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CSP 700−6
Volume 1
02−00−3
Page
NAVIGATION SYSTEMS
Standby Instrument 02−09−7
Mode S Transponder Systems for Enhanced Surveillance 02−09−7
ELECTRICAL MANAGEMENT SYSTEM
Circuit Breakers for Disabled Systems 02−10−1
Green Airplanes 9005 thru 9010 not Incorporating Service Bulletin
700−24−045 02−10−1
Green Airplanes 9002, 9011 thru 9051 not Incorporating Service Bulletin
700−24−045 02−10−3
Green Airplanes 9003, 9004 and 9052 thru 9122 not Incorporating Service
Bulletin 700−24−045 02−10−5
Green Airplanes 9123 and Subsequent and Airplanes Incorporating SB
700−24−045 02−10−7
EMS CDU Switch Control Page Settings 02−10−9
Green Airplanes 9005 and Subsequent 02−10−9
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 02−05−11
OPERATING SPEEDS
Figure 02−06−1 Maximum Operating Speed and Mach Number 02−06−1
Figure 02−06−2 Design Maneuvering Speeds 02−06−4
LIMITATIONS
TABLE OF CONTENTS
Flight Crew Operating Manual REV 53, Jan 29, 2007
CSP 700−6
Volume 1
02−00−4
Page
1. INTRODUCTION
A. General
The limitations included in this chapter contain items peculiar to the GLOBAL EXPRESS®
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.
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.
LIMITATIONS
INTRODUCTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−01−1
LIMITATIONS
INTRODUCTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
02−01−2
THIS PAGE INTENTIONALLY LEFT BLANK
1. STRUCTURAL WEIGHT
A. Structural Weight Limitations
Maximum taxi and ramp weight: 42,525 kg (93,750 lb)
Maximum takeoff
weight: 42,415 kg (93,500 lb)
Maximum landing weight: 35,655 kg (78,600 lb)
Maximum zero fuel weight: 25,400 kg (56,000 lb)
Minimum flight weight: 21,856 kg (48,200 lb)
Minimum operating empty weight: 20,415 kg (45,000 lb)
(If 43,091 kg (95,000 lb) MTOW placard is installed)
Maximum taxi and ramp weight: 43,205 kg (95,250 lb)
Maximum takeoff
weight: 43,092 kg (95,000 lb)
Maximum landing weight: 35,655 kg (78,600 lb)
Maximum zero fuel weight: 25,400 kg (56,000 lb)
Minimum flight weight: 21,856 kg (48,200 lb)
Minimum operating empty weight: 20,415 kg (45,000 lb)
(If 43,545 kg (96,000 lb) MTOW placard is installed)
Maximum taxi and ramp weight: 43,659 kg (96,250 lb)
Maximum takeoff
weight: 43,546 kg (96,000 lb)
Maximum landing weight: 35,655 kg (78,600 lb)
Maximum zero fuel weight: 25,400 kg (56,000 lb)
Minimum flight weight: 21,856 kg (48,200 lb)
Minimum operating empty weight: 20,415 kg (45,000 lb)
(If 44,452 kg (98,000 lb) MTOW placard is installed)
Maximum taxi and ramp weight: 44,565 kg (98,250 lb)
Maximum takeoff
weight: 44,452 kg (98,000 lb)
Maximum landing weight: 35,655 kg (78,600 lb)
Maximum zero fuel weight: 25,400 kg (56,000 lb)
Minimum flight weight: 21,856 kg (48,200 lb)
Minimum operating empty weight: 20,415 kg (45,000 lb)
NOTE
The maximum takeoff
weight (MTOW) and/or maximum landing
weight (MLW) may be further limited due to performance
considerations.
LIMITATIONS
STRUCTURAL WEIGHT
REV 42, Nov 26, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−02−1
1. STRUCTURAL WEIGHT (CONT'D)
B. Buoyancy Limitations
(1) TAKE-OFF ON RUNWAYS NEAR BODIES OF WATER
· For takeoff
at weights above the maximum landing weight, OUTFLOW VLV 2 must
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