AD 2005-24-13

final rule
Data completeness: 80%

Airworthiness Directives; Learjet Model 45 Airplanes

AD Number
2005-24-13
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-23144
FR Citation
70 FR 72358

Applicability

TypeManufacturerModelDetails
aircraft Learjet 45 Airworthiness Directives; Learjet Model 45 Airplanes

Unsafe Condition

Chafing between the wire bundle for the alternator on each engine and the hydraulic lines, which could result in a fire in the engine nacelle.

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

Required Actions

Modify the electrical wire bundle for the alternator on the left-hand engine, inspect for clearance between wire harnesses and engine tubing for each engine, and take corrective actions if necessary. For certain airplanes, replace the fuses for the hydraulic shutoff valves with fuses having higher amperage.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

Learjet Model 45 airplanes, certificated in any category; serial numbers (S/Ns) 45-005 through 45-273 inclusive, and 45-2001 through 45-2029 inclusive.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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