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SWA-737 > Limitations (good to know) > Flashcards

Limitations (good to know) Flashcards

1
Q

Max headwind component for HGS AIII mode

A

25 kts

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2
Q

Max allowable in-flight difference between CA and FO altimeters for RVSM opps

A

200 ft

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3
Q

Max x-wind for landing with Braking Action FAIR

A

15 kts

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4
Q

When can VNAV be engaged

A

VNAV will not be engaged for takeoff, initial climb or missed approach until flap retraction is complete

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5
Q

When is flaps 40 landing recommended

A

~ Negative [bracketed] OPC stopping margin under Min (2) for flaps 30

~ Reported braking action less then GOOD

~ Wx is at or near minimums for the approach to be flown

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6
Q

Min engine oil qty requirements for NG

A

60% (regardless if mtx station or not) OR

70% for departing a mtx base

The CA must arrange for engine oil servicing when terminating at a non-mtx base when the oil qty is less than 65%

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7
Q

Max tire speed

A

195 kts

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8
Q

What steps should be accomplished when operating in or near moderate to heavy rain, hail or sleet

A

follow turbulent air penetration procedures and set Engine Start Switches to FLT

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9
Q

How long should the APU be operated before opening the bleed valve

A

1 minute

NOTE: on the Classics, the APU bleed air switch should be OFF for at least 2 minutes before the APU is shutdown

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10
Q

Max Pressure Altitude for takeoff and landing

A

8400 ft

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11
Q

Max wind velocity for all takeoffs and landings

A

50 kts steady

70 kts peak gusts

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12
Q

Max gear extension speed

A

270 its or 0.82 Mach

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13
Q

Normal AC voltage output

A

115 Volts +/- 5 volts

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14
Q

Max cabin differential pressure for takeoff and landing

A

0.125 psi

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15
Q

When is the use of LNAV prohibited

A

Do not use LNAV if the message

“UNABLE REQD NAV PERF-RNP”

is active

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16
Q

Minimum runway MU value for takeoff and landing

A

Takeoff and Landing is not authorized if the most current runway friction MU report includes a value of 20 OR LESS for any section of the runway

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17
Q

Max operating speed with Mach Trim INOP

NG?

CL?

A

NG: 0.82 Mach

CL: 0.74 Mach

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18
Q

Minimum altitude for engaging the autopilot

A

1000 ft AGL

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19
Q

Max x-wind for takeoff and landing

A

35 kts

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20
Q

Min ground turn time for an -800 if max quick turnaround weight is exceeded?

A

48 mins, non reducible

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21
Q

Max gear retraction speed

A

235 kts

22
Q

max x-wind component for landing with RVR less than 4000 or vis less than 3/4 sm.

A

15 kts

23
Q

Min onboard fuel for ground operation of the electric hydraulic pumps

A

1675 lbs

24
Q

Max gear extended speed

A

320 kts

0.82 Mach

25
Q

With the speed brake load alleviation system INOP, what are the speed and weight limitations?

A
  • 700 w/ winglets - 320 kts and 143,000 lbs

- 300 w/ winglets - 320 kts and 125,000 lbs

26
Q

When are you allowed to cycle a circuit breaker

A

Only when directed by the QRH, OR directed by a procedure in the AOM, FOM, MEL, or Ops binder, or when coordinated and approved by Mtx.

27
Q

What are the engine starter duty cycle limitations

A

NG: 2 mins ON with 10 secs between start attempts

CL: 2 mins ON - 20 secs OFF - 2 mins ON, then 3 mins cooling before next and each subsequent attempt

28
Q

What are the minimum engine oil qty requirements for the CL

A

2 gallons - flight schedule block less than 2 hours

2.5 gallons - flight scheduled block 2 hours or more

3 gallons - leaving a Mtx base

29
Q

What is the requirement for starting the APU while airborne

A

Only when directed by QRH or but the OPC

30
Q

When must the AUTOBRAKES be used for landing

A

~ On any runway that is not DRY

~ reported vis less than 4000 RVR or 3/4 SM

~ landing less than flaps 30

31
Q

When must gasper fan be turned OFF

A

CL: Above 10,000 ft

32
Q

Max brake temperature for ground turn around on the Classics and the -700s

A

425 F

Temp must be measured between 10 & 15 minutes after arrival parking

33
Q

Can an aircraft be dispatched on revenue flights if the aircraft must remain unpressurized

A

NO

34
Q

When must the APU bleed air valve be closed

A

~ When ground air is connected and isolation valve is OPEN

~ OR when isolation valve and #2 engine bleed valve are OPEN

~ OR when the #1 engine bleed valve is OPEN

NOTE: The APU bleed valve may be open during engine start provided engine power is not above idle.

35
Q

Max fuel imbalance

A

1000 lbs

36
Q

When is Engine Anti-Ice required

A

1) In icing conditions during climb and cruise above -40 degrees C
2) in icing conditions AND in any temperature during descent

37
Q

Max Turbulence Penetration Speed below 15,000 ft

A

250 kts

38
Q

Normal AC frequency

A

400 cps +/- 10 cps

39
Q

Max x-wind component for landing with braking action reported as POOR

A

10 kts

40
Q

Can an aircraft be dispatched on a revenue flight if ALL lavatories are INOP

A

No

41
Q

Can an aircraft be dispatched on a revenue flight if the landing gear must remain down

A

No

42
Q

What is a important consideration regarding thrust reverser operation during takeoff and landing

A

Takeoff and landing are not authorize if either thrust reverser is INOP

AND

the runway is contaminate with clutter or the braking action is less than GOOD

43
Q

What is the safety relief differential pressure

A

NG: 9.10 psi

CL: 8.65 psi

44
Q

List 4 times when the auto throttles are required to be disengaged

A

~ severe turbulence

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

~ During cruise, descent, or approach, autothrottle is allowed only when the autopilot is engaged in the CMD mode. Momentary use of CWS pitch is allowed with the auto throttle engaged

~ while responding to TCAS RA

45
Q

Max tailwind component (including gusts)

A

10 kts

46
Q

How long should you wait AFTER APU shutdown before turning the battery OFF

A

NG: at least 2 mins after APU GEN OFF BUS light extinguishes

CL: at least 20 seconds after APU shutdown

47
Q

When is verification of the overwind exit handle cover required

A

prior to departure with PAX

48
Q

Normal BATT voltage range

A

22 - 30 volts

49
Q

Max turbulence penetration speed above 15,000 ft

A

NG: 280 kts / 0.76 Mach

CL: 280 kts / 0.73 Mach

50
Q

Min altitude for disengaging the autopilot during approach

A

DA / DDA - 50 ft, but not less that 50 ft AGL

51
Q

How long should you wait before turing on the Engine and APU bleeds after de-icing?

A

1 minute

52
Q

Min altitude for LNAV engagement after takeoff or missed approach

NG? CL?

A

CL: 400 ft AGL

NG: can be engaged on ground

SWA-737 (21 decks)

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