AD 98-18-13

final rule
Data completeness: 70%

Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB20 and TB21 Airplanes

AD Number
98-18-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-CE-64-AD
FR Citation
Federal Register: September 03, 1998 (Volume 63, Number 171)

Applicability

TypeManufacturerModelDetails
aircraft SOCATA TB 20 Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB20 and TB21 Airplanes
aircraft SOCATA TB 21 Airworthiness Directives; SOCATA - Groupe AEROSPATIALE Models TB20 and TB21 Airplanes

Unsafe Condition

Cracks in the main landing gear (MLG) attachment bearing could result in collapse of the main landing gear during taxi and landing operations.

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

Required Actions

Inspect the MLG attachment bearing using a dye penetrant method at specified intervals. If cracks are found, replace the bearing before further flight. Repeat inspections after replacement as required.

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

Compliance Time

Within the next 100 hours time-in-service after the effective date of this AD, or upon accumulation of 6,000 landings or 4,000 hours time-in-service, whichever occurs later. Subsequent inspections must be done within 1,500 landings or 1,000 hours time-in-service after the previous inspection.

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

Affected Aircraft

SOCATA-Groupe AEROSPATIALE Models TB20 and TB21 airplanes, serial numbers 1 through 9999.

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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