AD 2001-15-25

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Model Hawker 800XP Series Airplanes and Model Hawker 800 (U-125A Military) Airplanes

AD Number
2001-15-25
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-274-AD
FR Citation
66 FR 40867

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Hawker 800XP Airworthiness Directives; Raytheon Model Hawker 800XP Series Airplanes and Model Hawker 800 (U-125A Military) Airplanes

Unsafe Condition

The attachment bolt in the main landing gear (MLG) door system may not have had its protruding threads peened, which could lead to disconnection of the retaining hook from its means of actuation, resulting in a gear-up landing and possible injury to passengers and crew.

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

Required Actions

Within 100 flight hours after the effective date, perform a general visual inspection of the MLG attachment bolt to determine if the bolt's protruding threads next to the nuts have been peened. If not peened, peen the threads prior to further flight in accordance with Raytheon Service Bulletin SB 32-3386.

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

Compliance Time

Within 100 flight hours after the effective date

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Affected Aircraft

Raytheon Model Hawker 800XP series airplanes and Model Hawker 800 (U-125A military) airplanes, certificated in any category, as listed in Raytheon Service Bulletin SB 32-3386, dated June 2000.

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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