Airworthiness Directive

AD 2003-06-07 68 FR 14892 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-7185
Amendment
39-13095
Published
2003-03-27
Effective
2003-05-16
Models covered
1
Last live check
2026-10-02
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

2003-06-07

FR doc 03-7185 · 68 FR 14892

AD 2003-06-07Published 2003-03-27Effective 2003-05-16

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 repetitively inspect any engine mount assembly that is not part number 892-51-0-035-0 (or FAA-approved equivalent part number) for cracks; repair cracks that do not exceed a certain length; and replace the engine…

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 2002- 05-04, which applies to certain Socata--Groupe Aerospatiale (Socata) Models MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 150T, and Rallye 150ST airplanes. AD 2002-05-04 requires you to repetitively inspect any engine mount assembly that is not part number 892-51-0-035-0 (or FAA-approved equivalent part number) for cracks; repair cracks that do not exceed a certain length; and replace the engine mount when the cracks exceed a certain length and cracks are found on an engine mount that already has been repaired twice. This AD is the result of the French airworthiness authority's determination that airplanes equipped with an engine mount assembly part number 892- 51-0-035-0 also display the unsafe condition. This AD retains the repetitive inspection and repair requirements of AD 2002-05-04, changes the applicability section, removes the terminating action, and requires replacement of all part number 892-51-0-035-0 engine mount assemblies. The actions specified by this AD are intended to prevent failure of the engine mount assembly. Such failure could result in loss of control of the airplane.

More directives for SOCATA Rallye / MS 880

  1. AD 2024-19-09 Airworthiness Directives; DAHER (Type Certificate Previously Held by SOC... 2024-10-22
  2. AD 2016-08-08 Airworthiness Directives; SOCATA Airplanes 2016-04-13
  3. AD 2002-05-04 Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models MS 892A-150,... 2002-03-11
  4. AD 2000-22-17 Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models MS 880B, MS ... 2000-11-14

All SOCATA Rallye / MS 880 directives

Applies to 1 model in our index