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2021-11-13 |
BELL TEXTRON CANADA LIMITED: Amendment 39-21575; Docket No. FAA2020-1170; Project Identifier MCAI-2020-00720-R. |
(a) APPLICABILITY This airworthiness directive (AD) applies to Bell Textron Canada Limited (Bell) Model 429 helicopters, certificated in any category, with a Bell Emergency Flotation System (EFS) kit part number (P/N) 429-706-069-101/-103/-105/-121/-123/-125/-139/-141/-143/ or -157 manu- factured before July 2019, with a float supply hose manufactured be- fore January 2014, installed, except for float supply hoses marked with "SB 025-69-21" above the external identification marking. (b) UNSAFE CONDITION This AD defines the unsafe condition as a blocked float supply hose installed on an EFS. This condition could result in partial inflation of an EFS float during an emergency landing on water and subsequently preventing a timely egress from the helicopter. (c) EFFECTIVE DATE This AD is effective July 15, 2021. (d) COMPLIANCE You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accom- plished prior to that time. (e) REQUIRED ACTIONS (1) Within 100 hours time-in-service (TIS): (i) Remove each EFS supply hose from the float and inspect each end of the EFS supply hose by inserting a plastic cable tie 300 mm minimum × 5 mm maximum (11.811 in. minimum × .196 in. maximum), into the holes of the related fitting as shown in Figure 1 of Safran Aerosystems Services Service Bulletin No. 025-69-21, Revision 00, dated March 23, 2020 (SB 025-69-21). Note 1 to paragraph (e)(1)(i): Each end of the supply hose may also be re- ferred to as fitting or banjo. (ii) If the cable tie does not pass through the hose, before further flight, remove the EFS supply hose from service and replace it with an airworthy part. (iii) If the cable tie passes through the supply hose, mark a green dot with indelible ink on the base of the supply hose and write "SB 025- 69-21" above the external identification marking of the EFS with in- delible ink. (2) As of the effective date of this AD, do not install an EFS supply hose manufactured before January 2014 on any helicopter unless the require- ments in paragraph (e)(1) of this AD have been completed. (f) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS) (1) The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (g)(1) of this AD. Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal in- spector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (g) RELATED INFORMATION (1) For more information about this AD, contact Matt Fuller, AD Program Manager, Operational Safety Branch, Airworthiness Products Section, General Aviation & Rotorcraft Unit, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email matthew.fuller@faa.gov. (2) The subject of this AD is addressed in Transport Canada AD CF-2020- 212R1, dated August 19, 2020. You may view the Transport Canada AD on the Internet at https://www.regulations.gov in Docket No. FAA-2020- 1170. (h) MATERIAL INCORPORATED BY REFERENCE (1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Safran Aerosystems Services Service Bulletin No. 025-69-21, Revision 00, dated March 23, 2020 (SB 025-69-21). Note 2 to paragraph (h)(2)(i): SB 025-69-21 is attached to Bell Alert Serv -ice Bulletin No. 429-20-52, dated March 30, 2020, which is not incorpo- rated by reference in this AD. (ii) [Reserved] (3) As the design approval holder for the product identified in paragraph (a) of this AD, contact Bell Textron Canada Limited for the Safran Aerosystems Services service information identified in this AD, at Bell Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone 450-437-2862 or 800-363-8023; fax 450-433-0272; or at https://www.bellcustomer.com. (4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. (5) You may view this service information that is incorporated by refer- ence at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email: fedreg.legal@nara.gov, or go to: https://www.archives.gov/federal- register/cfr/ibr-locations.html. Issued on May 18, 2021. Lance T Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: Matt Fuller, AD Program Manager, Opera- tional Safety Branch, Airworthiness Products Section, General Aviation & Rotorcraft Unit, FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone 817-222-5110; email matthew.fuller@faa.gov.
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