Boeing 737 Study Flash Cards

Front 1

Maximum Takeoff and Landing Tailwind Component

Back 1

10 Kts.

Front 2

Maximum speeds - VMO / MMO

Back 2

340 / .82

Front 3

Turbulence Penetration Speed

Back 3

280 / .76

Front 4

Maximum Operating Altitude

Back 4

41,000 Ft.

Front 5

The maximum cabin differential pressure (relief valves) is ?

Back 5

9.1 psi.

Front 6

With engine bleed air switches ON, do not operate the air conditioning packs in ?

Back 6

HIGH for takeoff, approach or landing.

Front 7

Engine TAI must be on when icing conditions exist or are anticipated, except during
climb and cruise 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.

Back 7

See other side.

Front 8

Icing Conditions exist when the OAT on the ground and for takeoff, or TAT
inflight is 10°C or below, and visible moisture in any form is present (such as
clouds, fog with visibility of one mile or less, rain, snow, sleet and ice
crystals).

Back 8

See other side.

Front 9

Icing conditions also exist when the OAT on the ground and for takeoff is
10°C or below when operating on ramps, taxiways or runways where surface
snow, ice, standing water, or slush may be ingested by the engines or freeze
on engines or nacelles.

Back 9

See other side.

Front 10

Do not rely on airframe visual icing cues to turn engine anti-ice on. Delaying the use
of engine anti-ice until ice buildup is visible from the cockpit may result in severe engine
damage.

Back 10

See other side.

Front 11

Do not use wing anti-ice as a substitute for ground de-icing/antiicing and inspection
procedures which are necessary to comply with operating rules.

Back 11

See other side.

Front 12

Do not operate wing anti-ice on the ground when the OAT is above 10 degrees C.

Back 12

See other side.

Front 13

Do not engage the autopilot on takeoff below 500 feet AGL.

Back 13

See other side.

Front 14

For single channel operation, the autopilot shall not remain engaged below 50 feet.

Back 14

See other side.

Front 15

For non-precision approaches, the autopilot must be disengaged no lower than the
applicable minimums minus 50 feet.

Back 15

see other side.

Front 16

Use of aileron trim with the autopilot engaged is PROHIBITED.

Back 16

See other side.

Front 17

The Autopilot/Flight director system has been certified for Category II and IIIa
Automatic Approach and Landing operations.

Back 17

See other side.

Front 18

Maximum allowable wind speeds (FOR AUTOLAND):
• Headwind 25 knots
• Crosswind 20 knots (15 knots for lower than Category I minimums)
• Tailwind 10 knots.

Back 18

See other side.

Front 19

Autoland capability may only be used with flaps 30 and 40 with both engines
operative.

Back 19

See other side.

Front 20

Maximum weights ?

Back 20

Taxi: 155,000 pnds
Takeoff: 154,500 pnds
Landing: 128,000 pnds.
Zero Fuel: 120,500 pnds.

Front 21

Do not use VHF-3 for ATC communications with ?

Back 21

ACARS operational.

Front 22

Engine Limit Display Markings ?

Back 22

Max and Min limits = Red line

Cautionary Range = Amber arc

Normal Operating Range = White arc

Front 23

When must the engine ignition be on ?

Back 23

Operation in heavy rain.

Front 24

What is the minimum time required between start attempts ?

Back 24

10 seconds.

Front 25

Is takeoff with the EEC's in Alternate mode allowed ?

Back 25

Yes. If:

No Derate or Assumed temperature thrust is used,

AND

BOTH EEC's are selected to the alternate mode.

Front 26

APU bleed + electrical load: MAX altitude ?

Back 26

10,000 ft.

Front 27

APU Bleed MAX altitude ?

Back 27

17,000 ft.

Front 28

APU electrical load MAX altitude ?

Back 28

41,000 ft.

Front 29

APU valve must be closed when ?

Back 29

1. ground air connected and isolation valve open.

2. engine no. 1 bleed valve open

3. isolation and engine no. 2 bleed valves open.

Front 30

APU bleed valve may be open during engine start, but avoid engine power above ?

Back 30

IDLE.

Front 31

Do not start or shut down APU during refueling operations.

Back 31

See other side.

Front 32

Do not deploy the speedbrakes in flight at radio altitudes less than 1,000 feet.

In flight, do not extend the SPEED BRAKE lever beyond the FLIGHT DETENT.

Back 32

See other side.

Front 33

QFE Selection:

QFE selected is Prohibited.

Back 33

See other side.

Front 34

DO NOT OPERATE WX RADAR DURING FUELING, NEAR FUEL SPILLS OR PEOPLE.

Back 34

See other side.

Front 35

Total fuel capacity:

Back 35

28,800 lbs center tank.

8,600 lbs main tanks.

Total: 46,000 lbs.

Front 36

Fuel tanks can be loaded individually, simultaneously, or in any sequence. Main
wing tanks must be scheduled to be full if the center wing tank contains more than
1,000 pounds of fuel.

Back 36

See other side.

Front 37

Allowable lateral imbalance between main tanks 1 and 2 must be scheduled to be
zero. Random fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or
landing.

Back 37

See other side.

Front 38

Intentional dry running of a center tank pump (low pressure light illuminated) is
prohibited

Back 38

See other side.

Front 39

Do not apply brakes until after touchdown.

Max flap extension altitude is 20,000 ft.

Holding in icing conditions with flaps extended is prohibited.

Back 39

See other side.

Front 40

Use of assumed temperature reduced takeoff thrust is prohibited under the following
conditions:

Back 40

Contaminated Runway,

Anti-skid Inoperative,

Windshear (known or suspected)

Front 41

Pilots are authorized to deviate from their current ATC clearance to the extent
necessary to comply with a TCAS II resolution advisory.

Back 41

See other side.