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Airworthiness Directive

AD 98-12-10 63 FR 31104 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-15085
Amendment
39-10566
Published
1998-06-08
Effective
1998-07-17
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/98-12-10 · 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.

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AD

98-12-10

FR doc 98-15085 · 63 FR 31104

AD 98-12-10Published 1998-06-08Effective 1998-07-17

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 installing an inspection opening in the wing, repetitively inspecting the upper wing spar cap for cracks, and repairing any cracks on all Avions Mudry et Cie (Avions) Model CAP 10B airplanes.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 93-10- 11, which currently requires installing an inspection opening in the wing, repetitively inspecting the upper wing spar cap for cracks, and repairing any cracks on all Avions Mudry et Cie (Avions) Model CAP 10B airplanes. This AD will retain the same actions already required by AD 93-10-11, and will add inspecting, and repairing if necessary, the lower surface of the wing spar. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to prevent structural cracks in the wing spar, which could lead to loss of a wing and loss of control of the airplane.

More directives for Mudry / APEX CAP 10

  1. AD 2011-06-01 Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes 2011-03-09
  2. AD 2008-17-07 Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes 2008-08-19
  3. AD 2008-13-32 Airworthiness Directives; APEX Aircraft Model CAP 10B Airplanes 2008-07-08
  4. AD 2008-09-02 Airworthiness Directives; APEX Aircraft Model CAP 10B Airplanes 2008-04-21
  5. AD 2008-07-04 Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes 2008-03-26

All Mudry / APEX CAP 10 directives

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Applies to 1 model in our index