Wings – Main Landing Gear Attachment / Rib 5 Forward Lug – Inspection(s)
Proposal for consultation. Not binding until EASA issues the final AD; the requirements can still change.
- Published
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of affected Airbus A300-600, A310, and A300 F4-608ST aeroplanes must perform detailed visual inspections of the main landing gear Rib 5 forward lug within specified compliance times and at defined intervals thereafter. Any discrepancies found must be reported to Airbus and corrected according to approved instructions before further flight. Modifications outlined in the directive may be applied as terminating actions for repetitive inspections. Inspection results must be reported within 30 days after each inspection.
Summary
EASA Airworthiness Directive PAD No. 26-109 is a proposed directive addressing inspection requirements for the main landing gear Rib 5 forward lug on Airbus A300-600, A310, and A300 F4-608ST aeroplanes. It mandates repetitive detailed visual inspections of the affected lugs to detect corrosion and cracking that could compromise the structural integrity of the landing gear attachment. The directive applies to specific serial numbers and configurations as defined in the document.
What changed
This new proposed Airworthiness Directive introduces mandatory repetitive inspections of the main landing gear Rib 5 forward lug for corrosion and cracking on affected Airbus A300-600, A310, and A300 F4-608ST aircraft. It also requires reporting inspection results to Airbus and specifies corrective actions if discrepancies are found. Additionally, it defines terminating actions through specific modifications for certain groups of aircraft.
Why it matters
This directive is critical for aviation professionals as it addresses a potential unsafe condition that could lead to failure of the main landing gear attachment structure. Operators and maintenance organizations must implement these inspections to ensure continued airworthiness and prevent structural failures. Compliance helps maintain fleet safety and avoids costly unscheduled repairs or replacements.
More for Airbus A300-600
All 62- EASA PAD 26-013Fuselage — Door Frames Holes — InspectionJan 26, 2026
- EASA AD 2018-0229R1Wings — Centre Wing Box Frame 47 Angle Fittings — Inspection / ModificationNov 20, 2025
- EASA AD 2025-0255Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitations Items — AmendmentNov 19, 2025
- EASA AD 2025-0236Fuselage — Frame Base Fitting between Frames 41 and 46 — Inspection / RepairOct 23, 2025
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New ADs and bulletins for Airbus A300-600, A300-600ST (Beluga), A310 and A300 F4-608ST, summarized like this page, every Monday.