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1. EP's & LIMITS > Avelo B737NG ALL limits - SHUFFLE THIS DECK > Flashcards

Avelo B737NG ALL limits - SHUFFLE THIS DECK Flashcards

[ Revision 3 - 30 Jun 2020 ] These limitations come from FCOM 1. They include all memory items AND non-memory item limitations. They also include the same items but possibly said in other ways.

1
Q

If both the reported braking​ action​ and​ the runway​ condition​ are​ known - which should be used?

A

the most restrictive.

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2
Q

[Anti–Ice,​ Rain] #​ Engine​ Anti-Ice​ System

A

The​ engine​ anti-ice​ system​ must​ be​ ON during all​ ground and flight​ ​operations​ when Icing​ Conditions​ exist​ or​ are​ anticipated,​ except​ during​ ​climb and cruise​ when​ Static​ Air​ Temperature​ (SAT)​ is​ below​ -40°C.​

Engine​ anti-ice​ must​ be​ on​ prior​ to​ and​ during descent​ in icing conditions,​ ​including​ temperatures​ below​ -40°​ SAT

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3
Q

[Fire​ Protection] Aircraft​ must​ land within…

A

60​ minutes after​ initial​ discharge​ of​ lower​ cargo ​fire​ suppression​ system.

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4
Q

Maximum​ Takeoff​ and​ Landing​ Altitude

A

8,400 feet​ pressure​ altitude

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5
Q

Use rolling takeoff procedures when crosswinds exceed

A

20 kts.

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6
Q

[Fuel] Center tank fuel qty (lbs)

A

28,973 lbs

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7
Q

Which winds should be used for crosswind computations

A

Steady state wind velocity

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8
Q

[Fuel] Center​ tank​ fuel pumps must​ be​ “OFF”​ during descent and landing when…

A

Center​ tank fuel​ reaches​ 3,000​ pounds

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9
Q

[Fuel] Center​ tank​ fuel pumps must​ be​ “OFF”​ during CLIMB when…

A

Center​ tank​ fuel reaches approximately​ 1,000 pounds

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10
Q

[Engines​ and​ APU] Engine​ Ignition - during takeoff​ and​ landing​ and during engine​ anti–ice​ operations

A

CONTINUOUS ignition​ must​ be​ ON (ENGINE START​ switch in​ the​ CONT ​position

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11
Q

[Engines​ and​ APU] Aborted​ start attempts cycle.

A

If​ there​ are​ multiple​ aborted​ start attempts,​ five​ minutes​ cooling is​ required ​between the​ second​ and​ third​ start​ attempt.​ A​ wait​ of​ one​ hour​ is​ required ​after​ the​ third​ start attempt

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12
Q

[Fuel] Fuel Loading - Main​ tanks 1 and​ 2 must​ be​ SCHEDULED​ to be​ full​ if​…

A

center​ tank contains​ ​more​ than 1,000​ pounds.​

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13
Q

[Autopilot/Flight​ Director​ System] Autothrottle​ use​ is recommended​ during…

A

takeoff​ and climb in either​ ​automatic​ or​ manual​ flight.​ During all​ other​ phases​ of​ flight,​ autothrottle​ ​use​ is​ recommended only when​ the​ autopilot​ is​ engaged

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14
Q

[Flight​ Controls] # Holding​ in​ icing​ conditions

A

with​ flaps​ extended​ is​ prohibited

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15
Q

[Air Systems] do not​ operate​ the​ air conditioning​ ​packs​ in HIGH​ for​ takeoff,​ approach, or​ landing when…

A

engine​ bleed air​ switches​ ON

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16
Q

[Air Systems] # Cabin​ Altitude​ Briefing

A

As part​ of​ the​ takeoff​ briefing​ before​ engine​ start​ for​ the​ first​ flight of​ the​ ​day or​ following​ any​ change​ of​ either​ flightcrew member,​ the​ PIC​ shall​ ​ensure​ the​ Cabin​ Altitude​ Warning indications and​ procedures​ are​ briefed​ ​in accordance​ with normal procedures​ of​ this manual.

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17
Q

Maximum​ flight operating latitude

A

82​​ ​North​ and 82​​ South *

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18
Q

[Flight​ Controls]

Alternate​ flap duty cycle

A

When extending​ or​ retracting flaps​ with the​ ALTERNATE FLAPS​ ​position​ switch,​ allow​ 15 seconds after​ releasing​ the​ ALTERNATE ​FLAPS​ position switch before​ moving the​ switch again to avoid​ ​damage​ to the​ alternate​ flap motor​ clutch

After​ a​ completed extend/retract​ cycle,​ i.e.,​ 0 to 15 and​ back to 0,​ ​allow 5​ minutes cooling before​ attempting another​ extension

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19
Q

[Fuel] Fuel​ Balance - Random​ fuel imbalance​ must​ not​ exceed

A

1,000​ pounds for​ taxi,​ ​takeoff,​ flight, or landing

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20
Q

[Engines​ and​ APU] Maximum​ Oil​ Temperature

A

155º​ C​ maximum​

140º​ C​ -​ 155​º​​ C​ allowable​ for​ 45​ ​minutes​

140​º​​ C​ maximum​ continuous

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21
Q

[Engines​ and​ APU] # With​ APU​ electrical​ load,​ maximum​ altitude​

A

41,000

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22
Q

Flight Maneuvering Load Acceleration ​Limits Flaps​ Up

A

+2.5g to -1.0g

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23
Q

[Air Systems] maximum​ allowable​ cabin differential​ pressure​ for​ takeoff​ and ​landing​

A

0.125​ psi​ (236​ feet​ below airport​ pressure​ altitude).

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24
Q

Contaminated Runway Takeoff & Landing Requirement

A

Takeoff​ or​ landing​ is​ not​ authorized with greater​ than​ 1/2​ inch of​ slush,​ ​standing​ water,​ or​ wet​ snow on the​ runway.​

For​ dry snow the​ maximum​ ​depth is 4 inches

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25
Q

[RVSM] maximum​ allowable ON THE GROUND altitude​ display​ differences for RVSM - [SL-5k, Capt OR FO & Field Elevation]

A

75 feet

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26
Q

[Fire​ Protection] Aircraft​ must​ land within 60​ minutes after

A

initial​ discharge​ of​ lower​ cargo ​fire​ suppression​ system.

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27
Q

[RVSM] maximum​ allowable ON THE GROUND altitude​ display​ differences for RVSM - [SL-5k, Capt vs FO]

A

50 feet

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28
Q

[Autopilot/Flight​ Director​ System] # Do not​ use​ LVL​ CHG​…

A

on​ final​ approach​ below 1,000 feet​ AFE.

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29
Q

[Fuel] No 1 or No 2 Main tank fuel qty (lbs)

A

9,144 lbs

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30
Q

[Engines​ and​ APU] # With​ APU​ bleed​ +​ electrical​ load,​ maximum​ altitude​

A

10,000​ ft

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31
Q

​ Turbulent​ airspeed​

A

280​ KIAS/.76M

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32
Q

[Engines​ and​ APU] APU bleed​ valve​ must​ be​ closed​ when:

A
  • ​ Ground air​ connected and​ isolation valve​ open​
  • ​ Engine​ no.​ 1 bleed valve​ open

​•​ Isolation​ valve​ and​ engine​ no.​ 2​ bleed valve​ open

APU bleed valve​ may be​ open during engine​ start,​ but​ avoid engine​ power ​above​ idle

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33
Q

Do​ not operate​ the weather​ radar​…

A

in​ a hangar​ or​ within​ 50 feet​ of any personnel​ or​ fuel​ ​spill.​ (hangar and personnel restrictions​ do not apply to​ the weather​ radar​ test​ mode.)

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34
Q

​ Maximum​ speeds

A

Observe​ Vmo pointer​ and​ ​gear/flap​ placards

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35
Q

[Flight​ Controls] # Holding​ in​ icing​ conditions with​ flaps​ extended​ is​

A

prohibited

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36
Q

Autothrottle​ use​ is recommended when…

A

Autothrottle​ use​ is recommended​ during takeoff​ and climb in either​ ​automatic​ or​ manual​ flight.​ During all​ other​ phases​ of​ flight,​ autothrottle​ ​use​ is​ recommended only when​ the​ autopilot​ is​ engaged

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37
Q

[Anti–Ice,​ Rain] #​ Engine​ Anti-Ice​ System - engine​ anti-ice​ system​ must​ be​ ON …

A

prior​ to​ and​ during descent​ in icing conditions,​ ​including​ temperatures​ below​ -40°​ SAT.

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38
Q

Which winds should be used for tailwind computations

A

Peak gust wind velocity.

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39
Q

Passenger​ Evacuation

A

On flights with​ one​ or​ more​ occupants​ in the​ cabin,​ all​ entry door​ ​evacuation slide​ systems​ must​ be​ armed and​ engagement​ of​ the​ girt​ bar​ ​with​ door​ sill​ verified prior​ to​ taxi,​ takeoff,​ or​ landing.​ On flights​ with​ no​ ​cabin​ occupants,​ only​ the​ two​ forward escape​ slide​ retention bars​ (girt ​bars)​ must​ be​ installed​ during​ taxi,​ takeoff, and landing.

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40
Q

[Engines​ and​ APU] Engine​ Ignition - Electronic​ Engine​ Control​ (EEC) - For takeoff in​ Alternate​ mode,​ BOTH EEC’s​ must​ be​ selected​ to

A

Alternate​ ​for​ takeoff.

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41
Q

[Autopilot/Flight​ Director​ System] # Use​ of​ aileron​ trim​ with​ autopilot engaged​ is

A

prohibited

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42
Q

[Anti–Ice,​ Rain] Takeoff​ is​ not​ permitted if​ there​ is​ …

A

any cold​ soaked fuel frost​ on the​ upper​ ​wing tank surfaces,​

or​ if​ the​ cold soaked fuel​ frost​ exceeds​ 1/8 inch (3mm) ​in thickness​ on the​ lower​ wing​ tank surfaces

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43
Q

[Engines​ and​ APU] Engine​ Ignition - CONTINUOUS ignition​ must​ be​ ON (ENGINE START​ switch in​ the​ CONT ​position) when:

A

during takeoff​ and​ landing​ and during engine​ anti–ice​ operations

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44
Q

[Air Systems] maximum​ cabin differential​ pressure​ (relief​ valves)​

A

9.10 psi

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45
Q

Max Taxi Weight

A

174,700#

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46
Q

[Engines​ and​ APU] Engine​ Ignition When flight​ in moderate​ or​ heavy​ rain,​ hail​ or​ sleet​ is​ encountered or​ ​anticipated except​ on short​ final​ when landing is​ ​assured the engine​ start​ switches​ must​ be​ set​ to

A

FLIGHT​ and a​ minimum​ ​of​ 45% N1 must​ be​ maintained

47
Q

[Flight​ Controls] # Do not​ deploy the​ speedbrakes in​ flight​ at​

A

radio​ altitudes less​ than​ ​1,000​ feet.

48
Q

[Flight Management,​ Navigation​] Do not operate​ the​ weather​ radar

A

in a hangar​ or within 50​ feet​ of any​ personnel or a fuel ​spill. Note: ​ The​ hangar and​ personnel restrictions do not apply to the​ weather​ radar test​ mode

49
Q

[Fuel] # Minimum fuel​ temperature​

A

fuel​ freeze​ point​ of the​ fuel​ being​ used​ ​+3°​ C or​ –43°​ C,​ whichever​ is higher.

50
Q

[Fuel] Center​ tank​ fuel pumps must​ be​ “OFF”​ when readied for initial taxi when…

A

Center​ tank​ fuel​ is < 5,000​ pounds​

51
Q

[Communications] Do not​ use​ VHF–3..

A

for​ ATC​ Communications​ with ACARS​ operational.

52
Q

[Autopilot/Flight​ Director​ System] # Do not​ use​ LVL​ CHG​ on​ final​ approach​

A

below 1,000 feet​ AFE

53
Q

[Weight Limits] Maximum​ Landing Weight​

A

146,300 lbs

54
Q

[Engines​ and​ APU] EGT​ limit​ for​ start​ or​ ​operation

A

APU is FADEC​ controlled,​ No applicable​ EGT​ limit

55
Q

[TCAS] Do not​ use​ the​ look-ahead terrain​ alerting and terrain display functions:

A

Within 15 nm​ of​ takeoff,​ approach or landing​ at​ an airport​ not​ ​contained in the​ GPWS​ terrain​ database

56
Q

[Fuel] Fuel​ Balance - Lateral​ imbalance​ between​ main​ tanks​ 1​ and​ 2 must​ be​ SCHEDULED​ to​ be…

A

0

57
Q

[Engines​ and​ APU] Engine​ Ignition - Electronic​ Engine​ Control​ (EEC) - For maximum​ thrust​ takeoff​ with EEC​ Alternate​ mode​ selected:

A

•​ Do not​ use​ FMC​ Takeoff​ N1 or​ Vspeed values​ •​ Use​ of​ Autothrottle​ for​ Takeoff is​ Prohibited

58
Q

[Anti–Ice,​ Rain] # Wing Anti-Ice​ System - Do not​ operate​ wing anti-ice​ on the​ ground when​

A

the​ OAT​ is​ above​ 10°C​ ​(50°F)

59
Q

[Engines​ and​ APU] Maximum​ and minimum​ limits​ are​ marked with…

A

a​ red​ line

60
Q

[Engines​ and​ APU] #​ Maximum​ Start​ EGT

A

725​º​​ C

61
Q

[Flight​ Controls] # Avoid​ rapid​ and​ large​ alternating​ control​ inputs,​ especially​…

A

in​ ​combination​ with​ large​ changes​ in​ pitch,​ roll,​ or​ yaw (e.g.,​ large​ side​ ​slip​ angles)​ as they​ may result in​ structural​ failure​ at​ any​ speed,​ ​including​ below VA

62
Q

[Engines​ and​ APU] Minimum​ Oil Pressure​

A

13 psi

63
Q

[Engines​ and​ APU] #​ Maximum​ Continuous​ EGT

A

925​º​​ C

64
Q

[Anti–Ice,​ Rain] #​ Engine​ Anti-Ice​ System - engine​ anti-ice​ system​ must​ be​ ON during all​ ground and flight​ ​operations​ when Icing​ Conditions​ exist​ or​ are​ anticipated,​ except​…

A

during​ ​climb and cruise​ when​ Static​ Air​ Temperature​ (SAT)​ is​ below​ -40°C

65
Q

[Autopilot/Flight​ Director​ System] # Do not​ engage​ the​ autopilot​ for​ takeoff​

A

below 400 feet​ AGL

66
Q

[Engines​ and​ APU] Maximum​ N1 RPM

A

104%

67
Q

[RVSM] Standby altimeters​…

A

do not​ meet​ altimeter​ accuracy​ requirements of RVSM airspace.

68
Q

[Flight​ Controls] # Maximum flap​ extension​ altitude​ is

A

20,000​ ft.​ pressure​ altitude

69
Q

[Fire​ Protection] No cargo​ may​ be​ carried in​ the​ forward​ and/or​ aft​ cargo compartment​ if​…

A

the​ ​corresponding​ cargo​ fire​ protection equipment​ is​ not​ operational

70
Q

[Engines​ and​ APU] Maximum​ N2 RPM

A

105%

71
Q

[Air Systems] With engine​ bleed air​ switches​ ON,​ do not​ operate​ …

A

the​ air conditioning​ ​packs​ in HIGH​ for​ takeoff,​ approach, or​ landing

72
Q

Runway contamination​ recommendations​ only apply​ when​ the​ contamination​ ​covers​ more​ than​

A

25 percent​ of the​ runway surface.​

73
Q

[RVSM] maximum​ allowable ON THE GROUND altitude​ display​ differences for RVSM - [5,001 feet to 10,000 ft, Capt vs 10,000]

A

60 feet

74
Q

Flight Maneuvering Load Acceleration ​Limits Flaps​ Down

A

+2.0g to 0.0g

75
Q

[Anti–Ice,​ Rain] # Wing Anti-Ice​ System

A

Do not​ use​ wing anti-ice​ as​ a​ substitute​ for​ ground deicing/anti-icing and ​inspection​ procedures that​ are​ necessary to comply​ with TEM​ Deicing ​manual​ procedures.​

Do not​ operate​ wing anti-ice​ on the​ ground when​ the​ OAT​ is​ above​ 10°C​ ​(50°F)

76
Q

Max Zero Fuel Wt

A

138,300#

77
Q

[Fuel] # Center​ tank​ fuel​ pumps​ must​ not​ be​ “ON” unless

A

personnel​ are​ ​available​ in​ the​ flight​ deck​ to monitor​ low pressure​ lights

78
Q

[Engines​ and​ APU] #​ Maximum​ Takeoff EGT

A

950​º​​ C

79
Q

Flight​ Deck​ Door​ Access System

A

Verify​ that​ an​ operational​ check​ of the​ flight​ deck door​ access​ system​ has​ ​been accomplished according to approved procedures​ once​ each​ flight​ day.

80
Q

Maximum Operating Altitude

A

41,000 feet

81
Q

[Fuel] # Do not​ reset

A

a​ tripped​ fuel​ pump​ circuit​ breaker.

82
Q

[Engines​ and​ APU] Cautionary range​ is​ marked by

A

an​ amber arc

83
Q

[Engines​ and​ APU] Engine​ Ignition - Use​ of​ Autothrottle​ for​ Takeoff is​ Prohibited

A

For maximum​ thrust​ takeoff​ with EEC​ Alternate​ mode​ selected

84
Q

​ Minimum Runway​ Width

A

98 feet​ (30 meters)

85
Q

[Performance Configuration] Takeoff​ or​ landing​ is​ not​ authorized with greater​ than (dry snow)

A

4 inches

86
Q

[Fuel] Center​ tank​ fuel pumps must​ be​ “OFF”​ when:

A
  • ​ Center​ tank​ fuel​ is < 5,000​ pounds​ and​ aircraft​ is​ readied​ for​ initial​ taxi ​
  • ​ Center​ tank​ fuel reaches approximately​ 1,000 pounds during climb​
  • ​ Center​ tank fuel​ reaches​ 3,000​ pounds during​ descent​ and​ landing
87
Q

[Fuel] Fuel​ types used

A

Jet A,​ A1.​ Other​ types require​ company approval.

88
Q

[Fuel] # Maximum fuel​ temperature

A

49°​ C

89
Q

Do not​ operate​ HF​ radios​..

A

during refueling

90
Q

[Flight​ Controls] # Flaps 15​ normal landings​ are

A

prohibited.​ A​ Flaps​ 15 landing​ may be​ ​performed​ when​ required​ by​ a non​ normal​ procedure

91
Q

[Engines​ and​ APU] # Reverse​ Thrust

A

Intentional selection​ of reverse​ thrust​ in flight​ is​ prohibited

92
Q

[RVSM] maximum​ allowable ON THE GROUND altitude​ display​ differences for RVSM - [5,001 feet to 10,000 ft, Capt OR FO & Field Elevation]

A

75 feet

93
Q

[Landing Gear] # Operation​ with​ assumed​ temperature​ reduced​ takeoff​ thrust​ is​ not​ ​permitted​ with…

A

anti-skid​ inoperative

94
Q

[Fuel] Defueling​ or​ transferring fuel​ with passengers on board​ is​

A

prohibited.

95
Q

Runway contamination​ recommendations​ only apply​ when​

A

the​ contamination​ ​covers​ more​ than​ 25 percent​ of the​ runway surface.​

96
Q

[Fuel] # FOR GROUND OPERATIONS,​ center​ tank​ fuel​ pump​ switches​ must​ not​ be​

A

positioned​ to “ON” unless the​ center​ tank​ fuel​ quantity​ exceeds​ 1000 ​pounds,​ except​ when​ defueling or​ transferring fuel.

97
Q

maximum​ demonstrated takeoff​ and​ landing​ crosswind

A

33​ knots​ on aircraft​ with blended winglets

98
Q

[Engines​ and​ APU] Maximum​ Time​ Limit​ for​ ​Takeoff thrust

A

5 minutes

99
Q

[Engines​ and​ APU] APU bleed valve​ may be​ open during engine​ start,​ but…

A

avoid engine​ power ​above​ idle

100
Q

[Autopilot/Flight​ Director​ System] # For​ single​ channel​ operation​ during​ approach,​ the​ autopilot​ shall​ ​not remain​ engaged

A

below 50 feet​ AGL.

101
Q

[Performance Configuration] # Certified​ for​ flaps…takeoff..

A

1,​ 5,​ 10,​ 15 and​ 25​ takeoffs

102
Q

[Engines​ and​ APU] Engine​ Ignition - Do not​ use​ FMC​ Takeoff​ N1 or​ Vspeed values​ when:

A

For maximum​ thrust​ takeoff​ with EEC​ Alternate​ mode​ selected

103
Q

[Performance Configuration] Takeoff​ or​ landing​ is​ not​ authorized with greater​ than (Slush, standing water, or wet snow)

A

1/2 inch

104
Q

[Flight​ Controls] # In​ flight,​ do not​ extend​ the​ SPEED BRAKE​ lever​ beyond​ the​

A

FLIGHT​ DETENT

105
Q

[Engines​ and​ APU] Normal​ operating​ range​ is marked by…

A

a​ white​ arc.

106
Q

[Engines​ and​ APU] # Reduced​ Thrust - Use​ of​ assumed temperature​ reduced thrust​ procedures​ is​ not​ allowed ​when:

A
  • ​ The​ runway is​ contaminated with​ standing water,​ ice,​ slush,​ or​ snow ​
  • ​ With anti-skid inoperative​
  • ​ With EEC​ is​ in​ Alternate​ mode​
  • ​ The​ probability of​ windshear​ exists
107
Q

Max Takeoff Weight

A

174,200#

108
Q

​ Maximum​ Takeoff and​ Landing​ ​Tailwind​ Component

A

15 knots

109
Q

[Flight Management,​ Navigation​] # Vertical Situation Display

A

When installed, all Non-ILS/Non-Precision Approaches, the​ PM must have the ​Vertical Situation Display (VSD) selected ON​ to enhance Ground/Terrain​ ​situational awareness.​

110
Q

[RVSM] maximum​ allowable​ IN FLIGHT difference between​ Captain​ and First Officer​ altitude​ ​displays for RVSM​ operations.

A

200 feet

111
Q

[Engines​ and​ APU] Engine​ Ignition - engine​ start​ switches​ must​ be​ set​ to FLIGHT​ and a​ minimum​ ​of​ 45% N1 must​ be​ maintained

A

When flight​ in moderate​ or​ heavy​ rain,​ hail​ or​ sleet​ is​ encountered or​ ​anticipated except​ on short​ final​ when landing is​ ​assured

112
Q

Runway​ slope​

A

+/- 2%

113
Q

When crosswinds exceed 20 kts - which type of takeoff should be used?

A

Rolling takeoff

114
Q

[Engines​ and​ APU] # With​ APU​ bleed​ maximum​ altitude​

A

17,000 ft

1. EP's & LIMITS (6 decks)

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