AIRPLANE FLIGHT MANUAL SUPPLEMENT 

DASSAUL T 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 

Perrzce ~ 

FAA Approved:.......,r.-r-----r- __ _£_~~+----

For Manager, Seattle Aircraft Certificatio 

Federal Aviation Administration 

Northwest Mountain Region/Renton, Washington 

Initial Release: April15, 2009 

Revision 4: June 1, 2012 

Code 001 Title Page 
Dassault 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. APF2-0601 
Dassault Aviation Falcon 2000EX with 

Aviation Partners, Inc. Blended Winglets 

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT 

FOR DASSAUL T 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. 

Approved 

Revision 4 

By: ~ 

_4L · / 

~~ 

~ Date: June 1, 2012 

(/ 

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. APF2-0601 
Dassault Aviation Falcon 2000EX 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 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. APF2-0601 
Section 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. APF2-0601 
Section I - Limitations 

Dassault Aviation Falcon 2000EX with 

Aviation Partners, Inc. Blended Winglets 

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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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12 14 16 18 20 22 24 26 28 30 32 34 

CENTER OF GRAVITY~ PERCENT MAC 

FAA Approved: June 1, 2012 Code 001 Page 1-2 

Document No. APF2-0601 
Section 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. APF2-0601 
Section 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. APF2-0601 
Section 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. APF2-0601 
Section 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. APF2-0601 
Section 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