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85 Cards in this Set
- Front
- Back
The maximum T/O and landing tailwind component on a dry or wet runway (non contaminated) is ?
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10 kts (or 15kts as certified) including gusts
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The maximum speed with the MACH TRIM system inoperative is?
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Classics:0.74M, NG's 280/0.82M
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The recommended turbulent penetration airspeed is
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Classics: 280Kts/0.73M, NG's: 280Kts/0.76M
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The maximum landing weight of the B737-300 is
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51,709 Kg
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The maximum time limit for take-off thrust is
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5 minutes
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The maximum speed for landing gear extension is
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270 kt. or .82M
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The maximum speed for landing gear retraction is
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235 Kts
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The maximum speed for landing gear extended is
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320 kt. or .82M
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The T.R. voltage range is
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24 - 30 volts.
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The maximum wind speed for airstair operation is
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40 Kts
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The runway slope limits are
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+/- 2 %
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The maximum differential pressure is
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Classics: 8.65 psi, NG: 9.1 psi
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The maximum cabin differential pressure for take-off and landing is
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.125 psi
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The operating differential pressure (FLT ALT set at 27,000 feet) is
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7.45 psi
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The APU maximum EGT is
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760C Garrett Only
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The maximum APU operating continuous EGT is
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710C Garrett only
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The maximum aircraft altitude for both APU bleed and electrical load is
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10,000 feet
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The maximum aircraft altitude for APU bleed only is
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17,000 feet
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The maximum aircraft altitude for APU generator use is
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Garrett: 35,000ft, Sundstrand: 37,000ft, NG: 41,000ft.
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The battery voltage range is
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22 - 30 volts
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The maximum Generator Drive oil temperature / temperature rise is
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157 degrees C / 20 degrees C
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The maximum flap extension altitude is
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20,000 feet
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The maximum fuel temperature is
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49 degrees C
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The minimum fuel temperature is
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Fuel freeze point plus 3 degrees C, or -45 degrees C, whichever is higher.
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The minimum fuel required for ground operation of the hydraulic electric pumps is
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760 KGS in respective wing tank
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When should window heat switched on
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10 minutes before take-off
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The maximum external air pressure (ground cart) is
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60 PSI (at 232 degrees C).
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The Maximum N1 RPM is
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106%.
NG 105% |
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The Maximum N2 RPM is
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105%
NG 104% |
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The maximum EGT for take-off is
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930 degrees C
NG 950 C |
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The maximum start engine EGT is
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725 degrees C
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The minimum engine oil pressure is
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13 psi
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The maximum continuous engine oil temperature is
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160 degrees C
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The minimum operating brake pressure indication is
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2800 psi
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The minimum start pressure at 2000 feet above sea level (prior to starter engagement) is
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29 psi
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The recommended refuelling nozzle pressure is
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50 psi
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Do not operate engine or wing anti-ice when the temperature is above
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10 degrees C TAT
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The manoeuvre speed with flap 5 (gross weight of 52,000 kgs) is
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180 Kts
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Starter assist (inflight engine start) should be used when N2 is below
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15%
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For all revenue flights, the escape slide retention bar must be installed during
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Taxy, take-off and landing
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The maximum operating altitude of the B737 is
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Classics: 37,000ft, NG's: 41,000ft
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The maximum altitude for take-off and landing is
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8,400 feet
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The flight operating latitude limits of the B737-3/4/500 are
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73 degrees North and 60 degrees South
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The maximum wind allowable for airstairs to remain extended is
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60 kts
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When engine bleeds are ON, both air conditioning packs must be set to
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AUTO or OFF for take-off, approach or landing
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The APU bleed valve must be closed whenever the
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Ground air connected and isolation valve open. L.H. engine bleed valve open (L.H. engine running above idle power) Isolation and R.H. engine bleed valves open (with the R.H. engine running above idle power).
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Except for ER operation, one air-conditioning pack may be inoperative provided altitude is limited to
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FL 250
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Speedbrake should not be deployed in flight at radio altitudes less than
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1000 feet
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The duty cycle of the Alternate flap system is
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Flaps 0-15; 5 minutes off.
Flaps greater than 15; 25 minutes off |
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The autopilot must not be engaged on take-off below
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Classics: 1000ftAGL - NG's: 400 feet AGL
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For single channel operation, the autopilot shall not be engaged below
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140 feet AGL
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During VOR approaches what must one pilot have displayed
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One pilot must have raw data, from the VOR associated with the approach, displayed in the HSI VOR/ILS mode not later than the final approach fix.
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The maximum fuel tank quantities (Classics) are
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4,828 kgs in each wing tank, 7449 kgs in the centre tank
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The maximum lateral fuel imbalance between wing tanks 1 and 2 must be scheduled to be zero and, for all phases of flight, must not exceed
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453 kgs
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The wing fuel tanks must be full if the centre tank contains more than
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453 kgs
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The engine Thermal Anti Ice must be on when icing conditions exist or are anticipated, except during climb or cruise when the temperature is below
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-40 degrees C SAT.
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Do not operate weather radar
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During fuelling, near fuel spills or people
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Engine ignition must be on for
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Take-off and landing
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The maximum continuous engine EGT is
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895 degrees C
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The maximum allowable engine oil temperature is
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165 degrees C
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The engine start duty cycle (normal start) is
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First attempt: 2 minutes on, 20 seconds off
Second and subsequent attempts: 2 minutes on, 3 minutes off |
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Both PMCs must be
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On or Off for take-off.
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What are the max differential restrictions when ANY window in the cockpit has a cracked outer pane
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No restrictions
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What is the minimum engine oil quantity (per engine) for despatch for an aircraft with EIS
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75% Full
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For an automatic landing the head and crosswind limits are
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Headwind limit is 25 kts and the crosswind limit is 15 kts.
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The maximum tailwind for T/O and landing on a contaminated runway is
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0 kts.
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The maximum windspeed for taxying is
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65 kts
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The maximum depth of Dry Snow (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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60 mm
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The maximum depth of Wet Snow (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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15 mm
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The maxImum depth of Compacted Snow/Slush (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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13 mm
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The engine start duty cycle (normal start) is
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First attempt: 2 minutes on, 20 seconds off
Second and subsequent attempts: 2 minutes on, 3 minutes off |
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Both PMCs must be
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On or Off for take-off.
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What are the max differential restrictions when ANY window in the cockpit has a cracked outer pane
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No restrictions
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What is the minimum engine oil quantity (per engine) for despatch for an aircraft with EIS
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75% Full
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For an automatic landing the head and crosswind limits are
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Headwind limit is 25 kts and the crosswind limit is 15 kts.
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The maximum tailwind for T/O and landing on a contaminated runway is
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0 kts.
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The maximum windspeed for taxying is
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65 kts
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The maximum depth of Dry Snow (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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60 mm
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The maximum depth of Wet Snow (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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15 mm
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The maxImum depth of Compacted Snow/Slush (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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13 mm
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The maximum depth of Standing Water (runway contaminant) for take-off based on maximum figures available for calculation of performance is
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13 mm
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The maximum crosswind component (including gusts) for taking-off and landing on a runway where braking action is reported as GOOD is
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35 kts
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The maximum crosswind component (including gusts) for taking-off and landing on a runway where braking action is reported as MEDIUM is
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25 kts
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The maximum crosswind component (including gusts) for taking-off and landing on a runway where braking action is reported as MEDIUM/POOR is
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20 kts
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What is the category of the B737 brakes
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A
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