AD 2007-09-06

final rule
Data completeness: 70%

Airworthiness Directives; APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes

AD Number
2007-09-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-27529
FR Citation
72 FR 21077

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes

Unsafe Condition

Cracks in the spar wooden centre blocks generated by wood drying.

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

Required Actions

Install two reinforcement plates on the wing spar to counter shear loading, implement corrective actions to slow wood drying, and introduce new repetitive inspections.

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

Compliance Time

Before further flight

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

Affected Aircraft

APEX Aircraft Model CAP 10 B airplanes, all serial numbers, 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.