AD 2003-26-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2 and B4 | Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; and A300 B4-600, B4-600R, C4-605R Variant F, and F4-600R (Collectively Called A300-600) Series Airplanes |
Unsafe Condition
Cracking of the lower outboard flange of gantry No. 4 in the main landing gear bay area, which could result in reduced structural integrity of the fuselage and consequent rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower outboard flange of gantry No. 4 in the main landing gear bay area for cracking. Repair any identified cracking as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B2 and B4 Series Airplanes, and A300 B4-600, B4-600R, C4-605R Variant F, and F4-600R (collectively called A300-600) Series Airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.