AD 80-15-02

final rule
Data completeness: 70%

Airworthiness Directives; Partenavia Costruzioni Model P.68 and P.68B Series Airplanes

AD Number
80-15-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Vulcanair S.p.A. P 68 Airworthiness Directives; Partenavia Costruzioni Model P.68 and P.68B Series Airplanes
aircraft Vulcanair S.p.A. P 68B Airworthiness Directives; Partenavia Costruzioni Model P.68 and P.68B Series Airplanes

Unsafe Condition

Loss of proper rudder cable tension and rudder control system failure due to cracks in the rudder pedal interconnecting bell crank bracket and frame number 3, and loose rivets in the rudder cable pulley bracket attachment.

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

Required Actions

Inspect the rudder pedal interconnecting bell crank bracket and frame number 3 for cracks and loose rivets per Service Bulletin 40. If cracks or loose rivets are found, stop drill cracks, replace loose rivets, and replace cracked brackets with P/N 2.3111-1. Alternatively, replace the bracket P/N 2.3097-1 with P/N 2.3111-1. Repeat inspections every 50 hours until replacement is done.

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

Compliance Time

Within the next 50 hours time in service after the effective date (July 21, 1980) for airplanes with over 500 hours time in service on that date; or before accumulating 500 hours time in service or within 50 hours after the effective date, whichever is later, for airplanes with under 500 hours time in service. Inspections must be repeated every 50 hours until replacement.

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

Affected Aircraft

Partenavia Costruzioni Model P.68 and P.68B airplanes, serial numbers 1 through 165 (excluding serial 40), with rudder cable pulley brackets P/N 2.3097-1 installed.

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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