Aircraft model

Mudry / APEX CAP 10

APEX Aircraft (formerly Avions Mudry)

Airworthiness Directives
13
Service Bulletins
0
Last live check
2026-08-1713 of 13 re-verified
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.

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13 records · 2 superseded records nested above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

2008-17-07

FR doc E8-18807 · 73 FR 48297

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

2008-13-32

FR doc E8-14484 · 73 FR 38889

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

2008-09-02

FR doc E8-8360 · 73 FR 21244

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

2008-07-05

FR doc E8-5955 · 73 FR 15868

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

2008-07-04

FR doc E8-5961 · 73 FR 15872

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

2007-13-14

FR doc E7-12319 · 72 FR 35639

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

2007-10-13

FR doc E7-9393 · 72 FR 27721

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

2007-09-06

FR doc E7-7980 · 72 FR 21077

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

2007-09-05

FR doc E7-7994 · 72 FR 21086

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

AD

2003-04-02

FR doc 03-3450 · 68 FR 7904

AD 2003-04-02Published 2003-02-19Effective 2003-04-04

APEX Aircraft Model CAP 10B Airplanes

Supersedes 99-21-23, 98-12-10 — see below

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 one retired · 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

Avions Mudry et Cie Model CAP 10B Airplanes

Superseded by 2003-04-02 — see above

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

AD

98-12-10

FR doc 98-15085 · 63 FR 31104

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

Avions Mudry et Cie Model CAP 10B Airplanes

Superseded by 2003-04-02 — see above

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

Full official abstract

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

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 13 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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