# Proposed AD FAA-2024-1882: The Boeing Company Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2024-19-01
- Products: Boeing
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: July 3, 2024, 89 FR 55128
- Comments due: August 19, 2024
- Became: [AD 2024-19-01](https://openairdocs.org/ad/2024-19-01)
- Docket: FAA-2024-1882 (https://www.regulations.gov/docket/FAA-2024-1882, where comments are filed)
- Project: AD-2024-00227-T
- FR document: 2024-14608
- Official PDF: https://openairdocs.org/files/sha256/a6/f0/a6f037aa4dc4fb4eccbe7d5670a1d7550031fb256cef15385b1fa3f5c0045473 (from https://www.govinfo.gov/content/pkg/FR-2024-07-03/pdf/2024-14608.pdf)
- Federal Register: https://www.federalregister.gov/documents/2024/07/03/2024-14608/airworthiness-directives-the-boeing-company-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FR-ADNPRM-2024-14608-00000000000.0001
- Page: https://openairdocs.org/proposed/FAA-2024-1882

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SP, and 747SR series airplanes. This proposed AD was prompted by a report indicating cracks at eight fastener hole locations in the fuselage skin lap splice between certain stations (STAs) at certain stringers. This proposed AD would require repetitive inspections of the upper fastener row of the fuselage skin lap splice in a certain area for any crack, and applicable on-condition actions. The FAA is proposing this AD to address the unsafe condition on these products.

## Notices in this docket

- Jul 3, 2024: Notice of proposed rulemaking (NPRM). (first notice), FR document 2024-14608, comments due Aug 19, 2024 (https://www.federalregister.gov/documents/2024/07/03/2024-14608/airworthiness-directives-the-boeing-company-airplanes)

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