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时间:2011-03-20 15:27来源:蓝天飞行翻译 作者:admin
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Non–AFM Operational Information
Do not start or shut down APU during refueling operations.
Airplane Structure Flap Operation
Do not extend flaps above 20,000 feet.
Non-AFM Operational Information
Use of speed brakes in flight with flaps extended past 20 is not recommended. Ground wind limits for all doors:
.
40 knots while opening or closing

.
65 knots while open


Warning Systems TCAS
Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS II resolution advisory (RA).
Copyright . The Boeing Company. See title page for details.
L.10.4 D6-30151-425 April 01, 2001


Introduction........................................ NP.10.1

General ........................................... NP.10.1 ControlsandIndicators–Nomenclature............... NP.10.1 NormalProcedures.................................. NP.10.1 AutopilotFlightDirectorSystemandFlight ManagementSystemMonitoring.................... NP.10.3 CDUOperation.................................. NP.10.3 PreflightandPostflightAreasofResponsibilityand PanelFlow........................................ NP.10.4 PilotFlyingandPilotNotFlyingAreasof Responsibility...................................... NP.10.5
AmplifiedProcedures ................................ NP.20.1

ExteriorInspection.................................. NP.20.1
PreflightProcedure–FirstOfficer...................... NP.20.1
PreflightProcedure–Captain......................... NP.20.10
BeforeStartProcedure .............................. NP.20.14
EngineStartProcedure.............................. NP.20.18
AfterStartProcedure ............................... NP.20.19
BeforeTakeoffProcedure............................ NP.20.19
TakeoffProcedure.................................. NP.20.20
ClimbandCruiseProcedure.......................... NP.20.21
ApproachandLandingProcedure...................... NP.20.22
Go–AroundProcedure .............................. NP.20.23
LandingRollProcedure ............................. NP.20.24
AfterLandingProcedure............................. NP.20.24
ShutdownProcedure................................ NP.20.25
SecureProcedure................................... NP.20.26

Copyright.TheBoeingCompany.Seetitlepagefordetails.
April01,2001 D6-30151-425 NP.TOC.0.1
Normal Procedures -Table of Contents

FlightPatterns ...................................... NP.30.1

Takeoff............................................ NP.30.1
ILSApproach ...................................... NP.30.2
ILSApproach(Manual) .............................. NP.30.3
Non–PrecisionApproach.............................. NP.30.4
Circling ........................................... NP.30.5
VisualTrafficPattern................................. NP.30.6

Copyright.TheBoeingCompany.Seetitlepagefordetails.

NP.TOC.0.2 D6-30151-425 April 01, 2001

747 Operations Manual

General
This chapter contains Normal Procedures. It incorporates routine normal procedures and associated flight patterns.
Controls and Indicators – Nomenclature
Controls and indications appear in all UPPERCASE type to correspond to the words on the control panel or display. For example, the following item has UPPERCASE words to match what is found on the panel:
PASSENGER OXYGEN switch .................... NORM (guarded position) The word PASSENGER is spelled out, even though it is abbreviated on the panel. The following appears in all lower case because there are no words identifying the
panel name:
Fuel panel............................................................................................ Set

Normal Procedures
Normal procedures are used by the trained flight crew to ensure airplane condition is acceptable and the flight deck is correctly configured for each phase of flight. These procedures assume all systems are operating normally and automated features are fully used.
Procedures are performed from recall and follow a panel flow. These procedures are designed to minimize crew workload and are consistent with flight deck technology. If the correct indication is not observed during accomplishment of procedures, verify controls are positioned correctly. If necessary, check the appropriate circuit breaker(s) and test the related system light(s).
Before engine start, lights or indications verify systems’ condition or configuration. Review EICAS alert messages and status display before engine start to determine if messages are displayed which may affect dispatch and require maintenance action or compliance with the Minimum Equipment List (MEL).
After engine start, it is not necessary to check status messages as any message having an adverse effect on safe continuation of the flight, and requiring crew attention, will appear as an EICAS alert message (warning, caution, or advisory).
 
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