AD 80-19-06

final rule
Data completeness: 70%

Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes

AD Number
80-19-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2-1A Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes
aircraft Airbus A300 B2-1C Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes
aircraft Airbus A300 B2-203 Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes
aircraft Airbus A300 B2K-3C Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes
aircraft Airbus A300 B4-103 Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes
aircraft Airbus A300 B4-203 Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes
aircraft Airbus A300 B4-2C Airworthiness Directives; GROUPEMENT d'INTERET ECONOMIQUE (AIRBUS INDUSTRIE) Model A300 Airplanes

Unsafe Condition

In-flight loss of wing slat closing plates due to cracks in piano hinges, failure of rivets, or cracks/distortion at spring strut attachment lugs.

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

Required Actions

Within the next 20 flights or prior to 800 flights since new, inspect No. 1 L.H. and R.H. wing slat closing plate assemblies for cracks in piano hinges, rivet failures, and cracks/distortion at spring strut attachment lugs. Repeat inspections at intervals not exceeding 1,400 flights until modified. If cracks <2.0 inches, verify pin installation and repeat inspections every 800 flights. If cracks ≥2.0 inches, rivet failures, or bracket issues, incorporate AI Service Bulletin No. A300-57-065, replace rivets/hinges, and replace closing plates as needed before further flight.

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

Compliance Time

Within the next 20 flights after the effective date of this AD, or prior to accumulation of 800 flights since new, whichever occurs later, and at intervals not exceeding 1,400 flights since the previous inspection until modified.

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

Affected Aircraft

Airbus Model A300 B2-1A, B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C airplanes not incorporating AI Modification No. 1909/AI Service Bulletin No. A300-57-065.

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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