Opportunity
Federal Register #2026-13481
FAA Airworthiness Directive: Inspections for Rolls-Royce Trent XWB Engines and Boeing 787 Door Handle Retainers
Buyer
Federal Aviation Administration
Posted
July 02, 2026
Identifier
2026-13481
NAICS
541690
The Federal Aviation Administration (FAA), part of the Department of Transportation, has issued new airworthiness directives (ADs) impacting specific aircraft engines and airframes: - Government Buyer: - Federal Aviation Administration (FAA), AIR520 Continued Operational Safety Branch - OEMs Highlighted: - Rolls-Royce Deutschland Ltd & Co KG (RRD) - Boeing (for related airframe directive) - Products/Services and Requirements: - Rolls-Royce Trent XWB-75, XWB-79, XWB-79B, XWB-84, and XWB-97 engines: - Mandatory repetitive visual and dimensional inspections of the main fuel hose assembly of the fuel manifold - Inspections must check for softness, compliance, resistance, shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire - Replacement of the main fuel hose assembly if any damage is found - Optional terminating actions are available to end repetitive inspections - Boeing 787-8, 787-9, and 787-10 airplanes: - Installation of a new retainer above the lower keyway of the door assist handle support bracket assembly - Placard installation or part marking, and inspection/on-condition actions for door assist handles - Notable Requirements: - The directive is a regulatory safety action, not a procurement for new products or services - No specific part numbers or purchase quantities are provided - The AD addresses potential engine fire and airplane damage risks - Compliance times and ongoing inspection intervals are specified in the incorporated EASA AD
Description
The FAA is superseding Airworthiness Directive (AD) 2024-25-10 for certain Rolls-Royce Deutschland Ltd & Co KG Model Trent XWB-97 engines. The directive requires visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to check for softness, compliance, resistance, shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire, with replacement if necessary. The new AD expands applicability to include additional engine models and requires repetitive inspections for some engines. It also provides criteria for installation of affected parts and optional terminating actions for inspections to address an unsafe condition that could lead to engine fire and damage to the airplane.