AD Amdt-39-10253

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Model Hawker 1000 Series Airplanes

AD Number
Amdt-39-10253
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 97-NM-140-AD
FR Citation
62 FR 66511

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Hawker 1000 Airworthiness Directives; Raytheon Model Hawker 1000 Series Airplanes

Unsafe Condition

The sealant on the core cowl nozzles may extend higher than the forward flange of the core cowl nozzles, which could result in contact between the cowl sealant surface and the lever of the engine mechanical over-speed control system.

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

Required Actions

Modify the aft core cowl nozzles of the left- and right-hand engine nacelles in accordance with Raytheon Service Bulletin SB.71-48-25F021B. Compliance must be within 150 flight hours or 3 months after the effective date of this AD, whichever comes first.

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

Compliance Time

Within 150 flight hours or 3 months after the effective date of this AD, whichever occurs first

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

Affected Aircraft

Raytheon Model Hawker 1000 series airplanes with serial numbers 258151, 258159, and 259003 through 259052 inclusive, certificated in any category.

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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