AD 2008-23-13

final rule
Data completeness: 80%

Airworthiness Directives; Hawker Beechcraft Corporation Model 390 Airplanes

AD Number
2008-23-13
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2008-0492
FR Citation
73 FR 67714

Applicability

TypeManufacturerModelDetails
aircraft Beechcraft Corporation Model 390 Airworthiness Directives; Hawker Beechcraft Corporation Model 390 Airplanes

Unsafe Condition

Hydraulic fluid leaking from the engine hydraulic pump output fitting due to an improperly installed elbow connecting the output port to the pulse dampener hose.

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

Required Actions

Remove current preformed packing, elbow fitting, and jam nut from the left and right hydraulic pump pressure output port and install new parts. Install a hydraulic pump case drain check valve.

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

Compliance Time

Within the next 200 hours time-in-service after December 22, 2008, or within the next 6 months after December 22, 2008, whichever occurs first.

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

Affected Aircraft

Hawker Beechcraft Corporation Model 390 airplanes, serial numbers RB-4 through RB-224, 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 4, 2026

Rights: U.S. Government Public Domain

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