AD 98-04-10

final rule
Data completeness: 70%

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

AD Number
98-04-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-240-AD
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Cracking of the lugs of center hinge brackets of spoilers No. 1 and No. 2 could result in detachment of the spoilers 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 high frequency eddy current (HFEC) inspection for cracking of the lugs of the center hinge brackets of spoilers No. 1 and No. 2, and repeat the inspection at intervals not exceeding 8,200 flight cycles. Replace brackets as required using specified British Aerospace Repair Drawings.

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

Compliance Time

Required as indicated, unless accomplished previously. Compliance deadlines vary based on flight cycles as of the effective date (March 24, 1998): (1) Airplanes with <23,200 cycles must inspect prior to 16,000 cycles or within 1,000 flight cycles after the effective date, whichever is later. (2) Airplanes with 23,200-36,499 cycles must inspect within 500 flight cycles after the effective date. (3) Airplanes with ≥36,500 cycles must inspect within 50 flight cycles after the effective date.

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

Affected Aircraft

Airbus Model A300 and A300-600 series airplanes, all serial numbers, certificated in any category.

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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