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AD 83-07-19 ACTIVE

Primary Flight Control
Key Information
AD Number 83-07-19 Status Active
Effective Date Not specified Issue Date Not specified
Docket Number Unknown Amendment 39-4621
Product Type ["Aircraft"] Product Subtype ["Small Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Polskie Zaklady Lotnieze Spolka zo.o
Model(s) PZL M18
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.