AD 2001-03-05

final rule
Data completeness: 70%

Airworthiness Directives; Learjet Model 45 Airplanes

AD Number
2001-03-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-11-AD
FR Citation
66 FR 10353

Applicability

TypeManufacturerModelDetails
aircraft Learjet 45 Airworthiness Directives; Learjet Model 45 Airplanes

Unsafe Condition

Fatigue cracking on the anti-ice manifold splitter vanes could result in metal fragments breaking off and blocking a duct in the anti-ice system, leading to an unannunciated loss of ice protection.

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

Required Actions

Revise the airplane flight manual (AFM) to prohibit flight into known icing conditions; inspect the anti-ice manifold assembly for missing material and perform corrective actions if necessary; replace the anti-ice manifold assembly with a new assembly; revise the Learjet 45 maintenance program to incorporate additional inspections and maintenance practices for the anti-ice manifold assembly.

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

Compliance Time

Within 100 flight hours

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

Affected Aircraft

Learjet Model 45 airplanes

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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