# Proposed AD FAA-2005-21356: Boeing Model 777-200 and -300 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2005-25-24
- Products: Boeing
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: June 3, 2005, 70 FR 32524
- Comments due: July 18, 2005
- Became: [AD 2005-25-24](https://openairdocs.org/ad/2005-25-24)
- Docket: FAA-2005-21356 (https://www.regulations.gov/docket/FAA-2005-21356, where comments are filed)
- Project: 2004-NM-223-AD
- FR document: 05-11049
- Official PDF: https://openairdocs.org/files/sha256/16/19/1619e850ae6144677045856c5da14649ae6e98d9691776b04dcb9da054737ca8 (from https://www.govinfo.gov/content/pkg/FR-2005-06-03/pdf/05-11049.pdf)
- Federal Register: https://www.federalregister.gov/documents/2005/06/03/05-11049/airworthiness-directives-boeing-model-777-200-and--300-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/89CB65123B8E523486257015005C9C5C.0001
- Page: https://openairdocs.org/proposed/FAA-2005-21356

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 777-200 and -300 series airplanes. This proposed AD would require repetitive detailed inspections of the forward lugs of the power control unit (PCU), yoke assembly, and forward attachment hardware of the left inboard, left outboard, right inboard, and right outboard flaperon PCUs; and other specified/ corrective actions if necessary. For certain airplanes, the proposed AD also would require other related concurrent actions. This proposed AD is prompted by reports indicating that operators have found worn, fretted, and fractured bolts that attach the yoke assembly to the flaperon PCU. We are proposing this AD to prevent damage and eventual fracture of the yoke assembly, pin assembly, and attachment bolts that connect the inboard and outboard PCUs to a flaperon, which could lead to the flaperon becoming unrestrained and consequently departing from the airplane. Loss of a flaperon could resultin asymmetric lift and reduced roll control of an airplane. A departing flaperon could also cause damage to the horizontal and vertical stabilizers, which could result in loss of control of the airplane if damage is significant.

## Notices in this docket

- Jun 3, 2005: Notice of proposed rulemaking (NPRM). (first notice), FR document 05-11049, comments due Jul 18, 2005 (https://www.federalregister.gov/documents/2005/06/03/05-11049/airworthiness-directives-boeing-model-777-200-and--300-series-airplanes)

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