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H4ADR788

Issue 28 of 111

AMENDMENT RECORD

ISSUE DATE REASON FOR AMENDMENT AUTHOR APPROVED BY

1 4/11/13 Initial Issue. F. Baldwin R. Wenman

2 11/02/14 Raised in issue to include 737NG aircraft.

C. Webb R. Wenman

3 29/04/14 Effectivity list replaced with reference and appendix 4 added.

F. Baldwin R. Wenman

4 23/04/15 Contents and Approvals, “(G) Appendix 5, (H) Appendix 6 & Appendix 7 (I) added”. Appendix 5 pages and Appendix 6 pages added.


5 19/06/15 Amd’t Rec’d iss4 date was 23/04/25. Contents and Approvals, “(J) Appendix 8A / 8B, (K) Appendix 9, (L) Appendix 10 added”. Appendix 8A/8B, 9 & 10 pages added.

W.E. Pitts F. Baldwin

6 17/08/15 Contents and Approvals, “(M) Appendix 11, (N) Appendix 12 added”. Appendix 11 & 12 pages added.


7 01/10/15 Para “A” description - 940-0351-010 added. Contents and Approvals “(O) Appendix 13 added. Appendix 13 pages added.


8 16/11/15 Contents and Approvals “(P), (Q) & (R) Appendix 14, 15 &16 added. Appendix 14, 15 &16 pages added.


9 26/11/15 Contents and Approvals (S), (T) Appendix 17, 18 pages added.


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AMENDMENT RECORD (continued)

ISSUE DATE REASON FOR AMENDMENT AUTHOR APPROVED BY

10 21/01/16 Pg1 Customer was Honeywell. Pg5 (T) corrected typo B737 was B747, Pg5 & 8 (U) Appendix 19 added. Pg 49 Appendix 19 pages added.

F. Baldwin R Wenman

11 28/01/16 Pg5 & 8 (V) Appendix 20 added. Pg 66 Appendix 20 pages added.

F. Baldwin R Wenman

12 26/04/16 Verification signature added to front sheet. Appendix 19 revised to add A/C MSN30231 (YC409). Appendix 19 pages revised.


13 06/06/16 Appendix 16 revised to add A/C MSN30705 (YK162). Appendix 16 pages revised.

W. E. Pitts N. Knox

14 29/06/16 Appendix 21 added A/C MSN28537 (PQ996). Appendix 22 added A/C MSN28655 (YC426), MSN32412 (YB116) and MSN32413 (YB117).

W. E. Pitts N. Knox

15 12/09/16 Appendix 23 added A/C MSN25419 (PT614). W. E. Pitts N. Knox

16 18/11/16 Appendix 24 added A/C MSN34280 and 34281. W. E. Pitts N. Knox

17 4/01/17 Appendix 25 added A/C MSN28475. W. E. Pitts N. Knox



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AMENDMENT RECORD (continued)

ISSUE DATE REASON FOR AMENDMENT

AUTHOR APPROVED BY

20 17/05/17 Appendix 16, Title corrected Appendix 28 added A/C MSN’s 26452, 26459, 26462, 27083, 27085 & 27097. Appendix 29 added A/C MSN’s 30159 & 30160.

I. Craney N. Knox

21 5/06/17 Appendix 29 added A/C MSN’s 30072 & 30073.

W. E. Pitts N. Knox

22 17/07/17 Appendix 30 and 31 added A/C MSN’s 27352, 27384 & 27930 added.

W. E. Pitts N. Knox

23 31/07/17 Appendix 32 and 33 added A/C MSN’s 34022, 37088 & 37421 added.

W. E. Pitts N. Knox

24 14/11/2017 A/C MSN 34538 added to Appendix 32.

W. E. Pitts N. Knox

25 20/03/2018 A/C MSN’s 25249, 26070, 26072 and Appendix 34 and 35 added.

W. E. Pitts N. Knox

26 18/06/18 Appendix 29A added to cover new aircraft A/C MSN 30071. MSN’s 30072 & 30073 moved from Appendix 29 to 29A,

C. G. Webb N. Knox

27 27/09/18 A/C MSN’s 27191 and Appendix 36 added.

C. G. Webb N. Knox

28 See Page 1

A/C MSN 30712 and Appendix 37 added.

W. E. Pitts N. Knox

© H4 Aerospace. All rights Reserved. H4 Aerospace own the copyright of this document which is supplied in confidence and must not be used for any purpose other than that which it is supplied and must not be reproduced without permission in writing from the owner, H4 Aerospace (UK) Ltd. Blue Court, 39 Queensway, Hemel Hempstead, Herts. HP2 5HE

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CONTENTS

AMENDMENT RECORD ................................................................................................. 2

A) INTRODUCTION .................................................................................................. 7

B) APPROVAL ........................................................................................................... 8

C) APPENDIX 1 - SYSTEM DESCRIPTIONS SECTION, 15.20.25 ‘TCAS AURAL MESSAGES’ VSI/WXR DISPLAY - B737-300/400/500 ...................................... 11

D) APPENDIX 2 - SYSTEM DESCRIPTIONS SECTION, 15.20.25 ‘TCAS AURAL MESSAGES’ EFIS. - B737-300/400/500 ............................................................. 13

E) APPENDIX 3 - SYSTEM DESCRIPTIONS SECTION, 15.20.26.1 ‘RESOLUTION ADVISORY AURALS’. - B737-600/700/800/900/900ER ..................................... 15

F) APPENDIX 4 - SYSTEM DESCRIPTIONS SECTION, 15.20.19.1 ‘RESOLUTION ADVISORY AURALS’. - B737-8 .......................................................................... 17

G) APPENDIX 5 - SYSTEM DESCRIPTION SECTION 15.20.28 'RESOLUTION ADVIORY AURALS'. - B737-800 19

H) APPENDIX 6 - SYSTEMS DESCRIPTION - CHAPTER 10 FLIGHT INSTRUMENTS, DISPLAYS, SYSTEM DESCRIPTION CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-800/900 21

I) APPENDIX 7 - B737-35BSF FCOM D6-27370-301-CGE MSN23237 & MSN23970 29

J) APPENDIX 8A - B737-300/400 FCOM D6-27370-3B3-EUE MSN27347, MSN29333, MSN29336, MSN25595. 31

APPENDIX 8B - B737-700 - SECTION 15 WARNING SYSTEMS - 'RESOLUTION ADVIORY AURALS'.B737-700 MSN32414 & MSN32418 30

K) APPENDIX 9 - B737-329 FCOM D6-27370-3/400-TRX(TX) MSN24355. 32

L) APPENDIX 10 -737-3H9 - SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN2332, MSN23416, MSN23714, MSN23715. 33

M) APPENDIX 11 - B737-36N - FCOM D6-27370-36NJ-GEF SECTION 15 WARNING SYSTEMS - 'RESOLUTION ADVISORY AURALS' MSN28561, MSN28562 35

N) APPENDIX 12 - B737-8KN - FCOM D6-27370-800-CDY SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' 37

O) APPENDIX 13 - B737-301/3M8 - FCOM D6-27370-375-SWF SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN23512 MSN24022 39

P) APPENDIX 14 - B737-43QHGW - D6-27370-528-DAU SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN28494 41

Q) APPENDIX 15 - B7373-4QHGW - D6-27370-46Q-SNU SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN29000 43

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R) APPENDIX 16 - B737-86N, B737-8Q8 - D6-27370-8Z0-XIN SECTION 15

WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN29889,. 45

S) APPENDIX 17 - B737-76Q, B737-85F, B737-86N - D6-27370-800-SKK SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN30293, MSN28825, MSN28617. 47

T) APPENDIX 18 - B737-4YO - D6-27370-301-CGE SECTION 15 WARNING SYSTEMS 'RESOLUTION ADVISORY AURALS' MSN24691 49

U) APPENDIX 19 - B737-86N - D6-27370-86N-HNA CHAPTER 10 FLIGHT INSTRUMENTS, DISPLAYS, SYSTEM DESCRIPTION CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-800/900 50

V) APPENDIX 20 - B737-8GQ - D6-27370-700-AWW CHAPTER 10 FLIGHT INSTRUMENTS, DISPLAYS, SYSTEM DESCRIPTION CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-700/800 67

W) APPENDIX 21 - B737-37Q - D6-27370-5H6-VGS CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-300 76

X) APPENDIX 22 - B737-73V AND 86N - D6-27370-86N-ETJ CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-700/800 78

Y) APPENDIX 23 - B737-500 – FCOM SUPPLEMENT CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-500 80

Z) APPENDIX 24 - B737-700/-800 – FCOM SUPPLEMENT CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-8EH 82

AA) APPENDIX 25 - B737-300/400/500– FCOM SUPPLEMENT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-55S…………………… 84

AB) APPENDIX 26 - B737-300/400/500– FCOM SUPPLEMENT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-4B7 ……………… 86

AC) APPENDIX 27 - B737-86N – D6- 27370-76N SYSTEM DESCRIPTION SECTION 15.20.23 ‘RESOLUTION ADVISORY AURALS B737-800 ……… 88

AD) APPENDIX 28 - B737-4H6 – D6- 27370-4H6 SYSTEM DESCRIPTION SECTION 15.20.22 ‘RESOLUTION ADVISORY AURALS B737-400 ……… 90

AE) APPENDIX 29 - B737-89L – FCOM SUPPLEMENT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)……… 92

APPENDIX 29A - B737-8Z0 – FCOM SUPPLEMENT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)……… 94

AF) APPENDIX 30 - B737-4H6 – FCOM SUPPLEMENT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) ……… 96

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AG) APPENDIX 31 - B737-3H4 – FCOM SUPPLEMENT TRAFFIC ALERT AND

COLLISION AVOIDANCE SYSTEM (TCAS) ……… 98

AH) APPENDIX 32 - B737-79L – FCOM D6- 27370-89L-BEJ SYSTEM DESCRIPTION SECTION 15.20.32.1 ‘RESOLUTION ADVISORY AURALS 100

AI) APPENDIX 33 - B737-7CT – FCOM D6- 27370-8AL-SIL SYSTEM DESCRIPTION SECTION 15.20.40.1 ‘RESOLUTION ADVISORY AURALS 102

AJ) APPENDIX 34 - B737-500 – FCOM SUPPLEMENT CHAPTER 15 WARNING SYSTEMS - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) B737-500…………………………………………………………………………… 104

AK) APPENDIX 35 - B737-3Y0 – D6- 27370-3Y0J-GUI SYSTEM DESCRIPTION SECTION 15.20.22 ‘RESOLUTION ADVISORY AURALS B737-300 106

AL) APPENDIX 36 - B737-4H6 – D6- 27370-4H6 SYSTEM DESCRIPTION SECTION 15.20.22 ‘RESOLUTION ADVISORY AURALS B737-400 ……… 108

AM) APPENDIX 37 - B737-7CT – FCOM D6- 27370-76N-WJI SYSTEM DESCRIPTION SECTION 15.20.25.1 ‘RESOLUTION ADVISORY AURALS 110

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A) INTRODUCTION

Effectivity

For aircraft effectivity refer to mod document H4A1675.

Description Modification H4A1675 installs a Honeywell TPA-100B TCAS II version 7.1 in place of a Honeywell TPA-81A or TPA-100A TCAS II version 7.0 on the Boeing B737 - Series aircraft listed above. An EC mandate was issued on December 20th 2011 for implementing TCAS Change 7.1 for aircraft operating in European airspace. The mandate calls for Change 7.1 software to be installed on all existing aircraft using TCAS II products by December 2015. Once Change 7.1 is installed, operators will be compliant with MOPS D0185B. The Honeywell TPA-100B TCAS II Traffic Computer, p/n 940-0351-001 or 940-0351-010 is installed in place of the existing Honeywell TPA-81A TCAS computer p/n 066-50000-xxxx or TPA-100A computer p/n 940-0300-XXX in the same location. The original tray remains and no wiring changes are necessary. The TPA-100B is fully compliant with ETSO-119c including both RTCA/DO-185B for TCAS II change 7.1. As well as several operational improvements, Change 7.1 introduces two main safety improvements to the TCAS system;

corrects missed and late reversals

changes the current aural warning from ‘Adjust Vertical Speed, Adjust’ to ‘Level Off, Level Off’.

The incorporation of H4Aerospace (UK) Ltd. modification H4A1675 to the aircraft obligates the aircraft operator to include the following information provided by this report in the owner/operators Flight Crew Operating Manual. This Flight Crew Operating Manual Supplement refers to the changes required in the Warning Systems - System Descriptions section, 15.20.25 ‘TCAS Aural Messages’ for the aircraft listed above. The data provided herein is intended to support the compliance demonstration for the following paragraphs. FAR 25.1581 (a) Correspondence H4 Aerospace is responsible for the Continued Airworthiness of this modification. In the event of a problem with this document, H4 Aerospace is to be notified immediately at the contact address below.

H4 Aerospace Ltd Blue Court, 39 Queensway, Hemel Hempstead, Hertfordshire HP2 5HE England E mail [email protected] Telephone +44(0)1442 257 468

mailto:[email protected]

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B) APPROVAL

The technical content of this document and supporting reports and drawings listed herein are approved under the authority of EASA DOA no.EASA.21J.087 and H4 Aerospace modification H4A1675.

C) APPENDIX 1 - System Descriptions section, 15.20.25 ‘TCAS Aural Messages’ VSI/WXR display - B737-300/400/500.

D) APPENDIX 2 - System Descriptions section, 15.20.25 ‘TCAS Aural Messages’ EFIS. - B737-

300/400/500.

E) APPENDIX 3 - System Descriptions section, 15.20.26.1 ‘Resolution Advisory Aurals. - B737-600/700/800/900/900ER.

F) APPENDIX 4 - System Descriptions section, 15.20.19.1 ‘Resolution Advisory Aurals.

B737-800 (VP-BPI, VP-VPY ONLY).

G) APPENDIX 5 - System Description section, 15.20.28.1 ‘Resolution Advisory Aurals B737-800 (TC-TJN ONLY).

H) APPENDIX 6 - Systems Description Chapter 10 & 15 Traffic Alert and Collision Avoidance

System (TCAS) (UR-PSA, UR-PSB, UR-PSC, UR-PSD, UR-PSK, UR-PSL ONLY). I) APPENDIX 7 - B737-35BSF FCOM D6-27370-301-CGE MSN23237 (LZ-CGO) & MSN23970

(LZ-CGP). J) APPENDIX 8A - B737-300/400 FCOM D6-27370-3B3-EUE MSN27347 (F-GIXS), MSN29333 (F-

GZTA), MSN29336 (F-GZTB) MSN25595 (F-GZTJ). APPENDIX 8B - B737-700 FCOM D6-27370-73V-EUE MSN32414 (F-GZTC) & MSN32418 (F-GZTD.

K) APPENDIX 9 - B737-329 FCOM D6-27370-3/400-TRX MSN24355 (EI-CXR). L) APPENDIX 10 - B737-3H9 FCOM D6-27370-3H9-JAT MSN23329 (YU-AND), MSN23416 (YU-

ANI), MSN23714 (YU-ANJ), MSN23715 (YU-ANK).

M) APPENDIX 11 - B737-36N FCOM D6-27370-36NJ-GEF MSN28561 (EI-IGR), MSN28562 (EI-IGS)

N) APPENDIX 12 - B737-8KN FCOM D6-27370-800-CDY MSN35795 (PH-CDE). O) APPENDIX 13 - B737-301 FCOM D6-27370-375-SWF MSN23512 (EC-LJI), MSN24022 (EC-

LAC) P) APPENDIX 14 - B737-4QHGW FCOM D6-27370-528-DAU MSN28494 (HA-FAU) Q) APPENDIX 15 - B737-4QHGW FCOM D6-27370-46Q-SNU MSN29000 (HA-FAV) R) APPENDIX 16 - B737-86N, B737-8Q8 FCOM D6-27370-8Z0-XIN MSN29889 (TBD). S) APPENDIX 17 - System Description section, 15.20.25.1 ‘Resolution Advisory Aurals’ VQ-

BEO (MSN30293), VQ-BOY (MSN28825), VQ-BMP (MSN28617). T) APPENDIX 18 - System Description section, 15.20.31 ‘Resolution Advisory Aurals’ LZ-CGT

(MSN24691). U) APPENDIX 19 - Systems Description Chapter 10 & 15 Traffic Alert and Collision Avoidance

System (TCAS) (MSN28614), (MSN30231).

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V) APPENDIX 20 - Systems Description Chapter 10 & 15 Traffic Alert and Collision Avoidance

System (TCAS) (MSN35793). W) APPENDIX 21 - System Description section, 15.20.25.1 ‘Resolution Advisory Aurals’ CP-3020 (SX-BDW) (MSN28537). X) APPENDIX 22 - System Description section, 15.20.31.1 ‘Resolution Advisory Aurals’ HL8036 (MSN28655), HL8205 (MSN32412), HL8207 (MSN32413). Y) APPENDIX 23 - System Description section, 15.20.31.1 ‘Resolution Advisory Aurals’ HZ-HAA (MSN25419). Z) APPENDIX 24 - System Description section, 15.20.32.1 ‘Resolution Advisory Aurals’ PR-GTI (MSN34280), PR-GTK (MSN34281). AA) APPENDIX 25 - System Description section, Resolution Advisory Aurals’ OK-EGO (MSN28475). AB) APPENDIX 26 - System Description section, Resolution Advisory Aurals’ 9M-GSA (MSN24559). AC) APPENDIX 27 - System Description section, 15.20.23.1 ‘Resolution Advisory Aurals B737-

800 (MSN35632). AD) APPENDIX 28 - System Description section, 15.20.22.1 ‘Resolution Advisory Aurals B737-

400 (MSN’s 26452, 26459, 26462, 27083, 27085 & 27097). AE) APPENDIX 29 - System Description section, 15.20.31.1 ‘Resolution Advisory Aurals B737-

800 (MSN’s 30159 & 30160). APPENDIX 29A - System Description section, 15.20.20.1 ‘Resolution Advisory Aurals B737-800 (MSN’s 30071, 30072 & 30073).

AF) APPENDIX 30 - System Description section, Resolution Advisory Aurals’ YV621T (MSN27352), YV622T (MSN27384). AG) APPENDIX 31 - System Description section, Resolution Advisory Aurals’ N612SW (MSN27930). AH) APPENDIX 32 - System Description section, Resolution Advisory Aurals’ B-5217 (MSN34022), B-5203 (MSN34538). AI) APPENDIX 33 - System Description section, Resolution Advisory Aurals’ C-FBWS (MSN37088) & C-GWSY (MSN37421). AJ) APPENDIX 34 - System Description section, 15.20.31.1 ‘Resolution Advisory Aurals’ Z3-AAM (MSN25249). AK) APPENDIX 35 - System Description section, 15.20.22.1 ‘Resolution Advisory Aurals B737-

300 (MSN’s 26070 & 26072). AL) APPENDIX 36 - System Description section, 15.20.22.1 ‘Resolution Advisory Aurals B737-

400 (MSN 27191). AM) APPENDIX 37 - System Description section, 15.20.25.1 ‘Resolution Advisory Aurals B737-

7CT (MSN 30712). See following pages. Note: The relevant supplement page must be inserted in the appropriate section of the existing

aircraft FCOM

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APPENDIX 1

TCAS AURALS RA/VSI - B737-300/400/500

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737 Flight Crew Operations Manual

Resolution Advisory Aurals

The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.

AURAL ALERTS VERTICAL RESTRICTIONS/MANEUVER

CLIMB, CLIMB Climb at the rate depicted by the green (fly to) arc on the VSI.

DESCEND, DESCEND Descend at the rate depicted by the green (fly to)arc on the VSI normally between 1,500 and 2,000 ft/min

MONITOR VERTICAL SPEED Ensure that vertical speed is out of the illuminated VSI red arc until the RA is complete.

LEVEL OFF, LEVEL OFF Reduce vertical speed to zero feet per min. A green arc will be illuminated beginning at zero feet per min. This can be issued as the initial RA or as a subsequent RA.

CLEAR OF CONFLICT Range is increasing, and separation is adequate. Expeditiously return to applicable ATC clearance, unless otherwise directed by ATC.

CLIMB, CROSSING CLIMB, CROSSING CLIMB

Climb at the rate depicted by the green (fly to) arc on the VSI, normally between 1,500 and 2,000 ft/min. Safe separation will be best achieved by climbing through the threats flight path.

DESCEND, CROSSING DESCEND, DESCEND, CROSSING DESCEND

Descend at the rate depicted by the green (fly to) arc on the VSI, normally between 1,500 and 2,000 ft/min. Safe separation will be best achieved by descending through the threats flight path.

MAINTAIN VERTICAL SPEED, MAINTAIN

Continue the existing climb or descent rate, or other vertical speed, as depicted by the green (fly to) arc on the VSI

MAINTAIN VERTICAL SPEED, CROSSING MAINTAIN

Continue the existing climb or descent rate, or other vertical speed, as depicted by the green (fly to) arc on the VSI. Safe separation will be best achieved by not altering the existing vertical speed and climbing or descending through the threats flight path.

The following are enhanced TCAS maneuvers required when the initial RA does not provide sufficient vertical; separation.

TONE and INFLECTION indicate increased URGENCY

INCREASE CLIMB, INCREASE CLIMB

Climb at the rate depicted by the green (fly to) arc on the VSI, normally between 2,500 and 3,000 ft/min. Received after “CLIMB” advisory, and indicates additional climb rate required to achieve safe vertical separation from the maneuvering aircraft.

INCREASE DESCENT, INCREASE DESCENT

Descend at the rate depicted by the green (fly to) arc on the VSI, normally between 2,500 and 3,000 ft/min. Received after “DESCEND” advisory, and indicates additional descend rate required to achieve safe vertical separation from the maneuvering aircraft.

CLIMB – CLIMB NOW, CLIMB – CLIMB NOW

Climb at the rate depicted by the green (fly to) arc on the VSI, normally between 2,500 and 3,000 ft/min. Received after a “DESCEND” resolution advisory and indicate a reversal in direction is required to achieve safe vertical separation from maneuvering aircraft.

DESCEND – DESCEND NOW, DESCEND – DESCEND NOW

Descend at the rate depicted by the green (fly to) arc on the VSI, normally between 2,500 and 3,000 ft/min. Received after a “CLIMB” resolution advisory and indicate a reversal in direction is required to achieve safe vertical separation from maneuvering aircraft.

B737-300/400/500 15.20.25 FCOM Supplement Oct 13

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APPENDIX 2

TCAS AURALS EFIS - B737-300/400/500

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CLIMB, CLIMB Climb at the rate depicted by the green area on the PFD

DESCEND, DESCEND Descend at the rate depicted by the green (fly to) area on the PFD normally between 1,500 and 2,000 ft/min

MONITOR VERTICAL SPEED Ensure that vertical speed is out of the red area on the PFD until the RA is complete.

LEVEL OFF, LEVEL OFF Reduce vertical speed to zero feet per min. The green area will show on the PFD beginning at zero feet per min. This can be issued as the initial RA or as a subsequent RA.

CLEAR OF CONFLICT Range is increasing, and separation is adequate. Expeditiously return to applicable ATC clearance, unless otherwise directed by ATC.

CLIMB, CROSSING CLIMB, CROSSING CLIMB

Climb at the rate depicted by the green (fly to) area on the PFD, normally between 1,500 and 2,000 ft/min. Safe separation will be best achieved by climbing through the threats flight path.


Descend at the rate depicted by the green (fly to) area on the PFD, normally between 1,500 and 2,000 ft/min. Safe separation will be best achieved by descending through the threats flight path.


Continue the existing climb or descent rate, or other vertical speed, as depicted by the green (fly to) area on the PFD


Continue the existing climb or descent rate, or other vertical speed, as depicted by the green (fly to) area on the PFD. Safe separation will be best achieved by not altering the existing vertical speed and climbing or descending through the threats flight path.

The following are enhanced TCAS maneuvers required when the initial RA does not provide sufficient vertical; separation.

TONE and INFLECTION indicate increased URGENCY


Climb at the rate depicted by the green (fly to) area on the PFD, normally between 2,500 and 3,000 ft/min. Received after “CLIMB” advisory, and indicates additional climb rate required to achieve safe vertical separation from the maneuvering aircraft.


Descend at the rate depicted by the green (fly to) area on the PFD, normally between 2,500 and 3,000 ft/min. Received after “DESCEND” advisory, and indicates additional descend rate required to achieve safe vertical separation from the maneuvering aircraft.


Climb at the rate depicted by the green (fly to) area on the PFD, normally between 2,500 and 3,000 ft/min. Received after a “DESCEND” resolution advisory and indicate a reversal in direction is required to achieve safe vertical separation from maneuvering aircraft.


Descend at the rate depicted by the green (fly to) area on the PFD, normally between 2,500 and 3,000 ft/min. Received after a “CLIMB” resolution advisory and indicate a reversal in direction is required to achieve safe vertical separation from maneuvering aircraft.

B737-300/400/500 15.20.25 FCOM Supplement Oct 13

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APPENDIX 3

RESOLUTION ADVISORY AURALS. - B737-600/700/800/900/900ER

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MONITOR VERTICAL SPEED

Present pitch attitude is outside the RA pitch command area. Keep pitch attitude away from red area.



CLIMB, CLIMB Climb at the displayed pitch

DESCEND, DESCEND Descend at the displayed pitch

LEVEL OFF, LEVEL OFF Reduce climb or descent rate to zero

CLIMB, CROSSING CLIMB, CLIMB, CROSSING CLIMB

Climb at the displayed pitch. Airplane climbs through traffic’s altitude


Descend at the displayed pitch. Airplane descends through traffic’s altitude.

The following are enhanced TCAS maneuvers required when the initial RA does not provide sufficient vertical; separation. TONE and INFLECTION indicate increased URGENCY


Increase climb rate from initial pitch attitude


Increase descent rate from initial pitch attitude


Reversal maneuver from initial descent RA


Reversal maneuver from initial climb RA

CLEAR OF CONFLICT RA encounter terminated. Maneuver guidance no longer displayed

15.20.26.1 H4ADR788_2 February 11, 2014

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APPENDIX 4

RESOLUTION ADVISORY AURALS.- B737-800

VP-BPI, VP-BPY

Supplement AURALS page to D6-27370-83N-NRW dated March 27, 2014

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D6-27370-83N-NRW 15.20.19.1 H4ADR788_3 April 29, 2014

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APPENDIX 5


TC-TJN

Supplement AURALS page to D6-27370-86J-HVA dated March 26, 2015

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D6-27370-86J-HVA 15.20.28.1 H4ADR788_4 April 13, 2015

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APPENDIX 6 - Systems Description - Chapter 10 Flight Instruments, Displays, System Description Chapter 15 Warning Systems - Traffic Alert and Collision Avoidance System (TCAS) (UR-PSA, UR-PSB, UR-PSC, UR-PSD, UR-PSK, UR-PSL ONLY)

FCOM Master heading - Systems Description

Chapter 10 - Flight Instruments, Displays

Sub Chapter 10.11.1 - PFD/ND - Displays 10.11.74 - Navigation Displays - Advisory messages - TCAS Messages. 10.41.24 - ND Symbols - TCAS

Chapter 15 - Warning Systems

Sub Chapter 15.10.14 - TCAS controls (Transponder Panel) 15.20.24 - Traffic Alert and Collision Avoidance System (TCAS)

- Advisories and Displays - Inhibits - Mode Control - Resolution Advisory, Aurals

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Flight Instruments, Displays - PFD/ND - Displays

PFD/ND Display System – Overview Display Units

D6-27370-8HX - 94XER-UKR

10.11.1. H4ADR788_4 April 13, 2015

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Flight Instruments, Displays - Advisory messages

TCAS Messages

TCAS Navigation Display

Navigation display showing TCAS messaging and TA symbol format.

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Flight Instruments, Displays - ND - Symbols

TCAS

SYMBOL NAME MODE REMARKS

TCAS resolution advisory (RA), relative altitude (R)

MAP, MAP CTR, VOR, APP

These symbols are displayed only when the EFIS control panel traffic (TFC) switch is selected on. Refer to Chapter 15, Warning Systems. The arrow indicates traffic climbing or descending at a rate >= 500 fpm. At rates < 500 fpm, the arrow is not displayed. The number and associated signs indicate altitude of traffic in hundreds of feet relative to the airplane. The number is below the traffic symbol when the traffic is below, and above the traffic symbol when the traffic is above the airplane. Absence of the number implies altitude unknown.

TCAS traffic advisory (TA), relative altitude (A)

TCAS proximity traffic, relative altitude (W)

TCAS other traffic, relative altitude (W)

TCAS no bearing message (RA-R, TA-A)


Message provides traffic type, range in NM, altitude and vertical direction. TFC must be selected on.

TCAS traffic alert message (RA-R, TA-A)

All Displayed whenever a TCAS RA or TA is active. EFIS control panel TFC switch does not have to be selected on.

TCAS off scale message (RA-R, TA-A)


Displayed whenever RA or TA traffic is outside the traffic area covered by the ND range. Displayed only if the EFIS control panel TFC switch is selected on.

TCAS mode (C) MAP, MAP CTR, VOR, APP

Indicates the ND TCAS display is active; the EFIS control panel TFC switch is selected on.


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TCAS mode (C) All Indicates TCAS computer is not computing RAs. Displayed whether the EFIS control panel TFC switch is selected on or off.

TCAS mode (C) All Indicates TCAS is operating in the test mode. Displayed whether EFIS control panel TFC switch is selected on or off.

TCAS mode (A) All Displayed when the TCAS/ATC mode switch is not in TA ONLY or TA/RA. Not displayed if TCAS is failed.

TCAS mode (A) All Indicates TCAS failure, if traffic is selected.

Range Ring (W) MAP, MAP CTR, VOR APP

Displayed when TFC selected on EFIS Control Panel. Shows 3 NM range ring oriented to aircraft heading. Displayed at ranges of 80 NM or less.


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Warning Systems - Control and Indication

TCAS Controls (Transponder Panel) UR-PSA, UR-PSB, UR-PSC, UR-PSD UR-PSK, UR-PSL

TA (Traffic Advisory) - enables the display of traffic advisory (TA) targets. TA/RA (Resolution Advisory) - enables the display of traffic advisory (TA) and resolution advisory (RA) targets.


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Traffic Alert and Collision Avoidance System (TCAS) TCAS alerts the crew to possible conflicting traffic. TCAS interrogates operating transponders in other airplanes, tracks the other airplanes by analysing the transponder replies, and predicts the flight paths and positions. TCAS provides advisory and traffic displays of the other airplanes to the flight crew. Neither advisory, guidance, nor traffic display is provided for other airplanes which do not have operating transponders. TCAS operation is independent of ground–based air traffic control. To provide advisories, TCAS identifies a three dimensional airspace around the airplane where a high likelihood of traffic conflict exists. The dimensions of this airspace are based upon the closure rate with conflicting traffic. TCAS equipment interrogates the transponders of other airplanes to determine their range, bearing, and altitude. A traffic advisory (TA) is generated when the other airplane is approximately 40 seconds from the point of closest approach. If the other airplane continues to close, a resolution advisory (RA) is generated when the other airplane is approximately 25 seconds from the point of closest approach. The RA provides aural warning and guidance as well as manoeuvre guidance to maintain or increase separation from the traffic. Non–transponder equipped airplanes are invisible to TCAS. RAs can be generated if the other airplane has a mode C transponder. Coordinated RAs require both airplanes to have TCAS. Advisories and Displays Annunciations associated with TCAS and the traffic displays are discussed further in Chapter 10. TAs are indicated by the aural “TRAFFIC, TRAFFIC” which sounds once and is then reset until the next TA occurs. The TRAFFIC annunciation appears on the navigation display. The TA symbol appears at the proper range and relative bearing of the other airplane. Altitude and vertical motion are included with the symbol if the other airplane is using transponder mode S or C. RAs are indicated by one or more aural listed in the RA aural table. The TRAFFIC annunciation and RA symbol which depicts the traffic’s relative bearing, range, altitude, and vertical motion are on the navigation display similar to the TA symbol. Additional symbols are proximate traffic and other traffic. Proximate traffic is within six miles and 1200 feet vertically, but is not expected to cause a TA or RA alert. Other traffic is beyond the six mile and 1200 feet vertical criteria. Traffic symbols are revised as the TCAS system constantly re-evaluates the motion of other airplanes. If the range of the navigation display does not permit the display of a TA or RA an OFFSCALE annunciation appears on the navigation display. TA or RA traffic detected by TCAS which do not provide a bearing generate no–bearing text block beneath the TRAFFIC text on the navigation display. The text block contains distance, altitude, and vertical motion information.


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Vertical motion information is indicated by an arrow depicting a climb or descent if a change of greater than 500 feet per minute is detected. TCAS display automatically shows when:

• the transponder mode selector is in TA ONLY or TA/RA, and • a TCAS TA or RA occurs, and • neither pilot has the TCAS (TFC) display selected, and • in MAP, center MAP, VOR, or APP modes.

Inhibits INCREASE DESCENT RAs are inhibited below approximately 1,500 feet radio altitude. DESCEND RAs are inhibited below approximately 1,100 feet radio altitude. All TCAS voice annunciations and all RAs are inhibited below approximately 1,000 feet radio altitude. Below 1,000 feet when the TA/RA mode is selected on the transponder panel, TA only mode is enabled automatically and the TCAS message TA ONLY displays on the ND. All TCAS alerts are inhibited by GPWS and windshear warnings. Mode Control The TCAS operating mode is controlled from the TCAS/ATC transponder panel. TCAS is normally operated in the TA/RA mode. However, sometimes it is necessary to operate in the TA ONLY mode to prevent undesired RAs. For example, TA ONLY may be selected when intentionally operating near other airplanes such as might be found in VFR conditions at a busy airport, or on parallel approach. ATC transponders on TCAS equipped airplanes communicate to provide appropriate coordinated avoidance manoeuvre’s. When performance is limited, such as with an inoperative engine, select TA ONLY to prevent receiving RAs beyond the airplane’s capabilities, and to prevent communicating to other airplanes an ability to perform a RA manoeuvre. Resolution Advisory Aural The following table(s) identifies the possible callouts associated with RAs and the vertical restrictions or manoeuvre recommended in each case.


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APPENDIX 7 B737-35BSF FCOM D6-27370-301-CGE MSN23237 (LZ-CGO) & MSN23970 (LZ-CGP)

No change to existing operators FCOM supplement D6-27370-301-CGE Rev 16 dated Dec 15/2014

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APPENDIX 8A TCAS AURALS EFIS - B737-300/400/500 MSN27347 (F-GIXS), MSN29333 (F-GZTA), MSN29336 (F-GZTB) MSN25595 (F-GZTJ)

No change to existing operators FCOM supplement

D6-27370-3B3-EUE Dated April 18 2014.

APPENDIX 8B Systems Description - Chapter 15 Warning Systems - Traffic Alert and Collision Avoidance

System (TCAS) MSN32414 (F-GZTC), MSN32418 (F-GZTD) Only. FCOM Master heading - Systems Description


Sub Chapter 15.20.23 - Resolution Advisory, Aurals

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D6-27370-73V - EUV 15.20.23. H4ADR788_5 June 19, 2015

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APPENDIX 9 B737-35BSF FCOM D6-27370-3/400-TRX MSN24355 (EI-CXR).

No change to existing operators FCOM supplement D6-27370-3/400-TRX Rev 2 dated Dec 5/2014

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APPENDIX 10 737-3H9 FCOM D6-27370-3H9-JAT SYSTEM DESCRIPTION SECTION 15.20.27.1 'RESOLUTION

ADVISORY AURALS' MSN23329 (YU-AND), MSN23416 (YU-ANI), MSN23714 (YU-ANJ) MSN23715 (YU-ANK).

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Resolution Advisory Aurals (With TCAS Version 7.1) The above table identifies the possible callouts associated with RAs and the vertical restrictions or manoeuvre recommended in each case.

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APPENDIX 11 737-36N FCOM D6-27370-36NJ-GEF SYSTEM DESCRIPTION SECTION 15.20.27.1 'RESOLUTION

ADVISORY AURALS' MSN28561 (EI-IGR), MSN28652 (EI-IGS).

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EI-IGR, EI-IGS The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-36NJ-GEF

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APPENDIX 12 737-8KN FCOM D6-27370-800-CDY SYSTEM DESCRIPTION SECTION 15.20.21.1 'RESOLUTION

ADVISORY AURALS' MSN35795 (PH-CDE).

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PH-CDE The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-800-CDY

15.20.21.1 H4ADR788_6 Aug 17, 2015

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APPENDIX 13

B737-301 FCOM D6-27370-375-SWF MSN23512 (EC-LJI), MSN24022 (EC-LAC)

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EC-LJI, EC-LAC The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-375-SWF

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APPENDIX 14 B737-4QHGW FCOM D6-27370-528-DAU SYSTEM DESCRIPTION SECTION 15.20.25.1

'RESOLUTION ADVISORY AURALS' MSN28494 (HA-FAU).

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Warning Systems - System Description


HA-FAU The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-528-DAU

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APPENDIX 15 B737-4QHGW FCOM D6-27370-46Q-SNU SYSTEM DESCRIPTION SECTION 15.20.25.1

'RESOLUTION ADVISORY AURALS' MSN29000 (HA-FAV).

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HA-FAV The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-46Q-SNU

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APPENDIX 16 B737-86N FCOM D6-27370-8Z0-XIN SYSTEM DESCRIPTION SECTION 15.20.20.1

‘RESOLUTION ADVISORY AURALS’ MSN29889 (YC428)

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YC428, YK162 The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-8Z0-XIN

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APPENDIX 17

SYSTEM DESCRIPTION SECTION, 15.20.25.1 ‘RESOLUTION ADVISORY AURALS’ VQ-BEO (MSN30293), VQ-BOY (MSN28825), VQ-BMP (MSN28617).

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YB911, YC463, YC705 The following table identifies the possible callouts associated with RAs and the vertical restriction or maneuvers recommended in each case.























D6-27370-800-SKK

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APPENDIX 18 SYSTEM DESCRIPTION SECTION, 15.20.31 ‘RESOLUTION ADVISORY AURALS’ LZ-CGT

(MSN24691).

D6-27370-301-CGE NO CHANGE TO EXISTING FCOM

PW036

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APPENDIX 19 D6-27370 - 86N-HNA

Systems Description - Chapter 10 Flight Instruments, Displays, System Description Chapter 15

Warning Systems - Traffic Alert and Collision Avoidance System (TCAS) (MSN28614 & MSN30231 ONLY)

FCOM Master heading - Supplementary Procedures.

Chapter SP - General TCAS Change 7.1

Sub Chapter 05.3. - Supplementary Procedures TCAS General. 05.4 - Supplementary Procedures TCAS General.



10.11.29.01 - PFD/ND - Displays. 10.11.39.01 - PFD/ND - Displays. 10.11.78.01 - Navigation Displays - Advisory messages - TCAS Messages. 10.16.3.01 - Flight Instruments, Displays - EFIS Control Panel - Controls. 10.16.4.01 - Flight Instruments, Displays - EFIS Control Panel - Controls. 10.16.5.01 - Flight Instruments, Displays - EFIS Control Panel - Controls. 10.41.26 - ND Symbols - TCAS 10.41.27 - ND Symbols - TCAS


Sub Chapter 15.10.19 - TCAS controls (Transponder Panel) 15.20.26.01 - TCAS - Warning Systems - Advisories and Displays 15.20.27.01 - TCAS - Warning Systems - Inhibits & Mode Control 15.20.30.01 - TCAS - Warning Systems - Resolution Advisory, Aurals 15.20.30.02 - TCAS - Warning Systems - Resolution Advisory, Aurals

NOTE: - IT IS THE OWNER / OPERATORS RESPONSIBILITY TO AMEND THIS AIRCRAFTS FCOM WITH THE FOLLOWING PAGES. THE FCOM TABLE OF CONTENTS (TOC) FOR THE APPROPRIATE CHAPTERS SHALL BE AMENDED ACCORDINGLY. Where the existing FCOM pages have been amended for TCAS 7.1 for the effectivity (YC409 & YC452) of this aircraft then the corresponding following pages can be ignored.

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TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)

SUPPLEMENTARY PROCEDURES TCAS CHANGE 7.1 GENERAL Applicable to – MSN28614 (YC452) MSN30231 (YC409)

Following the identification of two severe safety issues in TCAS II version 7.0, EUROCONTROL has commissioned the Safety Issue Rectification (SIR) initiative, culminating with the present SIRE+ project, to address these two issues. This initiative has proposed to resolve these safety issues through two changes to the TCAS II Minimum Operational Performance Standards (MOPS) ([DO185A]), identified as Change Proposals (CP) 112E and 115. Both EUROCAE Working Group 75 (WG75) and RTCA Special Committee 147 (SC147) have evaluated and endorsed these proposals.

The first, CP-112E, addresses the safety issues referred to as SA01. SA01 events have to do with the Resolution Advisory (RA) reversal logic contained in the TCAS algorithm, e.g. when TCAS reverses the sense of an RA from climb to descend. Typically, reversals occur to resolve deteriorating conditions during an encounter. V7.0 contained reversal logic based on certain assumptions and engineering judgement, but operational experience obtained since deployment has compelled a re-evaluation in areas of that logic, specifically having to do with late reversals.

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SUPPLEMENTARY PROCEDURES TCAS CHANGE 7.1 GENERAL

Applicable to – MSN28614 (YC452) MSN30231 (YC409)

The second change proposal, CP-115, rectifies observed confusion surrounding the aural annunciation “Adjust Vertical Speed, Adjust" (AVSA) during an RA by replacing it with the annunciation “Level Off, Level Off" (LOLO), and changing the TCAS V7.0 display and logic to appropriately support the change. AVSA RAs, introduced with TCAS V7.0, were included in the logic to allow pilots to continue their climb or descent, but to adjust their vertical speed to avoid a potentially dangerous situation with a nearby aircraft. They broadly fall under two categories: weakening RAs and vertical rate magnitude reductions. Weakening RAs resulting in AVSAs include “Do Not Climb" and “Do Not Descend" RAs; these RAs are unaffected by CP-115. Vertical rate magnitude reduction RAs include instructions to limit a climb or descend to a certain vertical speed; for instance, to _500, 1000 or 2000 ft/min. The recommended vertical speed to achieve is indicated by a green bar on the pilot's vertical speed indicator. CP-115 changes the aural annunciation for all AVSA vertical rate reductions to “Level Off, Level Off" and changes the accompanying TCAS display to indicate that a level off manoeuvre will satisfy the RA.

Response to “Level off, level off” RA: Reduce the vertical rate to 0 ft/min (i.e. level off).

The level off must be achieved promptly, not at the next flight level.

“Adjust vertical speed” RAs will become defunct.

Some aircraft will level off hundreds of feet before their cleared level while responding to this new RA. However, the RA will not result in more frequent conflicts with third party aircraft than is experienced with the current version of TCAS.

For further reading see: -

EUROCONTROL Document “TCAS II version 7.1 – Overview for Pilots” EUROCONTROL Document “TCAS II version 7.1 – ACAS II Guide”

www.eurocontrol.int/acas

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B737-800 April 26 2016 H4ADR788_12 10.11.1.

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Flight Instruments, Displays - Advisory messages


TCAS Messages

TCAS Navigation Display

Navigation display showing TCAS messaging and TA symbol format.

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Flight Instruments, Displays - EFIS Control Panel - Controls.


B737-800 April 26 2016 H4ADR788_12 10.16.3.01

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B737-800 April 26 2016 H4ADR788_12 10.16.4.01

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Flight Instruments, Displays - ND - Symbols


TCAS


TCAS resolution advisory (RA), relative altitude (R)


These symbols are displayed only when the EFIS control panel traffic (TFC) switch is selected on. Refer to Chapter 15, Warning Systems. The arrow indicates traffic climbing or descending at a rate >= 500 fpm. At rates < 500 fpm, the arrow is not displayed. The number and associated signs indicate altitude of traffic in hundreds of feet relative to the airplane. The number is below the traffic symbol when the traffic is below, and above the traffic symbol when the traffic is above the airplane. Absence of the number implies altitude unknown.

TCAS traffic advisory (TA), relative altitude (A)

TCAS proximity traffic, relative altitude (W)

TCAS other traffic, relative altitude (W)

TCAS no bearing message (RA-R, TA-A)


Message provides traffic type, range in NM, altitude and vertical direction. TFC must be selected on.

TCAS traffic alert message (RA-R, TA-A)

All Displayed whenever a TCAS RA or TA is active. EFIS control panel TFC switch does not have to be selected on.

TCAS off scale message (RA-R, TA-A)


Displayed whenever RA or TA traffic is outside the traffic area covered by the ND range. Displayed only if the EFIS control panel TFC switch is selected on.

TCAS mode (C) MAP, MAP CTR, VOR, APP

Indicates the ND TCAS display is active; the EFIS control panel TFC switch is selected on.

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TCAS mode (C) All Indicates TCAS computer is not computing RAs. Displayed whether the EFIS control panel TFC switch is selected on or off.

TCAS mode (C) All Indicates TCAS is operating in the test mode. Displayed whether EFIS control panel TFC switch is selected on or off.

TCAS mode (A) All Displayed when the TCAS/ATC mode switch is not in TA ONLY or TA/RA. Not displayed if TCAS is failed.

TCAS mode (A) All Indicates TCAS failure, if traffic is selected.

Range Ring (W) MAP, MAP CTR, VOR APP

Displayed when TFC selected on EFIS Control Panel. Shows 3 NM range ring oriented to aircraft heading. Displayed at ranges of 80 NM or less.

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TCAS Controls (Transponder Panel)

TA (Traffic Advisory) - enables the display of traffic advisory (TA) targets. TA/RA (Resolution Advisory) - enables the display of traffic advisory (TA) and resolution advisory (RA) targets.

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Traffic Alert and Collision Avoidance System (TCAS) TCAS alerts the crew to possible conflicting traffic. TCAS interrogates operating transponders in other airplanes, tracks the other airplanes by analysing the transponder replies, and predicts the flight paths and positions. TCAS provides advisory and traffic displays of the other airplanes to the flight crew. Neither advisory, guidance, nor traffic display is provided for other airplanes which do not have operating transponders. TCAS operation is independent of ground–based air traffic control. To provide advisories, TCAS identifies a three dimensional airspace around the airplane where a high likelihood of traffic conflict exists. The dimensions of this airspace are based upon the closure rate with conflicting traffic. TCAS equipment interrogates the transponders of other airplanes to determine their range, bearing, and altitude. A traffic advisory (TA) is generated when the other airplane is approximately 40 seconds from the point of closest approach. If the other airplane continues to close, a resolution advisory (RA) is generated when the other airplane is approximately 25 seconds from the point of closest approach. The RA provides aural warning and guidance as well as manoeuvre guidance to maintain or increase separation from the traffic. Non–transponder equipped airplanes are invisible to TCAS. RAs can be generated if the other airplane has a mode C transponder. Coordinated RAs require both airplanes to have TCAS. Advisories and Displays Annunciations associated with TCAS and the traffic displays are discussed further in Chapter 10. TAs are indicated by the aural “TRAFFIC, TRAFFIC” which sounds once and is then reset until the next TA occurs. The TRAFFIC annunciation appears on the navigation display. The TA symbol appears at the proper range and relative bearing of the other airplane. Altitude and vertical motion are included with the symbol if the other airplane is using transponder mode S or C. RAs are indicated by one or more aural listed in the RA aural table. The TRAFFIC annunciation and RA symbol which depicts the traffic’s relative bearing, range, altitude, and vertical motion are on the navigation display similar to the TA symbol. Additional symbols are proximate traffic and other traffic. Proximate traffic is within six miles and 1200 feet vertically, but is not expected to cause a TA or RA alert. Other traffic is beyond the six mile and 1200 feet vertical criteria. Traffic symbols are revised as the TCAS system constantly re-evaluates the motion of other airplanes. If the range of the navigation display does not permit the display of a TA or RA an OFFSCALE annunciation appears on the navigation display. TA or RA traffic detected by TCAS which do not provide a bearing generate no–bearing text block beneath the TRAFFIC text on the navigation display. The text block contains distance, altitude, and vertical motion information.

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Applicable to – MSN28614 (YC452) MSN30231 (YC409) Vertical motion information is indicated by an arrow depicting a climb or descent if a change of greater than 500 feet per minute is detected. TCAS display automatically shows when:

• the transponder mode selector is in TA ONLY or TA/RA, and • a TCAS TA or RA occurs, and • neither pilot has the TCAS (TFC) display selected, and • in MAP, center MAP, VOR, or APP modes.

Inhibits INCREASE DESCENT RAs are inhibited below approximately 1,500 feet radio altitude. DESCEND RAs are inhibited below approximately 1,100 feet radio altitude. All TCAS voice annunciations and all RAs are inhibited below approximately 1,000 feet radio altitude. Below 1,000 feet when the TA/RA mode is selected on the transponder panel, TA only mode is enabled automatically and the TCAS message TA ONLY displays on the ND. All TCAS alerts are inhibited by GPWS and winds hear warnings. Mode Control The TCAS operating mode is controlled from the TCAS/ATC transponder panel. TCAS is normally operated in the TA/RA mode. However, sometimes it is necessary to operate in the TA ONLY mode to prevent undesired RAs. For example, TA ONLY may be selected when intentionally operating near other airplanes such as might be found in VFR conditions at a busy airport, or on parallel approach. ATC transponders on TCAS equipped airplanes communicate to provide appropriate coordinated avoidance manoeuvre’s. When performance is limited, such as with an inoperative engine, select TA ONLY to prevent receiving RAs beyond the airplane’s capabilities, and to prevent communicating to other airplanes an ability to perform a RA manoeuvre. Resolution Advisory Aural The following table(s) identifies the possible callouts associated with RAs and the vertical restrictions or manoeuvre recommended in each case.

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Applicable to – MSN28614 (YC452) MSN30231 (YC409).

























Resolution Advisory Aurals (With TCAS Version 7.1)

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Warning Systems - Control and Indication Applicable to – MSN28614 (YC452) MSN30231 (YC409)

Use positive control inputs in the direction and with the magnitude TCAS advises while attempting to sight the conflicting traffic. For TCAS to properly function, initial vertical speed response is expected within 5 seconds of an RA with manoeuvring G forces similar to those felt when responding to an ATC clearance to climb or descend “immediately” (approximately ±0.25 G change in load factor). If possible, visually confirm the necessity and suitability of the avoidance manoeuvre, but recognize that any other aircraft sighted visually may not necessarily be the threat aircraft or the only aircraft to which TCAS is responding.

AURAL INCREASE OR REVERSAL RESOLUTION ADVISORIES RA CATEGORY CORRECTIVE PREVENTATIVE

INCREASE CLIMB RATE

“Increase Climb, Increase Climb”

N/A

INCREASE DESCENT RATE

“Increase Descent, Increase Descent”

N/A

RA REVERSAL TO CLIMB RA

“Descend, Descend Now, Descend, Descend Now”

N/A

RA REVERSAL TO DESCEND

“Climb, Climb Now, Climb, Climb Now”

N/A

Respond immediately to any increase or reversal RA maneuver advisories. Initial vertical speed response to an increase or reversal RA is expected by TCAS within 2-1/2 seconds of issuance of the advisory; use a maneuvering G force of approximately ±0.35 G change in load factor. The pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS II RA. When a TCAS II voice message, “CLEAR OF CONFLICT” is announced, the pilot must promptly return to the previous ATC clearance. Ground proximity leads to the inhibition of those advisories liable to cause a hazardous situation at this level. In decreasing altitude, these are: below 1550 +/- 100ft above ground level (AGL) inhibition of "Increase Descend" RA, below 1100 +/- 100ft AGL, inhibition of "Descend" resolution advisories (RA), below 1000 ft +/- 100ft AGL, TCAS automatic switching to TA Only mode (inhibition all RA’s), below 500 +/- 100ft AGL (600ft in climb, 400ft in descent), inhibition of all RAs and inhibition of aural TAs. NOTE: It is expected that the maneuvering required to achieve the vertical speed

commanded by the RA will be initiated, but not completed, within the above-mentioned response time.

CAUTION Once the RA has been issued, safe separation could be compromised if current vertical speed is changed, except as necessary to comply with the RA. This is because TCAS II-to-TCAS II coordination may be in progress with the intruder airplane, and any change in vertical speed that does not comply with the RA may negate the effectiveness of the other airplane’s compliance with the RA.

If a conflict exists between ATC clearance and RA, follow the Resolution Advisory and advise ATC.

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APPENDIX 20 D6-27370 - 700-AWW

Systems Description - Chapter 10 Flight Instruments, Displays, System Description Chapter 15

Warning Systems - Traffic Alert and Collision Avoidance System (TCAS) (MSN35793 ONLY)

FCOM Master heading - Supplementary Procedures.

Chapter SP - General TCAS Change 7.1

Sub Chapter 05.3. - Supplementary Procedures TCAS General. 05.4 - Supplementary Procedures TCAS General.



10.11.29.01 - PFD/ND - Displays. 10.11.39.01 - PFD/ND - Displays.


Sub Chapter 15.20.36.01 - TCAS - Warning Systems - Resolution Advisory, Aurals 15.20.36.02 - TCAS - Warning Systems - Resolution Advisory, Aurals

NOTE: - IT IS THE OWNER / OPERATORS RESPONSIBILITY TO AMEND THIS AIRCRAFTS FCOM WITH THE FOLLOWING PAGES. THE FCOM TABLE OF CONTENTS (TOC) FOR THE APPROPRIATE CHAPTERS SHALL BE AMENDED ACCORDINGLY. Where the existing FCOM pages have been amended for TCAS II. (effectivity YL282). These pages have not been amended and included in this supplement.

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SUPPLEMENTARY PROCEDURES TCAS CHANGE 7.1 GENERAL Applicable to – MSN35793 (YL282)

Following the identification of two severe safety issues in TCAS II version 7.0, EUROCONTROL has commissioned the Safety Issue Rectification (SIR) initiative, culminating with the present SIRE+ project, to address these two issues. This initiative has proposed to resolve these safety issues through two changes to the TCAS II Minimum Operational Performance Standards (MOPS) ([DO185A]), identified as Change Proposals (CP) 112E and 115. Both EUROCAE Working Group 75 (WG75) and RTCA Special Committee 147 (SC147) have evaluated and endorsed these proposals.

The first, CP-112E, addresses the safety issues referred to as SA01. SA01 events have to do with the Resolution Advisory (RA) reversal logic contained in the TCAS algorithm, e.g. when TCAS reverses the sense of an RA from climb to descend. Typically, reversals occur to resolve deteriorating conditions during an encounter. V7.0 contained reversal logic based on certain assumptions and engineering judgement, but operational experience obtained since deployment has compelled a re-evaluation in areas of that logic, specifically having to do with late reversals.

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SUPPLEMENTARY PROCEDURES TCAS CHANGE 7.1 GENERAL Applicable to – MSN35793 (YL282)

The second change proposal, CP-115, rectifies observed confusion surrounding the aural annunciation “Adjust Vertical Speed, Adjust" (AVSA) during an RA by replacing it with the annunciation “Level Off, Level Off" (LOLO), and changing the TCAS V7.0 display and logic to appropriately support the change. AVSA RAs, introduced with TCAS V7.0, were included in the logic to allow pilots to continue their climb or descent, but to adjust their vertical speed to avoid a potentially dangerous situation with a nearby aircraft. They broadly fall under two categories: weakening RAs and vertical rate magnitude reductions. Weakening RAs resulting in AVSAs include “Do Not Climb" and “Do Not Descend" RAs; these RAs are unaffected by CP-115. Vertical rate magnitude reduction RAs include instructions to limit a climb or descend to a certain vertical speed; for instance, to _500, 1000 or 2000 ft/min. The recommended vertical speed to achieve is indicated by a green bar on the pilot's vertical speed indicator. CP-115 changes the aural annunciation for all AVSA vertical rate reductions to “Level Off, Level Off" and changes the accompanying TCAS display to indicate that a level off manoeuvre will satisfy the RA.

Response to “Level off, level off” RA: Reduce the vertical rate to 0 ft/min (i.e. level off).

The level off must be achieved promptly, not at the next flight level.

“Adjust vertical speed” RAs will become defunct.

Some aircraft will level off hundreds of feet before their cleared level while responding to this new RA. However, the RA will not result in more frequent conflicts with third party aircraft than is experienced with the current version of TCAS.

For further reading see: -

EUROCONTROL Document “TCAS II version 7.1 – Overview for Pilots” EUROCONTROL Document “TCAS II version 7.1 – ACAS II Guide”

www.eurocontrol.int/acas

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Applicable to – MSN35793 (YL282)


B737-800 February 27 2016 H4ADR788_11 10.11.1.01

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B737-800 February 27 2016 H4ADR788_11 10.11.29.01

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B737-800 February 27 2016 H4ADR788_11 10.11.39.01

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Resolution Advisory Aurals (With TCAS Version 7.1)

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SUPPLEMENTARY PROCEDURES GENERAL Applicable to – MSN35793 (YL282)

Use positive control inputs in the direction and with the magnitude TCAS advises while attempting to sight the conflicting traffic. For TCAS to properly function, initial vertical speed response is expected within 5 seconds of an RA with manoeuvring G forces similar to those felt when responding to an ATC clearance to climb or descend “immediately” (approximately ±0.25 G change in load factor). If possible, visually confirm the necessity and suitability of the avoidance manoeuvre, but recognize that any other aircraft sighted visually may not necessarily be the threat aircraft or the only aircraft to which TCAS is responding.

AURAL INCREASE OR REVERSAL RESOLUTION ADVISORIES RA CATEGORY CORRECTIVE PREVENTATIVE

INCREASE CLIMB RATE

“Increase Climb, Increase Climb”

N/A

INCREASE DESCENT RATE

“Increase Descent, Increase Descent”

N/A

RA REVERSAL TO CLIMB RA

“Descend, Descend Now, Descend, Descend Now”

N/A

RA REVERSAL TO DESCEND

“Climb, Climb Now, Climb, Climb Now”

N/A

Respond immediately to any increase or reversal RA maneuver advisories. Initial vertical speed response to an increase or reversal RA is expected by TCAS within 2-1/2 seconds of issuance of the advisory; use a maneuvering G force of approximately ±0.35 G change in load factor. The pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS II RA. When a TCAS II voice message, “CLEAR OF CONFLICT” is announced, the pilot must promptly return to the previous ATC clearance. Ground proximity leads to the inhibition of those advisories liable to cause a hazardous situation at this level. In decreasing altitude, these are: below 1550 +/- 100ft above ground level (AGL) inhibition of "Increase Descend" RA, below 1100 +/- 100ft AGL, inhibition of "Descend" resolution advisories (RA), below 1000 ft +/- 100ft AGL, TCAS automatic switching to TA Only mode (inhibition all RA’s), below 500 +/- 100ft AGL (600ft in climb, 400ft in descent), inhibition of all RAs and inhibition of aural TAs. NOTE: It is expected that the maneuvering required to achieve the vertical speed

commanded by the RA will be initiated, but not completed, within the above-mentioned response time.

CAUTION Once the RA has been issued, safe separation could be compromised if current vertical speed is changed, except as necessary to comply with the RA. This is because TCAS II-to-TCAS II coordination may be in progress with the intruder airplane, and any change in vertical speed that does not comply with the RA may negate the effectiveness of the other airplane’s compliance with the RA.

If a conflict exists between ATC clearance and RA, follow the Resolution Advisory and advise ATC.

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APPENDIX 21 SYSTEM DESCRIPTION SECTION, 15.20.25.1 ‘RESOLUTION ADVISORY AURALS’

CP-3020 (SX-BDW) (MSN28573)

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Applicable to – MSN28537 (PQ996)

























D6-27370-5H6-VGS

15.20.25.1 H4ADR788_21 Jun 29, 2016

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HL8036 (MSN28655), HL8205 (MSN32412) and HL8207 (MSN32413).

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Applicable to – MSN28655 (HL8036), MSN32412 (HL8205) and MSN32413 (HL8207)

























D6-27370-86N-ETJ

15.20.31.1 H4ADR788_22 Jun 29, 2016

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HZ-HAA (MSN25419).

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Applicable to – MSN25419 (HZ-HAA)

























FCOM SUPPLEMENT B737

15.20.31.1 H4ADR788_23 Sept 12, 2016

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PR-GTI (MSN34280), PR-GTK (MSN34281).

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Applicable to – MSN34280 (PR-GTI), MSN34281 PR-GTK)

























D6-27370-76N-GOT

15.20.32.1 H4ADR788_24 Nov 18, 2016

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APPENDIX 25 SYSTEM DESCRIPTION SECTION, RESOLUTION ADVISORY AURALS’

OK-EGO (MSN28475)

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Policy and Procedures for the use of TCAS / ACAS II

Applicable to – MSN28475 (OK-EGO)

























PART A, SUBPART 8

Section 8.3.6 H4ADR788_25 Jan 04, 2017

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APPENDIX 26 SYSTEM DESCRIPTION SECTION, RESOLUTION ADVISORY AURALS’

9M-GSA (MSN24559)

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Policy and Procedures for the use of TCAS / ACAS II

Applicable to – MSN24559 (9M-GSA)

























D6-27370-46Q-GDN(GN)

15.20.25.1 H4ADR788_26 Jan 18, 2017

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APPENDIX 27


5Y-KYD

Supplement AURALS page to D6-27370-76N-KEN dated September 24, 2015

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Applicable to – MSN35632 (5Y-KYD)

























D6-27370-76N-KEN 15.20.23.1 H4ADR788_27 February 17, 2017

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APPENDIX 28

RESOLUTION ADVISORY AURALS. B737-400

9M-MMX (9M-SUD), 9M-RKA, 9M-MQE (9M-SUE), 9M-RKB, 9M-MML (9M-SUB) & 9M-SUA

Supplement AURALS page to D6-27370-4H6-MAS(MH) dated December 6, 2016

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Applicable to – MSN’s 26452, 26459, 26462, 27083, 27085 & 27097

























D6-27370-4H6-MAS(MH) 15.20.22.1 H4ADR788_28 May 17, 2017

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(MSN30159 & MSN30160).

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Applicable to – MSN30159, 30160


























15.20.31.1 H4ADR788_29 June 14, 2018

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APPENDIX 29A SYSTEM DESCRIPTION SECTION, 15.20.20.1 ‘RESOLUTION ADVISORY AURALS’

(MSN30071, 30072 & 30073).

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Applicable to – MSN30071, 30072, 30073




MONITOR VERTICAL SPEED MONITOR VERTICAL SPEED


CLIMB, CLIMB, CLIMB Climb at the displayed pitch

DESCEND, DESCEND, DESCEND Descend at the displayed pitch
















15.20.20.1 H4ADR788_29A June 14, 2018

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APPENDIX 30 SYSTEM DESCRIPTION ‘RESOLUTION ADVISORY AURALS’

(MSN27352, MSN27384).

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Applicable to – MSN27352, 27384


























H4ADR788_30 July 13, 2017

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APPENDIX 31 SYSTEM DESCRIPTION SECTION, ‘RESOLUTION ADVISORY AURALS’

(MSN27930).

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Applicable to – MSN27930


























H4ADR788_31 July 13, 2017

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APPENDIX 32

RESOLUTION ADVISORY AURALS. B737-79L

MSN 34022 (YB590), MSN 34538 (YB593)

Supplement AURALS page to D6-27370-89L-BEJ dated September 15, 2016

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Applicable to – MSN 34022 (YB590), MSN 34538 (YB593)

























D6-27370-89L-BEJ 15.20.32.1 H4ADR788_32 Nov 15, 2017

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APPENDIX 33

RESOLUTION ADVISORY AURALS. B737-7CT

MSN 37088 & MSN 37421

Supplement AURALS page to

D6-27370-8AL-SIL dated December 15, 2016

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Applicable to – MSN 37088 (YB990) MSN 37421 (YB995)

























D6-27370-8AL-SIL 15.20.40.1 H4ADR788_33 July 27, 2017

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Z3-AAM (MSN25249).

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Applicable to – MSN25249 (Z3-AAM)


























15.20.31.1 H4ADR788_34 Mar 16, 2018

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APPENDIX 35


ZS-SBA (MSN26070) & ZS-SBB (MSN26072)

Supplement AURALS page to D6-27370-3Y0J-GUI dated December 11, 2015

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Applicable to – MSN’s 26070 & 26072

























D6-27370-3Y0J-GUI

15.20.22.1 H4ADR788_35 Mar 16, 2018 APPENDIX 28

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APPENDIX 36


N650CS

Supplement AURALS page to D6-27370-4H6-MAS(MH) dated December 6, 2016

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Applicable to – MSN 27191

























D6-27370-4H6-MAS(MH) 15.20.22.1 H4ADR788_36 Sept 25, 2018

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APPENDIX 37

RESOLUTION ADVISORY AURALS. B737-7CT

MSN 30712

Supplement AURALS page to D6-27370-76N-WJI dated September 20, 2018

H4ADR788

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Applicable to – MSN 30712 (YB966)

























D6-27370-76N-WJI 15.20.25.1 H4ADR788_37 March 18, 2019

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