曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

CSP 700−1A
02−00−3
Page
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 02−06−3
LIMITATIONS
TABLE OF CONTENTS
DOT Approved
REV 52, Nov 10, 2006
Airplane Flight Manual
CSP 700−1A
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
DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−01−1
LIMITATIONS
INTRODUCTION
DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−01−2
THIS PAGE INTENTIONALLY LEFT BLANK
1. STRUCTURAL WEIGHT
A. Structural Weight Limitations
Maximum taxi and ramp weight: 42,524 kg (93,750 lb)
Maximum takeoff
weight: 42,411 kg (93,500 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 21,863 kg (48,200 lb)
Minimum operating empty weight: 20,412 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: 43,091 kg (95,000 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 21,863 kg (48,200 lb)
Minimum operating empty weight: 20,412 kg (45,000 lb)
(If 43,545 kg (96,000 lb) MTOW placard is installed)
Maximum taxi and ramp weight: 43,658 kg (96,250 lb)
Maximum takeoff
weight: 43,545 kg (96,000 lb)
Maximum landing weight: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 21,863 kg (48,200 lb)
Minimum operating empty weight: 20,412 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: 35,652 kg (78,600 lb)
Maximum zero fuel weight: 25,401 kg (56,000 lb)
Minimum flight weight: 21,863 kg (48,200 lb)
Minimum operating empty weight: 20,412 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
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
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
be closed and one airconditioning
pack must be shutdown for takeoff.
(2) LANDING ON RUNWAYS NEAR BODIES OF WATER
· For forced / emergency landing at weights above the maximum landing weight,
OUTFLOW VLV 2 must be closed and one airconditioning
pack must be shutdown for
landing.
LIMITATIONS
STRUCTURAL WEIGHT
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
02−02−2
1. CENTRE OF GRAVITY
A. Centre Of Gravity Limits
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−1.
The airplane including interior payload, passengers and fuel must be loaded such that the
airplane weight and centre of gravity are maintained within the specified limits (including any
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Bombardier LIMITATIONS(2)