Airworthiness Directive

AD 99-17-10 64 FR 44823 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-21177
Amendment
39-11258
Published
1999-08-18
Effective
1999-09-02
Models covered
1
Last live check
2026-10-03
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AD

99-17-10

FR doc 99-21177 · 64 FR 44823

AD 99-17-10Published 1999-08-18Effective 1999-09-02

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires inspecting the tail rotor swashplate shaft (shaft) nut for looseness and, if loose, inspecting the shaft for proper size; subsequently inspecting the shafts not previously inspected; and replacing any undersized shaft…

Full official abstract

This amendment adopts a new airworthiness directive (AD) applicable to Schweizer Aircraft Corporation (SAC) Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D helicopters. This action requires inspecting the tail rotor swashplate shaft (shaft) nut for looseness and, if loose, inspecting the shaft for proper size; subsequently inspecting the shafts not previously inspected; and replacing any undersized shaft prior to further flight. This amendment is prompted by the discovery of an undersized replacement shaft during routine maintenance. The actions specified in this AD are intended to prevent failure of the shaft and subsequent loss of control of the helicopter.

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All Schweizer 269 / 300 directives

Applies to 1 model in our index