曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

operations, in the following conditions when the appropriate equipment and instruments required by
the airworthiness and operating regulations are approved, installed, and in an operable condition :
‐ VFR and IFR
‐ Extended overwater flight
‐ Flight in icing conditions
‐ Maximum number of passenger seats : 180.
KIND OF OPERATIONS
Applicable to: ,
, MSN,,
This airplane is certified in the public transport category (passengers and freight) for day and night
operations, in the following conditions when the appropriate equipment and instruments required by
the airworthiness and operating regulations are approved, installed, and in an operable condition :
‐ VFR and IFR
‐ Extended overwater flight
‐ Flight in icing conditions
‐ Maximum number of passenger seats : 220.
KIND OF OPERATIONS
Applicable to:
This airplane is certified in the public transport category (passengers and freight) for day and night
operations, in the following conditions when the appropriate equipment and instruments required by
the airworthiness and operating regulations are approved, installed, and in an operable condition :
‐ VFR and IFR
‐ Extended overwater flight
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
GENERAL LIMITATIONS
A318/A319/A320/A321 FLEET LIM-10 P 2/2
FCOM 19 AUG 10
‐ Flight in icing conditions
‐ Maximum number of passenger seats : 145.
MINIMUM FLIGHT CREW
Applicable to: ALL
The minimum flight crew consists of 2 pilots.
FLIGHT MANEUVERING LOAD ACCELERATION LIMITS
Applicable to: ALL
Clean configuration........................................................................................................ –1 g to +2.5 g
Slats and flaps extended......................................................................................................0 g to +2 g
Slats extended and flaps retracted.......................................................................................0 g to +2 g
MAXIMUM RECOMMENDED ALTITUDE IN CRUISE
Applicable to:
In manual mode, or with the AP engaged, it is recommended — for longitudinal stability reasons
— not to exceed the altitudes indicated on page Refer to PER-FPL-FLP-ALT-15 MAXIMUM
RECOMMENDED IN-CRUISE ALTITUDE, which differ from the ALL ENG MAX/OPT ALTITUDES.
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY
LIMITS
Intentionally left blank
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 FLEET LIM-11-PLP-TOC P 1/2
FCOM 19 AUG 10
LIM-11-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
CENTER OF GRAVITY LIMITS.........................................................................................................................1/10
WEIGHT LIMITATIONS.................................................................................................................................... 7/10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A318/A319/A320/A321 FLEET LIM-11-PLP-TOC P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 1/10
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to: ,
, MSN,
CG limits are given in percentage of the reference chord ‐ length aft of the leading edge.
‐ The reference chord length is 4.193 m (13.76 ft). It is 20.58 m (67.53 ft) aft of the aircraft nose.
‐ The CG must always be within these limits, regardless of fuel load.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 2/10
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to:
CG limits are ‐ given in percentage of the reference chord length aft of the leading edge.
‐ The reference chord length is 4.193 m (13.76 ft). It is 14.71 m (48.26 ft) aft of the aircraft nose.
‐ The CG must always be within these limits, regardless of fuel load.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
WEIGHT AND CENTER OF GRAVITY LIMITS
A318/A319/A320/A321 FLEET LIM-11 P 3/10
FCOM 19 AUG 10
CENTER OF GRAVITY LIMITS
Applicable to:
‐ CG limits are given in percentage of the reference chord length aft of the leading edge.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機(jī)組操作手冊FLIGHT CREW OPERATING MANUAL 5(62)