AD 90-02-13

final rule
Data completeness: 70%

Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes

AD Number
90-02-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 310 Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310A Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310B Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310C Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310D Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310E Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310F Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310G Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310H Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes
aircraft Cessna Aircraft Company 310I Airworthiness Directives; CESSNA Models 310, 320, 340, 401, 402, 411, 414 and 421 Airplanes

Unsafe Condition

Cracks in the main gear barrel inner bearing and external lock rings or extended stop spacers could cause jamming of the inner and outer barrels of the main landing gears, leading to loss of structural integrity.

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

Required Actions

Inspect the left and right main gear strut barrel inner bearings (Part Numbers 5041108-1 and 5041108-2) for cracks by removing the lower barrel and axle assemblies, cleaning components, visually inspecting for cracks, and performing magnetic particle inspection per Cessna Service Bulletin MEB88-7. Replace cracked external lock rings or extended stop spacers with serviceable parts and replace cracked inner bearings with Part Number 5141109-1. The 1,000-hour repetitive inspections are waived if P/N 5141109-1 bearings are installed.

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

Compliance Time

Within 300 hours time-in-service after the effective date (February 5, 1990) or upon reaching 1,300 hours time-in-service, whichever occurs later, and thereafter every 1,000 hours time-in-service unless replaced with P/N 5141109-1 bearings.

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

Affected Aircraft

Cessna Models 310 (serial 310L0001-310R1690), 320 (320E0001-320F0045), 340 (340-0001-340A0801), 401 (401-0001-401B0221), 402 (402-0001-402C0125), 411 (411-0001-411A0300), 414 (414-0001-414A0340), and 421 (421-0001-421C0715).

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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