AD Amdt-39-10682

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A310 Series Airplanes

AD Number
Amdt-39-10682
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-44-AD
FR Citation
63 FR 40819

Applicability

TypeManufacturerModelDetails
aircraft Airbus A310 Airworthiness Directives; Airbus Model A310 Series Airplanes

Unsafe Condition

Corrosion between scuff plates at exit and cargo doors and fatigue cracks originating from certain fastener holes in adjacent structures could reduce structural integrity of the door surroundings.

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

Required Actions

Inspect lower door surrounding structure for cracks and corrosion, repair if necessary. Inspect corner doublers, fail-safe ring, and door frames for hole cracking, repair if necessary. Optional terminating actions are provided for certain inspections.

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 A310 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

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