AD 83-07-19

final rule

Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes

AD Number
83-07-19
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
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.

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

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.

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

Compliance Time

within the next 100 hours time-in-service after effective date of this AD, unless already accomplished

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

Affected Aircraft

Wytwornia Model PZL M18 (Serial Numbers 1Z005-11 through 1Z005-14)

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

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
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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Superseded AD: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Superseded By: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

Show stored source text (verify against official source)
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

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