AD 62-16-04

final rule
Data completeness: 70%

Airworthiness Directives; PIAGGIO Model P.166 Aircraft

AD Number
62-16-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Industrie Aeronautiche e Meccaniche P.166 Airworthiness Directives; PIAGGIO Model P.166 Aircraft

Unsafe Condition

Failure of the frame 20 angle bar at the attachment of the elevator control sector bracket.

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

Required Actions

Inspect the frame 20 angle bar for cracks near the elevator control sector bracket attachment within 10 hours' time in service after the effective date and every 20 hours thereafter. If cracks are found, repair using Piaggio Service Bulletin 166-16 or FAA-approved equivalent before further flight. Discontinue inspections after incorporating the reinforcement specified in Piaggio Service Bulletin 106-16 or FAA-approved equivalent.

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

Compliance Time

Within the next 10 hours' time in service after the effective date of this AD and thereafter within each 20 hours' time in service

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

Affected Aircraft

PIAGGIO Model P.166 Aircraft, Serial Numbers 341 to 403 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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