AD 2017-15-03

final rule
Data completeness: 80%

Airworthiness Directives; Airbus Airplanes

AD Number
2017-15-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-9572
FR Citation
82 FR 33787

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B4-600 and A300 B4-600R Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracking in the bottom wing skin stringers at Rib 14, which could impair the structural integrity of the wings.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the fastener holes of stringers 10, 11, 12, 17, and 19 using high frequency eddy current (HFEC) inspection for defects. Modify the profile of stringer run-outs of both wings. Remove the stringer end run-out plate at stringer 19 on the bottom wing skin. Perform repairs if necessary.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 12 months of the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Airbus Model A300-B4-601, B4-603, B4-620, B4-622, and Model A300-B4-605R and B4-622R airplanes, certificated in any category, except airplanes on which Airbus Modification 10324 or 10325 has been embodied in production.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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