FAA Spots Cracks in Boeing's Mysterious 'Bear Strap'—Planes Growling?
Published Date: 9/17/2026
Rule
Summary
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. This AD requires inspections for existing repairs; an inspection 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 FAA is issuing this AD to address the unsafe condition on these products.
Analyzed Economic Effects
2 provisions identified: 1 benefits, 1 costs, 0 mixed.
Mandatory inspections and repairs for 737 galley cutout
You (aircraft operators) must inspect certain Boeing Model 737-8, 737-9, and 737-8200 airplanes for cracks at the forward galley door cutout (STA 290 to STA 296, between stringers S-8R and S-9R). The AD requires initial inspections for existing repairs, inspections for any crack of the fuselage skin, bear strap, and stub frame, repetitive inspections of the bear strap and stub frame, and applicable on-condition actions; it is effective October 22, 2026.
Estimated compliance costs for U.S. operators
The FAA estimates this AD affects 476 U.S.-registered airplanes. Estimated costs: Option 1 initial inspections are 31 work-hours × $85 = $2,635 per airplane ($1,254,260 for U.S. operators); Option 2 initial inspections are 7 work-hours × $85 = $595 per airplane ($283,220 total); repetitive internal HFEC inspections are 29 work-hours × $85 = $2,465 per inspection cycle ($1,173,340 per cycle); replacing a stub frame is estimated at 35 work-hours × $85 = $2,975 labor plus $4,334 parts = $7,309 per product.
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