AD 2020-15-11

Recurring final rule
Data completeness: 70%

Airworthiness Directives; PZL Swidnik S.A. Helicopters

AD Number
2020-15-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2020-0675
FR Citation
85 FR 45073

Applicability

TypeManufacturerModelDetails
aircraft PZL Swidnik S.A. Airworthiness Directives; PZL Swidnik S.A. Helicopters

Unsafe Condition

Corrosion was found on the main rotor vibration absorber star during routine maintenance, which could lead to structural failure of the vibration absorber star, possibly resulting in damage to the main or tail rotor and subsequent loss of control of the helicopter.

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

Required Actions

Visually inspect the main rotor vibration absorber star within an initial compliance time based on the helicopter serial number, and thereafter, repeat the inspections at intervals not to exceed 300 hours time-in-service (TIS) or 12 months, whichever occurs first. Inspect the main rotor vibration absorber star for paint coating delamination, blistering, and discoloration, and missing paint coating, a scratch, a dent, a nick, and corrosion. If there is any paint coating delamination, blistering, or discoloration, or missing paint, a scratch, a dent, a nick, or corrosion, mechanically remove any remaining paint coating. If there is no scratch, dent, nick, or corrosion, repair the paint coating. If there is a scratch, a dent, a nick, or corrosion less than the accumulated maximum total polishing depth of 0.5 mm, repair the surface. If there is a scratch, a dent, a nick, or corrosion that exceeds the accumulated maximum total polishing depth of 0.5 mm, remove the main rotor vibration absorber star from service. Inspect under each bolt head P/N 30.23.000.08.04 for corrosion. Inspect a main rotor vibration absorber star before being installed on any helicopter.

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

Compliance Time

Within 300 hours time-in-service (TIS) or 12 months, whichever occurs first

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

Affected Aircraft

PZL Swidnik S.A. Model PZL W-3A helicopters with main rotor vibration absorber star part number (P/N) 30.23.005.01.04 installed

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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