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
26 records · 1 superseded record nested above
AD
2015-25-07
FR doc 2015-31716 · 80 FR 79256
AD 2015-25-07Published 2015-12-21Effective 2016-01-25
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 · re-verified against the live Federal Register API 2026-08-17
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 · re-verified against the live Federal Register API 2026-08-17
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 · re-verified against the live Federal Register API 2026-08-17
AD 2014-18-03Published 2014-09-12Effective 2014-10-17
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 · re-verified against the live Federal Register API 2026-08-17
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 · re-verified against the live Federal Register API 2026-08-17
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 · re-verified against the live Federal Register API 2026-08-17
AD 2012-11-10Published 2012-06-07Effective 2012-07-12
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 · re-verified against the live Federal Register API 2026-08-17
AD 2008-03-11Published 2008-02-05Effective 2008-03-11
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 · re-verified against the live Federal Register API 2026-08-17
AD 2007-20-08Published 2007-10-05Effective 2007-11-09
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 · re-verified against the live Federal Register API 2026-08-17
AD 2007-13-15Published 2007-07-06Effective 2007-08-10
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 · re-verified against the live Federal Register API 2026-08-17
AD 2007-06-16Published 2007-03-20Effective 2007-04-24
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 · re-verified against the live Federal Register API 2026-08-17
AD 2007-05-03Published 2007-03-05Effective 2007-04-09
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 · re-verified against the live Federal Register API 2026-08-17
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 · re-verified against the live Federal Register API 2026-08-17
AD 2006-26-03Published 2006-12-26Effective 2007-01-30
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-10-01Published 1999-05-05Effective 1999-06-18
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-10-02Published 1999-05-05Effective 1999-06-18
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-09-08Published 1999-04-26Effective 1999-06-07
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-07-20Published 1999-04-06Effective 1999-05-17
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-02-15Published 1999-03-19Effective 1999-03-29
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-02-15Published 1999-01-26Effective 1999-03-29
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 · re-verified against the live Federal Register API 2026-08-17
AD 99-01-04Published 1998-12-31Effective 1999-03-12
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 · re-verified against the live Federal Register API 2026-08-17
AD 98-09-08Published 1998-04-24Effective 1998-05-22
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 · re-verified against the live Federal Register API 2026-08-17
AD 98-08-28Published 1998-04-20Effective 1998-05-15
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 · re-verified against the live Federal Register API 2026-08-17
AD 97-23-08Published 1997-11-13Effective 1997-12-05
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 · re-verified against the live Federal Register API 2026-08-17
AD 97-23-05Published 1997-11-07Effective 1997-12-01
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 · re-verified against the live Federal Register API 2026-08-17
AD 97-06-05Published 1997-03-13Effective 1997-05-16
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 · re-verified against the live Federal Register API 2026-08-17