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

S4-41 thru S4-70 Revised 1 S4-AA
S4-71 thru S4-85/S4-86 Added 1 S4-AA
S4-2 S4-AA 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
SERVICE BULLETIN CONFIGURATION LIST
The following is a list of Service Bulletins that are applicable to the operation of the airplane, and
have been incorporated into this supplement. This list contains only those Service Bulletins that are
currently active.
Number Title
Airplane Serial
Effectivity
Revision
Incorporated
Incorporated
in Airplane
SB510-03-01 Certification Requirements -
FAA to EASA Registration
Conversion
510-0001 thru
-0020
0
SB510-34-02 Navigation - Hardware and
Software Update for Garmin
G1000 Avionics
510-0001 thru
-0065
2
510FM-S4-02 S4-AA S4-3
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
AIRPLANE CONFIGURATION CODES
The following is a list of airplane configuration codes which appear at the bottom of each page of this
supplement to the basic FAA Approved Airplane Flight Manual. The codes indicate page effectivity
by serial number. This list contains only the configurations which have been incorporated into this
supplement.
Configuration
Code
Effectivity by
Serial Number
Applicable
Configuration Code
S4-AA Airplanes 510-0001 thru -0020 Incorporating SB510-03-01
and 510-0021 and On
S4-AH Airplanes 510-0001 thru -0065 incorporating SB510-34-02
(Navigation - Hardware and Software Update for Garmin
G1000 Avionics) and Airplanes 510-0066 and On
S4-AI Airplanes 510-0001 thru -0065 not incorporating
SB510-34-02 (Navigation - Hardware and Software Update
for Garmin G1000 Avionics)
S4-4 S4-AA 510FM-S4-02
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
EASA CERTIFIED AIRPLANES
INTRODUCTION
This supplement is part of, and must be placed in the basic FAA Approved Airplane Flight Manual for
EASA Certified Airplanes. The information contained herein supplements the information of the basic
FAA Approved Airplane Flight Manual. For limitations, procedures, and performance information not
contained in the supplement, consult the basic FAA Approved Airplane Flight Manual.
OPERATING LIMITATIONS
Crews must use supplemental oxygen continuously any time the cabin altitude exceeds 10,000 feet.
Use of the lavatory is prohibited during taxi, takeoff and landing, or during periods of turbulence. The
lavatory seat is limited to one occupant in flight.
Any carry-on items stowed on the lavatory seat must be verified to be adequately secured using the
supplied cargo net. Maximum total weight for items stowed on the lavatory seat is 13kg (30lbs).
Dispatch with antiskid inoperative is prohibited on wet or contaminated runways.
OPERATING PROCEDURES
The operating procedures are the same as those in the basic FAA Approved Airplane Flight Manual
except as follows:
EMERGENCY PROCEDURES
No change.
ABNORMAL PROCEDURES
CABIN ALTITUDE - WHITE
This message is displayed when the pressurization system is operating in the High Altitude Airfield
mode and the cabin altitude exceeds 10,000 feet for less than 30 minutes. The crew is required to
use supplemental oxygen continuously any time the cabin altitude exceeds 10,000 feet.
NORMAL PROCEDURES
No change.
510FM-S4-00 S4-AA S4-5
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 4
FAA APPROVED
U.S. Configuration
PERFORMANCE
TABLE OF CONTENTS
Page
WET RUNWAY TAKEOFF PERFORMANCE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . S4-7
TAKEOFF FIELD LENGTH - FEET, FLAPS UP ANTI-ICE OFF . . . . . . . . . . . . . . . . . . . . S4-9
TAKEOFF FIELD LENGTH - FEET, FLAPS UP ANTI-ICE ON . . . . . . . . . . . . . . . . . . . S4-25
TAKEOFF FIELD LENGTH - FEET, FLAPS 15° ANTI-ICE OFF . . . . . . . . . . . . . . . . . . S4-41
TAKEOFF FIELD LENGTH - FEET, FLAPS 15° ANTI-ICE ON . . . . . . . . . . . . . . . . . . . S4-57
LANDING PERFORMANCE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . S4-73
DATA FOR WATER, SLUSH, SNOW, AND ICE COVERED RUNWAYS . . . . . . . . . . . . . . . S4-76
ADVERSE RUNWAY TAKEOFF PERFORMANCE. . . . . . . . . . . . . . . . . . . . . . . . . . . . S4-78
ADVERSE RUNWAY LANDING PERFORMANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . S4-81
S4-6 S4-AA 510FM-S4-01
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 4
FAA APPROVED
Configuration U.S.
WET RUNWAY TAKEOFF PERFORMANCE
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 2(22)