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Airworthiness Directive

AD 2000-16-51 65 FR 50632 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-20777
Amendment
39-11869
Published
2000-08-21
Effective
2000-08-21
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2000-16-51 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2000-16-51

FR doc 00-20777 · 65 FR 50632

AD 2000-16-51Published 2000-08-21Effective 2000-08-21

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to repetitively replace the front tailplane to fuselage joint connector and bushing.

Full official abstract

This document publishes in the Federal Register an amendment adopting emergency Airworthiness Directive (AD) 2000-16-51. The Federal Aviation Administration (FAA) previously sent emergency AD 2000-16-51 to all known U.S. owners and operators of Wytwornia Sprzetu Komunikacyjnego (PZL "Warszawa-Okecie") Model PZL-104 Wilga 80 airplanes. This AD requires you to repetitively replace the front tailplane to fuselage joint connector and bushing. This AD is the result of an incident report where the pin that fastens the tailplane to the fuselage fractured and separated on an airplane of similar design to that of the affected airplanes. The actions specified by this AD are intended to prevent failure of the front tailplane to fuselage joint connector, which could result in loss of control of the airplane if the tailplane and fuselage become disconnected during flight.

More directives for PZL-104 Wilga

  1. AD 2009-14-10 Airworthiness Directives; EADS-PZL “Warszawa-Okęcie” S.A. Model PZL-104 ... 2009-07-08
  2. AD 2009-09-04 Airworthiness Directives; EADS-PZL “Warszawa-Okęcie” S.A. Model PZL-104 ... 2009-04-27

All PZL-104 Wilga directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index