| AD Number | 83-07-02 | Status | Active |
| Effective Date | April 07, 1983 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-4601 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Polskie Zaklady Lotnieze Spolka zo.o |
| Model(s) | PZL M18 |
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.
Thisamendment becomes effective on April 7, 1983.