AD 83-07-02

final rule

Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes

AD Number
83-07-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Polskie Zaklady Lotnieze Spolka zo.o PZL M18 Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes

Unsafe Condition

Flutter and buffeting which could cause structural damage to the airplane

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

Required Actions

Reinforce all counterweights (elevator and rudder) as prescribed in Mandatory Bulletin Nos. I/010/81 and U/019/81. Aircraft may be flown under FAR 21.197 to a location where this AD can be accomplished. Equivalent methods of compliance must be approved by the Manager, Aircraft Certification Staff.

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

Compliance Time

Within the next 50 hours time-in-service after the effective date of the AD

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

Affected Aircraft

Wytwornia Sprzetu Komunikacyjnego "PZL Mielec" Model PZL M18 Serial Nos. 1Z003-01 through 1Z003-010, 1Z004-05 through 1Z004-010, 1Z005-01 through 1Z005-15

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

Federal Register Abstract

Counterweights Reinforcement

Applicability Source Text

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AD Number:
83-07-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes
Subject:
Counterweights Reinforcement
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/07/1983
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Superseded AD: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Superseded By: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: 83-07-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4601

AD NUMBER:   83-07-02

SUBJECT HEADING:   Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 7, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   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.

This amendment becomes effective on April 7, 1983.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_83-07-02.html
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Print/Save as PDF
Document Versions
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Details
AD Number:
83-07-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes
Subject:
Counterweights Reinforcement
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/07/1983
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: 83-07-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4601

AD NUMBER:   83-07-02

SUBJECT HEADING:   Airworthiness Directives; Wytwornia Model PZL M18 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 7, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   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.

This amendment becomes effective on April 7, 1983.

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.