AD 98-14-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A300 B2-1C | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus SAS | A300 B2-203 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus SAS | A300 B2K-3C | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus SAS | A300 B4-203 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Airbus SAS | A300 B4-2C | Airworthiness Directives; Airbus Model A300 Series Airplanes |
Unsafe Condition
Fatigue cracking between fuselage frames 47a and 48 from stringer (STGR) 41 to STGR 43 in the forward canted frames, which could result in failure of the forward canted frame and consequent reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive eddy current inspections to detect cracks in the forward canted frames between fuselage frames 47a and 48 from STGR 41 to STGR 43. Perform temporary repair or replace the forward canted frame with a new frame if cracks are found. Repairs must be accomplished using methods approved by the FAA or DGAC.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Required as indicated, unless accomplished previously.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 series airplanes: B2-1C (all serial numbers), B2K-3C (all serial numbers), B2-203 (all serial numbers), B4-203 (serial number 255), and B4-2C (serial number 256).
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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