AD 83-07-19

Airworthiness directive · Primary Flight Control · Polskie Zaklady Lotnieze Spolka zo.o PZL M18

Model
PZL M18
Data sheet
TCDSA47EU
Product
Aircraft · Small airplane
Amendment
39-4621

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.

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The airworthiness directive

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.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft

No registered aircraft matched this AD’s modelsForeign aircraft aren’t included, and ADs on propellers and appliances aren’t matched by model.