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59 Cards in this Set
- Front
- Back
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The B-737 airplanes are certified for __________ category Instrument Approaches
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C
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The maximum operating altitude for the B737-(700/800/900) is
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41,000 feet
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The runway slope limit is
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+/- 2%
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The maximum unrestricted takeoff / landing tailwind component is
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10 kts
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The maximum takeoff / landing altitude (300/500) is
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8,400 feet
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The maximum takeoff / landing altitude (700/800/900) is
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10,000 Feet
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What is the maximum flight operating latitude (700/800/900)?
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82 deg. North, 82 deg. South
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If landing weight exceeds the chart value in the Maximum Quick Turn Around Weight Limits chart,
wait at least ___________ then check thermal plugs (700) |
62 minutes
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If landing weight exceeds the chart value in the Maximum Quick Turn Around Weight Limits chart,
wait at least __then check thermal plugs (800/900) |
67 minutes
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(700/800/900) Installation of handle covers on the overwing exits must be verified prior to
departure whenever __________. |
passengers are carried
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The maximum safety relief differential pressure is (700/800/900)
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9.10 psi
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Takeoff in Moderate / Heavy Freezing Rain or Hail is __________.
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Prohibited
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__________ and __________ must be on during all ground operations when icing conditions exist
or are anticipated. |
Engine, wing anti-ice
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Do not operate wing anti-ice on the ground when OAT is above
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10-deg C / 50-deg F
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The minimum altitude for autopilot engagement (climb and cruise) is
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800 feet AGL
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Use of Aileron Trim with the Autopilot engaged is
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Prohibited
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The ILS autoland capability may only be used with flaps __________ and __________ with
__________ engine(s) operative |
30 and 40, both
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The maximum and minimum glideslope angles for autoland are ___ and __ respectively
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3.25 deg & 2.5 deg
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Maximum allowable headwind for autoland is __________ knots
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25
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Maximum allowable crosswind for autoland is __________ knots
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15
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Maximum allowable tailwind for autoland is __________ knots
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10
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APU bleed and electrical (simultaneous use) maximum altitude
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10,000 feet
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APU bleed (only) maximum altitude
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17,000 feet
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APU electrical load maximum altitude (300/500)
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35,000 feet
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APU electrical load maximum altitude (700/800/900)
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41,000 feet
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Do not use ___________ for ATC communications with ACARS operational, or if audio
entertainment system is in use |
VHF-3
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Do not use VHF COMM #2 or VHF COMM #3 on __________ MHZ as a primary means of
communications |
120.00 MHZ
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(700/800/900) Prohibited HF frequencies
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11.133, 22.434, 22.683, 22,766
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(700/800/900) Maximum single engine drive generator load (ground operations) __________ KVA
and __________ amps |
75 KVA - 215 amps
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Operation with assumed temperature reduced takeoff thrust and anti-skid inoperative is
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75 KVA - 215 amps
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Intentional use of reverse thrust in flight is
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Prohibited
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Operation with assumed temperature reduced takeoff thrust and anti-skid inoperative is
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not permitted
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Maximum N1 (700/800/900)
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104%
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Maximum N2 (700/800/900)
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105%
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Maximum EGT for Takeoff (5 minutes) [300/500]
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930 deg C
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Maximum EGT for Takeoff (5 minutes [700/800/900]
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950 deg C
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Maximum EGT for Continuous operations (700/800/900)
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925 deg. C
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Maximum EGT for Start
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725 deg. C
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Minimum Oil Pressure
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13 psi
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Maximum Oil Temperature (300/500)
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165 deg. C
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Maximum Oil Temperature (700/800/900)
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155 deg C
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Maximum Continuous Oil Temperature (700/800/900)
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140 deg C
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(700/800/900) Oil temperature are allowed to operate between 140 deg. C and 155 deg. C for
__________ minutes |
45
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(700/800/900) Operation with assumed temperature reduced for takeoff thrust is not permitted
with the Electronic Engine Control (EEC) in __________ mode. |
Alternate
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Maximum flap extension altitude
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20,000 feet
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(700/800/900) Holding in icing conditions with flaps extended
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is prohibited
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In flight, do not extend the SPEED BRAKE lever beyond
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FLIGHT DETENT
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Rapid and large alternating control inputs, in combination with large changes in pitch, roll, and
yaw may result in structural failure at __________ speed. |
Any
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Flap limit speeds for Flaps 1, 2, and 5 respectively (700/800/900)
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250kts
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Maximum Tank Fuel Temperature
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49C
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Random fuel imbalance must not exceed
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1,000 lbs.
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The Fuel Crossfeed valve must be ___________ for takeoff and landing
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closed
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Inflight tank fuel temperature must be maintained at least __________ above the freezing point of
the fuel being used or __________ whichever is higher (300/500) |
3 deg C, -45 deg. C
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For ground operations, center tank fuel pump switches must not be positioned to ON unless the
center tank fuel quantity exceeds __________ pounds |
1,000
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Maximum speed for Landing Gear Retraction
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235 kts
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Maximum speed for Landing Gear Extend
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270 kts/.82 mach
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Maximum speed for Landing Gear Extended
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320 knots / .82M
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For takeoff, use of Terrain Awareness and Terrain Display functions are prohibited until position
verification |
has been accomplished
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The use of Terrain Awareness and Terrain Display functions are prohibited the FMC is in
__________ only operation |
IRS
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