU Generator 30 KVA

35,001 to 36,000 ft.
Main Generator (each) 25 KVA
APU Generator 30 KVA

99
Q

Maximum continuous load on each TRU

A

100 Amps

100
Q

Length of the CRJ200

A

Length: 87’1”

101
Q

Wingspan of the CRJ200

A

Wingspan: 69’8”

102
Q

Height of the CRJ200

A

Height: 20’8”

103
Q

General Electric CF34-3B1 thrust rating at sea level

A

8,729 lbs. of thrust at sea level with an APR of 9,220 lbs. of thrust

104
Q

Max taxi and ramp weight (700)

A

75,250

105
Q

Maximum Take Off Weight (700)

A

75,000

106
Q

Maximum Landing Weight (700)

A

67,000

107
Q

Maximum Zero Fuel Weight (700)

A

62,300

108
Q

Pressure Refueling (700)

A

Left Tank 7,492
Right Tank 7,492
Center Tank 4,610
Total 19,594

109
Q

Gravity Refueling (700)

A

Left Tank 7,290
Right Tank 7,290
Total 14,580

110
Q

Bleed Air retraction from the APU is not permitted above (700)

A

25,000

111
Q

Max Operating altitude (700)

A

41,000

PSA (4 decks)

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