EASA Regulations for Piper PA-28R-200

5 airworthiness directives and regulations affecting Piper PA-28R-200.

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New ADs and bulletins for Piper PA-28R-200, summarized like the ones below, every Monday.

EASA AD US-2020-26-16

Feb 9, 2021

NOT ADOPTED - EASA DECISION ATTACHED

The Federal Aviation Administration (FAA) Final Rule titled Airworthiness Directive 2020-26-16 addresses certain Piper Aircraft, Inc. models including PA-28-151, PA-28-161, PA-28-181, PA-28-235, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T airplanes. This directive responds to a safety concern involving wing separation caused by fatigue cracking in the lower main wing spar cap. It mandates inspections and potential replacement of affected wing spars to ensure continued airworthiness.

Airworthiness Directive
  • Piper Aircraft PA-28 (Archer)
  • Piper Aircraft PA-28 (Cadet)
  • Piper Aircraft PA-28 (Cherokee)
  • Piper Aircraft PA-28 (Warrior)
  • Piper Aircraft PA-28R (Arrow)
  • Piper Aircraft PA-32 (Cherokee Six)
  • Piper Aircraft PA-32R (Lance)
  • Piper PA-28-151
  • Piper PA-28-161
  • Piper PA-28-181
  • Piper PA-28-235
  • Piper PA-28R-180
  • Piper PA-28R-200
  • Piper PA-28R-201
  • Piper PA-28R-201T
  • Piper PA-28RT-201
  • Piper PA-28RT-201T
  • Piper PA-32-260
  • Piper PA-32-300
  • Piper PA-32R-300
  • Piper PA-32RT-300
  • Piper PA-32RT-300T

EASA AD US-2018-07-03

Apr 9, 2018

Placard and Markings - Preflight Check of the Fuel Selector Cover

The Federal Aviation Administration's Airworthiness Directive 2018-07-03 supersedes AD 2018-02-05 and applies to certain Piper Aircraft, Inc. models including PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-236, PA-28-201T, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, and PA-28RT-201T airplanes. This directive mandates a preflight check of the fuel tank selector cover placards to ensure correct positioning and requires replacement if placards are improperly located. It allows pilots holding at least a private pilot certificate to perform this check.

Airworthiness Directive
  • Piper Aircraft PA-28 (Archer)
  • Piper Aircraft PA-28 (Cadet)
  • Piper Aircraft PA-28 (Cherokee)
  • Piper Aircraft PA-28 (Dakota)
  • Piper Aircraft PA-28 (Warrior)
  • Piper Aircraft PA-28R (Arrow)
  • Piper PA-28-140
  • Piper PA-28-150
  • Piper PA-28-151
  • Piper PA-28-160
  • Piper PA-28-161
  • Piper PA-28-180
  • Piper PA-28-181
  • Piper PA-28-236
  • Piper PA-28-201T
  • Piper PA-28R-180
  • Piper PA-28R-200
  • Piper PA-28R-201
  • Piper PA-28R-201T
  • Piper PA-28RT-201
  • Piper PA-28RT-201T

EASA AD US-2018-02-05

Jan 24, 2018

Superseded by FAA AD 2018-07-03

FAA Airworthiness Directive 2018-02-05 is a final rule addressing certain Piper Aircraft, Inc. models including PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-236, PA-28-201T, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, and PA-28RT-201T airplanes. The directive requires inspection and, if necessary, replacement of fuel tank selector placards to ensure correct left and right positioning. This AD was issued due to a manufacturer quality control issue resulting in reversed placard installation, which could lead to fuel starvation and engine power loss in flight.

Airworthiness Directive
  • Piper Aircraft PA-28 (Archer)
  • Piper Aircraft PA-28 (Cadet)
  • Piper Aircraft PA-28 (Cherokee)
  • Piper Aircraft PA-28 (Dakota)
  • Piper Aircraft PA-28 (Warrior)
  • Piper Aircraft PA-28R (Arrow)
  • Piper PA-28-140
  • Piper PA-28-150
  • Piper PA-28-151
  • Piper PA-28-160
  • Piper PA-28-161
  • Piper PA-28-180
  • Piper PA-28-181
  • Piper PA-28-236
  • Piper PA-28-201T
  • Piper PA-28R-180
  • Piper PA-28R-200
  • Piper PA-28R-201
  • Piper PA-28R-201T
  • Piper PA-28RT-201
  • Piper PA-28RT-201T

EASA SIB CE-14-22

Aug 26, 2014

Piper PA-28 Aeroplanes — Fuel Selector/Shut-Off Valve

Special Airworthiness Information Bulletin SAIB: CE-14-22 is an FAA informational bulletin addressing a fuel selector valve issue in Piper Aircraft Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28R-180, and PA-28R-200 airplanes. It highlights the risk of inadvertent fuel selector valve shutoff or binding during fuel tank switching, which can cause engine power loss in flight. The bulletin provides recommendations to prevent such occurrences but does not mandate regulatory action.

Safety Information Bulletin
  • Piper PA-28-140
  • Piper PA-28-150
  • Piper PA-28-160
  • Piper PA-28-180
  • Piper PA-28R-180
  • Piper PA-28R-200

EASA SIB NE-13-32

May 14, 2013

Hartzell Propeller Spinner Assemblies P/N 835-54(P) and P/N 835-58(P) — Potential for Cracking of the Spinner Dome

The FAA Special Airworthiness Information Bulletin SAIB: NE-13-32 informs owners, operators, and repair facilities of Piper PA-24, Piper PA-28R-180, Piper PA-28R-200, and Mooney M20 airplanes (except Mooney M20(J)) equipped with Hartzell Propeller spinner assemblies P/N 835-54(P) and P/N 835-58(P) about the potential for cracking in the spinner dome. This cracking could lead to spinner failure and separation during flight. The bulletin provides safety information but does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin
  • Piper PA-24
  • Piper PA-28R-180
  • Piper PA-28R-200
  • Mooney M20