AD 2008-12-13

final rule
Data completeness: 70%

Airworthiness Directives; GENERAL AVIA Costruzioni Aeronatiche Models F22B, F22C, and F22R Airplanes

AD Number
2008-12-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2008-0423 Directorate Identifier 2008-CE-010-AD
FR Citation
73 FR 34620

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; GENERAL AVIA Costruzioni Aeronatiche Models F22B, F22C, and F22R Airplanes

Unsafe Condition

Cracks found in the Firewall-to-Engine mounting attachments, which could lead to detachment of the engine mounts from the structure.

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

Required Actions

Inspect the structure surrounding the heads of the four bolts of the engine mount attachment bracket for cracks or damages. Repair any cracks or damages found. Repetitive inspections are required at intervals not to exceed 100 hours TIS. If discrepancies are found, repair the aircraft following approved instructions or methods.

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

Compliance Time

Before further flight and repetitively thereafter at intervals not to exceed 100 hours TIS.

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

Affected Aircraft

GENERAL AVIA Costruzioni Aeronatiche Models F22B, F22C, and F22R 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

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