# Proposed AD FAA-2005-22169: Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, and 25F Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2005-23-03
- Products: Learjet
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: August 23, 2005, 70 FR 49210
- Comments due: October 7, 2005
- Became: [AD 2005-23-03](https://openairdocs.org/ad/2005-23-03)
- Docket: FAA-2005-22169 (https://www.regulations.gov/docket/FAA-2005-22169, where comments are filed)
- Project: 2005-NM-094-AD
- FR document: 05-16752
- Official PDF: https://openairdocs.org/files/sha256/2d/bc/2dbce5060d9c864302e872991115a30262940d1188122f111c65c85210578363 (from https://www.govinfo.gov/content/pkg/FR-2005-08-23/pdf/05-16752.pdf)
- Federal Register: https://www.federalregister.gov/documents/2005/08/23/05-16752/airworthiness-directives-learjet-model-23-24-24a-24b-24b-a-24c-24d-24d-a-24e-24f-24f-a-25-25a-25b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5E6B527EDD42174D862570660067B716.0001
- Page: https://openairdocs.org/proposed/FAA-2005-22169

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, and 25F airplanes. This proposed AD would require replacement of the spherical accumulator for the main hydraulic system with a new cylindrical accumulator. For certain airplanes, this proposed AD would also require modification of the accumulator pressure gauge. This proposed AD is prompted by reports of the failure of two thrust reverser accumulators (which are similar to the main hydraulic system's spherical accumulator) and fatigue cracks found on four thrust reverser accumulators. We are proposing this AD to prevent failure of the spherical accumulator for the main hydraulic system, due to fatigue cracking on the threads, which could result in the loss of hydraulic power, damage to the surrounding airplane structure, and loss of airplane control. The failure of the accumulator could also result in injuryto any persons in the surrounding area. The loss of hydraulic fluid could also leak onto a potential source of ignition and result in a consequent fire.

## Notices in this docket

- Aug 23, 2005: Notice of proposed rulemaking (NPRM). (first notice), FR document 05-16752, comments due Oct 7, 2005 (https://www.federalregister.gov/documents/2005/08/23/05-16752/airworthiness-directives-learjet-model-23-24-24a-24b-24b-a-24c-24d-24d-a-24e-24f-24f-a-25-25a-25b)

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