Airworthiness Directive

AD 2002-11-07 67 FR 38849 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-13764
Amendment
39-12768
Published
2002-06-06
Effective
2002-07-15
Models covered
1
Last live check
2026-09-30
This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

2002-11-07

FR doc 02-13764 · 67 FR 38849

AD 2002-11-07Published 2002-06-06Effective 2002-07-15

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 inspect the Instrument Subpanel electroluminescent panel retaining screw for proper length and the rotating beacon circuit breaker switch (or any other switch in the same location) for damage and replace any screw…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Models E55, E55A, A56TC, 58, 58A, 58P, 58PA, 58TC, and 58TCA airplanes. This AD requires you to inspect the Instrument Subpanel electroluminescent panel retaining screw for proper length and the rotating beacon circuit breaker switch (or any other switch in the same location) for damage and replace any screw or circuit breaker switch as necessary. This AD is the result of a report that an improper length electroluminescent panel retaining screw damaged the rotating beacon circuit breaker switch, which resulted in damaged wiring. The actions specified by this AD are intended to prevent damage to the rotating beacon circuit breaker switch or any other switch in the same location because of an incorrect length electroluminescent panel retaining screw. This condition could result in failure of the circuit breaker and lead to smoke and/or fire in the cockpit.

More directives for Beechcraft Baron

  1. AD 2014-26-05 Airworthiness Directives; Beechcraft Corporation Airplanes 2015-01-05
  2. AD 2013-16-01 Airworthiness Directives; Beechcraft Corporation and Hawker Beechcraft C... 2013-08-20
  3. AD 2012-21-05 Airworthiness Directives; Hawker Beechcraft Corporation Airplanes 2012-10-23
  4. AD 2012-10-02 Airworthiness Directives; Hawker Beechcraft Corporation Airplanes 2012-05-17
  5. AD 2011-27-04 Airworthiness Directives; Hawker Beechcraft Corporation Airplanes Equipp... 2011-12-29

All Beechcraft Baron directives

Applies to 1 model in our index