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Airworthiness directives › 2006-25-15

AD 2006-25-15 Airworthiness Directives; Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series

2007-01-19
2006-12-15
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Appliance
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Applicability*9

This AD applies to Sicma Aero Seat third occupant seat assemblies, 133 series, with the part numbers (P/Ns) and serial numbers (SNs) in the following Table 1: Table 1.—Applicable Seat Assemblies Seat P/N Seat SN 1330622-070 1 through 212. 1330622-070-1 1 through 212. 1330622-070-2 1 through 6. 1330622-100 1 through 13. 1330622V100-1 1 through 16. These third occupant seats are installed on, but not limited to, Airbus A319, A320, and A321 series airplanes.

Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Installing Protective Fairings (f) Within 90 days after the effective date of this AD, visually check the installation of the two headrest bushings and install Mecanindus pins, P/N GPMECAE2-5x5, to secure the bushings. Use the instructions in paragraph 2 of Sicma Aero Seat Service Bulletin No. 133-25-006, dated May 12, 1999, to perform the visual inspection and install the pins. Alternative Methods of

Unsafe condition

This AD results from Sicma's determination that missing or incorrectly secured bushings could loosen and cause disengagement of the headrest from the seat during a high-energy stop of the airplane, possibly injuring the seat occupant. We are issuing this AD to prevent disengagement of the headrest from the seat during a high-energy stop of the airplane that could injure the seat occupant.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1