AD 98-21-30

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes

AD Number
98-21-30
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-74-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2-1A Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2-1C Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2-203 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B2K-3C Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-103 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-203 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-2C Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-601 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-603 Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes
aircraft Airbus A300 B4-605R Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes

Unsafe Condition

Wear damage of the aft attachment fittings of the articulated seats and dummy tracks in the passenger compartment could cause the floor panels to sag and result in failure of flight control systems and consequent reduced controllability of the airplane.

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

Required Actions

Perform a detailed visual inspection for wear damage of the aft attachment fittings using specified Airbus Service Bulletins. If wear exceeds 1 mm, repair prior to further flight. Repeat inspections at intervals not to exceed 6,000 flight cycles.

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

Compliance Time

Inspect prior to the accumulation of 6,000 total flight cycles or within 18 months after the effective date (whichever is later) for airplanes with less than 12,000 flight cycles as of 11/20/1998; within 12 months after 11/20/1998 for those with 12,000+ cycles.

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

Affected Aircraft

Airbus Model A300 series airplanes with Modification 3599/3135 (SB A300-53-0188), all Model A310 and 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 8, 2026

Rights: U.S. Government Public Domain

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