AD 2006-25-15

final rule
Data completeness: 80%

Airworthiness Directives; Sicma Aero Seat; Third Occupant Seat Assemblies, 133 Series

AD Number
2006-25-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-22959
FR Citation
71 FR 75411

Unsafe Condition

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Visually inspect 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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 90 days after the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Sicma Aero Seat third occupant seat assemblies, 133 series, with part numbers 1330622-070, 1330622-070-1, 1330622-070-2, 1330622-100, and 1330622V100-1, and serial numbers as listed in Table 1 of the AD. These seats are installed on, but not limited to, Airbus A319, A320, and A321 series airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗