AD 98-12-13

final rule
Data completeness: 70%

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

AD Number
98-12-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-CE-141-AD
FR Citation
Federal Register: June 8, 1998 (Volume 63, Number 109)

Applicability

TypeManufacturerModelDetails
aircraft Piaggio Aero Industries S.p.A. P-180 Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Unsafe Condition

Low pitch stop switch support displacement could result in an improper cockpit indication that the propeller is in the Beta range and cause loss of control of the airplane.

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

Required Actions

Modify the low pitch stop switch support in accordance with Industrie Aeronautiche e Meccaniche Piaggio Service Bulletin (Mandatory) No. SB-80-0080, dated July 3, 1997. Special flight permits may be issued to operate the airplane to a location where the AD requirements can be accomplished.

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

Compliance Time

within the next 150 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished

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

Affected Aircraft

Model Piaggio P-180 airplanes, serial numbers 1001, 1002, 1004, and 1006 through 1033, 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 8, 2026

Rights: U.S. Government Public Domain

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