AD 98-02-06 R1

final rule
Data completeness: 70%

Airworthiness Directives; Boeing 777-200 Series Airplanes

AD Number
98-02-06 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-NM-03-AD
FR Citation
(Federal Register: November 02, 1999 )

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 777-200 Series Airworthiness Directives; Boeing 777-200 Series Airplanes

Unsafe Condition

Failure of the lock link mechanism to lock the main landing gear (MLG) in the down position, and consequent collapse of the MLG during ground operation.

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Required Actions

Perform a visual inspection to determine the presence and condition of the cotter pin and nut of the lock link mechanism on the side struts and drag struts on the left- and right-hand MLG, in accordance with Boeing Alert Service Bulletin 777-32A0015. Repeat the inspection at intervals not to exceed 75 days or 400 flight cycles, whichever occurs first. Alternatively, replace the existing retention bolt, end caps, washer, and nut with a new lock link assembly per Boeing Service Bulletin 777-32-0016 as a terminating action.

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Compliance Time

Within 30 days after February 9, 1998. Repeat inspections at intervals not to exceed 75 days or 400 flight cycles, whichever occurs first.

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Affected Aircraft

Boeing 777-200 series airplanes, line positions 1 through 40 inclusive.

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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