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Page
Number
Page
Status
Revision
Number
Configuration
Code
S12-1 thru S12-7/S12-8 Original 0 S12-AA
S12-2 S12-AA 510FM-S12-00
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 12
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
510FM-S12-00 S12-AA S12-3
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 12
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
S12-AA Airplanes 510-0001 and On operating under Japanese
Registration.
S12-4 S12-AA 510FM-S12-00
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 12
FAA APPROVED
Configuration U.S.
JAPANESE REGISTERED AIRPLANES
INTRODUCTION
This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for Japanese Registered 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 this supplement, consult the basic FAA Approved Airplane Flight
Manual.
AIRWORTHINESS CATEGORY
Normal Category.
OPERATING LIMITATIONS
KINDS OF OPERATIONS
This airplane may be operated in the following kinds of operations when the appropriate equipment
is installed.
• Flight in accordance with Instrumental Flight Method.
• IFR.
• Flight in accordance with Instrumental Navigation.
• VFR except flight in accordance with Instrumental Navigation.
• Night Flight.
• Day Flight.
• Flight into Known Icing Conditions.
• High Altitude Flight.
PLACARDS
Refer to the Model 510 Illustrated Parts Catalog for Japanese placards.
OPERATING PROCEDURES
No change.
EMERGENCY PROCEDURES
No change.
510FM-S12-00 S12-AA S12-5
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 12
FAA APPROVED
U.S. Configuration
ABNORMAL PROCEDURES
No change.
NORMAL PROCEDURES
No change.
PERFORMANCE
NOISE VALUE
This aircraft complies with the requirements of Japan Civil Aeronautics Regulations, Appendix 2,
“Aircraft Noise Standard” and ICAO Annex 16, Vol. 1, Part II, Chapter 4. The Certified noise values
are as follows:
(Continued Next Page)
1. State of Registry
Japan
2. NOISE DOCUMENT
3. Document Number
N/A
4. Nationality and
Registration Marks
5. Manufacturer and
Manufacturer’s
Designation Of Aircraft
Cessna Model 510
Cessna Aircraft Company
6. Aircraft Serial Number
7. Engine
Pratt & Whitney Canada PW615F-A Turbofan
8. Propeller
N/A
9. Maximum Take-Off Mass
3,921 kg
(8,645 lbs)
10. Maximum Landing Mass
3,629 kg
(8,000 lbs)
11. Noise Certification
Standard
Chapter 4
12. Additional modifications incorporated for the purpose of compliance with the applicable
noise certification Standards.
None
13. Lateral /
Full-Power
Noise Level
85.0 EPN dB
14. Approach
Noise Level
86.0 EPN dB
15. Flyover
Noise Level
73.9 EPN dB
16. Over-flight
Noise Level
N/A
17. Take-off
Noise Level
N/A
Remarks
S12-6 S12-AA 510FM-S12-00
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 12
FAA APPROVED
Configuration U.S.
NOISE VALUE (Continued)
This Noise Document is made pursuant to Annex 16, volume 1, Attachment G to the Convention on
International Civil Aviation (hereinafter referred to as “ICAO Format”) and approved as a part of
Airplane Flight Manual. In Japan, Compliance to the Noise Requirement is certified as a part of
Airworthiness Certification. Noise Certificate is not issued and Noise Characteristics are described in
the Airplane Flight Manual. Therefore, Japan determined to incorporate this Noise Document into the
　
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