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longitude > Limitations > Flashcards

Limitations Flashcards

1
Q

45 Minute IFR Reserve

A

1627 lb

(FL330, M.80, GW 33,500lb, Anti-Ice Off)

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2
Q

Hot Spare Fuel Quantity

A

5400 lb
DO/ADO may authorize reduction

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3
Q

Emergency Fuel

A

1367 lb

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4
Q

Inclement Weather Fuel Quantity

A

9500 lb

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5
Q

Minimum Runway Length

A

4,000’

For Release Only, Use LPA

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6
Q

Minimum Runway Width

A

65’

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7
Q

Max Runway Slope

A

+/-2%

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8
Q

Ops Review Required If Runway Is…

A

Contaminated Less Than 5500

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9
Q
  • Max X-Wind Dry/Wet Runway for T/O and LND
A
  • 25 kt
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10
Q
  • Max X-Wind Contaminated Runway Width
A
  • > than or = 150’
    15 kt
    < than 150’
    10kt
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11
Q
  • Max Tailwind T/O or LND
A
  • 10 kt
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12
Q

Equipment That Must Be Operational In RVSM Airspace

A

Pilot/Co-Pilot Primary Altimeters

Autopilot (1)

Altitude Alerting Device (1)

ATCRBS Transponder (1)

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13
Q

Minimum Airspeed in RVSM

A

190 kt

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14
Q

Max T/O Weight Is Limited By The Most Restrictive of …

A

Max Certificated T/O Weight

Max Runway-Limited T/O Weight

Tire Speed and Brake Energy Limit Weights

Max T/O Weight (Climb Limited)

Obstacle Clearance, En Route & LND Weight Limits

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15
Q

Max LND Weight Is Limited By The Most Restrictive of…

A

Max Certificated LND Weight

Max LND Weight
(Runway Length plus Obstacle)

Max LND Weight
(Climb Limit Or Brake Energy Limits)

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16
Q
  • Max Ramp & Taxi Weight
A

*39,700 lb

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17
Q
  • Max T/O Weight
A
  • 39,500 lb
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18
Q
  • Max LND Weight
A
  • 33,500 lb
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19
Q

Max Zero Fuel Weight

A

26,800 lb

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20
Q

Interior Baggage Compartment Door Must Be:

A

Latched Closed For T/O & LND

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21
Q

If Cargo Is Carried In The Baggage Compartment, Verify…

A

The Smoke Detection System Is Operational

The Lav PBE And Fire Extinguisher Are Serviced And Accessible

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22
Q
  • Max Operating Altitude
A
  • FL450
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23
Q

Max Flaps Extended Altitude

A

FL180

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24
Q

Max Gear Extended Altitude

A

FL180

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25
Q

Max T/O & LND Altitude

A

10,000’

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26
Q
  • Minimum Speed Brake Extension Altitude
    (Retracted Prior To)
A
  • 500’
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27
Q

Max Operating Speed
(VMo)

A

325 kt
Below 8,000’ - 290 kt

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28
Q

Max Operating Mach (MMo)

A

M.84

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29
Q
  • Turbulent Air Penetration Speed
    (VRa/MRa)
A
  • 235/M.75
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30
Q
  • Max LND Gear Operating/Extended Speed (VLo/VLe)
A
  • 230 kt
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31
Q

Max Tire Ground Speed

A

195 kt

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32
Q
  • Flaps 1 Speed (VFe)
A
  • 250 kt
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33
Q
  • Flaps 2 Speed (VFe)
A
  • 230 kt
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34
Q
  • Flaps Full Speed (VFe)
A
  • 180 kt
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35
Q
  • Minimum Speed In Icing
A
  • 200 kt
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36
Q
  • Unless Directed By AFM Procedures, ECS Knob Selection To Heat Exchange Only Is:
A
  • Prohibited
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37
Q

Operations Above FL410, The Following Must Be Selected To Norm:

A

Both Press Source Buttons

Both Engine Bleed Buttons

ECS Knob

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38
Q

Normal Differential Pressure

A

10.2 psi

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39
Q

Max Differential Overpressure

A

10.3 psi

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40
Q
  • Cabin Must Be Depressurized Prior To:
A
  • Opening The Cabin Door
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41
Q

Do Not Start APU During:

A

Pressure Refueling

Engine Shutdown

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42
Q
  • Limit For Successful APU Starts
A
  • 6 Consecutive Start Attempts At 10-min Intervals With A 1-hr Rest
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43
Q

Limit for Unsuccessful APU Starts

A

3 Consecutive Start Attempts, Then 20 min Off

2 Consecutive Start Attempts, Then 1-hr Off

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44
Q
  • Max Altitude For APU Start
A
  • FL 310
45
Q

Max Altitude For Ground APU Start

A

13,500’

46
Q

Minimum Battery Temp For APU Start

A

-20*C

47
Q

APU Ground Start Is Prohibited With Ambient Temp below:

A

-40*C

48
Q

EICAS Messages That Prohibit An APU Start Attempt

A

Amber BATTERY VOLT

Amber BATTERY OFF

White BATTERY OFF

49
Q
  • Max Operating Altitude for APU
A
  • FL 350
50
Q

When Not To Use Autopilot

A

T/O or LND

Severe Icing
(Unusual Lateral Trim)
(Autopilot Trim Alerts)

51
Q
  • Autopilot Minimum Altitudes
A
  • En Route or Descent 1,000’
  • Approach 160’
  • T/O, Climb and Missed 400’
    Approach
52
Q

Do Not Use Autothrottle Unless:

A

Comparison Monitor Messages And Appropriate Sensor Reversions Are Selected

53
Q

When Can’t You Use Or Arm The Autothrottles

A

During Taxi Operations

(Arm ONLY When Cleared For T/O)

54
Q

Minimum Battery Temp For APU or Battery Start Is:

A

-20*C

55
Q

If BATTERY O’TEMP L or R EICAS Message Displays On Ground…

A

T/O is Prohibited
(Regardless If Message Clears)

56
Q

Use Of Hydraulic Generator Is Prohibited Unless:

A

Required By The QRH

57
Q
  • Voltage Value Displayed In Green On EICAS Indicates:
A
  • Sufficient Voltage For Battery Start
58
Q
  • Max GPU Voltage
A
  • 30V
    (Batteries May Discharge If Voltage Is Below 28.5V)
59
Q

Max GPU Load

A

1,500A

60
Q

Max Engine Generator Load
(In Flight Or On The Ground)

A

100%

61
Q

Max APU Generator Load
(In Flight Or On The Ground)

A

100%

62
Q

Galley Pocket Door Must Be Latched Open When?

A

Taxi, T/O & LND

63
Q

Do NOT Operate Radar System Where?

A

+/- 90* Of The Nose

Within 16’ Of Personnel or Flammable Material

64
Q

Pressure Refueling Limits

A

10-55psi

65
Q

Total Fuel Quantity

A

14,511 lb

66
Q
  • Max Fuel Imbalance
A
  • 500 lb
    (2,000 lb Fuel Imbalance Was Demonstrated For Emergency)
67
Q

Fuel Temp Limits

A

-37C-57C

68
Q

PBCS Ops Are Authorized As Follows:

A

Required Communication Performance (RCP) 240sec

Required Surveillance Performance (RSP) 180sec

69
Q

On The Ground, The ENGINE ICE PROTECTION Buttons Must Be Selected ON when in:

A

Icing Conditions, Except During DeIcing/Anti-Icing Procedures

70
Q

Before TakeOff

When Operating In Visible Moisture And 10*C Or Below or If Expecting To Encounter Icing Conditions At Or Below 400’

What Would Need To Be On?

A

L & R ENGINE -ON

WING- ON

STAB - ON

71
Q

Can You Hold With Flaps Extended In Icing Conditions?

A

NO

72
Q

Except For Ground Pre-Flt Check, What’s The Max Temp For Operation Of Wing Ice Protection?

A

15*C
(Use SAT for Ground, RAT In Flight)

73
Q

Max Temp For Stabilizer Ice Protection

A

25C (SAT)
(Operations Above 25C (SAT) For Up To 2 Min Are Permitted)

74
Q

Do NOT Change FLOW, ENGINE ICE Or WING ICE Until…

A

> 400’

75
Q

Flight In Freezing Rain Is…

A

Prohibited

76
Q
  • Limit Ground Operations Of The Pitot/Static Button ON to…
A

2 Minutes

77
Q

At One Minute Prior To Takeoff And In Ground Icing Conditions, Select:

A

Pitot/Static ON For 15 Sec, Then NORM

78
Q

If On The Ground At Idle In Visible Moisture Of 1 Mile Or Less With Temp/Dew Pt Are Equal, Adhere To These Restrictions

A

Outside Throttles to 70% Max
Temp N1 For 10 Sec Time
Every

> -2*C 30 Minutes No Limit

-2C- -9C 15Min 1 Hr

<-9*C 10 Min 50 Min

79
Q

Time With WING ICE PROTECTION Button ON And Thrust Higher Than Idle While Stationary On The Ground Must Not Exceed…

A

15 Sec

80
Q

Except For Pre-Flt Ck, Max Temp For Operation Of WING ICE PROTECTION Is…

A

15*C

81
Q

In Icing Conditions, Maintain Flaps Up Configuration Except During…

A

Approach and Landing

82
Q

If Temp Is 35C to 45C And 45*C And Above, Respectively, Begin Using Conditioned Air And Close Doors After

A

60 Min and 30 Min, Respectively
(Except During Loading And Unloading Of Passengers)

83
Q

If Any GDU Is In Reversion Mode…

A

Do NOT Depart

84
Q

Do NOT Transmit On HF When Navigation Is Based On…

A

ADF

85
Q

GPS Approaches Must Be Retrieved From

A

Current Database

86
Q

Manually Inserted Runway Coordinates are…

A

Prohibited

87
Q

Takeoff And Landing Data (TOLD)
Do Not Mix Sources Of Performance Information, The Flight Release Is…

A

Controlling

88
Q

Verify All Inputs Regarding Aircraft Configuration , Runway Information and Ambient Conditions Are In The…

A

Takeoff Data Window

89
Q

SurfaceWatch
Must Be Inhibited For T/O And LND At An Airport With…

A

No Runway Position Data

90
Q

SurfaceWatch
Must Not Be Used As The Primary Means To Determine If The Aircraft Can…

A

Safely Operate Onto A Runway

91
Q

VNAV
If The Aircraft Is Below The VNAV Path, Altitude Preselector Must Be Set To The…

A

Active Altitude Constraint

92
Q

Approach
Straight-In Vref At Max LND Wt With Anti-Ice System ON is…

A

125 Kt

93
Q
  • Approach
    Aircraft Is Certificated In Approach Category…
A
  • Cat C
    (If Operational Requirements Dictate Appr Airspeed Faster Than 140 Kt, Then Use Cat D)
94
Q

GPS/GNSS Approach
Applicable Annunciator ( FMS, LPV, LP, L/VNAV Must Be Displayed…

A

At The FAF

95
Q

GPS/GNSS Approach
RF Legs Are…

A

Not Authorized

96
Q

GPS/GNSS Approach
Initiate A Missed Approach If These Annunciators Are Displayed

A

GPS NOT USED

RAIM Not Available From FAF to MAP

DR

GPS LOI

97
Q

GPS/GNSS Authorized Minima

A

LPV

LP

WAAS to LNAV/VNAV

Baro-VNAV to LNAV/VNAV

LNAV

98
Q

Visual Approach
Crew Must Visually Verify…

A

That The Course And Path Are Acceptable

99
Q
  • Engine Limitations

Min Start Pressure

A
  • 32 psi
100
Q
  • Engine Limitations
  • Max Tailwind Component For Engine Start
A
  • 16 Kt
101
Q

Engine Limitations

Engine Thrust Between 45-55% N1 Is Prohibited with Tailwinds Greater Than _____ And X-Winds Greater Than _____

A

10 Kt

25 Kt

102
Q

*Engine Limitations

*Takeoff Thrust:

*Transient N2%:

A

*AEO - 5 Min
*OEI - 10 Min

*99.9%N2

103
Q

Oil Limitations

Minimum Oil Temp For Motor Or Start

A

-40*C

104
Q

Oil Limitations

Minimum Oil Temp Above Idle

A

10*C

105
Q

Oil Limitations

Minimum Oil Temp Acceleration To Climb Thrust Or Higher

A

15C
(If Throttle Is Advanced After Oil Temp Reaches 15C, The Engine Can Continue To Be Operated At Climb Thrust Or Above As Long As The Oil Temp Remains > or = 5*C

106
Q

Starter Limitations

Engine Start

How Many Start Attempts And What’s The Cooldown Time?

A

3 Attempts

15 Min Cooldown

107
Q

Starter Limitations

How Much Rest Is Required After A 5 Min Dry Motor

A

15 Min Rest
(Dry Motoring Longer Than 20 Sec Counts As One Normal Start)

108
Q

Thrust Reversers

Reverse Thrust Must Be Idle By?

A

45 Kt On LND Roll

109
Q

Thrust Reversers

Thrust Reverse Is Prohibited When Conducting _____________
Or _____________

A

Touch N Go’s
Or
To Back Up The Aircraft

longitude (18 decks)

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