AIRPLANE FLIGHT MANUAL SUPPLEMENT DASSAULT AVIATION FALCON 2000 with CFE 738 Engines Blended Winglets Installation Aviation Partners, Inc. 7299 Perimeter Road South Seattle, WA 98108 FAA STC No. ST01987SE Document No. APF2-0601 

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This supplement must be attached to the basic Dassault Aviation Airplane Flight Manual (Document Number DTM537 or equivalent) when Aviation Partners, Inc. Blended Winglets are installed. The information contained in this document supplements or supersedes the basic manual only in those areas listed. For limitations, procedures, and performance information not contained in this supplement, consult the basic Dassault Aviation Airplane Flight Manual or applicable appendix. Introduction Section 1. Limitations Section 2. Emergency Procedures Section 3. Abnormal Procedures Section 4. Normal Procedures 

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# FMApproved~/_ **~** For Manager, Seattle Aircraft Certification Office Federal Aviation Administration Northwest Mountain Region/Renton, Washington Initial Release: April 15, 2009 Revision 3: June 1, 2012

Code 002 Title PageDassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets 

### Revision Highlights Airplane Flight Manual Supplement Document No. APF2-0601, Code 002 Revision: 3 Date: June 1, 2012 This revision adds Weights and Loading to Section 1. Pages Code Explanation Title 001 Updated for Revision 3. 001 Updated Log of Pages for Revision 3. 1-1 001 Added Weights and Loading as Section 1 .1. Sections 1 .2 and 1.3 moved to page 1-3. 1-2 001 Added Center of Gravity Limits as page 1-2. 1-3 001 Sections 1.2 and 1.3 moved from page 1-1 and Section numbers increased. No text changes from Revision 2.

Code 002 Page 1 Document No. APF2-0601Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR DASSAULT AVIATION FALCON 2000 AIRCRAFT EQUIPPED WITH AVIATION PARTNERS, INC. BLENDED WINGLETS MODEL Falcon 2000 Airplanes LOG OF PAGES The following pages comprise the Aviation Partners, Inc. Airplane Flight Manual Supplement for the Dassault Aviation Falcon 2000 when equipped with STC No. ST01987SE. Revision 3

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# ~SEATTLE AIR MOUNTAIN REGION. PAGE CODE DATE Title Page 002 6/1/12 i 002 6/1/12 ii 002 5/7/09 SECTION 1 1-1 002 6/1/12 1-2 002 6/1/12 1-3 002 6/1/12 SECTION 2 2-1 002 4/15/09 SECTION 3 3-1 002 4/15/09 SECTION 4 4-1 002 4/15/09 SECTION 5 5-1 002 4/15/09 Date: June 1, 2012 RAFT CERTIFICATION OFFICE, FAA NORTHWEST

Applicable Airplane Serial Numbers: Airplanes equipped with STC No. ST01987SE.

FAA Approved: June 1, 2012 Code 002 Page i Document No. APF2-0601Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets INTRODUCTION This supplement provides the additional limitations, emergency procedures, abnormal procedures, normal procedures, and performance to reflect changes necessary due to the addition of blended winglets (STC ST01987SE) to the Falcon 2000 airplane. This supplement is used in conjunction with Sections 1, 2, 3, 4, and 5 of the basic Airplane Flight Manual and other applicable appendices.

FAA Approved: May 7, 2009 Code 002 Page ii Document No. APF2-0601Section I - Limitations Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets 

### SECTION 1- LIMITATIONS Limitations in Section 1 of the basic Airplane Flight Manual are unchanged by the addition of winglets except as amended herein. 

### SECTION 1.1 -WEIGHTS AND LOADING Structural limitations are unchanged by the addition of winglets. Center of Gravity Limits are updated for 20° flaps + slats to meet trim requirements by moving the forward limit aft to 16% MAC for this takeoff flap configuration. Clean and 1

# oo flaps+ slats are unchanged from the basic AFM and limits presented there remain valid. Winglet Center of Gravity Limits are presented on page 1-2.

FAA Approved: June 1, 2012 Code 002 Page 1-1 Document No. APF2-0601Section I - Limitations Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets CENTER OF GRAVITY LIMITS co ....J 0 0 0 THIS CENTER OF GRAVITY LIMITS ENVELOPE MUST BE USED IN CONJUNCTION WITH THE LIMITS PRESENTED IN THE BASIC DASSAULT AVIATION AFM. THE MOST RESTRICTIVE OF THESE LIMITS MUST BE USED.

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FAA Approved: June 1, 2012 Code 002 Page 1-2 Document No. APF2-0601Section I - Limitations Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets SECTION 1.2- ROCKWELL COLLINS HEAD UP GUIDANCE SYSTEM (IF INSTALLED) Manual Head up Guidance System Category lilA (HUD3) operations are not approved for Falcon 2000 series aircraft with API winglets installed. Existing HGS Category II (HUD2) certification categories remain valid with API winglets installed. SECTION 1.3 - STEEP APPROACH Steep Approach Landing is not approved for F2000 aircraft with API winglets installed.

FAA Approved: June 1, 2012 Code 002 Page 1-3 Document No. APF2-0601Section II - Emergency Procedures Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets SECTION 2 - EMERGENCY PROCEDURES 

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Emergency procedures in Section 2 of the basic Airplane Flight Manual are unchanged by the addition of winglets.

FAA Approved: April15, 2009 Code 002 Page 2-1 Document No. APF2-0601Section Ill - Abnormal Procedures Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets SECTION 3 -ABNORMAL PROCEDURES Abnormal procedures in Section 3 of the basic Airplane Flight Manual are unchanged by the addition of winglets.

FAA Approved: April 15, 2009 Code 002 Page 3-1 Document No. APF2-0601Section IV - Normal Procedures Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets SECTION 4- NORMAL PROCEDURES Normal procedures in Section 4 of the basic Airplane Flight Manual are unchanged by the addition of winglets. Note: Winglets replace the basic airplane wing tip fairing. Any text that previously referenced the wing tip fairing is now applicable to the winglet.

FAA Approved: April15, 2009 Code 002 Page 4-1 Document No. APF2-0601Section V- Performance Dassault Aviation Falcon 2000 with Aviation Partners, Inc. Blended Winglets SECTION 5 - PERFORMANCE Performance presented in Section 5 of the basic AFM is applicable to Falcon 2000 aircraft equipped with API Blended Winglets except as amended herein. NOISE STANDARDS: DASSAULT FALCON 2000 WITH API WINGLETS The following noise levels comply with 14 CFR Part 36, Appendix B, Stage 4 maximum noise level requirements and were obtained by analysis of approved data from noise tests conducted under the provisions of Part 36 Amendment 20 (demonstrated to be equivalent to Part 36 Amendment 27). The noise measurement and evaluation procedures used to obtain these noise levels are considered by the FAA to be equivalent to the Chapter 4 noise level required by the International Civil Aviation Organization (ICAO) in Annex 16, Volume I, Appendix 2, Amendment 8, effective July 11, 2005. The EPNLs at the given MTOW and MLW with CFE738-1-1 B engines are: MTOW/MLW Flap Noise Levels Setting (EPNdB) Flyover 36,500 lb. 20° 77.3 Lateral 36,500 lb. 20° 86.4 Approach 33,000 lb. 40° 93.3 No determination has been made by the Federal Aviation Administration that the noise levels of this aircraft are or should be acceptable or unacceptable for operation at, into, or out of, any airport.

FAA Approved: April 15, 2009 Code 002 Page 5-1 Document No. APF2-0601