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737 Training > Limits > Flashcards

Limits Flashcards

0
Q

Maximum Unrestricted TO/Landing Tailwind Component

A

10 knots

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1
Q

Maximum Pressure Altitude

A

41,000 feet

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2
Q

Maximum Restricted TO/Landing Tailwind Component

A

15 knots

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3
Q

Maximum Restricted Takeoff Parameters

A
  • Actual TW does not exceed Accuload authorized value
  • Runway clear and dry
  • Anti skid and TRs fully operational
  • Max TO thrust used
  • Speed brakes used and fully functional
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4
Q

Maximum Restricted Landing Parameters

A
  • Antiskid and TRs fully operational
  • Landing flaps 15/30/40
  • Speed brakes used, fully functional
  • Braking action reported at least good
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5
Q

MMO

A

.82 Mach

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6
Q

Max gear retraction speed

A

235 knots

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7
Q

Max gear extension speed

A

270 knots/.82 Mach

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8
Q

Max gear operating/extended speed

A

320 knots/.82 Mach

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9
Q

Recommended Severe Turbulence Penetration Speed

  • Cruise
  • Climb and Descent
A

Cruise: TURB N1 on cruise page

Climb/Descent: 280 knots/.76 Mach

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10
Q

Flap Speeds (-700)

A
  1. 250
  2. 250
  3. 250
  4. 210
  5. 195
  6. 170
  7. 165
  8. 156
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11
Q

Flap Speeds (-800)

A
  1. 250
  2. 250
  3. 250
  4. 210
  5. 200
  6. 190
  7. 175
  8. 162
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12
Q

Flap Speeds (-900)

A
  1. 250
  2. 250
  3. 250
  4. 205
  5. 200
  6. 195
  7. 180
  8. 170
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13
Q

Minimum Ground Time if Max Quick Turn Weight exceeded

Steel brakes
Carbon Brakes

A

Steel brakes: 67 minutes

Carbon brakes: 48 minutes

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14
Q

Recommended X-wind Component

Dry vs Wet

A

Dry takeoff: 34/33 knots
Wet takeoff: 25/25 knots

Dry Landing: 40/37 knots
Wet Landing: 40/37 knots

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15
Q

Max Takeoff Weights

-700
(-800)
(-900)
(-9ER)

A

(-700): 154,500 lbs
(-800): 174,200 lbs
(-900): 174,200 lbs
(-9ER): 187,700 lbs

*add 500# for Max Taxi Wts.

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16
Q

Max Landing Weight

-700
(-800)
(-900)
(-9ER)

A

(-700): 129,200
(-800): 144,000/146,300*
(-900): 147,300
(-9ER): 157,300

*planned future increase

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17
Q

Minimum number O2 bottles

A

One for each assigned flight attendant.

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18
Q

Max cabin pressure differential

A

9.1 psid

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19
Q

Max differential pressure for Takeoff and Landing

A

.125 psid

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20
Q

Use of Wing Anti-Ice on Ground?

A

Must use between engine start and takeoff when icing conditions exist or are anticipated, unless Type 2 or Type 4 fluid used.

Do not operate on ground if OAT > 10C

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21
Q

Minimum Autopilot Engagement Height

A

800 ft AGL

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22
Q

Max Winds for Autopilot

A

Headwind: 25 knots
Crosswind: 15 knots
Tailwind (flaps 30 and 40)*: 10 knots

*(-900[401-412]):
FE 6000 ft: 0 knots

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23
Q

Minimum Altitude for use of Autopilot on Approach

  1. ILS approach (no Autoland)
    2, non-precision approaches
A
  1. 50 ft AGL (ILS - no autoland

2. 50 ft below MDA/DA - non-precision

24
Q

Autoland Flap and Engine Restrictions

A

Flaps 30 or 40

Two engines required

25
Q

Maximum/Minimum Glideslope Angle for Autoland

A

3.25 to 2.5 degrees

26
Q

Restrictions associated with LiveTV system?

A

Do not operate KA system in OVERRIDE position in hangar, getting deiced or when MX performed in vicinity of antenna.

27
Q

Minimum battery voltage for APU start

A

23 volts

28
Q

Engine ignition must be on for:

A

Takeoff - Engine A/I operation

Landing - Heavy rain

29
Q

Minimum oil pressure

A

13 psi

30
Q

Maximum EGT limits

Takeoff
Max continuous
Start

A

Takeoff (5 minutes) - 950 deg. C
Maximum continuous - 925 deg. C
Start - 725 deg. C

31
Q

Engine starter duty cycle

Normal

A

Multiple consecutive attempts allowed. Each attempt limited to 2 minutes starter usage.
Minimum 10 seconds between attempts.

32
Q

Starter duty cycle

Extended engine motorings

A

Starter usage limited to 15 minutes for the first 2 extended engine motorings.

A minimum of 2 minutes needed between each attempt.

For 3rd and subsequent times, starter usage limited to 5 minutes. 10 minutes required between each attempt.

33
Q

RPM Maximum

A

N1- 104%

N2- 105%

34
Q

Limits on Use of Reduced Thrust

A

Not permitted with Antiskid inop.

Not permitted when runway contaminated with standing water, ice, slush or snow.

35
Q

Limits EEC control

A

Must be in ON or ALT for takeoff.

Reduced thrust not permitted with EEC in ALTN mode.

36
Q

APU MAXIMUM ALTITUDES

A

APU bleed and electrical 10,000 ft
APU bleed 17,000 ft
APU electrical load 41,000 ft

37
Q

Minimum Oil Quantity prior to start.

A

60%

38
Q

APU Starter Duty Cycle

A

For both ground and air starts, 15 minutes cooling required after 3rd attempt.

39
Q

APU bleed air restriction after start?

A

Wait one minute after start before using bleed air.

40
Q

APU shutdown restriction?

A

Wait minimum of 2 minutes for APU shutdown before switching batteries off.

41
Q

When must APU bleed valve be closed?

A
  • Ground pneumatic air is connected and isolation valve is open.
  • Engine No. 1 bleed valve is open
  • Isolation valve is open and engine No. 2 bleed valve is open

Note: APU bleed valve may be open during engine start, but avoid power above idle.

42
Q

Engine fire extinguisher bottle pressure

A

800 psi at 70 deg. F

43
Q

Maximum flap extension altitude?

A

20,000 feet

44
Q

Holding in icing conditions

A

Prohibited with flaps extended.

45
Q

Alternate flap duty cycle?

A

Allow 15 seconds after releasing alternate flaps position switch before moving switch again.

After complete cycle (0-15-0), allow 5 minutes cooling.

46
Q

Max airspeed for alternate flaps?

A

230 knots.

47
Q

Maximum speed if Mach Trim Fail (both channels)?

A

280 knots, .82 Mach.

48
Q

Maximum in-flight altimeter difference for RVSM?

A

200 feet.

49
Q

Maximum altimeter difference on ground for RVSM?

A

Field elev. Cap-FO Alt/Field

SL-5000 50 75

10,000 60 75

50
Q

WX radar use on ground?

A

Not during fueling, within 50 feet of fuel spill, or within 15 feet of people except in test mode.

51
Q

Fuel Temp Limitations

A

Jet A: -37 deg C to +49 deg C

52
Q

Fuel Tank Capacity

A

Wing tanks:
8630#
Center tank: 28,803#

53
Q

Fuel Loading Limitation

A

Main wing tanks 1 and 2 must be full if >1000# in center tank.

Okay if <1000# and partial wing tank fuel if balance okay.

54
Q

If center tank fuel <5000 lbs…

A

Center tank pumps must be off for takeoff.

55
Q

Fuel CONFIG annunciator?

A

Center tank fuel >1,600 lbs, and the center pump switches are off.

56
Q

Minimum fuel for ground operation of hydraulic pumps?

A

1675 lbs. in related tank

57
Q

Max tire groundspeed?

A

195 knots

58
Q

Max fuel imbalance?

A

Must be scheduled 0 imbalance.

Imbalance in flight should not exceed 1000 lbs.

737 Training (4 decks)

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