Engines,APU........................................ SP.7.1
EngineContinuousIgnition............................. SP.7.1
EngineCrossbleedStart ............................... SP.7.1
EngineGroundPneumaticStart ......................... SP.7.1
EngineManualStart.................................. SP.7.1
FireProtection....................................... SP.8.1
Engine/APU/Cargo/Fire/OverheatTest ................... SP.8.1
SquibTest .......................................... SP.8.1
FlightInstruments,Displays........................... SP.10.1
HeadingReferenceSwitchOperation.................... SP.10.1
FlightManagement,Navigation........................ SP.11.1
IRSFastRealignment................................ SP.11.1
IRSHighLatitudeAlignment.......................... SP.11.1
WeatherRadarTest.................................. SP.11.1
Fuel ............................................... SP.12.1
FuelBalancing...................................... SP.12.1
AdverseWeather .................................... SP.16.1
Introduction........................................ SP.16.1
ColdWeatherOperation .............................. SP.16.1
Preflight........................................ SP.16.2
EngineStart..................................... SP.16.3
AfterStart....................................... SP.16.3
Taxi–Out........................................ SP.16.4
BeforeTakeoff................................... SP.16.5
ClimbandCruise................................. SP.16.5
Secure ......................................... SP.16.6
HotWeatherOperation............................... SP.16.7
EngineOperationinHeavyRainorHail ................. SP.16.8
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747 Operations Manual
Turbulence.......................................... SP.16.8
SevereTurbulence................................. SP.16.9
Windshear......................................... SP.16.10
WindshieldWasherandRainRepellent.................. SP.16.10
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General
This chapter contains procedures (adverse weather operation, engine crossbleed start, and so on) accomplished as required rather than routinely performed on each flight. Systems tests are described in the System Description chapter of the applicable system.
Note: System tests are not normally a flight crew action.
Procedures accomplished in flight, or those that are an alternate means of accomplishing normal procedures (such as manual engine start), are usually accomplished by recall. Infrequently used procedures, not normally accomplished (such as engine crossbleed start) are usually accomplished by reference.
Supplementary procedures are provided by section. Section titles correspond to the related chapter title for the system being addressed except for the Adverse Weather section.
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Oxygen Test
Oxygen Mask................................................................................Stowed Verify doors closed. FLIGHT INTERPHONE TRANSMITTER Selector.......................MIC SPEAKER Selector ............................................................................ON STATUS DISPLAY Switch...............................................................Push Crew Oxygen Pressure.......................................................Check EICAS Note oxygen pressure. RESET/TEST Slide Lever ................................................ Push and Hold Verify yellow cross appears momentarily in flow indicator. EMERGENCY/TEST Selector.........................................Push and Hold Simultaneously push Emergency/Test selector and Reset/Test slide lever. Verify yellow cross appears continuously in flow indicator. PUSH-TO-TALK Switch...................................................................INT Verify oxygen flow sound is heard through the flight deck loudspeaker. EMERGENCY/TEST Selector....................................................Release RESET/TEST Slide Lever ........................................................... Release Verify yellow cross no longer appears in flow indicator. NORMAL/100% Selector .............................................................. 100% Leave N/100% selector in 100% position. Crew Oxygen Pressure.......................................................Check EICAS Verify pressure decreases no more than 30 psi during test and pressure adequate for dispatch.
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