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 

Section 5. Performa:!~ 

For 

FMApproved~/_ 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 Page 
Dassault 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. APF2-0601 
Dassault Aviation Falcon 2000 with 

Aviation Partners, Inc. Blended Winglets 

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT 

FOR DASSAUL T 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 ~ LJ 

Approved By: f 7":. 

FOR MANA ~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. APF2-0601 
Dassault 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. APF2-0601 
Section 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. APF2-0601 
Section 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. 

•••• 1 :: •. 

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0 ··::'C:-U ::· --·- --·-• ·--- -·· 

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... : .. !: .... ·· 

11 .;__;: 

1--------·-•-:-'----'-'-l-'-'-----·-:-•-•----'l:-•-•-•--•;--'-'-'--·l·-'-'-'---:--• __ -'-'.-·.·l--·. :----_----_-· 

----·-···· _-__ • ___ • -___ _-_ ' __ -____ · ·_----· .. ___ , __ • __ • __ • __ ·, i • ... ,------___ -_____ ; ..:.:.:.:.j .. :.:.:.:., .. :.:.:.:.l--'--'-'-'-!-----'-'-'-l----'-'-'-i--------'-'-l--------'-'-•-·-----'-+'--------+···----+·-·-----•:--•-•-·---+-'-'-------!-'-'-'-'-1 · _ _-__ - , _ _-__ _- _ _- _ _-_ 

:::: ::-.::::: :·: 

. : r:;< :::::.: .. : ... : ~----.-_-- -·--------·-·-·-----·-·--·-·-·-----1-'-'-'--+'-'-'-'+'-'-'-'-f""',: :..J:.::· .. :._::: i :: :: :: :: ::: : .. . 

10 •••• -~ •.. ~~.:. ::••' 

-•---·-_--:_._ ·_·,c;._e:- _- ._. • ' . ''' .. '. ' .. ' . ::: "::',_k ._, .. _ _._,!_,:.'I •• ..:::• .• -.:.;. _ _-_ _-__ :_+_. _ _. _ _. __ ,,_, _ _-_ _-__ +-'-'---i-----·-·----1-'-'-'----i--'-'-'--1 I .... · •----·-·-.-·_-· 

··: :"'~~· 

~.-.. . ...... , .. _ .............. >~··· .. ·-·•: 

1-'_--__ --'--_-;-:,--..,----'- 1-'_.--__ ---- F'·---'F-------+-'·'-----F-'-'---+---'·'·-·1--'-'·'·'-!--'-'·'·'·1--·-'---'·!-- __ . : : :::: ::. _ : •• : : : : •• :~~. :, •. :: 

&..U 

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

CENTER OF GRAVITY - PERCENT MAC 

./ 

FAA Approved: June 1, 2012 Code 002 Page 1-2 

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