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NAVIGATION SYSTEMS Navigation Systems 02.09.1 Flight Management System 02.09.1 Standby Instrument 02.09.3 Mode S Transponder Systems for Enhanced Surveillance 02.09.4
LIMITATIONS
TABLE OF CONTENTS
Page
ELECTRICAL MANAGEMENT SYSTEM
Circuit Breakers for Disabled Systems 02.10.1
Green Airplanes 02.10.1
EMS CDU Switch Control Page Settings 02.10.3
Green Airplanes 9005 and Subsequent 02.10.3
LIST OF ILLUSTRATIONS
CENTRE OF GRAVITY
Figure 02.03.1 Centre of Gravity (CG) Envelope 02.03.2
OPERATING LIMITATIONS
Figure 02.04.1 Altitude and Temperature Operating Limit 02.04.2
POWER PLANT
Figure 02.05.1 Engine Air Start Envelope 02.05.3
Figure 02.05.2 Engine Oil Pressure Limits 02.05.8
OPERATING SPEEDS
Figure 02.06.1 Maximum Operating Speed and Mach Number 02.06.1
Figure 02.06.2 Design Maneuvering Speeds 02.06.3
1. INTRODUCTION
A. General
The limitations included in this chapter contain items peculiar to the GLOBAL 5000. airplane. Observance of these limitations is mandatory.
B. Kinds of Airplane Operation
The airplane is certified for day and night operations, in the following conditions when the equipment and instruments required by the airworthiness and operating regulations are approved, installed and in an operable condition:
. VFR and IFR
The airplane is certified for ditching when the safety equipment specified by the applicable
regulations is installed.
The airplane is certified for flight in icing conditions.
The airplane is not to be used for transportation of passengers or cargo unless it has been
completed by the installation of an approved interior.
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1. STRUCTURAL WEIGHT
A. Structural Weight Limitations
Maximum taxi and ramp weight: 39,893 kg (87,950 lb)
Maximum take-off weight: 39,780 kg (87,700 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 23,224 kg (51,200 lb)
Minimum operating empty weight: 21,772 kg (48,000 lb)
Aircraft incorporating 40,687 kg (89,700 lb) MTOW placard
Maximum taxi and ramp weight: 40,801 kg (89,950 lb)
Maximum take-off weight: 40,687 kg (89,700 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 23,224 kg (51,200 lb)
Minimum operating empty weight: 21,772 kg (48,000 lb)
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