AD 90-08-06

final rule
Data completeness: 70%

Airworthiness Directives; AEROSPATIALE Model ATR42 Series Airplanes

AD Number
90-08-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-251-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft ATR - GIE Avions de Transport R gional ATR42-200 Airworthiness Directives; AEROSPATIALE Model ATR42 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR42-300 Airworthiness Directives; AEROSPATIALE Model ATR42 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR42-320 Airworthiness Directives; AEROSPATIALE Model ATR42 Series Airplanes
aircraft ATR - GIE Avions de Transport R gional ATR42-500 Airworthiness Directives; AEROSPATIALE Model ATR42 Series Airplanes

Unsafe Condition

Failure of the main landing gear wheel due to cracked spokes.

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

Required Actions

Perform a visual inspection of the inboard wheel halves within 7 days or 100 landings after the last inspection under AD 88-09-04, whichever occurs later. Repeat inspections at intervals not exceeding 7 days or 100 landings. At each tire change, conduct an eddy current or nondestructive test. Replace cracked inboard wheel halves before further flight. Terminate repetitive inspections by replacing with reinforced halves and modified hub spacers per service bulletins.

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

Compliance Time

Within 7 days or 100 landings after the last inspection in accordance with AD 88-09-04, whichever occurs later. Repeat inspections at intervals not to exceed 7 days or 100 landings, whichever occurs later.

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

Affected Aircraft

All Model ATR42 series airplanes, certificated in any category, with Loral Part Numbers 5006856, 5006856-1, and 5006856-2, serial numbers OCT83-001 through OCT86-377, excluding OCT86-001 through OCT86-071.

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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