AD 83-07-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Polskie Zaklady Lotnieze Spolka zo.o | PZL M18 | Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes |
Unsafe Condition
Loss of primary flight control about the airplane roll axis due to failure of the aileron push rods connecting segment.
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Required Actions
Replace the connecting segment of the aileron push rods with Part No. 3-26x1-430 ZN-72/L-381-307 as per Mandatory Bulletin No. I/012/81 dated 4/81. Use an equivalent method approved by the FAA if required.
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Compliance Time
within the next 100 hours time-in-service after effective date of this AD, unless already accomplished
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Affected Aircraft
Wytwornia Model PZL M18 (Serial Numbers 1Z005-11 through 1Z005-14)
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Federal Register Abstract
Primary Flight Control
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_83-07-19.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-07-19 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes Subject: Primary Flight Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Polskie Zaklady Lotnieze Spolka zo.o Model: PZL M18 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 83-07-19 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4621 AD NUMBER: 83-07-19 SUBJECT HEADING: Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-07-19 WYTWORNIA SPRZETU KOMUNIKACYJNEGO PZL-MIELEC: Amendment 39-4621. Applies to Model PZL M18 (Serial Numbers 1Z005-11 through 1Z005-14) airplanes certificated in any category. Compliance: Required within the next 100 hours time-in-service after effective date of this AD, unless already accomplished. To prevent loss of primary flight control about the airplane roll axis, accomplish the following: a) Replace the connecting segment of the aileron push rods with Part No. 3-26x1- 430 ZN-72/L-381-307 as prescribed in Mandatory Bulletin No. I/012/81 dated 4/81. b) Aircraft may be flown in accordance with Federal Aviation Regulation 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. FOOTER:
Document Text
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AD Final Rules - DRS_83-07-19.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-07-19 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes Subject: Primary Flight Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Polskie Zaklady Lotnieze Spolka zo.o Model: PZL M18 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 83-07-19 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4621 AD NUMBER: 83-07-19 SUBJECT HEADING: Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-07-19 WYTWORNIA SPRZETU KOMUNIKACYJNEGO PZL-MIELEC: Amendment 39-4621. Applies to Model PZL M18 (Serial Numbers 1Z005-11 through 1Z005-14) airplanes certificated in any category. Compliance: Required within the next 100 hours time-in-service after effective date of this AD, unless already accomplished. To prevent loss of primary flight control about the airplane roll axis, accomplish the following: a) Replace the connecting segment of the aileron push rods with Part No. 3-26x1- 430 ZN-72/L-381-307 as prescribed in Mandatory Bulletin No. I/012/81 dated 4/81. b) Aircraft may be flown in accordance with Federal Aviation Regulation 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. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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