AD 2003-06-51

final rule
Data completeness: 70%

Airworthiness Directives; Learjet Model 45 Airplanes

AD Number
2003-06-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-88-AD
FR Citation
68 FR 19328

Applicability

TypeManufacturerModelDetails
aircraft Learjet 45 Airworthiness Directives; Learjet Model 45 Airplanes

Unsafe Condition

Severe vibration followed by a rapid nose down pitch change, potentially leading to structural failure of the horizontal stabilizer actuator assembly (A66).

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

Required Actions

Inspect the part number of the horizontal stabilizer actuator assembly (A66). Replace any suspect actuator assembly (A66) with a new or serviceable one.

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 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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