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General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.1
Airplane General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.1
Operational Limitations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.1
Non–AFMOperational Information . . . . . . . . . . . . . . . . . . . L.10.1
Weight Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.2
Door Mounted Power Assists and Escape Slides . . . . . . . . . L.10.2
Air Systems. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.2
Cabin Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.2
Autoflight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.2
Autopilot/Flight Director System . . . . . . . . . . . . . . . . . . . . . L.10.2
Automatic Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.3
Communications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.3
VHF Radios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.3
Engines, APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.3
Engine Limit DisplayMarkings . . . . . . . . . . . . . . . . . . . . . . L.10.3
Engine Fuel System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.3
Engine Ignition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.3
Reverse Thrust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.4
Non–AFMOperational Information . . . . . . . . . . . . . . . . . . . L.10.4
Airplane Structure. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.4
Flap Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.4
Warning Systems. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.4
TCAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.4
October 1, 2000
747 Operations Manual
Copyright © The Boeing Company. See title page for details.
L.TOC.0.2 D6-30151-425
Limitations -
Table of Contents
Intentionally
Blank
October 1, 2000
747 Operations Manual
Limitations Chapter L
Operating Limitations Section 10
Copyright © The Boeing Company. See title page for details.
D6-30151-425 L.10.1
General
This chapter contains Airplane Flight Manual (AFM) limitations and Boeing
recommended non-AFM operating limitations. Boeing recommended limitations
are provided for flight crew information. Limitations that are obvious, shown on
displays or placards, or incorporated within an operating procedure are not
contained in this chapter.
Airplane General
Operational Limitations
Non–AFM Operational Information
The turbulent air penetration speed is 290 to 310 KIAS/.82 to .85M.
The maximum takeoff and landing crosswind is 30 knots (not limiting).
Do not operate HF radios or weather radar during refueling operations.
Altitude Display Limits for RVSM Operations
Standby altimeters do not meet altimeter accuracy requirements of RVSM
airspace.
The maximum allowable in-flight difference between Captain and First Officer
altitude displays for RVSM operations is 200 feet.
Runway slope +/- 2%
Maximum Takeoff and Landing Tailwind
Component
15 knots
Maximum Operating Altitude 45,100 feet pressure altitude
Maximum Takeoff and Landing Altitude 10,000 feet pressure altitude
Maximum speed operating in Reduced Vertical
Separation Minimum (RVSM) Airspace
0.90 Mach
QFE Operations Prohibited
April 01, 2001
747 Operations Manual
Copyright © The Boeing Company. See title page for details.
L.10.2 D6-30151-425
Limitations -
Operating Limitations
The maximum allowable on-the-ground altitude display differences for RVSM
operations are:
Weight Limitations
Door Mounted Power Assists and Escape Slides
Main and upper deck door emergency power assists and evacuation slide systems
must be armed with the mode select lever in the AUTOMATIC position prior to
taxi, takeoff, and landing whenever passengers are carried in the respective area.
Air Systems
Cabin Pressurization
Autoflight
Autopilot/Flight Director System
The autopilot must not be engaged below a minimum engage altitude of 250 feet
after takeoff.
The autopilot must be disengaged before the airplane descends more than 50 feet
below the MDA unless it is coupled to an ILS glideslope and localizer or in the
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