- Effective
- April 7, 1983
- Model
- PZL M18
- Data sheet
- TCDSA47EU
- Product
- Aircraft · Small airplane
- Amendment
- 39-4601
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
The airworthiness directive
83-07-02 WYTWORNIA SPRZETU KOMUNIKACYJNEGO, "PZL MIELEC": Amendment 39-4601. Applies to Model PZL M18 Serial Nos. 1Z003-01 through 1Z003-010, 1Z004-05 through 1Z004-010, 1Z005-01 through 1Z005-15 airplanes certificated in any category.
Compliance: Required as indicated, unless already accomplished.
To prevent flutter and buffeting which could cause structural damage to the airplane, accomplish the following: a) Within the next 50 hours time-in-service after the effective date of the AD, reinforce all counterweights (elevator and rudder) as prescribed in Mandatory Bulletin Nos. I/010/81 dated February 1981 and U/019/81 dated November 1981.
b) Aircraft may be flown in accordance with FAR 21.197 to a location where this AD can be accomplished.
c) An equivalent method of compliance with this AD if used must be approved by the Manager, Aircraft Certification Staff, AEU-100, Europe, Africa and Middle East Office, FAA, c/o American Embassy, 1000 Brussels, Belgium.
Thisamendment becomes effective on April 7, 1983.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.