AD Amdt-39-10105

final rule
Data completeness: 70%

Airworthiness Directives; Ayres Corporation S2R Series Airplanes

AD Number
Amdt-39-10105
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-CE-65-AD
FR Citation
62 FR 43926

Applicability

TypeManufacturerModelDetails
aircraft Ayres Corporation S2R Series Airworthiness Directives; Ayres Corporation S2R Series Airplanes

Unsafe Condition

Fatigue cracking of the lower spar caps could result in the wing separating from the airplane with consequent loss of control.

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

Required Actions

Inspect the 1/4-inch and 5/16-inch bolt hole areas on the lower spar caps for fatigue cracking and replace any lower spar cap if fatigue cracking is found.

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

Affected Aircraft

Ayres Corporation S2R series airplanes, including Model S2R-R1340 (previously misdesignated as S2R-1340R)

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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