B737-600/-700/-800/-900
AFM SUPPLEMENT
PREFACE
TITLE PAGE
Fokker Services B.V.
Hoeksteen 40
2132 MS Hoofddorp
The Netherlands
AIRPLANE FLIGHT MANUAL SUPPLEMENT
FOR THE
ADS-B OUT VERSION 2 FUNCTION
AS INSTALLED IN
BOEING B737-600/-700/-800/-900 SERIAL NUMBERS:
WITH EASA STC 10066148 INSTALLED
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
EASA STC 10066148
FS-0.0.1
Date: 23-01-2019
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.
B737-600/-700/-800/-900
AFM SUPPLEMENT
PREFACE
RECORD OF REVISIONS
Revision
Pages
Description of revision
Affected
Fokker Services B.V.
Signature(s) & date
1
ALL
First release
23 JANUARY 2019
2
FS-0.1.1
Introduction of DOA
statement
23 MARCH 2020
FS-0.3.1
FS-0.4.1
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
EASA STC 10066148
FS-0.1.1
Date: 23-03-2020
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.
B737-600/-700/-800/-900/ER TBD
AFM SUPPLEMENT
PREFACE
TABLE OF CONTENTS
Preface
Title Page ............................................................................................................. FS-0.0.1
Record of Revisions ............................................................................................. FS-0.1.1
Table of Contents ................................................................................................. FS-0.2.1
List Effective Pages ............................................................................................... FS-0.3.1
Introduction
General ............................................................................................................ FS-0.4.1
Organization of the AFM Supplement ............................................................. FS-0.4.1
Supplement Revisions ..................................................................................... FS-0.4.1
Page Identification ........................................................................................... FS-0.4.2
Section 1
Certificate Limitations ..................................................................................NO CHANGES
Section 2
Non-Normal Procedures ..............................................................................NO CHANGES
Section 3
Normal Procedures
Mode S – ELS Elementary Surveillance .......................................................... FS-3.0.1
Mode S – EHS Enhanced Surveillance ........................................................... FS-3.0.1
ADS-B OUT (Extended Squitter) ..................................................................... FS-3.0.1
Section 4
Performance ................................................................................................NO CHANGES
Appendices ......................................................................................................NO CHANGES
Supplements ....................................................................................................NO CHANGES
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
EASA STC 10066148
FS-0.2.1
Date: 23-01-2019
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.
B737-600/-700/-800/-900
AFM SUPPLEMENT
PREFACE
LIST OF EFFECTIVE PAGES
Page
Date
FS-0.0.1
23-01-2019
FS-0.1.1
23-03-2020
FS-0.2.1
23-01-2019
R
FS-0.3.1
23-03-2020
R
FS-0.4.1
23-03-2020
FS-0.4.2
23-01-2019
FS-3.0.1
23-01-2019
R
An “A” in front of the page number indicates that the page is Added.
An “R” in front of the page number indicates that the page is Revised.
A “D” in front of the page number indicates that the page is Deleted.
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
EASA STC 10066148
FS-0.3.1
Date: 23-03-2020
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.
B737-600/-700/-800/-900
AFM SUPPLEMENT
PREFACE
INTRODUCTION
GENERAL
This Airplane Flight Manual Supplement (AFM-S) has been approved by the European Aviation
Safety Agency (EASA) and must be attached to the EASA approved Airplane Flight Manual (AFM)
of the Boeing B737-600/-700/-800/-900. This supplement contains Limitations for the operation
of Boeing B737-600/-700/-800/-900 aircraft with an ADS-B Out Version 2 ATC Transponder
Installation, installed in accordance with a Fokker Services Engineering Bulletin.
The information herein supplements and/or supersedes the information in the EASA approved
AFM of the Boeing B737-600/-700/-800/-900. For information not contained in this AFM-S
supplement, consult the B737-600/-700/-800/-900 AFM.
The technical content of this document is approved under the authority of DOA ref.
EASA.21J.059.
APPROVAL
The technical content of this document is approved under the authority of the DOA ref.
EASA.21J.059.
ORGANIZATION OF THE AFM SUPPLEMENT
The AFM-S includes:
- A Title Page corresponding to the certified model and MSN number.
- A Record of Revisions page concerning the revisions of this AFM-S.
- A Table of Contents concerning the technical content of this AFM-S.
- A List of Effective Pages indicating all the effective pages of this AFM-S.
- An Introduction with a functional description, and explanation of the organization and page
identification of this AFM-S.
- Technical information concerning the applicable modification.
To avoid confusion with the Boeing AFM, the section/subsection/page numbering of this
supplement is identified by the prefix “FS”. Explanatory text is done in italic text.
SUPPLEMENT REVISIONS
When a revision to this AFM-S is initiated it is mentioned in the Record of Revisions with a revision
number, affected pages and revision date.
For each revision, a new List of Effective Pages listing is issued.
A “black bar” in the margin of the revised pages locates the modified part.
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
EASA STC 10066148
FS-0.4.1
Date: 23-03-2020
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.
B737-600/-700/-800/-900
AFM SUPPLEMENT
PREFACE
INTRODUCTION
PAGE IDENTIFICATION
To identify a page, the following information is used:
UPPER PART OF THE PAGE
AIRCRAFT TYPE AND SUPPLEMENT TYPE
B737-600/-700/-800/-900
AFM SUPPLEMENT
PREFACE
INTRODUCTION
COMPANY LOGO
SECTION /SUBSECTION
NAME
LOWER PART OF THE PAGE
APPROVED BY
EASA APPROVED
SUPPLEMENTAL TYPE
CERTIFICATE NUMBER
EASA STC 10066148
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
FOKKER DOCUMENT
REGISTRATION NUMBER
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
SECTION / SUBSECTION /
PAGE NUMBER
FS-0.4.2
Date: 23-01-2019
DATE OF PAGE
EASA STC 10066148
FS-0.4.2
Date: 23-01-2019
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.
B737-600/-700/-800/-900
AFM SUPPLEMENT
SECTION 3
NORMAL PROCEDURES
The normal procedures established in Section 3 - NORMAL PROCEDURES, Subsection Air
Traffic Control Radar Beacon System, of the approved B737-600/-700/-800/-900 Airplane Flight
Manual are supplemented and/or superseded as indicated below.
Paragraph: Elementary Surveillance (if installed), is superseded by:
MODE S – ELS ELEMENTARY SURVEILLANCE
The ATC transponder in this aircraft has shown to meet EASA requirements of CSACNS.D.ELS.
Paragraph: Enhanced Surveillance (if installed), is superseded by:
MODE S – EHS ENHANCED SURVEILLANCE
The ATC transponder in this aircraft has shown to meet EASA requirements of CSACNS.D.EHS.
Paragraph: Extended Squitter (if installed,) is superseded by:
ADS-B OUT (EXTENDED SQUITTER)
The ATC transponder in this aircraft has shown to meet the EASA requirements of CS
ACNS.D.ADSB.
GPS provides the positioning information for ADS-B OUT, so when GPS data is not available,
your aircraft will be invisible to ADS-B surveillance. The ADS-B OUT failure conditions can be
identified when there is an ATC FAIL or XPNDR FAULT* annunciation on the ATC Transponder
Panel in combination with the messages in the table below:
Failure
ADS-B OUT function fault
ADS-B OUT system fault.
Annunciations
 ATC FAIL or XPNDR FAULT* on ATC
Transponder Panel.
 ATC FAIL or XPNDR FAULT* on ATC
Transponder Panel and TCAS FAIL
on the ND.
Result of
Loss of GPS data.
Failure
of
equipment.
ATC
Upon an ATC FAIL or XPNDR FAULT* annunciation (ADS-B OUT function failure or system
failure), the selection of the alternate system will restore ATC transponder function (ELS / EHS /
ADS-B OUT / TCAS).
* Fault indication depending on panel type.
An ADS-B out function failure (failure of the GPS position source) may also cause FMS scratch
pad and MCDU messages or possibly EGPWS terrain faults, etc. if sharing the same GPS
sources as the transponder
EASA APPROVED
FS ref. nr.: B737-ADSB-AFM-S-001-CUS
EASA STC 10066148
FS-3.0.1
Date: 23-01-2019
Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement.
Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except
with the prior written permission of Fokker Services B.V.