AD 59-17-05

Active

Horizontal Tail Spar Fitting

Key Information
59-17-05
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Small Airplane"]
Helio Aircraft LLC
H-391B H-395 (USAF L-28A or U-10B)
Regulatory Text

59-17-05 HELIO: Applies to All Model H-391B Aircraft Except Serial Numbers 093, 094, and 098; and Model H-395, Serial Numbers 502 Through 510.

Compliance required as indicated.

Within the next 10 hours unless already accomplished inspect the horizontal tail front spar splice plate, P/N 391-020-305, for cracks around all bolt holes and the 2.0-inches diameter lightening hole. If cracks are found, the fitting should be replaced with an identically dimensioned part 0.063-inch 4130 steel. If no cracks are found the original aluminum fitting shall be inspected at each 25 hours thereafter until the next 100-hour inspection or October 1, 1959, whichever occurs first, when it must be replaced with a steel part.

(Helio Service Bulletin No. 21 covers this subject.)

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References
This information is not available.
--- - Part 39
FAA Documents