AD 2004-22-28

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Company Model B100 Airplanes

AD Number
2004-22-28
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2004-CE-11-AD
FR Citation
69 FR 64858

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Aircraft Company Model B100 Airworthiness Directives; Raytheon Aircraft Company Model B100 Airplanes

Unsafe Condition

Loose 'B' nuts on the engine inlet that may loosen and permit a leak in the engine inlet anti-ice system, leading to failure of the system and consequent ice buildup.

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

Required Actions

Drill a 0.035-inch hole in each of the hot tube 'B' nuts (part numbers AN818-6D and AN818-8D), tighten the 'B' nuts to specified torque ranges, and secure the 'B' nuts with safety wire.

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

Compliance Time

Within the next 150 hours time-in-service (TIS) or 6 calendar months after December 27, 2004, whichever occurs first.

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

Affected Aircraft

Raytheon Aircraft Company Model B100 airplanes, serial numbers BE-1 through BE-136, 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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