Airworthiness Directive

AD 2007-08-08 72 FR 19785 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E7-7048
Amendment
39-15025
Published
2007-04-20
Effective
2007-05-25
Models covered
3
Last live check
2026-10-03
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

2007-08-08

FR doc E7-7048 · 72 FR 19785

AD 2007-08-08Published 2007-04-20Effective 2007-05-25

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 determine if each uplock roller is of the greasible type (one having a drilled and grooved inner race), replace any nongreasible uplock roller (one having a solid inner race) with the greasible type before further…

Full official abstract

We are adopting a new airworthiness directive (AD) that supersedes AD 72-22-01, which applies to certain Raytheon Aircraft Company (RAC) (The Beech Aircraft Company and BEECH previously held Type Certificate Nos. 3A15, 3A16, 5A3, and A-777) Models 33, 35, 36, 45, and 95 series airplanes. AD 72-22-01 currently requires you to determine if each uplock roller is of the greasible type (one having a drilled and grooved inner race), replace any nongreasible uplock roller (one having a solid inner race) with the greasible type before further flight, install hollow zerk-ended mounting bolts on the uplock rollers, and repetitively lubricate the uplock mechanism. Since we issued AD 72- 22-01, there was a recent incident involving a RAC Model 95-B55B (T- 42A) airplane where a seizure of the uplock rollers occurred. This malfunction of the uplock rollers is addressed in AD 72-22-01. Thus, the FAA has determined that the actions of AD 72-22-01 should also apply to certain serial numbers of the Model 95-B55B (T-42A) airplanes. Consequently, this AD retains all the actions of AD 72-22-01, adds those Model 95-B55B (T-42A) airplanes to the applicability of this AD, and lists the specific serial numbers. We are issuing this AD to decrease the possibility of gear-up landings caused by seizure of the uplock rollers.

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 3 models in our index