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737 Info > Limitations/Procedures > Flashcards

Limitations/Procedures Flashcards

1
Q

Minimum hydraulic pressure required before engine start?

A

2800 psi

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2
Q

Flap 1 VFE

A

250 kt CAS

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3
Q

Flap 2 VFE

A

250 kt CAS

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4
Q

Flap 5 VFE

A

250 kt CAS

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5
Q

Flap 10 VFE

A

210 kt CAS

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6
Q

Flap 15 VFE

A

200 kt CAS

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7
Q

Flap 25 VFE

A

190 kt CAS

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8
Q

Flap 30 VFE

A

175 kt CAS

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9
Q

Flap 40 VFE

A

162 kt CAS

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10
Q

Maximum Landing Gear Extension Speed

A

270 kt CAS / 0.82 M

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11
Q

Maximum Landing Gear Retraction Speed

A

235 kt CAS

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12
Q

Maximum Landing Gear Extended Speed

A

320 kt CAS / 0.82 M

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13
Q

Turbulence Penetration Speed

A

280 kt IAS / 0.76 M

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14
Q

Maximum Operating Altitude

A

41,000 ft

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15
Q

Maximum Take-off and Landing Altitude

A

8,400 ft

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16
Q

Maximum allowable in-flight difference between Capt & F/O altitude displays for RVSM operations

A

200 ft

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17
Q

Maximum difference between Capt or F/O altimeter & field elevation

A

75 ft

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18
Q

Maximum difference between Capt & F/O altimeter with field elevation from Sea Level to 5,000 ft

A

50 ft

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19
Q

Maximum difference between Capt & F/O altimeter with field elevation from 5,001 to 10,000 ft

A

60 ft

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20
Q

Minimum runway width?

A

30m

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21
Q

Sideslip only (zero crab) landings not permitted with crosswinds above : (F15 / F30 / F40)

A

F15 - 15 kt / F30 - 18 kt / F40 - 21 kt

Increase these numbers by 2 knots for non-winglet aircraft

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22
Q

Maximum tailwind component for take-off & landing

A

10 kt

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23
Q

Runway slope limits

24
Q

G-Load limits, flaps up

A

+2.5 g to -1.0 g

25
Q

G-Load limits, flaps down

A

+2.0 g to 0.0 g

26
Q

Maximum Dry snow depth for takeoff

A

4” / 101.6 mm

27
Q

Maximum Standing water, slush or wet snow depth for operation

A

0.5” / 12.7 mm

28
Q

Operation on contaminated / slippery runways with ATM

A

Prohibited

29
Q

Maximum Landing Weight

30
Q

Maximum cabin differential pressure (relief valves)

31
Q

Minimum autopilot engagement height on take-off

A

Jet2.com = 1,000ft
Boeing = 400 ft

32
Q

Engine TAI must be on when…

A

Icing conditions exist or are anticipated, except during climb and cruise when SAT is below -40 degrees Celsius

33
Q

MUH for single channel autopilot operation

A

158 ft AGL

34
Q

Starter duty cycle maximum

35
Q

Minimum time between start attempts (starter duty cycle)

A

10 seconds

36
Q

Oil temperature operation between 140 & 155 degrees Celsius limited to…

A

45 minutes

37
Q

Engine Ignition required for (4 conditions)

A
  • Take-off
  • Landing
  • Operation in heavy rain
  • Anti-Ice operation
38
Q

APU bleed + electrical load maximum altitude

39
Q

APU bleed maximum altitude

40
Q

APU electrical load maximum altitude

41
Q

APU starter duty cycle

A

On ground maximum 3 start attempts followed by 15 minutes cool down

42
Q

Maximum flap extension altitude

43
Q

Minimum speedbrake use height in flight

A

Less than 1,000 ft radio altitude

44
Q

Maximum fuel loading

45
Q

Maximum fuel imbalance between main tanks 1 & 2

46
Q

What call is required after flap retraction during an EFATO?

A

“LVL change, bug up, max continuous thrust”

47
Q

ATM prohibited for (4 situations)…

A

1) One or more anti-skid units inop
2) Runway contaminated with snow, slush, ice or standing water
3) Potential windshear conditions exist
4) When EEC is in ALTN mode

48
Q

Bank angle limit until reaching V2 + 15?

49
Q

Bank angle must be limited to 15º until which speed?

50
Q

What does the bottom of the amber bar on the PFD speed tape represent?

A
  • When flaps are UP - 1.3g margin to high speed buffet
  • When flaps not UP - Placard speed for next normal flap setting

1.3g occurs at approx 40º of bank in level flight (25º + 15º overshoot)

51
Q

What does the top of the lower amber bar on the PFD speed tape represent?

A

Below approx 20,000ft: 1.3g margin to stick shaker
Above approx 20,000ft: 1.3g margin to low speed buffet

1.3g occurs at approx 40º of bank in level flight (25º + 15º overshoot)

52
Q

When is the low speed amber bar displayed?

A
  • After first flap retraction on take off
    Or
  • When a valid Vref is entered
53
Q

What conditions require ABORTED ENGINE START NNC?

A
  • The N1 or N2 does not increase or increases very slowly after EGT increases
  • There is no oil pressure indication by the time the engine is at stable idle
  • The EGT does not increase by 15 seconds after the FUEL CONTROL lever is moved to IDLE detent
  • The EGT quickly nears or exceeds the start limit
54
Q

To what speed is the speed bug automatically driven on a G/A and what does it represent?

A

Target airspeed for current flaps at MTOW

172 knots F15 / 202 knots F1

55
Q

How many spools does the CFM56 have?

56
Q

What is the source of pressurised air on the 737?

A
  • Engine bleed air (5th or 9th stages)
  • APU bleed air
  • External air
57
Q

Push and Park

Briefing / Calculation requirements

A
  • Briefing should be re done
  • Calculation must be re done

737 Info (3 decks)

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