2026-17553RuleWallet

Boeing 787 Wings Get Ultrasonic Checks for Shim Gaps

Published Date: 8/27/2026

Rule

Summary

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. This AD was prompted by a Boeing investigation for manufacturing errors and excessive preload forces at the lower side of body (SOB) splice plates common to the lower outboard wing skins. That investigation concluded that shim gaps may have exceeded engineering allowances, and high pull up forces on the components may cause fatigue cracks to form at the fastener holes. This AD requires, depending on configuration, repetitive ultrasonic (UT) inspections at certain splice plates, rear spar terminal fittings, lower chords, front spar terminal fittings, and jack pads for any cracks; repetitive detailed inspections (DET) of certain splice plates for any cracks; and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

Analyzed Economic Effects

3 provisions identified: 1 benefits, 2 costs, 0 mixed.

Mandatory Inspections and Repairs for Boeing 787s

If you operate certain Boeing Model 787-8, 787-9, or 787-10 airplanes, you must perform repetitive ultrasonic (UT) and detailed (DET) inspections at specified splice plates, rear and front spar terminal fittings, lower chords, and jack pads, and do required on-condition repairs per Boeing Alert Requirements Bulletin B787-81205-SB570048-00 RB, Issue 001, dated August 11, 2025. The AD is effective October 1, 2026, applies to airplanes identified in that Boeing bulletin, and the FAA estimates it affects 17 U.S.-registered airplanes with inspection costs up to 286 work hours × $85 = $24,310 per inspection cycle and up to $413,270 total for U.S. operators per inspection cycle.

Equation-Based Compliance Time Tracking Required

The AD requires using equation-based compliance times that combine total flight hours/total flight cycles (TFH/TFC) for initial inspections and flight hours/flight cycles (FH/FC) for repetitive inspections, as specified in Boeing Alert Requirements Bulletin B787-81205-SB570048-00 RB, Issue 001 (dated August 11, 2025). The FAA reviewed a request to allow only simple TFH/TFC or FH/FC limits and rejected it, keeping the equation-based method.

FAA Finds No Significant Small-Entity Impact

The FAA certified that this AD "will not have a significant economic impact, positive or negative, on a substantial number of small entities" under the Regulatory Flexibility Act. That finding is part of the rule's regulatory analysis.

Personalized for You

How does this regulation affect your finances?

Personalize government policy and PRIA will tell you what this federal register document means for your household, plus every other regulation we track. PRIA reads each provision against your financial profile to show you exactly what matters to your wallet.

Key Dates

Published Date
Rule Effective
8/27/2026
10/1/2026

Department and Agencies

Department
Independent Agency
Agency
Transportation Department
Federal Aviation Administration
Source: View HTML

Related Federal Register Documents

Previous / Next Documents

Back to Federal Register