Opportunity
Federal Register #FAA20253439
FAA Airworthiness Directives for Boeing 737 and Airbus A330 Aircraft: Inspections, Repairs, and Modifications Required
Buyer
Federal Aviation Administration
Posted
September 17, 2026
Identifier
FAA20253439
NAICS
488190
This opportunity involves new airworthiness directives from the Federal Aviation Administration (FAA) targeting structural safety issues in commercial aircraft. - Government Buyer: - Federal Aviation Administration (FAA), Transportation Department - OEMs Mentioned: - The Boeing Company - Airbus SAS - Products/Services Requested: - For Boeing 737-8, 737-9, and 737-8200 airplanes: - Initial external and internal inspections (general visual and eddy current) of fuselage skin, bear strap, and stub frame - Repetitive internal high frequency eddy current (HFEC) inspections for cracks - Replacement of stub frame as an on-condition action - Compliance with Boeing Alert Requirements Bulletin 73753A1420 RB - For Airbus A330243, A330243F, A330341, A330342, and A330343 airplanes: - Modification of anti-ice piccolo tube restraint brackets - Repetitive special detailed inspections (SDIs) for discrepancies - Restrictions on certain repairs and installation limits - Unique/Notable Requirements: - Inspections and repairs must follow OEM bulletins and FAA directives - On-condition actions (e.g., replacement) required if cracks are found - Repetitive inspections mandated to ensure ongoing structural integrity - No specific part numbers or quantities; requirements apply to all affected aircraft - Prohibitions on certain repairs and installation of affected parts for Airbus models - Purpose: - Prevent structural failures and ensure continued flight safety for affected Boeing and Airbus aircraft models.
Description
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes. This AD was prompted by reports indicating cracks in the bear strap and stub frame at the forward galley door cutout. It requires inspections for existing repairs, inspections for any crack of the fuselage skin, bear strap, and stub frame, repetitive inspections for any crack of the bear strap and stub frame, and applicable on-condition actions. The AD aims to address the unsafe condition on these products to ensure structural integrity and safety.