Aircraft model

Piaggio P.180 Avanti

Piaggio Aero Industries S.p.A.

Airworthiness Directives
59
Service Bulletins
0
Last live check
2026-08-1859 of 59 re-verified, oldest 2026-08-17
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

59 records · 1 correction attached · 3 superseded records nested above
AD

2026-06-05

FR doc 2026-06599 · 91 FR 17132

AD 2026-06-05Published 2026-04-06Effective 2026-05-11

Baykar Piaggio Aerospace S.p.A. (Type Certificate Previously Held by Piaggio Aviation S.p.A.) Airplanes

Requires repetitive visual and non- destructive testing (NDT) inspections, a one-time NDT inspection of the vertical stabilizer assembly, and, depending on findings, accomplishment of corrective actions.

Full official abstract

Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certificate Previously Held by Piaggio Aviation S.p.A.) Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Baykar Piaggio Aerospace S.p.A. (type certificate previously held by Piaggio Aviation S.p.A.) (Piaggio) Model P-180 airplanes. This AD was prompted by reports of corrosion and cracks affecting the vertical stabilizer. This AD requires repetitive visual and non- destructive testing (NDT) inspections, a one-time NDT inspection of the vertical stabilizer assembly, and, depending on findings, accomplishment of corrective actions. In addition, this AD provides a terminating action for the repetitive inspections if certain actions of the service material are accomplished. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2026-06599, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2026-05-10

FR doc 2026-05576 · 91 FR 13706

AD 2026-05-10Published 2026-03-23Effective 2026-04-27

Baykar Piaggio Aerospace S.p.A. (Type Certificate Previously Held by Piaggio Aviation S.p.A.) Airplanes

Requires inspecting the flap transmission shaft for chafing or any damage (surface abrasions, grooves or rubbing tracks, and metallic smears or transfers), measuring specific gaps, and, depending on findings, accomplishing…

Full official abstract

Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certificate Previously Held by Piaggio Aviation S.p.A.) Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Baykar Piaggio Aerospace S.p.A. (type certificate previously held by Piaggio Aviation S.p.A.) (Piaggio) Model P-180 airplanes. This AD was prompted by a report of chafing in the flap transmission shafts. This AD requires inspecting the flap transmission shaft for chafing or any damage (surface abrasions, grooves or rubbing tracks, and metallic smears or transfers), measuring specific gaps, and, depending on findings, accomplishing applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2026-05576, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2025-26-05

FR doc 2026-00357 · 91 FR 1076

AD 2025-26-05Published 2026-01-12Effective 2026-02-17

Baykar Piaggio Aerospace S.p.A. (Type Certificate Previously Held by Piaggio Aviation S.p.A.) Airplanes

Requires replacing the affected flexible hydraulic hoses.

Full official abstract

Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certificate Previously Held by Piaggio Aviation S.p.A.) Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Baykar Piaggio Aerospace S.p.A. (type certificate previously held by Piaggio Aviation S.p.A.) (Piaggio) Model P-180 airplanes. This AD was prompted by a report of leakage from the flexible hydraulic hoses connected to the hydraulic pump package (HPP). This AD requires replacing the affected flexible hydraulic hoses. This AD also prohibits installing the affected flexible hydraulic hoses on any airplane. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2026-00357, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2025-15-10

FR doc 2025-14390 · 90 FR 35831

AD 2025-15-10Published 2025-07-30Effective 2025-09-03

Piaggio Aviation S.p.A. Airplanes

Supersedes 2023-25-03 — see below

The FAA is superseding Airworthiness Directive (AD) 2023-25- 03, which applied to certain Piaggio Aviation S.p.A.

1 AD superseded by this one retired · earliest 2023-12-29
AD

2023-25-03

FR doc 2023-28769 · 88 FR 90085

AD 2023-25-03Published 2023-12-29Effective 2024-02-02

Piaggio Aviation S.p.A. Airplanes

Superseded by 2025-15-10 — see above

Requires a one-time detailed inspection of the HS central box for corrosion; an assessment of the corrosion level; and depending on the determination, repetitive detailed inspections of the HS central box for corrosion and the…

Full official abstract

Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Piaggio Aviation S.p.A. (Piaggio) Model P-180 airplanes. This AD is prompted by a report of corrosion on the various aluminum alloy reinforcements in the horizontal stabilizer (HS) central box caused by a humid environment inside the box from water ingress and/or condensation. This AD requires a one-time detailed inspection of the HS central box for corrosion; an assessment of the corrosion level; and depending on the determination, repetitive detailed inspections of the HS central box for corrosion and the internal composite structure for surface cracks, distortion, and damage; and repair or replacement of the HS assembly. Repair or replacement of the HS assembly is terminating action for the repetitive inspections. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2023-28769, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes

The FAA is superseding Airworthiness Directive (AD) 2023-25- 03, which applied to certain Piaggio Aviation S.p.A. (Piaggio) Model P- 180 airplanes. AD 2023-25-03 required a one-time detailed inspection of the horizontal stabilizer (HS) central box for corrosion; an assessment of the corrosion level; and depending on the determination, repetitive detailed inspections of the HS central box for corrosion and the internal composite structure for surface cracks, distortion, and damage; and repair or replacement of the HS assembly. Repair or replacement of the HS assembly was terminating action for the repetitive inspections. Since the FAA issued AD 2023-25-03, it was determined that AD 2023-25-03 imposed an unintended restriction that is not in the mandatory continuing airworthiness information (MCAI). This AD retains certain actions of AD-2023-25-03 and removes the unintended restriction. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2025-14390, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2023-16-04

FR doc 2023-17575 · 88 FR 55362

AD 2023-16-04Published 2023-08-15Effective 2023-08-30

Piaggio Aviation S.p.A. Airplanes

Requires repetitively inspecting the HTTA fitting assembly for corrosion and cracking until the HTTA fitting assembly is replaced with a new part.

Full official abstract

Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Piaggio Aviation S.p.A. (Piaggio) Model P-180 airplanes. This AD was prompted by a report of corrosion-induced cracking on the horizontal tail trim actuator (HTTA) fitting assembly. This AD requires repetitively inspecting the HTTA fitting assembly for corrosion and cracking until the HTTA fitting assembly is replaced with a new part. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2023-17575, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2022-22-07

FR doc 2022-25029 · 87 FR 69158

AD 2022-22-07Published 2022-11-18Effective 2022-12-23

Piaggio Aviation S.p.A. (Type Certificate Previously Held by Piaggio Aero Industries S.p.A.) Airplanes

Requires repetitively inspecting the fuselage skin panels, visually inspecting the entire fuselage inner side skin if necessary, and taking any necessary corrective actions.

Full official abstract

Airworthiness Directives; Piaggio Aviation S.p.A. (Type Certificate Previously Held by Piaggio Aero Industries S.p.A.) Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Piaggio Aviation S.p.A. (type certificate previously held by Piaggio Aero Industries S.p.A.) (Piaggio) Model P-180 airplanes. This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as corrosion in the bottom fuselage area of the cabin compartment due to inner and outer sides of fuselage skin panels of certain airplanes treated with the less effective primer. This AD requires repetitively inspecting the fuselage skin panels, visually inspecting the entire fuselage inner side skin if necessary, and taking any necessary corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2022-25029, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2022-19-07

FR doc 2022-20957 · 87 FR 58947

AD 2022-19-07Published 2022-09-29Effective 2022-11-03

Piaggio Aviation S.p.A. Airplanes

Requires modifying the total air temperature (TAT) probe heater electrical circuit and revising your existing airplane flight manual (AFM).

Full official abstract

Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes

The FAA is adopting a new airworthiness directive (AD) for all Piaggio Aviation S.p.A. (Piaggio) Model P-180 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as accumulation of water and subsequent freezing in the pitot-tube, which results in pitot-tube blockage. This AD requires modifying the total air temperature (TAT) probe heater electrical circuit and revising your existing airplane flight manual (AFM). The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2022-20957, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-18

AD

2022-17-13

FR doc 2022-19055 · 87 FR 54358

AD 2022-17-13Published 2022-09-06Effective 2022-10-11

Piaggio Aero Industries S.p.A Airplanes

Requires amending the existing airplane flight manual (AFM), installing improved ADCs and a detachable configuration module (DCM), and revising the existing instructions for continued airworthiness.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A Airplanes

The FAA is adopting a new airworthiness directive (AD) for certain Piaggio Aero Industries S.p.A. (Piaggio) Model P-180 airplanes. This AD is prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as altimetry system errors in the air data computers (ADCs) and stand-by instrument systems. This AD requires amending the existing airplane flight manual (AFM), installing improved ADCs and a detachable configuration module (DCM), and revising the existing instructions for continued airworthiness. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2022-19055, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2020-19-10

FR doc 2020-21392 · 85 FR 60896

AD 2020-19-10Published 2020-09-29Effective 2020-11-03

Piaggio Aero Industries S.p.A.

Unsafe condition: insufficient sealing of a steering select/bypass valve installed in the nose landing gear (NLG) manifold.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A.

The FAA is adopting a new airworthiness directive (AD) for Piaggio Aero Industries S.p.A. Model P-180 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 insufficient sealing of a steering select/bypass valve installed in the nose landing gear (NLG) manifold. The FAA is issuing this AD to address the unsafe condition on these products.

Source: Federal Register document 2020-21392, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2017-20-13

FR doc 2017-21443 · 82 FR 47371

AD 2017-20-13Published 2017-10-12Effective 2017-11-16

PIAGGIO AERO INDUSTRIES S.p.A. Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A. Airplanes

We are adopting a new airworthiness directive (AD) for PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) originated 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 disbonding of the upper and lower metal skin from the honeycomb core on the elevator assembly and other flight control surfaces. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2017-21443, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2015-19-11

FR doc 2015-24257 · 80 FR 58349

AD 2015-19-11Published 2015-09-29Effective 2015-11-03

Piaggio Aero Industries S.p.A. Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A. Airplanes

We are adopting a new airworthiness directive (AD) for Piaggio Aero Industries S.p.A. Model P-180 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 need to restore the safe fatigue life of the bulkhead structure. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2015-24257, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2014-09-04

FR doc 2014-09431 · 79 FR 26603

AD 2014-09-04Published 2014-05-09Effective 2014-06-13

Piaggio Aero Industries S.p.A Airplanes

Supersedes 2009-21-08 R1 — see below

Requires actions to address the unsafe condition on these products.

1 AD superseded by this one retired · earliest 2010-01-07
AD

2009-21-08 R1

FR doc E9-31364 · 75 FR 904

AD 2009-21-08 R1Published 2010-01-07Effective 2009-12-14

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

Superseded by 2014-09-04 — see above

Requires repetitive functional tests of the manifold system and replacement of any system that does not pass the functional tests (i.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

We are clarifying information contained in Airworthiness Directive (AD) 2009-21-08, which applies to PIAGGIO AERO INDUSTRIES S.p.A. (Piaggio) Model PIAGGIO P-180 airplanes. AD 2009-21-08 currently requires repetitive functional tests of the manifold system and replacement of any system that does not pass the functional tests (i.e., movement of the steering system). The language in AD 2009-21-08 incorrectly references not passing the functional tests as "movement of the manifold," and it should read "movement of the steering system" as specified in the service bulletin. The notice of proposed rulemaking (NPRM) referenced it as specified in the service bulletin. This document incorporates the intent of the action as already proposed in the NPRM. We are issuing this AD to prevent a potentially dangerous veer along the runway. The steering system must be in the `off' position during landing and takeoff (in this case when airspeed is higher than 60 knots) according to the aircraft flight manual limitations.

Source: Federal Register document E9-31364, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A Airplanes

We are superseding Airworthiness Directive (AD) 2009-21-08 R1 for Piaggio Aero Industries S.p.A Model P-180 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 cases of un-commanded operation of switched off nose-wheel steering system caused by internal leakage of a steering select/bypass valve. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2014-09431, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2014-03-20

FR doc 2014-03243 · 79 FR 10346

AD 2014-03-20Published 2014-02-25Effective 2014-04-01

Piaggio Aero Industries S.P.A Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.P.A Airplanes

We are adopting a new airworthiness directive (AD) for certain Piaggio Aero Industries S.P.A Model P-180 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 insufficient clearance between one of the horizontal stabilizer end ribs and the corresponding elevator horn. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2014-03243, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2013-18-04

FR doc 2013-22203 · 78 FR 56589

AD 2013-18-04Published 2013-09-13Effective 2013-10-18

PIAGGIO AERO INDUSTRIES S.p.A Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Airplanes

We are adopting a new airworthiness directive (AD) for all PIAGGIO AERO INDUSTRIES S.p.A Model P-180 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 cracks at the joint between the hinge pin sub-assembly and the lock pin of the main landing gear lever hinge fitting. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2013-22203, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

99-07-10 R1

FR doc 2013-19816 · 78 FR 49662

AD 99-07-10 R1Published 2013-08-15Effective 2013-09-19

PIAGGIO AERO INDUSTRIES S.p.A Airplanes

Unsafe condition: partial detachment of the inner protective film of the composite nacelles.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Airplanes

We are rescinding an airworthiness directive (AD) for PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 airplanes. The rescinded AD resulted from mandatory continuing airworthiness information (MCAI) originated 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 partial detachment of the inner protective film of the composite nacelles. Since issuance of the rescinded AD, we have determined that the unsafe condition does not exist or is not likely to develop on affected type design airplanes.

Source: Federal Register document 2013-19816, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2003-17-03 R1

FR doc 2012-27051 · 77 FR 67764

AD 2003-17-03 R1Published 2012-11-14Effective 2012-11-14

PIAGGIO AERO INDUSTRIES S.p.A Airplanes

Requires replacement of any firewall shutoff or crossfeed valve with a serial number in a certain range even if it has been previously modified.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Airplanes

We are revising an existing airworthiness directive (AD) for certain Piaggio Aero Industries S.p.A. Model P-180 airplanes. That AD currently requires replacement of any firewall shutoff or crossfeed valve with a serial number in a certain range even if it has been previously modified. The way the applicability was written includes valves that should not be affected and are not included in the referenced service information. This AD requires the same actions as the current AD, but only affects those firewall shutoff valves referenced in the referenced service information. We are issuing this AD to clarify the affected parts required to correct the unsafe condition on these products.

Source: Federal Register document 2012-27051, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2000-07-11 R1

FR doc 2012-25254 · 77 FR 63712

AD 2000-07-11 R1Published 2012-10-17Effective 2012-11-21

Piaggio Aero Industries S.p.A.

Prompted by mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A.

We are rescinding an airworthiness directive (AD) for all Piaggio Aero Industries S.p.A Model P-180 airplanes. That AD was prompted by mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. We issued that AD to prevent the brake hydraulic fluid from leaking because of the brake assembly rods contacting the brake valve tubing, which could result in the inability to adequately stop the airplane during ground operations. Since we issued that AD, we have determined this is no longer an unsafe condition and that regularly scheduled annual inspections address this subject.

Source: Federal Register document 2012-25254, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2012-18-06

FR doc 2012-22542 · 77 FR 56987

AD 2012-18-06Published 2012-09-17Effective 2012-10-22

PIAGGIO AERO INDUSTRIES S.p.A Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Airplanes

We are adopting a new airworthiness directive (AD) for Piaggio Aero Industries S.p.A. Model P-180 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 jamming of the external bearing of the screwjack drive gear, which resulted in failure of the main wing outboard flap external actuator. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2012-22542, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2011-26-01

FR doc 2011-31623 · 76 FR 77369

AD 2011-26-01Published 2011-12-13Effective 2012-01-17

Piaggio Aero Industries S.p.A. Airplanes

Requires actions to address the unsafe condition on these products.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A. Airplanes

We are adopting a new airworthiness directive (AD) for Piaggio Aero Industries S.p.A. Model P-180 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 baggage door lockpins not engaging properly and the baggage door open light illuminating when the baggage door is not open, which could lead to the pilot disregarding a valid warning. We are issuing this AD to require actions to address the unsafe condition on these products.

Source: Federal Register document 2011-31623, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2011-24-01

FR doc 2011-29554 · 76 FR 71246

AD 2011-24-01Published 2011-11-17Effective 2011-12-22

Piaggio Aero Industries S.p.A. 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; Piaggio Aero Industries S.p.A. Airplanes

We are adopting a new airworthiness directive (AD) for Piaggio Aero Industries S.p.A. Model P-180 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:

Source: Federal Register document 2011-29554, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2011-10-16

FR doc 2011-11330 · 76 FR 27872

AD 2011-10-16Published 2011-05-13Effective 2011-05-31

PIAGGIO AERO INDUSTRIES S.p.A Model P-180 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; PIAGGIO AERO INDUSTRIES S.p.A Model P-180 Airplanes

We are adopting a new airworthiness directive (AD) for the products listed above that will supersede an existing AD. This emergency AD was sent previously to all known U.S. owners and operators of PIAGGIO AERO INDUSTRIES S.p.A (Piaggio) Model PIAGGIO P-180 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:

Source: Federal Register document 2011-11330, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2011-05-01

FR doc 2011-3923 · 76 FR 10224

AD 2011-05-01Published 2011-02-24Effective 2011-03-31

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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 2011-3923, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2011-01-53

FR doc 2011-1136 · 76 FR 4056

AD 2011-01-53Published 2011-01-24Effective 2011-01-24

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

Requires an immediate functional test of the fuselage drain holes, and requires sending a report of the results to the FAA.

1 correction to this AD FAA · 2011-02-11

Correction published 2011-02-11

Issued by
Federal Aviation Administration
Published
2011-02-11
Document
Federal Register 2011-3076 · Final rule; correction

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to the products listed above. The Piaggio service bulletin number specified in the Alternative Methods of Compliance (AMOCs) section is incorrect. This document corrects that error. In all other respects, the original document remains the same.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 2011-3076, retrieved 2026-08-17

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

We are adopting a new airworthiness directive (AD) for the products listed above. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD supersedes Emergency AD 2011-01-51, requires an immediate functional test of the fuselage drain holes, and requires sending a report of the results to the FAA. This AD also allows, with noted exceptions, for the return/ position of the airplane to a home base, hangar, maintenance facility, etc. This AD was prompted by reports of water accumulation in the belly of the fuselage that froze and caused the flight controls to jam. We are issuing this AD to prevent water or fluid from accumulating in the belly of the fuselage and freezing when the aircraft reaches and holds altitudes where the temperature is below the freezing point. This condition could cause the flight controls to jam with consequent loss of control.

Source: Federal Register document 2011-1136, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-23-01

FR doc 2010-27456 · 75 FR 68172

AD 2010-23-01Published 2010-11-05Effective 2010-12-10

Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 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; Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 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 2010-27456, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-21-09

FR doc 2010-25215 · 75 FR 63062

AD 2010-21-09Published 2010-10-14Effective 2010-11-18

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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 2010-25215, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-21-08

FR doc 2010-25217 · 75 FR 63060

AD 2010-21-08Published 2010-10-14Effective 2010-11-18

PIAGGIO AERO INDUSTRIES S.p.A. Model PIAGGIO P-180 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; PIAGGIO AERO INDUSTRIES S.p.A. Model PIAGGIO P-180 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 2010-25217, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-21-14

FR doc 2010-25284 · 75 FR 63058

AD 2010-21-14Published 2010-10-14Effective 2010-11-18

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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 2010-25284, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-09-09

FR doc 2010-9609 · 75 FR 22512

AD 2010-09-09Published 2010-04-29Effective 2010-06-03

Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 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; Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 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 2010-9609, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-03-04

FR doc 2010-1691 · 75 FR 5690

AD 2010-03-04Published 2010-02-04Effective 2010-03-11

PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 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; PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 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 2010-1691, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2010-03-09

FR doc 2010-2001 · 75 FR 5695

AD 2010-03-09Published 2010-02-04Effective 2010-03-11

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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 2010-2001, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2009-21-08

FR doc E9-24651 · 74 FR 57561

AD 2009-21-08Published 2009-11-09Effective 2009-12-14

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 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 E9-24651, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2008-03-14

FR doc E8-2040 · 73 FR 6601

AD 2008-03-14Published 2008-02-05Effective 2008-03-11

Piaggio Aero Industries S.p.A. Model P 180 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; Piaggio Aero Industries S.p.A. Model P 180 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 E8-2040, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-24-15

FR doc E7-23227 · 72 FR 67843

AD 2007-24-15Published 2007-12-03Effective 2008-01-07

Piaggio Aero Industries S.p.A. Model P-180 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; Piaggio Aero Industries S.p.A. Model P-180 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 E7-23227, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-18-07

FR doc E7-17304 · 72 FR 51167

AD 2007-18-07Published 2007-09-06Effective 2007-10-11

Piaggio Aero Industries S.p.A. Model P-180 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; Piaggio Aero Industries S.p.A. Model P-180 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 E7-17304, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2007-13-12

FR doc E7-12008 · 72 FR 35643

AD 2007-13-12Published 2007-06-29Effective 2007-08-03

PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 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; PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 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 E7-12008, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2003-17-03

FR doc 03-20963 · 68 FR 50693

AD 2003-17-03Published 2003-08-22Effective 2003-09-03

Piaggio Aero Industries S.p.A. Model P-180 Airplanes

Supersedes 2003-03-14 — see below

Requires you to inspect and determine whether any firewall shutoff or crossfeed valve with a serial number in a certain range is installed and requires you to replace or modify any valve that has a serial number within this range.

1 AD superseded by this one retired · earliest 2003-02-05
AD

2003-03-14

FR doc 03-2149 · 68 FR 5815

AD 2003-03-14Published 2003-02-05Effective 2003-03-08

Piaggio Aero Industries S.p.A. Model P-180 Airplanes

Superseded by 2003-17-03 — see above

Requires you to inspect and determine whether any firewall shutoff or crossfeed valve with a serial number in a certain range is installed and requires you to replace any valve that has a serial number within this range.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Piaggio Aero Industries S.p.A. (Piaggio) Model P-180 airplanes. This AD requires you to inspect and determine whether any firewall shutoff or crossfeed valve with a serial number in a certain range is installed and requires you to replace any valve that has a serial number within this range. This AD allows the pilot to check the logbook and does not require the inspection and replacement requirement if the check shows that one of these valves is definitely not installed. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent a faulty firewall shutoff or crossfeed valve from developing cracks and leaking fuel. This could result in an engine fire.

Source: Federal Register document 03-2149, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P-180 Airplanes

This document supersedes Airworthiness Directive (AD) 2003-03- 14, which applies to all PIAGGIO AERO INDUSTRIES S.p.A. (PIAGGIO) Model P-180 airplanes. AD 2003-03-14 currently requires you to inspect and determine whether any firewall shutoff or crossfeed valve with a serial number in a certain range is installed and requires you to replace or modify any valve that has a serial number within this range. The modification consisted of reworked valves that were re-identified with an "A" at the end of the serial number. AD 2003-03-14 allows the pilot to check the logbook and does not require the inspection and replacement requirement if the check shows that one of these valves is definitely not installed. Since AD 2003-03-14 became effective, the Federal Aviation Administration (FAA) has found that the valve manufacturer was not correctly incorporating the modification on reworked valves. Consequently, the installation of modified fuel valves installed per AD 2003-03-14 could allow the unsafe condition to remain on the affected airplanes. This AD would require you to replace any firewall shutoff or crossfeed valve with a serial number in a certain range even if it has been modified per AD 2003-03-14. The actions specified by this AD are intended to prevent a faulty firewall shutoff or crossfeed valve from developing cracks and leaking fuel. This could result in an engine fire.

Source: Federal Register document 03-20963, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2003-04-08

FR doc 03-3870 · 68 FR 7908

AD 2003-04-08Published 2003-02-19Effective 2003-04-11

Piaggio Aero Industries S.p.A. Model P-180 Airplanes

Requires you to install a placard on the inside of the lavatory door that prohibits occupying the lavatory seat during takeoff and landing.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Piaggio Aero Industries S.p.A. (Piaggio) Model P-180 airplanes. This AD requires you to install a placard on the inside of the lavatory door that prohibits occupying the lavatory seat during takeoff and landing. This AD also requires you to incorporate a temporary revision into the Limitations Section of the pilot operating handbook/airplane flight manual (POH/AFM). This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent passengers from occupying the lavatory seat during takeoff and landing. The lavatory/cabin partition could fail and lead to passenger injury in an emergency situation.

Source: Federal Register document 03-3870, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2002-23-10

FR doc 02-29133 · 67 FR 69994

AD 2002-23-10Published 2002-11-20Effective 2002-12-17

Piaggio Aero Industries S.p.A. Model P-180 Airplanes

Requires you to inspect for proper clearance between the first outboard flap control rod and the bleed air duct for interference, replace worn or damaged parts or correct interference, and adjust clearance.

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Piaggio Aero Industries S.p.A. Model P-180 airplanes. This AD requires you to inspect for proper clearance between the first outboard flap control rod and the bleed air duct for interference, replace worn or damaged parts or correct interference, and adjust clearance. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to detect and correct interference or damage of the first outboard flap control rod and bleed air duct, which could result in failure of the flap control rod. Such failure could lead to loss of airplane control.

Source: Federal Register document 02-29133, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2002-08-04

FR doc 02-9389 · 67 FR 19657

AD 2002-08-04Published 2002-04-23Effective 2002-06-10

PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 Airplanes

Requires you to replace the four defective horizontal stabilizer hinge bushings with replacement bushings.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain PIAGGIO AERO INDUSTRIES S.p.A. (PIAGGIO) Model P-180 airplanes. This AD requires you to replace the four defective horizontal stabilizer hinge bushings with replacement bushings. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to replace defective bushings before they cause failure of the horizontal stabilizer. Such failure could lead to reduced or loss of control of the aircraft.

Source: Federal Register document 02-9389, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2001-05-04

FR doc 01-5495 · 66 FR 14310

AD 2001-05-04Published 2001-03-12Effective 2001-04-27

Piaggio Aero Industries S.p.A Model P-180 Airplanes

Requires you to inspect the flap actuators for incorrect maneuvering and evidence of grease and oxidation around the gear box (actuators with any of these conditions are referred to as problem actuators).

Full official abstract

Airworthiness Directives; Piaggio Aero Industries S.p.A Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Piaggio Aero Industries S.p.A (PIAGGIO) Model P-180 airplanes. This AD requires you to inspect the flap actuators for incorrect maneuvering and evidence of grease and oxidation around the gear box (actuators with any of these conditions are referred to as problem actuators). If you find a problem actuator, this AD requires you to immediately replace the flap actuators with improved design actuators or repair the existing actuators to the improved design level. If you do not find a problem actuator, this AD requires you to repeat the inspection until the installed actuators are of improved design. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to detect and remove problem flap actuators from service. Continued operation with problem actuators could result in flap system failure, with consequent reduction in, or loss of, control of the airplane.

Source: Federal Register document 01-5495, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2000-03-19

FR doc 00-32935 · 66 FR 7

AD 2000-03-19Published 2001-01-02Effective 2001-01-02

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires revising the Airplane Flight Manual (AFM) to include requirements for activating the airframe pneumatic deicing boots.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment removes Airworthiness Directive (AD) 2000-03- 19, which currently applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes that are equipped with pneumatic deicing boots. AD 2000-03-19 requires revising the Airplane Flight Manual (AFM) to include requirements for activating the airframe pneumatic deicing boots. Since FAA issued AD 2000-03-19, I.A.M. has shown the language currently included in the AFM and the airplane configuration are satisfactory to address the conditions identified in AD 2000-03-19. Therefore, this action removes AD 2000-03-19.

Source: Federal Register document 00-32935, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2000-07-11

FR doc 00-8512 · 65 FR 19305

AD 2000-07-11Published 2000-04-11Effective 2000-05-29

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires repetitively inspecting the brake assembly rods and tubings for wear or damage, and replacing any worn or damaged parts.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires repetitively inspecting the brake assembly rods and tubings for wear or damage, and replacing any worn or damaged parts. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent the brake hydraulic fluid from leaking because of the brake assembly rods contacting the brake valve tubing, which could result in the inability to adequately stop the airplane during ground operations.

Source: Federal Register document 00-8512, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

2000-03-19

FR doc 00-3622 · 65 FR 7717

AD 2000-03-19Published 2000-02-16Effective 2000-04-07

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires you to revise the Airplane Flight Manual (AFM) to include requirements for activating the airframe pneumatic deicing boots.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This document adopts a new airworthiness directive (AD) that applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes that are equipped with pneumatic deicing boots. This AD requires you to revise the Airplane Flight Manual (AFM) to include requirements for activating the airframe pneumatic deicing boots. This AD is the result of reports of in-flight incidents and an accident that occurred in icing conditions where the airframe pneumatic deicing boots were not activated. The actions specified by this AD are intended to assure that flightcrews have the information necessary to activate the pneumatic wing and tail deicing boots at the first signs of ice accumulation. Without this information, flightcrews could experience reduced controllability of the aircraft due to adverse aerodynamic effects of ice adhering to the airplane prior to the first deicing cycle.

Source: Federal Register document 00-3622, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

99-11-06

FR doc 99-12828 · 64 FR 27661

AD 99-11-06Published 1999-05-21Effective 1999-07-05

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires inspecting both (left and right wing configurations) environmental control system bleed tubes for damage, leakage, and a correct gap between the tube and wing lower panel crossing area, inspecting the wiring and…

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires inspecting both (left and right wing configurations) environmental control system bleed tubes for damage, leakage, and a correct gap between the tube and wing lower panel crossing area, inspecting the wiring and surrounding structures for damage, and correcting any discrepancies found. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent thermal expansion from causing leakage of an environmental control system bleed tube because of improper installation, which could result in deterioration of the electrical wiring and the surrounding structure.

Source: Federal Register document 99-12828, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

99-07-10

FR doc 99-7382 · 64 FR 14824

AD 99-07-10Published 1999-03-29Effective 1999-05-10

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires inspecting the upper and lower engine nacelle inner panels for any loose or partially detached inner film, and removing any loose or partially detached inner film.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires inspecting the upper and lower engine nacelle inner panels for any loose or partially detached inner film, and removing any loose or partially detached inner film. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent the accumulation of loose particles on the engine inlet screen caused by film delamination, which could result in reduced engine power and possible loss of airplane control.

Source: Federal Register document 99-7382, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-23-14

FR doc 98-30166 · 63 FR 63598

AD 98-23-14Published 1998-11-16Effective 1998-12-18

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires inspecting the elevator and aileron control retaining pins for proper installation and damage, and replacing any improperly installed or damaged pins.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires inspecting the elevator and aileron control retaining pins for proper installation and damage, and replacing any improperly installed or damaged pins. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent the retaining pins from interfering with the flight control elements, which could result in loss of the cable retaining function with consequent loss of control of the airplane.

Source: Federal Register document 98-30166, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-13-07

FR doc 98-15886 · 63 FR 33536

AD 98-13-07Published 1998-06-19Effective 1998-08-01

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

Requires accomplishing a leakage check of all lavatory water tube/hose connections, and correcting the installation of these connections if leakage is found.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes.

This amendment adopts a new airworthiness directive (AD) that applies to certain Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires accomplishing a leakage check of all lavatory water tube/hose connections, and correcting the installation of these connections if leakage is found. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent water leakage from the lavatory water duct system, which could collect in the fuselage, freeze in cold weather conditions, and cause the rudder control system to jam.

Source: Federal Register document 98-15886, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-12-13

FR doc 98-15083 · 63 FR 31106

AD 98-12-13Published 1998-06-08Effective 1998-07-18

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires modifying the low pitch stop switch support.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires modifying the low pitch stop switch support. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent low pitch stop switch support displacement, which could result in an improper cockpit indication that the propeller is in the Beta range and cause loss of control of the airplane.

Source: Federal Register document 98-15083, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-08-05

FR doc 98-9154 · 63 FR 17321

AD 98-08-05Published 1998-04-09Effective 1998-05-26

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires inspecting the main landing gear (MLG) for interference between the MLG drag brace link and the MLG retraction actuator, and modifying this area if interference is found.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This AD requires inspecting the main landing gear (MLG) for interference between the MLG drag brace link and the MLG retraction actuator, and modifying this area if interference is found. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent MLG failure caused by interference between the MLG retraction actuator and the MLG drag brace link, which could result in loss of control of the airplane during landing operations.

Source: Federal Register document 98-9154, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

98-06-05

FR doc 98-6199 · 63 FR 11823

AD 98-06-05Published 1998-03-11Effective 1998-04-02

Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Requires incorporating airplane flight manual (AFM) and pilot's operating handbook (POH) supplements that include revised autopilot emergency disengagement procedures.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes that are equipped with a Rockwell Collins APS-65 autopilot system that incorporates an APC-65A autopilot computer. This AD requires incorporating airplane flight manual (AFM) and pilot's operating handbook (POH) supplements that include revised autopilot emergency disengagement procedures. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent pilot difficulty in disengaging the autopilot during flight, which could result in the pilot's lack of proper attention to critical flight tasks due to the increased pilot workload with possible consequent loss of airplane controllability.

Source: Federal Register document 98-6199, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

97-22-11

FR doc 97-28576 · 62 FR 56061

AD 97-22-11Published 1997-10-29Effective 1997-12-05

Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Requires amending the Limitations Section of the airplane flight manual (AFM) to prohibit the positioning of the power levers below the flight idle stop while the airplane is in flight.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to all Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. (Piaggio) Model P-180 airplanes. This AD requires amending the Limitations Section of the airplane flight manual (AFM) to prohibit the positioning of the power levers below the flight idle stop while the airplane is in flight. This AFM amendment will include a statement of consequences if the limitation is not followed. This AD results from numerous incidents and five documented accidents involving airplanes equipped with turboprop engines where the propeller beta was improperly utilized during flight. The actions specified by this AD are intended to prevent loss of airplane control or engine overspeed with consequent loss of engine power caused by the power levers being positioned below the flight idle stop while the airplane is in flight.

Source: Federal Register document 97-28576, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

97-15-14

FR doc 97-19439 · 62 FR 40264

AD 97-15-14Published 1997-07-28Effective 1997-09-19

Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

Requires inspecting for cracks around the vertical pin and the torque tube bottom flange of the rudder, and the fasteners that connect the torque tube to the bottom flange (torque tube bottom flange assembly).

Full official abstract

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to Industrie Aeronautiche e Meccaniche Rinaldo Piaggio S.p.A. (Piaggio) Model P-180 airplanes. This action requires inspecting for cracks around the vertical pin and the torque tube bottom flange of the rudder, and the fasteners that connect the torque tube to the bottom flange (torque tube bottom flange assembly). If cracks are not found, repetitively inspect until cracks are visible. If cracks are evident, this action requires modifying the rudder torque tube bottom flange assembly by replacing the cracked part with a part of improved design, which terminates the repetitive inspection. This AD is the result of several reports of fatigue cracks around the pin that vertically supports the rudder axle. The actions specified by this AD are intended to prevent fatigue cracks in the rudder torque tube bottom flange, which could result in loss of rudder control and possible loss of the airplane.

Source: Federal Register document 97-19439, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

97-14-14

FR doc 97-17732 · 62 FR 36448

AD 97-14-14Published 1997-07-08Effective 1997-08-29

Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

Requires inspecting the baggage compartment for stringer or air cycle machine (ACM) by-pass duct damage, repairing any damage found, and modifying the freon air inlet duct and electrical wiring.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Industrie Aeronautiche E Meccaniche (I.A.M.) Model Piaggio P-180 airplanes that are equipped with a certain freon air conditioning system. This AD requires inspecting the baggage compartment for stringer or air cycle machine (ACM) by-pass duct damage, repairing any damage found, and modifying the freon air inlet duct and electrical wiring. This AD results from trim system malfunction on one of the affected airplanes, resulting from contact between the freon air inlet duct and the electrical wiring. The actions specified by this AD are intended to prevent trim system malfunction caused by contact between the freon air inlet duct and electrical wiring, which could result in loss of control of the airplane.

Source: Federal Register document 97-17732, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

96-19-02

FR doc 96-22952 · 61 FR 48613

AD 96-19-02Published 1996-09-16Effective 1996-10-28

Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

Requires modifying the passenger seat cushion next to the emergency exit door handle.

Full official abstract

Airworthiness Directives; Industrie Aeronautiche E Meccaniche Model Piaggio P-180 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to Industrie Aeronautiche E Meccaniche (I.A.M.) Model Piaggio P-180 airplanes. This action requires modifying the passenger seat cushion next to the emergency exit door handle. Reports of interference between the passenger seat cushion and the emergency exit door handle, preventing the door from opening from the outside, prompted this AD action. The actions specified by the AD are intended to prevent the possibility of not being able to open the emergency exit door during an emergency evacuation of the airplane, which could result in injury to the passengers.

Source: Federal Register document 96-22952, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

96-18-20

FR doc 96-22597 · 61 FR 47409

AD 96-18-20Published 1996-09-09Effective 1996-10-15

Piaggio Model P-180 Airplanes

Requires replacement of outflow/safety valves with serviceable valves.

Full official abstract

Airworthiness Directives; Piaggio Model P-180 Airplanes

This amendment adopts a new airworthiness directive (AD), applicable to certain Piaggio Model P-180 airplanes, that requires replacement of outflow/safety valves with serviceable valves. This amendment is prompted by a report of cracking and subsequent failure of outflow safety valves in the pressurization system. The actions specified by this AD are intended to prevent such cracking and subsequent failure of the outflow/safety valves, which could result in rapid decompression of the airplane.

Source: Federal Register document 96-22597, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

AD

96-09-09

FR doc 96-10581 · 61 FR 19808

AD 96-09-09Published 1996-05-03Effective 1996-06-07

I.A.M. Rinaldo Piaggio S.p.A. Model P 180 Series Airplanes

Requires installing a shield on the front section of the engine cradle.

Full official abstract

Airworthiness Directives; I.A.M. Rinaldo Piaggio S.p.A. Model P 180 Series Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to I.A.M. Rinaldo Piaggio S.p.A. Model P 180 series airplanes. This action requires installing a shield on the front section of the engine cradle. A report of power control jamming as a result of freezing conditions during a high altitude flight prompted this AD action. The actions specified by this AD are intended to prevent loss of engine power or the propeller controls from jamming as a result of freezing rain entering the engine nacelle, which, if not detected and corrected, could result in loss of control of the airplane.

Source: Federal Register document 96-10581, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17

Corrections whose original AD is not yet indexed

1 record
Correction

2011-09-51

FR doc 2011-15810 · 76 FR 36980

AD 2011-09-51Published 2011-06-24Effective 2011-06-24

PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

Corrects: The AD number in the preamble on the first page of the AD is incorrect.

Full official abstract

Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to the products listed above. The AD number in the preamble on the first page of the AD is incorrect. This document corrects that error. In all other respects, the original document remains the same.

This document corrects or clarifies a previously issued AD of the same number — it is not a separate, additional requirement. Its "Effective" date above may predate its own "Published" date because it restates the original AD's effective date.

Source: Federal Register document 2011-15810, 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 59 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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