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SWA > Limitations > Flashcards

Limitations Flashcards

1
Q

Max operating Pressure Altitude

A

41,000 feet

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2
Q

Max TO/LDG Pressure Altitude

A

8400 feet

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3
Q

Flap Up flight maneuvering load

A

+2.5G / -1.0G

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4
Q

Flaps Extended flight maneuvering load

A

+2.0G / 0G

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5
Q

Mach Trim Inoperative Maximum speed

A

280 KIAS / .82 Mach

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6
Q

Turbulent Air penetration speed below 15,000 feet

A

250 kt

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7
Q

Turbulent Air penetration speed above 15,000 feet

A

280 KIAS / .76 Mach

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8
Q

Max tire speed for -700 and -800/MAX

A

NG: 195 / MAX: 205

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9
Q

Runway slope limit

A

+/- 2%

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10
Q

Braking Action NIL limitations for Takeoff/Landing

A

will not be attempted if ANY portion of the runway is reported NIL

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11
Q

Braking Action NIL limitations for Taxiing

A

will NOT be attempted on the portion of the taxiway reported as NIL

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12
Q

Takeoff/Landing not authorized if runway friction MU report includes a value of ________?

A

20 or Less

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13
Q

Dispatch to/from runways less than ____ is not allowed if _______ and ________are inoperative

A

45m (147.6ft)
-rudder pedal nose wheel steering inoperative
-one thrust reverser inoperative

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14
Q

if an alternate is available with runway at least 47m wide, Diversion to alternate shall be performed with

A

-jammed/resticted flight controls
-TE Flap asym
-LE flap/slat asym
-loss of A or B hydraulics

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15
Q

Takeoff Crosswind limits with RCC 6

A

35kts

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16
Q

Landing Crosswind limits with RCC 6

A

35kts unless runway is width limited under 47m (147 feet) then it is 25kts

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17
Q

Takeoff/Landing tailwind limits with RCC 6

A

10kts (15kts with RCC5 or greater at SJO/MROC

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18
Q

Bank angles greater than ____degrees will result in ventral strake strike

A

8.8 degrees

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19
Q

Do not use sideslip(wing low) crosswind landing technique alone when crosswinds exceed ____

A

15kts

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20
Q

In the MAX, limit thrust to setting normally used for taxi when crosswinds are greater than _____

A

43 kts

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21
Q

In the MAX, limit engine thrust to _______when winds greater than _______

A

idle, 58kts

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22
Q

Maximum headwind component for HGS AIII mode is

A

25 kts

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23
Q

Max wind velocity for takeoff and landing is _____steady and _____peak gusts

A

50 kts steady and 70 kts peak gust

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24
Q

Can a flight be dispatched on revenue flights if all Lavatories are inop

A

NO

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25
Q

Safety relief differential pressure

A

9.1

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26
Q

Max cabin pressure differential pressure for takeoff/landing

A

.125

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27
Q

When engine bleed air switches on, do not operate the air-conditioning PACKs in

A

HIGH for takeoff, approach or landing

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28
Q

Can you use a PACK with a pre-conditioned air source

A

No

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29
Q

If aircraft must remain unpressurized, can the aircraft be dispatched on revenue flights

A

No

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30
Q

In flight, In the MAX, how many PACKS may be powered by one engine. bleed source

A

2 PACKS

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31
Q

Engine Ignition must be ON for

A

heavy RA in, anti-ice, Takeoff Landing (+RATL)

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32
Q

Engine Anti Ice must be on for

A

=ground and flight operations when icing cond exist, except during climb and cruise below -40deg SAT
=before and during descent in all icing conditions below -40deg SAT

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33
Q

Can you hold in icing conditions with the flaps extended

A

No

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34
Q

Do not operate wing anti-ice when OAT is above

A

10deg C

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35
Q

Do not use wing anti-ice as substitute for

A

deicing/anti-icing

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36
Q

Window heat inoperative max speed speed

A

250kts below 10,000 feet

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37
Q

Do not operate weather radar when

A

during fueling, near fuel spills, or people,

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38
Q

Can you use wing anti-ice for takeoff

A

No

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39
Q

How long turning on engine bleed air or APU bleed air following deicing

A

1 minute

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40
Q

Can you use aileron trim with while Autopilot is on

A

No

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41
Q

Minimum altitude for Autopilot engagement

A

1000 feet

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42
Q

Minimum altitude for autopilot disengagement during approach

A

50ft below DA/DDA but no less than 50ft AGL

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43
Q

On the ground in the NG, limit one generator operation to a maximum of —-AMPs

A

215

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44
Q

In the MAX, on the ground or in the air, limit one generator operation to a maximum of —-AMPs

A

215

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45
Q

TR voltage range

A

22-30 volts

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46
Q

battery voltage range

A

22-30 volts

47
Q

How long to wait before removing AC power from the aircraft after shutting down the IRS?

A

30 sec

48
Q

Can you reset a CB inflight?

A

YES, when QRH directed.

49
Q

How long must you wait before resetting a CB

A

2 min for cooling purposes

50
Q

Resetting a CB, not directed by QRH, can be done if

A

CA deems critical to safety of flight, waiting. 2 minutes for cooling, and only reset once

51
Q

If reseting a CB in-flight, what else needs to happen

A

Maintenance notified and logbook entry must be made

52
Q

Can you reset a CB on the ground?

A

No, unless maintenance has deemed it safe to reset

53
Q

If tripped CB is not reset is logbook entry required

A

Yes, the fault must be entered

54
Q

If tripped CB is reset by Flight Deck crew member, does logbook entry need to be made?

A

Yes, Info Only entry is made in the logbook with Maintenance Controllers name

55
Q

Can you cycle a CB?

A

Yes, when directed by
-QRH
-Procedure
-Maintenace Control coordinated and approved
and logbook Info Only entry is made

56
Q

In the MAX, after engine starts, oil temp must rise to at least —–degs before setting takeoff thrust

A

31deg C

57
Q

Maximum ground start EGT in NG

A

725deg C

58
Q

In the MAX, with TakeOff Thrust set, can you takeoff with Oil Pressure in the yellow band

A

No

59
Q

If EEC in Alternate Mode, can you takeoff

A

Yes - Max power only
-reduced thrust is not allowed
-both EECs must be selected in Alternate

60
Q

What conditions must engine Ignition be on for?

A

+RA, Anti ice, Takeoff, Landing
in FLT for mod/sever. turbulence

61
Q

In the NG can oil pressure readouts be in yellow band?

A

No, only in the white band

62
Q

On first flight of the day, operate engines at Idle, after rollback for a minimum of — minutes prior to applying takeoff thrust

A

5 min (recommended)

63
Q

Prior to applying takeoff thrust, operate engines at idle, after rollback for a minimum —- NG and —–MAX

A

NG: 2min
MAX: 3min

64
Q

Prior to shutdown, operate engines at or near idle for a minimum of —-NG and —–Max

A

NG: 1min
MAX: 3min

65
Q

What is recommendation for engines idle time prior to shutting down engines

A

3 min

66
Q

NG starter duty cycle

A

2min ON
10 sec OFF between start attempts

67
Q

MAX starter duty cycle

A

3 min ON
10 sec OFF between start attempts

68
Q

NG - Fuel Off Motoring time limit

A

15min

69
Q

MAX - Fuel Off Motoring time limit

A

5min. and minimum of 5min between first two extended motorings

70
Q

Min oil quantity to depart from Non-Maintenance Base

A

NG / MAX
60 / 66

71
Q

Min oil quantity to depart from Maintenance base

A

NG / MAX
70 / 70

72
Q

When terminating, arrange for oil servicing when oil quantity is

A

NG / MAX
<65 / <70
may cause low oil qty alerts during initial takeoff and climb

73
Q

Thrust reverser inoperative limitations for takeoff or landing

A

not authorized if runway is contaminated with clutter or braking action is less the RCC 5 -Good

74
Q

Max altitude for APU operations, electric only

A

41,000 feet

75
Q

Max altitude for APU operations, bleed air only

A

17,000 feet

76
Q

Max altitude for bleed air and electric

A

10,000 feet

77
Q

How long to wait before APU start attempts?

A

90 secs

78
Q

How many consecutive APU start attempts are allowed

A

3, then must call Maintenance. Do not attempt 4 starts

79
Q

After APU GEN OFF BUS light extinguishes, how long must you wait before turning Battery Switch OFF in the NG / MAX

A

NG / MAX
2min / 5 min

80
Q

How long must you wait after APU start before operating as a bleed air source

A

2 min

81
Q

Do not extend the flaps above what altitude

A

20,000

82
Q

Limit associated with Alternate Flap Duty Cycle

A

-one cycle then 5 min off
-cycle is 0 to 15, then back to 0

83
Q

Alternate Flaps Position Switch must be in —– position for —– before reversing the direction of flap movement

A

OFF, 15 sec

84
Q

Do not extent speedbrake lever beyond

A

FLIGHT DETENT

85
Q

Do not use speedbrakes below

A

1000 feet AGL

86
Q

In flight, do not use speedbrakes with flaps greater than

A

Flaps 10

87
Q

With wing load alleviation system in operative, do not operate the aircraft at speeds in excess of ____kts at weights over ______ if

A

320kts at weights over 143,000 lbs

88
Q

Maximum allowed inflight difference between CA and FO altimeters for RVSM is

A

200ft

89
Q

From Sea Level to 5000’ Maximum allowable on the ground altimeter difference for RVSM operations between CA and FO

A

50 feet

90
Q

From 5001’ to 10,000 feet Maximum allowable on the ground altimeter difference for RVSM operations between CA and FO

A

60 feet

91
Q

From 5001’ to 10,000 feet Maximum allowable on the ground altimeter difference for RVSM operations between CA or FO and field elevation

A

75 feet

92
Q

From Sea Level to 5000 feet Maximum allowable on the ground altimeter difference for RVSM operations between CA or FO and field elevation

A

75 feet

93
Q

If “UNABLE REQD NAV PERF-RNP” message is active, do not use

A

LNAV

94
Q

What is required for RNAV operations with an RNP of 1.0nm or less

A

FD or Autopilot

95
Q

What is required for RNAV approaches with RNP less than .3NM?

A

Autopilot is required

96
Q

When can VNAV be engaged on GoAround or Missed approach?

A

once flaps are fully retracted

97
Q

Max fuel tank temperature

A

+49deg

98
Q

Min fuel tank temperature

A

-37deg

99
Q

Fuel tanks must be full if center tank quantity is —-

A

greater than 1,000 lbs

100
Q

center tank fuel pump switches must be on when center tanks have —-

A

more than 1,000 lbs

101
Q

For ground operations, Center tanks fuel pump switches must not be positioned ON unless center tank fuel quantity exceeds

A

1000 lbs

102
Q

Can you transfer fuel with passengers aboard.

A

Yes, provided 2000 is the minimum fuel in the tank being transferred from

103
Q

If fuel in the tank being transferred from will drop below 2,000lbs , what needs to happen

A

passengers and non-essenential crew need to deplane

104
Q

Center tanks must not be turned ON unless

A

crew is available to monitor for low pressure lights

105
Q

Crew must not reset which CB

A

Fuel pump, Fuel pump control, Fuel quantity indicator circuit breakers

106
Q

Landing gear extension airspeed limits

A

270kts

107
Q

landing gear retraction airspeed limits

A

235kts

108
Q

landing gear extended airspeed limit

A

320

109
Q

Can you use auto brakes with anti-skid inop

A

No

110
Q

Autobrakes must be used for landing when

A

-RCC is 5-Good or less
-visibility less than 4000RVR or 3/4mile
-if landing with less than Flaps 30

111
Q

What auto brake setting is not allowed for use

A

1

112
Q

-700 if discharge of fire suppression system, aircraft must land within ____

A

60min

113
Q

-800/MAX: if discharge of fire suppression system, aircraft must land within ____

A

180min

SWA (3 decks)

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