AD 2016-25-27

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus Airplanes

AD Number
2016-25-27
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0143
FR Citation
82 FR 712

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B4-603 Airworthiness Directives; Airbus Airplanes

Unsafe Condition

Cracks in the frame base fittings connecting the frame lower positions to the center wing box.

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

Required Actions

Conduct repetitive detailed inspections for cracking of the lower frame fittings of the frame foot. Replace with a new frame foot if cracking is found. Optional terminating action for repetitive inspections is provided.

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

Compliance Time

Within 60 days of the effective date for reporting inspection findings.

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

Affected Aircraft

Airbus Model A300 B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R variant F airplanes.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.