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737 Limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

Takeoff tailwind limit

A

15 knots

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2
Q

Landing tailwind limit

A

10 knots

  • except 15 knots at SJO and San Pedro Sula
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3
Q

Severe turbulent air penetration speed

A

280 knots / .76 Mach

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4
Q

Max altitude with flaps extended

A

20,000 feet

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5
Q

Speed brakes

A

Do not deploy in flight at altitudes less than 1,000 ft RA

3RA-3VM In flight, do not extend Speedbrake lever beyond ARMED
detent with Flaps 40 selected

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6
Q

Minimum altitude for autopilot
engagement for takeoff
(Minimum to engage)

A

400’ AGL

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7
Q

Minimum altitude for autopilot
engagement during approach
(Minimum to disengage)

A

50’ AGL

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8
Q

APU bleed air + electrical load max altitude in flight

A

10,000 feet MSL

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9
Q

APU bleed air max altitude

A

17,000 feet MSL

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10
Q

APU electrical load max altitude

A

41,000 feet MSL

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11
Q

Weather Radar

A

Avoid operation in a hangar

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12
Q

HF radio

A

Do not operate during refueling operations

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13
Q

Crosswind takeoff

A

3AA-3PX Dry …………………………………………………………………………….. 33 kts*
3RA-3VM Dry………………………………………………………………………………32 kts*
Wet …………………………………………………………………………………………….. 25 kts
Standing Water/Slush………………………………………………………………….15 kts
Snow (Wet and Dry) …………………………………………………………………… 25 kts
Compacted Snow ………………………………………………………………………. 20 kts
Ice………………………………………………………………………………………………….15 kts

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14
Q

Crosswind landing

A

3AA-3PX Dry, Good, Good to Medium (RCC 6, 5, 4)………………..33 kts*
3RA-3VM Dry, Good, Good to Medium (RCC 6, 5, 4)……………….32 kts*
Medium (RCC 3) ……………………………………………………………………….. 25 kts
Medium to Poor (RCC 2)……………………………………………………………..17 kts
Poor (RCC 1) ………………………………………………………………………………. 15 kts

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15
Q

Maximum Cabin Differential Pressure (system relief)

A

9.1 psi

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16
Q

Unpressurized flight

A

Maximum altitude for unpressurized flight, following an in flight depressurization, is 14,000 feet. This altitude may be exceeded when terrain clearance requirements dictate.

Maximum altitude when aircraft is dispatched for unpressurized flight is 10,000 feet.

17
Q

Engine anti ice use

A

Engine anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40°C SAT. Engine anti-ice must be on prior to and during descent in all Icing Conditions, including temperatures below -40°C SAT.

18
Q

Minimum oil quantity for engine start

A

3AA-3PX 12 quarts.

3RA-3VM 14 quarts.

19
Q

Fuel imbalance

A

fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing.

20
Q

Fuel loading

A

Main tanks 1 and 2 must be full if center tank contains more than 1000 lbs.

21
Q

Cat III WX

A

300 600/400/300

TDZ +1

22
Q

Takeoff alternate distance

A

330 nm

23
Q

HUD low visibility takeoff

A

<500 RVR

(2 of 3) • Touchdown: 300 RVR (75m) • Mid-field: 300 RVR (75m) • Roll-out: 300 RVR (75m)

PM “centerline”

24
Q

FO takeoff/ landing mins

A

1600 takeoff

1800 landing

25
Q

When must O2 be used

A

Smoke & fumes
Halon extinguisher used
Depressurization

26
Q

Minimum RNP

A

0.10

27
Q

Drift down procedure

A

— Disengage the autothrottle
— Thrust lever operating engine - Set to MCT
— Maximum engine out altitude - Set in MCP altitude window
— Engine out target speed* - Set in MCP IAS/MACH window
— LVL CHG - Select after aircraft decelerates to engine out target speed

PM

— Notify ATC and request altimeter setting
— Refer to QRH - “One Engine driftdown and cruise”

28
Q

Disengage APP mode

A
  • TO/GA
  • Disengage autopilot AND turn off both Flight Directors
  • Retune BOTH VHF navs to non ILS freq
29
Q

Max holding speeds

A

6,000 feet or less 200
Above 6,000 to 14,000 feet 230
Above 14,000 feet 265

30
Q

Maximum operating altitude

A

41,000 feet

31
Q

Maximum Takeoff and Landing Altitude

A

8,400 feet

32
Q

Maximum Landing Weight

A

NG 146,300

MAX 152,800

33
Q

If the elevation of the destination airport is over_____, set the LAND ALT window to ______.

A

6000 feet.

34
Q

Time limit between turning on APU and using it to run the AC packs

A

2 minutes

35
Q

Time limit for turning battery off after turning off the APU

A

3 minutes

36
Q

Wingspan

A

117’ 5”

37
Q

RFD (Ready For Departure) conditions

A

Delayed engine start due to ATC ACARS entry: RFD.

Ramp congestion due to aircraft or vehicular traffic ACARS entry: RAMP DELAY or Misc 59.

De/anti icing location congestion ACARS entry: DE-ICE DELAY or Misc 59.

38
Q

RVSM Altimeter Tolerances

A

In Flight: 200 feet
On Ground: 50 feet (elev 0 to 5000 feet)
60 feet (elev >5000 feet)
Max difference between CA or FO altimeter & elev: 75 feet
(The standby altimeter does not meet altimeter accuracy requirements of RVSM)

39
Q

Engine failure on takeoff, what can you do passing 400’?

A
  • Call ATC
  • Start the APU
  • Analyze the engine

737 Limitations (2 decks)

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