# PMV Engineering Service Bulletin AVI-00690-SB-S99-R01 Copy: Revision 01 ("AVI-00690-SB-S99-R01"), 10 pages: PDF https://openairdocs.org/files/sha256/c3/78/c378e5bab175e1b99666bfa55b7d25bdc1b8ab65d8288ace879f03d06770e59c; text https://openairdocs.org/service-documents/pmv/avi00690-sb-s99-r01/file/c378e5bab175.md. Rights: © PMV Engineering. Filed by the FAA in regulations.gov docket FAA-2018-0589; AD 2018-23-03 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [PMV Engineering](https://openairdocs.org/service-documents/pmv.md) - Type: Service bulletin (Service Bulletin) - Number: AVI-00690-SB-S99-R01 - Latest revision known: AVI-00690-SB-S99-R01, Revision 01, dated October 5, 2017 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/pmv/avi00690-sb-s99-r01 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2018-23-03](https://openairdocs.org/ad/2018-23-03.md), effective Dec 14, 2018: Revision 01 Also cited in [1 proposed AD](https://openairdocs.org/service-documents/pmv/avi00690-sb-s99-r01/proposed.md). ## Text (10 pages) Rights: © PMV Engineering. Filed by the FAA in regulations.gov docket FAA-2018-0589; AD 2018-23-03 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 1 / 10 Document based on template ref.: QUA-TEMP-SB-R03 Applicability NOTE: THIS SERVICE BULLETIN IS ONLY APPLICABLE TO THE AIRCRAFT LISTED IN THE ASSOCIATED MASTER DOCUMENT LIST (MDL) REF. AVI-00690-MDL. According to its Design Organisation Approval, PMV engineering undertakes to be compliant with Part 21A.3(a). Therefore, any occurrences which cause or might cause adverse effects on the continuing airworthiness of the product, part or appliance covered by this product change has to be reported to the following e-mail address: airworthiness.office@pmv-engineering.com Authoring (PCM) Verification (CVEs) Approval (HAO) Revision Date Subject of revision Name and sign. Name and sign. Name and sign. R00 18 SEPT 2017 Initial Release R01 05 OCT 2017 AD reference updated ### Page 2 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 2 / 10 Document based on template ref.: QUA-TEMP-SB-R03 TABLE OF CONTENTS 1. Planning information ..................................................................................................................... 3 1.1. Effectivity ............................................................................................................................... 3 1.2. Concurrent requirements ...................................................................................................... 3 1.3. Reason for the change ........................................................................................................... 3 1.4. Description ............................................................................................................................. 3 1.5. Service Bulletin classification ................................................................................................. 3 1.6. Compliance ............................................................................................................................ 3 1.7. Approval ................................................................................................................................. 3 1.8. Weight and balance changes ................................................................................................. 4 1.8.1. Removed load ................................................................................................................ 4 1.9. Electrical load data ................................................................................................................. 4 1.10. References ............................................................................................................................. 4 1.10.1. Existing data ................................................................................................................... 4 1.10.2. External data (not supplied with this Service Bulletin) .................................................. 4 1.10.3. Service bulletin and data supplied with this Service Bulletin ........................................ 4 1.10.4. Installation Drawings ..................................................................................................... 4 1.11. Publications affected ............................................................................................................. 4 1.12. Interchangeability and Intermixability ................................................................................... 4 2. Material Information ..................................................................................................................... 5 2.1. Parts necessary for each airplane .......................................................................................... 5 2.1.1. Equipment and Parts changes ....................................................................................... 5 2.1.2. Installation Kit ................................................................................................................ 5 2.1.3. Parts and Materials Supplied by the Operator .............................................................. 5 2.1.4. Parts Modified and Re-identified ................................................................................... 5 2.1.5. Parts Removed and not Replaced .................................................................................. 5 2.2. Special tooling ........................................................................................................................ 5 3. Accomplishment instructions ........................................................................................................ 6 3.1. General information .............................................................................................................. 6 3.2. Work instructions ................................................................................................................... 6 3.2.1. Preparation .................................................................................................................... 6 3.2.2. TCAS Replacement ......................................................................................................... 7 4. System test ..................................................................................................................................... 8 4.1. Caution and warnings ............................................................................................................ 8 4.2. Test procedure ....................................................................................................................... 8 5. Continuous Airworthiness ............................................................................................................. 8 ### Page 3 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 3 / 10 Document based on template ref.: QUA-TEMP-SB-R03 1. PLANNING INFORMATION 1.1. EFFECTIVITY Refer to the Master Document List AVI-00690-MDL at its latest approved revision for the applicability of this Service Bulletin. Application to any other Aircraft is void. 1.2. CONCURRENT REQUIREMENTS TCAS TPA100-B PN 940-0351-001 must be installed on A/C. 1.3. REASON FOR THE CHANGE This change is following Unjustified Traffic Alert and Collision Avoidance System (TCAS) resolution advisory (RA) triggered with Honeywell TCAS TPA100-B P/N: 940-0351-001. This is a means of compliance to the EASA Airworthiness Directive ref. AD 2017-0196. 1.4. DESCRIPTION The modification consists to upgrade (Software) or to replace existing Honeywell TPA100B TCAS computer P/N: 940-0351-001. 1.5. SERVICE BULLETIN CLASSIFICATION This modification is Optional (customer request) Mandatory CN/AD: AD 2017-0196 1.6. COMPLIANCE No compliance time is given. 1.7. APPROVAL The Technical content of this document is approved under the authority of DOA ref. EASA.21J.487. The approval is granted through the document Supplemental Type Certificate ref. 10050942 at its latest approved revision. ### Page 4 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 4 / 10 Document based on template ref.: QUA-TEMP-SB-R03 1.8. WEIGHT AND BALANCE CHANGES 1.8.1. Removed load No change. 1.9. ELECTRICAL LOAD DATA No Change 1.10. REFERENCES 1.10.1. Existing data Document Title Document Reference Rev Written by Effectivity AIPC AIPC Last AIRBUS All AMM AMM Last AIRBUS All AWM AWM Last AIRBUS All 1.10.2. External data (not supplied with this Service Bulletin) Not applicable. 1.10.3. Service bulletin and data supplied with this Service Bulletin Refer to the Master Document List AVI-00690-MDL at its latest approved revision. 1.10.4. Installation Drawings Refer to the Master Document List AVI-00690-MDL at its latest approved revision. 1.11. PUBLICATIONS AFFECTED The update of the following publication is performed by PMVE: - IPC The update of the following publication is under customer responsibility: - None. 1.12. INTERCHANGEABILITY AND INTERMIXABILITY Not applicable. ### Page 5 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 5 / 10 Document based on template ref.: QUA-TEMP-SB-R03 2. MATERIAL INFORMATION 2.1. PARTS NECESSARY FOR EACH AIRPLANE 2.1.1. Equipment and Parts changes Removed equipment: ITEM reference PART NUMBER MANUFACTURER QTY TPA-100B 940-0351-001 Honeywell 1 All removed material must be equipped with an identification tag for re-installation on this A/C or shipment to store! Installation material (fittings, screws, washers.) of all removed parts shall be collected and stored together with the equipment for identification of used P/N. Added equipment: ITEM reference PART NUMBER MANUFACTURER QTY TPA-100B 940-0351-005 Honeywell 1 2.1.2. Installation Kit Refer to Honeywell SB 940-0351-34-0005. 2.1.3. Parts and Materials Supplied by the Operator Refer to Honeywell SB 940-0351-34-0005. 2.1.4. Parts Modified and Re-identified ITEM reference PART NUMBER MANUFACTURER QTY TPA-100B 940-0351-001 (OLD) 940-0351-005 (NEW) Honeywell 1 2.1.5. Parts Removed and not Replaced Not applicable. 2.2. SPECIAL TOOLING Refer to Honeywell SB 940-0351-34-0005. ### Page 6 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 6 / 10 Document based on template ref.: QUA-TEMP-SB-R03 3. ACCOMPLISHMENT INSTRUCTIONS 3.1. GENERAL INFORMATION CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL, METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR OTHER ELECTRICAL DAMAGE. NOTE: Refer to the AIRBUS Electrical Standard Practices Manuals (ESPM) for the wire installation procedures. NOTE: Refer to Honeywell SB 940-0351-34-0005. All deviations to procedures described in this Service Bulletin shall be notified to PMV Engineering using the Deviation Request Form (last page of this document). 3.2. WORK INSTRUCTIONS 3.2.1. Preparation Description 1. Make sure that the aircraft is electrically grounded, (Refer to AMM Task 12-34-24). 2. Do the job set-up procedure as specified in the removal of the TCAS Computer (1SG) (Refer to AMM Task 34-43-34 PB 401). Performed By Checked By ### Page 7 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 7 / 10 Document based on template ref.: QUA-TEMP-SB-R03 3.2.2. TCAS Replacement Description 1. 2. Option 1 : On A/C Upgrade Apply Honeywell SB 940-0351-34-0005 for software update and re-identification of the TCAS computer. Option 2 : Service Center or Honeywell Authorized Repair Remove TCAS Computer in accordance with AMM 34-43-34 PB 401, Send the TCAS Computer to Service Center or Authorized Repair for Upgrade, Install new TCAS Computer in accordance with AMM 34-43-34 PB 401. Performed By Checked By ### Page 8 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 8 / 10 Document based on template ref.: QUA-TEMP-SB-R03 4. SYSTEM TEST 4.1. CAUTION AND WARNINGS WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. 4.2. TEST PROCEDURE 1. Perform an operational test of TCAS in accordance with AMM TASK 34-43-00 PB501 Performed By Checked By 5. CONTINUOUS AIRWORTHINESS Description 1. List the P/N and S/N of added equipment though the records sheet proposed in the next page or through your own document. 2. In order to issue the change approval, please send this SB signed with the list of P/N -S/N above, by e-mail to airworthiness.office@pmv-engineering.com or by e-fax to +33.9.72.22.84.10 Performed By Checked By ### Page 9 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 9 / 10 Document based on template ref.: QUA-TEMP-SB-R03 u P/N and S/N Records Sheet Send form by e-mail to airworthiness.office@pmv-engineering.com or by e-fax to +33.9.72.22.84.10 Reporting Organisation Name: Country/Site: Approval Ref.: Aircraft MSN : Date of the finding (d/m/y) Name of submitter Signature ……………. Telephone no. E-mail address Added Equipment P/N and S/N: Description P/N S/N TPA-100B 940-0351-005 Removed Equipment P/N and S/N: Description P/N S/N TPA-100B 940-0351-001 ### Page 10 Service Bulletin Ref : AVI-00690-SB-S99-R01 TCAS 7.1 on A320 family This document is the sole property of PMV Engineering and cannot be disclosed, reproduced, or used, in its totality or partially, without written authorisation from PMV Engineering. Page 10 / 10 Document based on template ref.: QUA-TEMP-SB-R03 Send form by e-mail to airworthiness.office@pmv-engineering.com or by e-fax to +33.9.72.22.84.10 The Technical content of this document is approved under the authority of DOA ref. EASA.21J.487. Reporting Organisation Organisation Name Country/Site Approval Ref. Name of submitter Telephone no. E-mail address Signature Aircraft MSN Date of the finding(d/m/y) Description of Deviation Proposed solution Reserved PMVE Classification of deviation (refer to QUA-0001-DOH and QUA-0001-PCD-S14)  Minor  Major PCM Name /Signature Validated solution DO Engineer Name /Signature Closure Date --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.