Aircraft model

Avions Pierre Robin

Avions Pierre Robin / Alpha Aviation

Airworthiness Directives
26
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-0226 of 26 re-checked, oldest 2026-09-30
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.

Also known as: Alpha Aviation R2160, R2160, R3000, Robin DR400

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What Airworthiness Directives apply to the Avions Pierre Robin

The FAA has published 26 Airworthiness Directives that name the Avions Pierre Robin (Avions Pierre Robin / Alpha Aviation), the earliest in 1997 and the newest on 2015-12-21.

Newest

  1. AD 2015-25-07 Airworthiness Directives; Alpha Aviation Concept Limited Airplanes 2015-12-21
  2. AD 2014-26-01 Airworthiness Directives; Alpha Aviation Concept Limited Airplanes 2014-12-24
  3. AD 2014-18-03 Airworthiness Directives; APEX Aircraft Airplanes 2014-09-12

See all 26 directives

The ones owners meet again

  1. AD 99-09-08 Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes 1999-04-26 Repetitive inspection or action
  2. AD 99-07-20 Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes 1999-04-06 Repetitive inspection or action
  3. AD 99-02-15 Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes 1999-03-19 Repetitive inspection or action
  4. AD 99-02-15 Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes 1999-01-26 Repetitive inspection or action
  5. AD 98-09-08 Airworthiness Directives; Avions Pierre Robin Model R3000/160 Airplanes. 1998-04-24 Repetitive inspection or action

We index directives by model, not by serial number or N-number; the record page and the official document say which serials apply.

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

Airworthiness Directives

26 records · 1 superseded record nested above
ADAD 2015-25-07Alpha Aviation Concept Limited Airplanes2016-01-25Active
AD

2015-25-07

FR doc 2015-31716 · 80 FR 79256

AD 2015-25-07Published 2015-12-21Effective 2016-01-25

Supersedes 2008-09-01

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.

Alpha Aviation Concept Limited Airplanes

Requires actions to address the unsafe condition on these products.

1 AD superseded by this one retired · earliest 2008-04-22
AD

2008-09-01

FR doc E8-8509 · 73 FR 21519

AD 2008-09-01Published 2008-04-22Effective 2008-05-27

Superseded by 2015-25-07 — see above

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.

Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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; Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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 E8-8509, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

Full official abstract

Airworthiness Directives; Alpha Aviation Concept Limited Airplanes

We are superseding Airworthiness Directive (AD) 2008-09-01 for certain Alpha Aviation Concept Limited Model R2160 airplanes. 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 a need to revise the maintenance program to include the revised airworthiness limitations for the internal wing structure and wing attachment inspections. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2015-31716, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2014-26-01Alpha Aviation Concept Limited Airplanes2015-01-28Active
AD

2014-26-01

FR doc 2014-29833 · 79 FR 77374

AD 2014-26-01Published 2014-12-24Effective 2015-01-28

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.

Alpha Aviation Concept Limited Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Alpha Aviation Concept Limited Airplanes

We are adopting a new airworthiness directive (AD) for Alpha Aviation Concept Limited Model R2160 airplanes. 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 paint adherence defects inside the engine air intake box and cohesion defects inside the laminated ducting from the filter to the air intake box. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2014-29833, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2014-18-03APEX Aircraft Airplanes2014-10-17Active
AD

2014-18-03

FR doc 2014-21270 · 79 FR 54577

AD 2014-18-03Published 2014-09-12Effective 2014-10-17

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.

APEX Aircraft Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; APEX Aircraft Airplanes

We are adopting a new airworthiness directive (AD) for APEX Aircraft Model R 3000/160 airplanes. 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 small pieces of paint from the engine air intake box blocking the engine carburetor. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2014-21270, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2014-09-12Alpha Aviation Concept Limited Airplanes2014-06-13Active
AD

2014-09-12

FR doc 2014-10058 · 79 FR 26608

AD 2014-09-12Published 2014-05-09Effective 2014-06-13

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.

Alpha Aviation Concept Limited Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Alpha Aviation Concept Limited Airplanes

We are adopting a new airworthiness directive (AD) for certain Alpha Aviation Concept Limited Model R2160 airplanes. 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 the metal screen shield over the ignition switch may ground out the ignition terminals. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2014-10058, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2012-20-02Alpha Aviation Concept Limited Airplanes2012-11-09Active
AD

2012-20-02

FR doc 2012-24278 · 77 FR 60887

AD 2012-20-02Published 2012-10-05Effective 2012-11-09

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.

Alpha Aviation Concept Limited Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Alpha Aviation Concept Limited Airplanes

We are adopting a new airworthiness directive (AD) for Alpha Aviation Concept Limited Model R2160 Airplanes. 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 possible installation of non-conforming air filter elements that are not fitted with metallic mesh and could internally collapse resulting in disruption of the powerplant operation. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2012-24278, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2012-11-10Alpha Aviation Concept Limited (Type Certificate Previously Held by Alpha Aviation Design Limited) Airplanes2012-07-12Active
AD

2012-11-10

FR doc 2012-13558 · 77 FR 33622

AD 2012-11-10Published 2012-06-07Effective 2012-07-12

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.

Alpha Aviation Concept Limited (Type Certificate Previously Held by Alpha Aviation Design Limited) Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Alpha Aviation Concept Limited (Type Certificate Previously Held by Alpha Aviation Design Limited) Airplanes

We are adopting a new airworthiness directive (AD) for Alpha Aviation Concept Limited Model R2160 Airplanes. 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 oil lines fitted to affected aircraft are not fire resistant. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2012-13558, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2008-03-11Alpha Aviation Design Limited Model R2160 Airplanes2008-03-11Active
AD

2008-03-11

FR doc E8-1829 · 73 FR 6592

AD 2008-03-11Published 2008-02-05Effective 2008-03-11

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.

Alpha Aviation Design Limited Model R2160 Airplanes

Requires actions that are intended to address the unsafe condition described in the MCAI.

Full official abstract

Airworthiness Directives; Alpha Aviation Design Limited Model R2160 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 distortion of the rudder bars due to rudder control forces during aerobatic operation and nose wheel steering reaction forces. Rudder bar distortion could result in reduced control or loss of control. This AD requires actions that are intended to address the unsafe condition described in the MCAI.

Source: Federal Register document E8-1829, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2007-20-08Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by Apex Aircraft and Avions Pierre Robin) Model R2160 Airplanes2007-11-09Active
AD

2007-20-08

FR doc E7-19501 · 72 FR 56890

AD 2007-20-08Published 2007-10-05Effective 2007-11-09

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.

Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by Apex Aircraft and Avions Pierre Robin) Model R2160 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; Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by Apex Aircraft and Avions Pierre Robin) Model R2160 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 E7-19501, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2007-13-15Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 Airplanes2007-08-10Active
AD

2007-13-15

FR doc E7-12506 · 72 FR 36860

AD 2007-13-15Published 2007-07-06Effective 2007-08-10

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.

Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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; Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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 E7-12506, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2007-06-16Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 Airplanes2007-04-24Active
AD

2007-06-16

FR doc E7-4861 · 72 FR 12966

AD 2007-06-16Published 2007-03-20Effective 2007-04-24

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.

Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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; Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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 references Alpha Aviation Service Bulletin AA-SB-28-002, dated June 28, 2006, which describes the unsafe condition as:

Source: Federal Register document E7-4861, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2007-05-03Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 Airplanes2007-04-09Active
AD

2007-05-03

FR doc E7-3475 · 72 FR 9657

AD 2007-05-03Published 2007-03-05Effective 2007-04-09

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.

Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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; Alpha Aviation Design Limited (Type Certificate No. A48EU Previously Held by APEX Aircraft and AVIONS PIERRE ROBIN) Model R2160 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 E7-3475, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2007-04-25Alpha Aviation Design Limited R2160 Airplanes2007-04-03Active
AD

2007-04-25

FR doc E7-3163 · 72 FR 8613

AD 2007-04-25Published 2007-02-27Effective 2007-04-03

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.

Alpha Aviation Design Limited R2160 Airplanes

Requires actions to correct the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Alpha Aviation Design Limited R2160 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 a deficiency in compliance with 14 CFR 23.967(d). There have been instances indicating that production aircraft may not have a metal barrier between the cabin and the fuel tank bay. Lack of a barrier could allow flammable fuel vapors to enter the cabin. We are issuing this AD to require actions to correct the unsafe condition on these products.

Source: Federal Register document E7-3163, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 2006-26-03Alpha Aviation Design Limited (Type Certificate No. A48EU formerly held by APEX Aircraft and AVIONS PIERRE ROBIN), Model R2160 Airplanes2007-01-30Active
AD

2006-26-03

FR doc E6-21923 · 71 FR 77262

AD 2006-26-03Published 2006-12-26Effective 2007-01-30

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.

Alpha Aviation Design Limited (Type Certificate No. A48EU formerly held by APEX Aircraft and AVIONS PIERRE ROBIN), Model R2160 Airplanes

Requires you to inspect the fuel pressure indication system for leakage at the end of the adapter in the fuel pressure indication system.

Full official abstract

Airworthiness Directives; Alpha Aviation Design Limited (Type Certificate No. A48EU formerly held by APEX Aircraft and AVIONS PIERRE ROBIN), Model R2160 Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Alpha Aviation Model R2160 airplanes. This AD requires you to inspect the fuel pressure indication system for leakage at the end of the adapter in the fuel pressure indication system. This AD results from the possibility of fuel leakage at the end of the adapter in the fuel pressure indication system. We are issuing this AD to detect, correct, and prevent fuel leaks in the fuel pressure indicating system. This failure could allow fuel to leak near the exhaust manifold and lead to a fire.

Source: Federal Register document E6-21923, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 99-10-01Avions Pierre Robin Model R2160 Airplanes1999-06-18Active
AD

99-10-01

FR doc 99-10968 · 64 FR 24029

AD 99-10-01Published 1999-05-05Effective 1999-06-18

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.

Avions Pierre Robin Model R2160 Airplanes

Requires replacing the wing attachment bolts and associated hardware.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Avions Pierre Robin Model R2160 airplanes. This AD requires replacing the wing attachment bolts and associated hardware. 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 a wing from separating from the airplane caused by damaged wing attachment bolts, which could result in loss of control of the airplane.

Source: Federal Register document 99-10968, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 99-10-02Avions Pierre Robin Model R2160 Airplanes1999-06-18Active
AD

99-10-02

FR doc 99-10969 · 64 FR 24028

AD 99-10-02Published 1999-05-05Effective 1999-06-18

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.

Avions Pierre Robin Model R2160 Airplanes

Requires inspecting to assure that the fuel filler cap has a 2.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Avions Pierre Robin Model R2160 airplanes. This AD requires inspecting to assure that the fuel filler cap has a 2.5 millimeter (mm) diameter hole drilled through it or that a vinyl piping is connected to the filler neck inside the cabin. If neither of these items exists, this AD requires replacing the fuel filler cap with a fuel filler cap that has a 2.5 mm diameter hole drilled through it. 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 detect and correct the installation of improperly designed fuel venting system parts, which could result in an inadequate fuel supply to the engine with loss of engine power.

Source: Federal Register document 99-10969, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 99-09-08Avions Pierre Robin Model R2160 Airplanes1999-06-07Active
AD

99-09-08

FR doc 99-10173 · 64 FR 20148

AD 99-09-08Published 1999-04-26Effective 1999-06-07

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.

Avions Pierre Robin Model R2160 Airplanes

Requires repetitively inspecting the aileron/flap common support bracket for cracks, loose rivets, or separation of the bracket from the skin, and reinforcing the bracket either immediately or at a certain time period depending…

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin Model R2160 airplanes. This AD requires repetitively inspecting the aileron/flap common support bracket for cracks, loose rivets, or separation of the bracket from the skin, and reinforcing the bracket either immediately or at a certain time period depending on whether discrepancies are found during the inspections. Reinforcing the aileron/flap common support bracket terminates the repetitive inspection requirement. 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 detect defects in the aileron/flap common support bracket (cracks, loose rivets, or separation of the bracket from the skin), which could result in reduced or loss of control of the airplane.

Source: Federal Register document 99-10173, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 99-07-20Avions Pierre Robin Model R2160 Airplanes1999-05-17Active
AD

99-07-20

FR doc 99-8092 · 64 FR 16624

AD 99-07-20Published 1999-04-06Effective 1999-05-17

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.

Avions Pierre Robin Model R2160 Airplanes

Requires repetitively inspecting the vertical stabilizer spar in the area of the lower fitting of the rudder for cracks, loose rivets, or spar web distortion; and modifying the vertical stabilizer spar either immediately or at a…

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin Model R2160 airplanes. This AD requires repetitively inspecting the vertical stabilizer spar in the area of the lower fitting of the rudder for cracks, loose rivets, or spar web distortion; and modifying the vertical stabilizer spar either immediately or at a certain time period depending on whether discrepancies are found during the inspections. 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 detect defects (cracks, loose rivets, or spar web distortion) in the vertical stabilizer spar, which could result in structural failure of the vertical stabilizer with possible reduced or loss of control of the airplane.

Source: Federal Register document 99-8092, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 99-02-15Avions Pierre Robin Model R2160 Airplanes1999-03-29Active
AD

99-02-15

FR doc 99-6713 · 64 FR 13504

AD 99-02-15Published 1999-03-19Effective 1999-03-29

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.

Avions Pierre Robin Model R2160 Airplanes

Requires repetitively inspecting the engine bearer for cracks, and replacing the engine bearer with a reinforced part either immediately or at a certain time period depending on whether cracks are found during the inspections.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This action confirms the effective date of Airworthiness Directive (AD) 99-02-15, which applies to certain Avions Pierre Robin Model R2160 airplanes. AD 99-02-15 requires repetitively inspecting the engine bearer for cracks, and replacing the engine bearer with a reinforced part either immediately or at a certain time period depending on whether cracks are found during the inspections. Replacing the engine bearer with a reinforced part terminates the repetitive inspection requirement. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to detect and correct cracks in the engine bearer, which could result in the engine separating from the airplane.

Source: Federal Register document 99-6713, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 99-02-15Avions Pierre Robin Model R2160 Airplanes1999-03-29Active
AD

99-02-15

FR doc 99-1237 · 64 FR 3817

AD 99-02-15Published 1999-01-26Effective 1999-03-29

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.

Avions Pierre Robin Model R2160 Airplanes

Requires repetitively inspecting the engine bearer for cracks, and replacing the engine bearer with a reinforced part either immediately or at a certain time period depending on whether cracks are found during the inspections.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Avions Pierre Robin Model R2160 airplanes. This AD requires repetitively inspecting the engine bearer for cracks, and replacing the engine bearer with a reinforced part either immediately or at a certain time period depending on whether cracks are found during the inspections. Replacing the engine bearer with a reinforced part terminates the repetitive inspection requirement. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to detect and correct cracks in the engine bearer, which could result in the engine separating from the airplane.

Source: Federal Register document 99-1237, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 99-01-04Avions Pierre Robin Model R2160 Airplanes1999-03-12Active
AD

99-01-04

FR doc 98-34383 · 63 FR 72137

AD 99-01-04Published 1998-12-31Effective 1999-03-12

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.

Avions Pierre Robin Model R2160 Airplanes

Requires replacing the left and right rudder bars with improved design rudder bars.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Avions Pierre Robin Model R2160 airplanes. This AD requires replacing the left and right rudder bars with improved design rudder bars. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to prevent distortion of the original design rudder bars during operation, which could result in reduced or loss of control of the airplane.

Source: Federal Register document 98-34383, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 98-09-08Avions Pierre Robin Model R3000/160 Airplanes.1998-05-22Active
AD

98-09-08

FR doc 98-10595 · 63 FR 20306

AD 98-09-08Published 1998-04-24Effective 1998-05-22

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.

Avions Pierre Robin Model R3000/160 Airplanes.

Requires repetitively inspecting the flap control shaft and the welds of the flap levers for cracks; replacing the cracked part, if cracks are found; and adjusting the flap travel, if no cracks are found.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R3000/160 Airplanes.

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin (Avions) Model R3000/160 airplanes. This action requires repetitively inspecting the flap control shaft and the welds of the flap levers for cracks; replacing the cracked part, if cracks are found; and adjusting the flap travel, if no cracks are found. Reports of cracked flap control shafts found during routine maintenance prompted this action. The actions specified by this AD are intended to prevent cracks on the flap control shaft and around the welds of the flap levers, which, if not detected and corrected, could result in loss of airplane control during flight.

Source: Federal Register document 98-10595, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 98-08-28Avions Pierre Robin Model R3000/160 Airplanes1998-05-15Active
AD

98-08-28

FR doc 98-10177 · 63 FR 19388

AD 98-08-28Published 1998-04-20Effective 1998-05-15

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.

Avions Pierre Robin Model R3000/160 Airplanes

Requires replacing the top bolts in the front wheel fork assembly and the top bolts attaching the front landing gear to the engine mount.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R3000/160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin (Avions) Model R3000/160 airplanes. This action requires replacing the top bolts in the front wheel fork assembly and the top bolts attaching the front landing gear to the engine mount. 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 collapse of the nose landing gear, which could result in loss of control of the airplane during taxi and landing operations.

Source: Federal Register document 98-10177, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 97-23-08Avions Pierre Robin Model R3000 Airplanes1997-12-05Active
AD

97-23-08

FR doc 97-29535 · 62 FR 60772

AD 97-23-08Published 1997-11-13Effective 1997-12-05

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.

Avions Pierre Robin Model R3000 Airplanes

Requires inspecting the bridle cable ends for correct installation in the grooved screw, inspecting for correct cable winding on the capstan and correct cable tension, and correcting any discrepancies found.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R3000 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin Model R3000 airplanes that are equipped with yaw damper Modification No. 013. This AD requires inspecting the bridle cable ends for correct installation in the grooved screw, inspecting for correct cable winding on the capstan and correct cable tension, and correcting any discrepancies found. This AD also requires installing lockwire to the tension adjustment screw. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to prevent the rudder control from becoming jammed because of the yaw damper control cables slipping out of the groove on the tension adjustment screw, which could result in a reduction in the directional controllability of the airplane.

Source: Federal Register document 97-29535, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 97-23-05Avions Pierre Robin Model R3000 Airplanes1997-12-01Active
AD

97-23-05

FR doc 97-29232 · 62 FR 60161

AD 97-23-05Published 1997-11-07Effective 1997-12-01

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.

Avions Pierre Robin Model R3000 Airplanes

Requires replacing the attachment bolt between the pitch control cables and control column lever with a bolt of improved design.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R3000 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Avions Pierre Robin Model R3000 airplanes. This AD requires replacing the attachment bolt between the pitch control cables and control column lever with a bolt of improved design. This AD is the result of mandatory continued airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to prevent the pitch control cables on the control column from becoming jammed due to failure of the attachment bolt, which could result in a reduction in the directional controllability of the airplane.

Source: Federal Register document 97-29232, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

ADAD 97-06-05Avions Pierre Robin Model R2160 Airplanes1997-05-16Active
AD

97-06-05

FR doc 97-6256 · 62 FR 11763

AD 97-06-05Published 1997-03-13Effective 1997-05-16

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.

Avions Pierre Robin Model R2160 Airplanes

Requires repetitively inspecting the weld area between the strut and the lower plate of the nose landing gear leg for cracks, and replacing the strut when cracks are found.

Full official abstract

Airworthiness Directives; Avions Pierre Robin Model R2160 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to Avions Pierre Robin Model R2160 airplanes. This action requires repetitively inspecting the weld area between the strut and the lower plate of the nose landing gear leg for cracks, and replacing the strut when cracks are found. The AD is the result of several reports of cracks in the weld securing the nose wheel steering bottom bracket to the nose landing gear leg on the affected airplanes. The actions specified by this AD are intended to prevent nose landing gear failure caused by cracks in the weld area between the strut and the lower plate of the nose landing gear leg, which could result in loss of control of the airplane during landing operations.

Source: Federal Register document 97-6256, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-09-30

Service Bulletins

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