AD 64-04-02

Active

Stabilizer Attach Fittings

Key Information
64-04-02
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
707-100 Long Body 707-100B Long Body 707-100B Short Body 707-200 707-300 Series 707-300B Series 707-300C Series 707-400 Series 720 Series 720B Series
Regulatory Text

64-04-02 BOEING: Amdt. 687 Part 507 Federal Register February 20, 1964. Applies to All Airplanes Listed in Boeing Service Bulletin No. 942 On Which Service Bulletin No. 942 Has Not Been Accomplished. \n\n\tCompliance required at the next terminal where adequate facilities and personnel are available but not to exceed 30 hours' time in service after the effective date of this AD, unless already accomplished in accordance with Boeing Alert Service Bulletin No. 1967 dated January 31, 1964. \n\n\tInspect both stabilizer center section rear spar upper attach fittings visually for cracks. Inspect all visible areas of the lug area (left and right side). Use a mirror to inspect outboard edge of lug that is sandwiched between lugs of mating part. Replace any center section having cracked parts before further flight.\n \n\tThis directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated February 4, 1964.

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