Airworthiness Directive

AD 2004-22-28 69 FR 64858 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-24630
Amendment
39-13856
Published
2004-11-09
Effective
2004-12-27
Models covered
1
Last live check
2026-10-01
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AD

2004-22-28

FR doc 04-24630 · 69 FR 64858

AD 2004-22-28Published 2004-11-09Effective 2004-12-27

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to drill holes in the hot lip tube "B" nuts, tighten the "B" nuts to specified torque ranges, and secure the "B" nuts with safety wire.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) Model B100 airplanes. This AD requires you to drill holes in the hot lip tube "B" nuts, tighten the "B" nuts to specified torque ranges, and secure the "B" nuts with safety wire. This AD is the result of reports of loose "B" nuts on the engine inlet that may loosen and permit a leak in the engine inlet anti-ice system. We are issuing this AD to detect and correct loose "B" nuts on the engine inlet, which could result in failure of the engine inlet anti-ice system and consequent ice buildup. This failure and ice buildup could lead to an engine's ingestion of ice with loss of engine power or loss of engine.

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All Beechcraft King Air 100 directives

Applies to 1 model in our index