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EFB CMA-1310 – Battery Swelling

DASSAULT FALCON 2000EX EASY · Service Bulletins

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Overview

This document is a service bulletin for the Dassault Falcon 2000EX EASy, addressing issues related to battery swelling in the CMA-1310 Electronic Display Unit (EDU). It outlines the necessary actions and compliance requirements to ensure safety and airworthiness regarding the affected battery units.

  • Occurrences of battery swelling in CMA-1310 EDU reported.
  • Swelling can damage the unit's touchscreen or dislodge the LCD.
  • Service Bulletins developed to remove the internal battery.
  • Compliance with EASA and FAA Airworthiness Directives is mandatory.
  • Check for visible signs of swelling before each flight.
  • Charging the EFB should occur at least every 3 months.
  • Use of a swollen battery is prohibited until compliance is achieved.
  • Replacement of affected parts is required within specified timeframes.

Document

Source

Originally published by weststaraviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Service Bulletins
Year
·
2025
File size
·
4.0 MB
Publisher
·
weststaraviation.com
Language
·
en
About this document
What is the EFB CMA-1310 – Battery Swelling?

The EFB CMA-1310 – Battery Swelling is a service bulletins for the DASSAULT FALCON 2000EX EASY, dated 2025.

Where does the EFB CMA-1310 – Battery Swelling come from?

This copy of the EFB CMA-1310 – Battery Swelling was originally published by weststaraviation.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the EFB CMA-1310 – Battery Swelling published?

The EFB CMA-1310 – Battery Swelling — the DASSAULT FALCON 2000EX EASY service bulletins on file — is dated 2025.

Documentation completeness
1/7

Most owners only have the POH. Here's the essential set for the DASSAULT FALCON 2000EX EASY.

  • Pilot's Operating Handbook / AFM
  • Checklist
  • Maintenance Manual
  • Parts Catalog (IPC)
  • Systems & Wiring
  • Service Bulletins on file
  • Type Certificate (TCDS)

In this document

Introduction

The document discusses the issues related to swelling of lithium-polymer batteries in the CMA-1310 EDU and the associated risks.

Airworthiness Directives

EASA and FAA have issued directives mandating compliance with specific service bulletins to address battery swelling.

Required Actions

Details the required actions for compliance, including replacement of affected parts and inspection procedures.

Safety Instructions

Recommendations for checking the EFB for swelling and actions to take if swelling is detected.

Compliance Timeframes

Specifies the timeframes for compliance with the directives, including 12 months or 800 flight hours.

Contact Information

Provides contact details for technical assistance and support related to the service bulletin.

Safety notes

  • Use and charge of a CMA-1310 EFB with a swollen battery is prohibited.
  • Shut down and remove the EFB if swelling is detected before flight.
  • Perform specific emergency procedures if swelling is detected in flight.
  • Charge the EFB at least every 3 months to prevent swelling.
  • Inspect the external battery during service part installation.

Full document text

PAGE 1 FSN-271-R04-A Date: April 07, 2025 EFB CMA-1310 – Battery Swelling ATA 46 - INFORMATION SYSTEMS F10 Falcon 20 F200 Falcon 50 Falcon 900 Falcon 2000 Falcon 7X 6X -5 EX EX EASy DX LX EX EASy DX LX S LXS  8X Revision Date Description 0 Jan 09, 2023 Original Publication 1 Feb 05, 2024 Availability of SB, release of EASA PAD 2 Mar 20, 2024 Release of EASA AD 2024-0072 3 Sep 10, 2024 Release of FAA NPRM 2024-2022 4 Apr 07, 2025 Release of FAA AD 2025-06-05 Occurrences of swelling of the CMA-1310 PilotView® EDU (Electronic Display Unit) lithium-polymer batteries have been reported. The EFB CMA-1310 has two lithium-polymer battery packs : one external removable pack, and one internal backup battery. External battery swelling can be observed with visible deformation of the unit. Internal battery swelling can damage the unit touchscreen or dislodge the LCD from the unit. To prevent such situation Dassault Aviation has developed Service Bulletins 7X-632, F2000EX-507 and F900EX-614 to remove the internal battery from the EDU. PAGE 2 FSN-271-R04-A Date: April 2, 2025 EASA has published the attached Airworthiness Directive AD 2024-0072 which mandates the compliance with the relevant Dassault Service Bulletins no later than within 12 months or 800 flight hours, whichever occurs first after the effective date of this AD (29 March 2024). These Service Bulletins are available on the Falcon Portal and recommended to be complied with at the next Maintenance visit without waiting for the EASA AD compliance time or waiting for a similar Airworthiness Directive in the country of registration of your aircraft. FAA has published the attached Airworthiness Directive AD 2025-06-05 which mandates the compliance with the relevant Dassault Service Bulletins no later than within 12 months or 800 flight hours, whichever occurs first after the effective date of this AD (02 May 2025). Pending the compliance with these Service Bulletins, the use and the charge of a CMA-1310 EFB with a swollen battery is prohibited. And the following instructions are recommended:  Check the CMA-1310 EFB for visible signs of swelling before each flight.  If a swollen battery is detected before the flight, shut the EFB down and remove it from the aircraft as soon as possible.  If a swollen battery is detected in flight, shut the EFB down, remove it from the cockpit and if necessary perform the CODDE 2 / QRH 2 – Specific Emergency Situations - PED IN COCKPIT – THERMAL RUNAWAY procedure. To prevent swelling, charge the EFB at least every 3 months. If the EFB has not been charged for three months or more, attempt to charge it on ground outside the aircraft. During and after the charge, check for possible swelling. Note that the external battery can be replaced per AMM task 46-20-02-720-801. FALCON COMMAND CENTER FALCON SPARES FALCON OPERATIONAL SUPPORT FALCON DOCUMENTATION Teterboro, NJ USA PHONE: +1 201 541 4747 EMAIL: commandcenter@dassaultfalconjet.com Teterboro, NJ USA PHONE: +1 201 541 4809 EMAIL: customer.care@dassaultfalconjet.com Teterboro, NJ USA & Saint-Cloud, France FALCON PILOT SUPPORT EMAIL: falconpilot@dassault-aviation.com Teterboro, NJ USA PHONE: +1 201 541 4819 EMAIL: wh.doc-sales@dassaultfalconjet.com Mérignac, France PHONE: +33 5 56 18 47 47 EMAIL: commandcenter@dassault-aviation.com Mérignac, France PHONE: +33 5 56 18 44 44 EMAIL: dafsorders@dassault-aviation.com Little Rock, AR USA & Saint-Cloud, France FALCON CABIN SUPPORT EMAIL: falconcabin@dassault-aviation.com Mérignac, France PHONE: +33 5 56 14 59 25 EMAIL: documentation-sales-and-support@dassault- aviation.com EASA AD No.: 2024-0072 TE.CAP.00110-012 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Page 1 of 3 Airworthiness Directive AD No.: 2024-0072 Issued: 15 March 2024 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation. This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I Part M.A.301, or Annex Vb Part ML.A.301, as applicable, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I Part M.A.303, or Annex Vb Part ML.A.303, as applicable] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption]. Design Approval Holder’s Name: DASSAULT AVIATION Type/Model designation(s): Falcon 900EX, Falcon 2000EX and Falcon 7X aeroplanes Effective Date: 29 March 2024 TCDS Number(s): EASA.A.008, EASA.A.062 and EASA.A.155 Foreign AD: Not applicable Supersedure: None ATA 46 – Information Systems – Electronic Display Unit – Replacement Manufacturer(s): Dassault Aviation (Dassault) Applicability: Falcon 900EX, all manufacturer serial numbers (s/n) that have Dassault modification (mod) M3083 embodied (commercially known as Falcon 900EX Easy, Falcon 900LX and Falcon 900DX). Falcon 2000EX aeroplanes, all s/n that have Dassault mod M1691 embodied (commercially known as Falcon 2000EX Easy, Falcon 2000LX, Falcon 2000LXS, Falcon 2000S and Falcon 2000DX). Falcon 7X aeroplanes, s/n 2 through 400 (inclusive) and s/n 402 (inclusive) and up, including those that have embodied Dassault mod M1000 (commercially known as Falcon 8X). Definitions: For the purpose of this AD, the following definitions apply: The SB: Dassault Service Bulletin (SB) SB F900EX-614, SB F2000EX-507 or SB 7X-632, as applicable.

Show full text

Affected part: CMA-1310 electronic display units (EDU), having Part Number (P/N) 100-604073-000, and with a mod-status between 2 and 6 (inclusive). EASA AD No.: 2024-0072 TE.CAP.00110-012 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Page 2 of 3 Serviceable part: CMA-1310 EDU, having P/N 100-604073-000, and with mod-status 7 or higher. Groups: Group 1 are aeroplanes which have an affected part installed. Group 2 are aeroplanes which do not have an affected part installed. Reason: Occurrences of finding swelling of the lithium-polymer internal and external batteries of CMA-1310 EDU have been reported. The swelling occurs due to a high inrush charge and discharge current stress condition applied on a deeply discharged lithium-polymer battery. This condition, if not corrected, could lead to the thermal runaway of a battery, possibly resulting in in the release of heat, smoke, fire and explosion in the cockpit. To address this potential unsafe condition, Dassault developed a modification, removing the internal battery and updating the BIOS firmware, and issued the SB to provide instructions for affected part replacement with modified units and for modification of an affected part. For the reasons described above, this AD requires replacement of affected parts with serviceable parts and prohibits reinstallation of affected parts. Required Action(s) and Compliance Time(s): Required as indicated by this AD, unless the actions required by this AD have been already accomplished: Replacement: (1) For Group 1 aeroplanes: Within 12 months or 800 flight hours, whichever occurs first after the effective date of this AD, replace each affected part with a serviceable part. This can be accomplished in accordance with the instructions of the SB (see Note 1 of this AD). Note 1: The SB provides instructions to modify an affected part into a serviceable part. Inspection: (2) Concurrently with installation of a serviceable part as required by paragraph (1) of this AD, inspect the external battery of that serviceable part in accordance with the instructions of the SB. Corrective Action(s): (3) If, during the inspection as required by paragraph (2) of this AD, a defective external battery is found, as identified in the SB, before next flight, replace that external battery with a new battery in accordance with the instructions of the SB. Parts Installation: (4) Do not install (see Note 2 of this AD) an affected part on any aeroplane as required by paragraph (4.1) or (4.2) of this AD, as applicable. (4.1) For Group 1 aeroplanes: After modification of the aeroplane as required by paragraph (1) of this AD. EASA AD No.: 2024-0072 TE.CAP.00110-012 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Page 3 of 3 (4.2) For Group 2 aeroplanes: From the effective date of this AD. Note 2: Removing an affected part from an aeroplane and, during the same maintenance visit, re- installing that part on the same location of the same aeroplane, is not considered “install” as specified in paragraph (4) of this AD. Ref. Publications: Dassault SB F900EX-614 original issue dated 15 September 2023, including its ERRATUM dated 18 December 2023. Dassault SB F2000EX-507 original issue dated 15 September 2023, including its ERRATUM dated 18 December 2023. Dassault SB 7X-632 original issue dated 15 September 2023, including its ERRATUM dated 18 December 2023. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. Remarks: 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 05 February 2024 as PAD 24-016 for consultation until 04 March 2024. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs@easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification. 5. For any question concerning the technical content of the requirements in this AD, please contact your Dassault Falcon Technical Assistance: • For Europe, Middle East and Africa based operators: Hot Line: (33) 5 56 18 47 47 • For USA, Canada and Mexico based operators: Help Desk: (1) 800-2FALCON (2325266) • All other areas: Help Desk: (1) 201 541 4747.