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737 Max 8 > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Takeoff Weight

A

78,652 Kg

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2
Q

Maximum Landing Weight

A

69,308 Kg

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3
Q

Maximum Taxi Weight

A

78,879 Kg

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4
Q

Maximum Zero Fuel Weight

A

65,952 Kg

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5
Q

Maximum Takeoff and Landing Altitude

A

8,400 Ft Pressure Altitude

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6
Q

Maximum and Minimum Glide Slope Angle for Autoland

A

3.25 Deg / 2.5 Deg

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7
Q

Use of Aileron Trim with AP Engaged

A

Is Prohibited

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8
Q

Minimum Altitude For AP Engagement for Takeoff

A

400ft AGL

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9
Q

Approaching Minimum Descent Altitude using AP during Single Channel Operations

A

FAA: 50ft AGL

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10
Q

Wind Limits for Autoland

A

Headwind 25kts
Crosswind 20kts
Tailwind 15kts

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11
Q

Do not use LVL CHG

A

Below 1,000ft AFE

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12
Q

Autoland limitation

A

Only to be used with Flaps 30 or 40 and both engines operative

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13
Q

Thrust Reversers are for…

A

Ground Operations Only

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14
Q

Use of Thrust Reversers in flight…

A

Is prohibited

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15
Q

Backing the plane with reverse thrust

A

Is prohibited

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16
Q

Use of Reverse Thrust during a balked landing

A

Do not attempt to Go Around after Reverse Thrust deployment on landing

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17
Q

Altitude Display Limits for RVSM

A

On Ground
From SL to 5,000 difference between Captain and FO display must not exceed 50ft.

From 5,001 to 10,000 difference between Captain and FO display must not exceed 60ft.

Difference between either display and field elevation must not exceed 75ft

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18
Q

Use of stand by altimeters for RVSM

A

Stand by altimeters do not meet accuracy requirements for RVSM airspace

19
Q

Max Allowable inflight difference between Captain and FO altitude display for RVSM Operstions

A

200ft

20
Q

APU Inflight Limits

A

Bleed + Electrical Load Max Altitude 10,000ft

21
Q

APU Ground Limitations

A

Bleed + Electrical Load Max Altitude 15,000ft

22
Q

APU General Limitations

A

Bleed Max Altitude 17,000ft
Electrical Load Max Alt. 41,000ft

23
Q

Maximum Operating Altitude

A

41,000ft Pressure Altitude

24
Q

Maximum Takeoff and Landing Tailwind Component

A

15 Knots
10 Knots FAA

25
Q

Maximum Flap Extended Altitude and Limitations

A

Max. Altitude With Flaps Extended 20,000ft

Holding in icing conditions with Flaps extended is prohibited

26
Q

Maximum Runway Slope

A

+/- 2%

27
Q

Severe Turbulent Air Penetration Speed

A

280 KIAS / .76M whichever is lower.
Applicable to Climb and Descent Only.

For Cruise refer to SP.16

28
Q

Maximum Cabin Differential Pressure

A

9.1 PSI

29
Q

Minimum Altitude for Speed Brakes

A

1,000ft AGL

30
Q

Speed Brakes Inflight Limitations

A

Do not extend beyond the FLIGHT detent.

Do not extend beyond the ARMED detent with Flaps 40.

31
Q

Ground Wind Operating Envelope

A

For XW >43 use Thrust normally used for taxi

For winds >58kts, limit engine thrust to idle. Except for takeoff

32
Q

Maximum tank fuel temperature

A

49 Deg C

33
Q

Minimum Tank Fuel Temperature prior to takeoff and inflight

A

-43 deg C or 3 Deg C above the fuel freezing point, whichever is higher

34
Q

Use of Center Tank Fuel Pump

A

Intentional Dry Running the pump is prohibited (Low Pressure Light Illuminated)

35
Q

Fuel Imbalance

A

Must be scheduled to be zero. Must not exceed 453 Kg

36
Q

Fuel Loading

A

Main Tanks 1 and 2 must be full if center tank contains >453 Kg

37
Q

Weather Radar

A

Avoid Weather Radar Operation in a Hangar or personal within the area. In hangar the test mode doesn’t apply

38
Q

Flight Controls Limitation

A

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw as they may result in structural failure at any speed, including below VA

39
Q

Operations with Assumed Temperature RTO Thrust

A

Is not permitted with Anti Skid Inop

40
Q

Engine Limit Displays Markings

A

Maximum and Minimum are Red

Cautions are Amber

41
Q

Alternate Flaps Duty Cycles

A

When extending or retracting the flaps with the alternate flaps position switch allow 15 seconds after releasing the alternate flaps position switch before moving the switch again to avoid damage to the alternate flaps motor clutch

42
Q

After complete extend or retract cycles 0 to 15 and back

A

Allow 5 minutes cooling before attempting another extension

43
Q

ADIRU Alignment Limitation

A

Air Data Inertial Reference Unit. The alignment must not be attempted at latitudes greater than 78 degrees 15 minutes

737 Max 8 (2 decks)

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