AD 2005-23-06

final rule
Data completeness: 70%

Airworthiness Directives; Learjet Model 23, 24, 24A, 24B, 24B-A, 24D, 24D-A, 24E, 24F, 25, 25A, 25B, 25C, 25D, and 25F Airplanes Modified by Supplemental Type Certificate SA1731SW, SA1669SW, or SA1670SW

AD Number
2005-23-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-20947
FR Citation
70 FR 69059

Applicability

TypeManufacturerModelDetails
aircraft Learjet 23 Airworthiness Directives; Learjet Model 23, 24, 24A, 24B, 24B-A, 24D, 24D-A, 24E, 24F, 25, 25A, 25B, 25C, 25D, and 25F Airplanes Modified by Supplemental Type Certificate SA1731SW, SA1669SW, or SA1670SW

Unsafe Condition

Failure of the thrust reverser accumulator due to fatigue cracking on the female threads, which could result in the loss of hydraulic power and damage to the surrounding airplane structure.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove the thrust reverser accumulator and make the thrust reverser hydraulic system and the thrust reversers inoperable.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Learjet Model 23, 24, 24A, 24B, 24B-A, 24D, 24D-A, 24E, 24F, 25, 25A, 25B, 25C, 25D, and 25F airplanes modified by Supplemental Type Certificate SA1731SW, SA1669SW, or SA1670SW.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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