Airworthiness Directive

AD 99-18-11 64 FR 47660 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-22533
Amendment
39-11277
Published
1999-09-01
Effective
1999-10-06
Models covered
1
Last live check
2026-10-03
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AD

99-18-11

FR doc 99-22533 · 64 FR 47660

AD 99-18-11Published 1999-09-01Effective 1999-10-06

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 replacement of the existing bolts that secure the elevator control torque tube bearing housing retaining plate with hex head bolts.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Short Brothers Model SD3-SHERPA, SD3-60 SHERPA, SD3- 30, and SD3-60 series airplanes, that requires replacement of the existing bolts that secure the elevator control torque tube bearing housing retaining plate with hex head bolts. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent reduced movement of the elevator controls and consequent reduced controllability of the airplane, as a result of bolts coming loose on the elevator control torque tube bearing housing retaining plate.

More directives for Shorts SD3-30 / SD3-60

  1. AD 2010-24-06 Airworthiness Directives; Short Brothers PLC Model SD3 Airplanes 2011-01-12
  2. AD 2008-16-09 R1 Airworthiness Directives; Short Brothers Model SD3-60 Airplanes 2009-08-12
  3. AD 2008-16-09 Airworthiness Directives; Short Brothers Model SD3-60 Airplanes 2008-08-11
  4. AD 2008-12-08 Airworthiness Directives; Short Brothers Model SD3-60 Airplanes Equipped... 2008-06-10
  5. AD 2007-08-09 Airworthiness Directives; Short Brothers Model SD3-60 SHERPA, SD3-SHERPA... 2007-04-23

All Shorts SD3-30 / SD3-60 directives

Applies to 1 model in our index