AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 99-03-06 64 FR 5588 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-2496
Amendment
39-11020
Published
1999-02-04
Effective
1999-03-11
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/99-03-06 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

99-03-06

FR doc 99-2496 · 64 FR 5588

AD 99-03-06Published 1999-02-04Effective 1999-03-11

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 a one-time visual inspection to determine the part number of the power control cable assemblies and pulleys of the engine controls; and replacement of the power control cable assemblies and pulleys (as applicable) with…

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Short Brothers Model SD3-60 SHERPA series airplanes, that requires a one-time visual inspection to determine the part number of the power control cable assemblies and pulleys of the engine controls; and replacement of the power control cable assemblies and pulleys (as applicable) with new parts, if necessary. 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 breakage of the power control cable assemblies due to the inflexible construction of the cable, which could result in loss of engine power and consequent reduced controllability of the airplane.

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

View on Federal Register (opens in a new tab) Search DRS manually for AD 99-03-06 (opens in a new tab)

Applies to 1 model in our index