Opportunity

Federal Register #2026-15936

FAA Mandates Inspections and Repairs for Boeing 737-8, 737-9, and 737-8200 Aircraft

Buyer

Department of Transportation, Federal Aviation Administration

Posted

August 06, 2026

Identifier

2026-15936

NAICS

488190

This opportunity concerns a new FAA airworthiness directive for Boeing 737-8, 737-9, and 737-8200 aircraft: - Government Buyer: - Federal Aviation Administration (FAA), Aircraft Certification Service - OEM Highlight: - The Boeing Company is the sole OEM referenced, with the directive specifically targeting their 737-8, 737-9, and 737-8200 models - Products/Services Requested: - Mandatory inspection services for 471 U.S.-registered Boeing 737-8, 737-9, and 737-8200 aircraft - External general visual inspection of fuselage skin for existing repairs - External detailed and eddy current inspections for cracks in the fuselage skin and bear strap at the forward upper corner of the forward galley door cutout - On-condition actions, including repetitive inspections and repairs as required - All procedures must follow Boeing Alert Requirements Bulletin 737-53A1408 RB - Unique/Notable Requirements: - Inspections are required due to reported cracks that could compromise aircraft structural integrity - If cracks or repairs are found, operators must obtain and follow Boeing's instructions for further inspections or repairs - The directive is a service requirement, not a product procurement; no specific part numbers or hardware are being purchased - Estimated inspection costs per cycle range from $85 to $340 per aircraft - Additional Context: - The directive is mandatory for compliance and aims to ensure continued airworthiness and safety of the affected Boeing aircraft fleet

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 of cracks in the bear strap at the forward upper corner of the forward galley door cutout. It requires an inspection of the fuselage skin for existing repairs and applicable on-condition actions to address the unsafe condition. The AD aims to prevent structural integrity issues that could arise from these cracks.

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