AD 2005-08-12

final rule
Data completeness: 80%

Airworthiness Directives; CENTRAIR 101 Series Gliders

AD Number
2005-08-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-19522
FR Citation
70 FR 20715

Unsafe Condition

Cracks or poorly repaired cracks at the weld seam between the hinge tube and the vertical tube of the rudder pedal could lead to failure of the rudder controls, resulting in loss of directional control of the glider.

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Required Actions

Replace non-strengthened rudder pedals with reinforced rudder pedals (left-hand P/N $Y185A, right-hand P/N $Y196A). Do not install any non-strengthened rudder pedals as specified.

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Compliance Time

Within the next 25 hours time-in-service (TIS) after June 6, 2005, unless already done.

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Affected Aircraft

CENTRAIR Models 101, 101A, 101AP, and 101P gliders, serial numbers 101xx001 through 101xx285 and 101D0501 through 101D0530, 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 4, 2026

Rights: U.S. Government Public Domain

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