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

### This supplement must be attached to the basic Dassault Aviation Airplane Flight Manual (Document Number DGT88898 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.
Section 1. Section 2. Section 3. Section 4. Section 5. Introduction Limitations Emergency Procedures Abnormal Procedures Normal Procedures 

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Code 001 Title PageDassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets 

### Revision Highlights Airplane Flight Manual Supplement Document No. APF2-0601, Code 001 Revision: 4 Date: June 1, 2012 This revision adds Weights and Loading to Section 1. Pages Code Explanation Title 001 Updated for Revision 4. 001 Updated Log of Pages for Revision 4. 1-1 001 Added Weights and Loading as Section 1.1. Sections 1.2 through 1.4 moved to page 1-3. 1-2 001 Added Center of Gravity Limits as page 1-2. · 1-3 001 Sections 1.2 through 1.4 moved from page 1-1 and Section numbers increased. No text changes from Revision 3.

Code 001 Page 1 Document No. APF2-0601Dassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR DASSAULT AVIATION FALCON 2000EX SERIES EQUIPPED WITH AVIATION PARTNERS, INC. BLENDED WINGLETS MODEL Falcon 2000EX Series Airplanes LOG OF PAGES The following pages comprise the Aviation Partners, Inc. Airplane Flight Manual Supplement for the Dassault Aviation Falcon 2000EX series when equipped with STC No. ST01987SE. Revision 4 

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## (/ FOR MANAdfR, SEATTLE AIRCRAFT CERTIFICATION OFFICE, FAA NORTHWEST MOUNTAIN REGION. PAGE CODE DATE Title Page 001 6/1/12 i 001 6/1/12 ii 001 5/7/09 SECTION 1 1-1 001 6/1/12 1-2 001 6/1/12 1-3 001 6/1/12 SECTION 2 2-1 001 4/15/09 SECTION 3 3-1 001 4/15/09 SECTION 4 4-1 001 4/15/09 SECTION 5 5-1 001 4/15/09
Applicable Airplane Serial Numbers: Airplanes equipped with STC No. ST01987SE.

FAA Approved: June 1, 2012 Code 001 Page i Document No. APF2-0601Dassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets
INTRODUCTION 

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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 2000EX 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 001 Page ii Document No. APF2-0601Section I - Limitations Dassault Aviation Falcon 2000EX 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 SF 2 to meet trim requirements by moving the forward limit aft to 16% MAC for this takeoff flap configuration. Clean and SF 1 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 001 Page 1-1 Document No. APF2-0601Section I - Limitations Dassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets

0**~** 0 0 0 00 _J 0 0 0 .,.... CENTER OF GRAVITY LIMITS 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 001 Page 1-2 Document No. APF2-0601Section 1- Limitations Dassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets
SECTION 1.2- LUBRICATION SYSTEM LIMITATIONS For scheduled flight durations greater than 10 hours (including time to alternate) engine oil levels must be checked and verified to be above the MIN oil level indicator line by at least 50% of the distance between MAX and MIN level indicator markings on each engine. SECTION 1.3- 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 1.4 - STEEP APPROACH Steep Approach Landing is not approved for F2000EX aircraft with API winglets installed.

FAA Approved: June 1, 2012 Code 001 Page 1-3 Document No. APF2-0601Section II - Emergency Procedures Dassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets
SECTION 2- EMERGENCY PROCEDURES Emergency procedures in Section 2 of the basic Airplane Flight Manual are unchanged by the addition of winglets.

FAA Approved: April 15, 2009 Code 001 Page 2-1 Document No. APF2-0601Section Ill - Abnormal Procedures Dassault Aviation Falcon 2000EX 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: April15, 2009 Code 001 Page 3-1 Document No. APF2-0601Section IV - Normal Procedures Dassault Aviation Falcon 2000EX 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 wing lets. 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 001 Page 4-1 Document No. APF2-0601Section V- Performance Dassault Aviation Falcon 2000EX with Aviation Partners, Inc. Blended Winglets
SECTION 5 - PERFORMANCE Performance presented in Section 5 of the basic AFM is applicable to Falcon 2000EX aircraft equipped with API Blended Winglets.

FAA Approved: April 15, 2009 Code 001 Page 5-1 Document No. APF2-0601