What this page is: a restatement of what the official Federal Register
and manufacturer records show as of the date listed below each item. It is not
a determination that any specific aircraft or engine is, or is not, in compliance.
Under 14 CFR §91.403 and §91.417, the aircraft owner/operator is responsible
for maintaining airworthiness and required records. Always verify against the official FAA
and manufacturer sources linked below before making a maintenance or airworthiness decision.
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Airworthiness Directives
13 records · 2 superseded records nested above
AD
2011-06-01
FR doc 2011-5101 · 76 FR 12845
AD 2011-06-01Published 2011-03-09Effective 2011-04-13
APEX Aircraft Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document 2011-5101, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2008-17-07Published 2008-08-19Effective 2008-09-23
APEX Aircraft Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E8-18807, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2008-13-32Published 2008-07-08Effective 2008-08-12
APEX Aircraft Model CAP 10B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E8-14484, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2008-09-02Published 2008-04-21Effective 2008-05-27
APEX Aircraft Model CAP 10B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10B Airplanes
We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E8-8360, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2008-07-05Published 2008-03-26Effective 2008-04-30
APEX Aircraft Model CA 10B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CA 10B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E8-5955, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2008-07-04Published 2008-03-26Effective 2008-04-30
APEX Aircraft Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E8-5961, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2007-13-14Published 2007-06-29Effective 2007-08-03
APEX Aircraft Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E7-12319, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2007-10-13Published 2007-05-17Effective 2007-06-21
APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E7-9393, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2007-09-06Published 2007-04-30Effective 2007-05-21
APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft (Type Certificate No. A36EU Formerly Held by AVIONS MUDRY et CIE) Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as
Source: Federal Register document E7-7980, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2007-09-05Published 2007-04-30Effective 2007-06-04
APEX Aircraft Model CAP 10 B Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E7-7994, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
Requires installing an inspection opening in the wing, repetitively inspecting the upper and lower wing spars for structural cracking, and, if any cracks are found, repairing the cracks in accordance with a repair method.
2 ADs superseded by this oneretired · earliest 1998-06-08
AD
99-21-23
FR doc 99-26567 · 64 FR 55416
AD 99-21-23Published 1999-10-13Effective 1999-12-03
Requires restricting the entry speed for performing flick maneuvers to 97 knots.
Full official abstract
Airworthiness Directives; Avions Mudry et Cie Model CAP 10B Airplanes
This amendment adopts a new airworthiness directive (AD) that applies to all Avions Mudry et Cie (Avions Mudry) Model CAP 10B airplanes. This AD requires restricting the entry speed for performing flick maneuvers to 97 knots. Inserting a copy of this AD into the Limitations Section of the CAP 10B flight manual is also required, along with fabricating and installing a placard (in the cockpit of the airplane within the pilot's clear view) that indicates this limitation. 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 provide the flight information necessary to the pilot so that excessive speed is not used during aerobatic maneuvers, which could result in the wing separating from the airplane.
Source: Federal Register document 99-26567, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
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
Airworthiness Directives; Avions Mudry et Cie Model CAP 10B Airplanes
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.
Source: Federal Register document 98-15085, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
Airworthiness Directives; APEX Aircraft Model CAP 10B Airplanes
This amendment supersedes Airworthiness Directive (AD) 98-12- 10 and AD 99-21-23, which currently apply to APEX Aircraft (APEX) Model CAP 10B airplanes. AD 98-12-10 requires installing an inspection opening in the wing, repetitively inspecting the upper and lower wing spars for structural cracking, and, if any cracks are found, repairing the cracks in accordance with a repair method. AD 99-21-23 requires restricting the entry speed for performing flick maneuvers to 97 knots, inserting a copy of the AD into the Limitations Section of the CAP 10B flight manual, and fabricating and installing a placard (in the cockpit of the airplane within the pilot's clear view) that indicates this limitation. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. This AD retains the wing modification and repair requirements from AD 98-12-10. This AD also incorporates new repetitive inspection procedures, further reduces the flick maneuver speed specified in AD 99-21-23, and temporarily reduces the load factor limits prior to the initial inspection. The actions specified by this AD are intended to provide the flight information necessary to the pilot so that excessive speed is not used during aerobatic maneuvers and to detect and correct structural cracks in the wing spar, which could result in the wing separating from the airplane. Such failure could lead to loss of control of the airplane.
Source: Federal Register document 03-3450, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17