AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2000-07-11 65 FR 19305 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-8512
Amendment
39-11665
Published
2000-04-11
Effective
2000-05-29
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2000-07-11 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2000-07-11

FR doc 00-8512 · 65 FR 19305

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

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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

Full official abstract

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.

More directives for Piaggio P.180 Avanti

  1. AD 2026-06-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... 2026-04-06
  2. AD 2026-05-10 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... 2026-03-23
  3. AD 2025-26-05 Airworthiness Directives; Baykar Piaggio Aerospace S.p.A. (Type Certific... 2026-01-12
  4. AD 2025-15-10 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes 2025-07-30
  5. AD 2023-25-03 Airworthiness Directives; Piaggio Aviation S.p.A. Airplanes 2023-12-29

All Piaggio P.180 Avanti directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index