• 热门标签

当前位置: 主页 > 航空资料 > 飞行资料 >

时间:2010-09-25 20:27来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Airplane Flight Manual.
Accordingly, Item 18 “Statement of Compliance”, Item 19 “Date of Issuance” and Item 20 “Signature”,
which are parts of “ICAO Format” but not appropriate for inclusion in the Airplane Flight Manual, are
deleted. In respect of the Airplane Flight Manual which is published and managed by Aircraft Type, it
may be a case that Item 4 “Nationality and Registration Marks” and Item 6 “Aircraft Serial Number”
are blank.
ENGINE EMISSIONS
FUEL VENTING
This aircraft complies with the requirements of Japan Civil Aeronautics Regulations, Appendix 3,
"Engine Emission Standard", Chapter 1, "Fuel Venting".
NOTE
The above are in accordance with ICAO Annex 16, Vol. 2, Part II, Chapter 2.
EXHAUST EMISSIONS
This aircraft complies with the requirements of Japan Civil Aeronautics Regulations, Appendix 3,
"Engine Emission Standard", Chapter 2, "Exhaust Emissions".
SMOKE
The certified numbers shown are based on 6.49 kN (1460 lb) maximum thrust from the PW615F-A
turbofan engine.
NOTE
The above are in accordance with ICAO Annex 16, Vol. 2, Part III, Chapter 2.2.
HYDROCARBONS, CARBON MONOXIDE, AND OXIDES OF NITROGEN
Not applicable due to 6.49 kN (1460 lb) rated thrust on aircraft engine.
NOTE
The above are in accordance with ICAO Annex 16, Vol. 2, Part III, Chapter 2.3.
SMOKE NUMBER LIMIT
TAKEOFF 5.4 50.0
510FM-S12-00 S12-AA S12-7/S12/8

MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
FAA APPROVED
Configuration U.S.
WEIGHT AND BALANCE DATA AND AIRPLANE
EQUIPMENT LIST
This section consists of a copy of the Airplane Weighing Form and the Airplane Equipment List, both
of which are furnished with the airplane. For weight and center of gravity limitations refer to Section
2. For weight and balance information refer to the Model 510 Weight and Balance manual
(510WB-00 or latest revision)
510FM-06 AA 6-1/6-2

COPYRIGHT © 2006
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
U.S.
FAA Approved in normal category based on 14 CFR 23. This document must be carried in the airplane at all
times, and be kept within reach of the pilot during all flight operations. This manual includes the material required
to be furnished to the pilot by 14 CFR 23 and the applicable special conditions.
SERIAL NUMBER
REGISTRATION NUMBER
510WB-01
24 AUGUST 2006
REVISION 1 04 APRIL 2007

MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
LOG OF EFFECTIVE PAGES
FAA APPROVED
U.S.
LOG OF EFFECTIVE PAGES
Use this page to determine the currency and applicability of your FAA Approved Weight and Balance
Manual. Pages affected by the current revision are indicated by an asterisk (*) preceding the pages
listed under the Page Number column.
The following is a description of the columns in the Log of Effective Pages:
Page Number - FAA Approved Weight and Balance Manual page numbers.
Page Status - Indicates if the page has been added, revised or deleted by the current revision.
Revision Number - Indicates the revision number.
Revision Number Date
Original 24 August 2006
Revision 1 04 April 2007
Page
Number
Page
Status
Revision
Number
* Title Revised 1
* i thru ii Revised 1
Contents Original 0
6-1/6-2 thru 6-14 Original 0
* 6-15 thru 6-17/6-18 Revised 1
6-19 thru 6-38 Original 0
* 6-39 thru 6-40 Revised 1
6-41 thru 6-43 Original 0
* 6-44 thru 6-45 Revised 1
6-46 thru 6-53 Original 0
* 6-54 thru 6-55 Revised 1
6-56 thru 6-61 Original 0
* 6-62 thru 6-63 Revised 1
6-64 thru 6-69/6-70 Original 0
510WB-01 i
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
LOG OF EFFECTIVE PAGES
FAA APPROVED
U.S.
Weight and Balance Data Sheets
Form
Number
Original
Date
Revision
Date
2195 24 August 2006 04 April 2007
2234 24 August 2006 04 April 2007
2235 24 August 2006
2236 24 August 2006
2237 24 August 2006
2238 24 August 2006
2239 24 August 2006
2240 24 August 2006
2241 24 August 2006 04 April 2007
2242 24 August 2006 04 April 2007
2243 24 August 2006 04 April 2007
2244 24 August 2006 04 April 2007
2245 24 August 2006 04 April 2007
2246 24 August 2006 04 April 2007
2247 24 August 2006
2248 24 August 2006
ii 510WB-01
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
TABLE OF CONTENTS
FAA APPROVED
U.S.
TABLE OF CONTENTS
PAGE
INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1/6-2
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:Citation Mustang airplane flight manual 3(16)