AD 2001-12-17

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Model Hawker 800XP Series Airplanes

AD Number
2001-12-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-176-AD, Amendment 39-12273
FR Citation
66 FR 33013

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Hawker 800XP Airworthiness Directives; Raytheon Model Hawker 800XP Series Airplanes

Unsafe Condition

Fatigue cracking of the fuselage skin, and consequent loss of cabin pressurization.

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

Required Actions

Inspect to confirm the installation of rivets at fuselage stations 251.975, 262.35, 272.725, and 283.10. If any rivet is missing, install a new rivet before further flight.

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

Compliance Time

Within 600 flight hours or 12 months after the effective date, whichever occurs first.

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

Affected Aircraft

Raytheon Model Hawker 800XP series airplanes, certificated in any category, with serial numbers 258266, and 258277 through 258399 inclusive.

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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