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CRJ PSA Limitation Upgrade > Limitation CRJ > Flashcards

Limitation CRJ Flashcards

1
Q

Max Crosswind Takeoff and Landing

A

27 KNots

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2
Q

Max Crosswind Cat 2

A

15

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3
Q

Max Headwind Cat 2

A

16

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4
Q

Max Tailwind Takeoff and Landing

A

10

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5
Q

Max Runway Slop

A

+2.0 Uphill. -2.0 downhill

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6
Q

Max runway Width takeoff and Landing

A

100ft

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7
Q

Max Operating Alt

A

41000

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8
Q

Max Pressure Alt for Takeoff and Landing

A

8000ft

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9
Q

Max ambient temp for takeoff and landing

A

ISA +35c
limited to a maximum of OAT of 51c

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10
Q

Min ambient temp approaved for takeoff

A

-40C

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11
Q

Maneuvering Limit load Factors
Flaps Retracted
Flaps Extended

A

Retracted -1.0 to +2.5G
Extended 0.0 to +2.0G

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12
Q

Max Positive differential pressure

A

8.7 PSI

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13
Q

Max Neg differential pressure

A

-0.5psi

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14
Q

max pressure differential during ground maneuvering

A

0.1psi

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15
Q

max differential pressure during landing

A

1.0 PSI

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16
Q

Max alt for single pack

A

31,000FT

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17
Q

Use of Emergency Depress switch about Alt is prohibited

A

15000ft

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18
Q

Max turbulence Penetration speed

A

280kias/ .75m whichever is lower

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19
Q

Max gear extension speed

A

220Kias

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20
Q

Max gear extended speed

A

220kias

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21
Q

Max Gear Retract speed

A

200

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22
Q

Max speed windshield wiper opp

A

250Kias

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23
Q

Max speed wipers failed in nonpark position

A

250 Kias

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24
Q

Max Cruise in RVSM

A

.82M

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25
Q

Tire Limit speed 700

A

182

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26
Q

Tire limit speed 900

A

195

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27
Q

Flaps 1

A

230

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28
Q

Flaps 8

A

230

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29
Q

Flaps 20

A

220

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30
Q

Flaps 30

A

185

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31
Q

Flaps 45

A

170

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32
Q

Min Temp for cold soaked APU start on ground

A

-40C

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33
Q

APU Start Limit

A

Nore more than 3 Start attempts in 1
hour with a 2 min delay between cranking attempts

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34
Q

Max start ALT for APU

A

37000

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35
Q

Max operating alt

A

41,000

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36
Q

APU Bleed Air

Air Conditioning

A

Bleed Air extraction from the APU is not permitted above 25000

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37
Q

APU Bleed Air

Engine start during ground opps

A

Each engine may be started using the APU as bleed air source

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38
Q

APU Bleed air

Engine start during flight

A

Limited to 21000 or below

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39
Q

APU Door not closed or door position is unkown

A

THe APU must remain in operation
Limited to 220KIAS

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40
Q

APU Generator and main generator load limited to

A

40 kVA

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41
Q

Each load on TRU

A

120 AMPS

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42
Q

To protect the flight compartment CRT displays the max permissible time for ground opps with DC power only is

A

5 Mins

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43
Q

During all Starts do not exceed ___ N1 for _____ After starts, or until all operating indications are in normal range which ever is longer

A

75% N1
2 Minutes

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44
Q

Operate engine at or near idel for ____ prior to shutdown

A

2 Minutes

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45
Q

Max Itt Ground start
Engine

A

815C ITT

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46
Q

Max Itt air-assisted start
Engine

A

815C ITT

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47
Q

Windmill Start ITT
Engine

A

927C ITT

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48
Q

Ground Start oil Pressure
Assisted air start
Windmill Start
Engine PSI

A

182PSI (95 PSI) after 10 Mins

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49
Q

Normal Takeoff Power and Max Power 2 engines

A

Limited to 5 mins

50
Q

APR Power 1 engine limited to

A

10 MIns

51
Q

APR power thrust is prohibited for the first ______ after any engine start and at ALT below _______
and at all time above_______

A

30 mins
7500msl
7500MSL

52
Q

Itt must be below______ before attempting ground starts

A

120C

53
Q

ITT must below before attemtping air start

A

90C

54
Q

Cold Soaked plane is

A

Ambient temp of -30C or below for more than 8 hours

55
Q

Cold soak start
engine?

A

Engine must be dry motored for 60 seconds and fan rotation must be verified before start

56
Q

Cold soak Thurst Revers

A

Must be actuated until they deploy and stow cycles are 2 seconds or less

57
Q

Min oil temp for start engine

A

-40C

58
Q

Max continuous Oil temp

A

155C

59
Q

Max permissible Oil temp

A

163C 15 mins max

60
Q

Steady state idel

A

25PSI minimum

61
Q

takeoff power oil

A

45Psi minimum

62
Q

Max continuous oil PSI

A

95psi max

63
Q

After cold start engines must remain idel

A

until oil pressure returns to normal

64
Q

Continuous ignition

A

-takeoff and landing on contaminated runway

-Takeoff with high crosswind component 15knots or greater

-Flight though mod or heavy-intensity rain

-Flight though mod or heavy intensity turbulance

-Flight in the vicinity of Thunderstorms

65
Q

Starter Crank limits Ground

A
  1. 90 seconds on 10 seconds off
  2. 90 seconds on 10 seconds off
  3. 90 seconds on 5 mins off
66
Q

Flight Crank limits

A
  1. 2 mins on 10 seconds off
  2. 1 min on 5 mins off
67
Q

The start must not be engaged if indicated n2 RPM exceeds

A

45%

68
Q

Dry Motor Cycle limits

A
  1. 90 seconds on 5 mins off
  2. 30 seconds on 5 mins off
69
Q

Thurst reverse during landing

A

Prohibited max below 75Kias
reverse idle should be achieved by 60Kias

70
Q

30 Degrees either direction from airplane nose; no wind speed limit
Or
> 30 Dergees either direction of from airplane nose <5 knots windspeed

A

No limitation - Toga thrust maybe applied before brakes release but must be set by 60 kias.

71
Q

> 30 dregrees either direction from airplane nose between 5-30 knots windspeed

A

A max of 75% N1 may be applied before brakes release then set toga thrust by 60 kias

72
Q

> 30 degrees either direction from airplane nose ; >30 knot windspeed

A

Only idle taxi thrust maybe applied before brakes release then set toga thrust by 60kias

73
Q

Flex Takeoff

A
  1. Anti skid must be operative
  2. Prohibited on contaminated runways
  3. Prohibited if the airplane has been de iced.
  4. prohibited if wings and or cowls anti iceing bleeds are in use
  5. Windshear or downdrafts have been forcasted
  6. engine cannot avhice full rated thrust
  7. Special departure procedure specifies full rated takeoff
74
Q

Use of slats and flaps en-route

A

Prohibited

75
Q

Max slats and flaps extended alt

A

15,000

76
Q

Flight spoilers min alt

A

1,000

77
Q

To ensure adequate maneuver margins flight spoilers must not be extended in flight at airspeed below

A

Ref+10

78
Q

Fuel imbalance takeoff

A

300lbs

79
Q

Fuel imbalance all phases of flight

A

800lbs

80
Q

Refuel/ Defuel imbalance

A

2,500lbs

81
Q

Total fuel Pressure

A

19594

82
Q

Gravifty refuel 700

A

14,580

83
Q

Gravity refuel 900

A

14,810

84
Q

Takeoff with fuel load of excess of 500lbs in center tank is not permitted unless each wing take is

A

4,400

85
Q

Powered Crossflow and Gravity crossflow

A

must be off for takeoff

86
Q

takeoff fuel temp indication below

A

5C is prohibited

87
Q

Ground contamination defined as

A

Runways, Ramps taxiways with surface snow, ice, slush or standing water

88
Q

Visible moisture defined as

A

Visible moisture or precipitant in any form such as Fog with visibility as 1 mile or less, mist, rain, snow, sleet and ice crystal or clouds in flight

89
Q

if Visibile moisture is present at 400ft agl with

A

10C cowl anti ice for takeoff
5c cowl and wing anti ice for takeoff

90
Q

Taxi anti-ice

A

Ground or visible moisture
10C or below Cowls only

91
Q

Takeoff anti ice

A

10C Cowls only
5C Cowls and wings

92
Q

Flight anti ice Visible mostiure

A

Below 230 wings and cowls
above 230 Cowls
TAT 10C- SAT -39C

93
Q

Ice annunciated inflight

A

Wings and cowls

94
Q

Holding in icing conditions

A

Prohibited with slats and Flaps

95
Q

Tactile check

A

Oat 10C or less
The bulk fuel temp is 0 or less
the atmospheric conditions have been conductive to frost formation
ice and frost may continue to adhere to wing surface for some time even at oat above 10C

96
Q

Taxi light

A

Off when stationary for more than 10mins

97
Q

Wheel brake cooling limits

A

15mins and all BTMS indicator must be green and not increasing

98
Q

CAT 2 Approach

A

Prohibited when braking action is reported less than medium

99
Q

Live animals

A

prohibited in forward cargo

100
Q

Autopilot engaged is prohibited

A

Below 600Ft

101
Q

Visual approach and non precision approach

A

400Ft agl min hight for auto pilot

102
Q

Precision approaches or approaches with vertical guidance

A

80Ft agl
110 agl single engine

103
Q

Cat 2 approach automation

A

must be flown with autopilot

104
Q

Use of speed mode with flight director or autopilot coupled during approach

A

not permitted

105
Q

Use of Vnav for climb

A

not permitted

106
Q

Use of Vnav for approach is

A

ONLY Permitted for Lnav and Vnav approaches

107
Q

RVSM equipment

A
  1. autopilot with alt holding/ Must be operational
  2. Alt alerting system/ Must be operational
  3. Alt reporting transponder/ 1 must be operational
  4. Air date computer/ two must be working
108
Q

700 Taxi ramp

A

75,250

109
Q

700 Takeoff

A

75000

110
Q

max landing 700

A

67,000

111
Q

zero fuel 700

A

62,300

112
Q

900 taxi and ramp

A

85,000

113
Q

takeoff 900

A

84,500

114
Q

landing 900

A

75,100

115
Q

zerofuel 900

A

70,750

116
Q

Foward cargo 700

A

1,000

117
Q

Forward cargo 900

A

1,700

118
Q

all flight must be 60 mins of a suitable landing airport

A

if any cargo is carried

119
Q

Smoke FIRE fumes

A

Oxygen Mask(if required). Don and 100%
Crew Communication Establish

120
Q

Cabin pressure loss

A

Oxegen mask. Don and 100%
Crew Communication Establish
Capt assumes PF Duties.

121
Q

Wheel break assimily

A

Wheel brakes…….Release momentarily
PM will Select anti-skid to off
Wheel brakes. Re-apply as required
Reverse Thrust. Apply maximum until stopping assured

122
Q

pitch trim runaway

A

Control Wheel Assume Manuel Control and override runaway
Stab Trim Disc Push hold and release

CRJ PSA Limitation Upgrade (5 decks)

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