EASA Regulations for Piper PA-32

11 airworthiness directives and regulations affecting Piper PA-32.

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New ADs and bulletins for Piper PA-32, summarized like the ones below, every Monday.

EASA AD 2021-0107R2

May 20, 2022

Wings — Lower Main Wing Spar Caps — Inspection

EASA Airworthiness Directive 2021-0107R2 is an updated safety directive addressing inspection requirements for the lower main wing spar caps on Piper Aircraft, Inc. PA-28 and PA-32 aeroplanes. It mandates inspections to detect fatigue cracks in the lower main wing spar caps, which could lead to wing separation if undetected. The directive applies to multiple PA-28 and PA-32 models with specific serial numbers and includes detailed definitions and inspection procedures.

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
  • Piper PA-32

EASA AD 2005-0035-CN

Feb 20, 2020

CANCELLED: Landing Gear - Main Undercarriage Structure - Inspection

EASA Airworthiness Directive 2005-0035-CN is a cancellation notice for the previous directive concerning the inspection of the main landing gear cylinder torque link attachment lugs on Piper Aircraft PA-28 and PA-32 aeroplanes. The affected aircraft include various PA-28 models and the PA-32-260, with specific serial numbers detailed in the directive. This cancellation reflects updated safety assessments and improved inspection procedures.

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-32 (Cherokee Six)
  • Piper PA-28
  • Piper PA-32

EASA SIB CE-14-23

Aug 26, 2014

Piper PA-28, PA-32, PA-34, PA-44 and PA-46 Aeroplanes — Air Inlet Hose

The Special Airworthiness Information Bulletin SAIB: CE-14-23 is an FAA informational bulletin addressing an airworthiness concern for Piper Aircraft Models PA-28, PA-32, PA-34, PA-44, and PA-46 series airplanes. It highlights the risk of structural deterioration and possible collapse of the air inlet hose, which can reduce engine airflow and cause rough running or power loss. The bulletin does not mandate corrective action but provides important safety information for these Piper models.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34
  • Piper PA-44
  • Piper PA-46

EASA SIB CE-11-42

Jun 30, 2011

Piper PA-28, PA-32, PA-34 and PA-44 Series - Flight Control Cable/Pulley Inspections

The Special Airworthiness Information Bulletin SAIB: CE-11-42 is an FAA informational bulletin addressing a potential airworthiness issue with flight control cables and pulleys on Piper PA-28, PA-32, PA-34, and PA-44 series airplanes. It highlights a manufacturing flaw in pulleys that can cause aileron control cables to fail, potentially resulting in loss of aileron control. The bulletin applies to all serial numbers of the specified Piper models and provides inspection guidance but does not mandate regulatory action.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34
  • Piper PA-44

EASA SIB CE-11-14

Jan 17, 2011

Piper PA-28, PA-32 and PA-34 - Vertical Stabilizer Forward Attachment Point Corrosion

The Special Airworthiness Information Bulletin CE-11-14 issued by the FAA on January 5, 2011, addresses potential corrosion on the vertical stabilizer forward attachment point of Piper PA-28, PA-32, and PA-34 aircraft. It highlights corrosion risks on specific parts, including steel fitting 62453-00 and aluminum bulkhead/frame assembly 62444-xx, based on service data from routine maintenance inspections. The bulletin provides inspection guidance from Piper service manuals and reminds operators to focus on corrosion prevention and detection.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34

EASA SIB CE-11-13

Jan 17, 2011

Piper PA-34 aeroplanes - Forward Wing Spar Corrosion

The FAA Special Airworthiness Information Bulletin CE-11-13 is an informational bulletin addressing potential corrosion on the forward wing spar of Piper PA-28, PA-32, and PA-34 aircraft. It highlights corrosion risks at the fuselage attach fitting, landing gear attach point, and behind the leading edge fuel tank, and recommends incorporating Piper Service Bulletin 1006 to mitigate these issues. This bulletin does not mandate regulatory action but serves as guidance for owners and operators of the affected Piper models.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34

EASA SIB CE-11-11

Jan 14, 2011

Piper PA-28, PA-32, and PA-34 - Aileron Hinge Fitting Corrosion

The FAA Special Airworthiness Information Bulletin CE-11-11 provides information regarding potential corrosion on the aileron hinge fittings of Piper PA-28, PA-32, and PA-34 aircraft. This bulletin is informational only and does not mandate any regulatory action but highlights the importance of inspections as outlined in the aircraft service manuals.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34

EASA SIB CE-11-10

Jan 14, 2011

Piper PA-28, PA-32, PA-34, and PA-44 - Corrosion on Flap Hinges, Brackets, and Ribs

The Special Airworthiness Information Bulletin FAA SAIB CE-11-10 is an informational bulletin addressing potential corrosion issues on flap hinges, brackets, and ribs of Piper Aircraft models PA-28, PA-32, PA-34, and PA-44. It highlights corrosion found on specific parts including hinges (part numbers 62324-xx), ribs (62328-xx), and brackets (62323-00 and 65899-00). The bulletin provides guidance to operators to focus on inspections outlined in the aircraft service manuals to mitigate corrosion risks.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34
  • Piper PA-44

EASA SIB CE-11-01

Oct 15, 2010

Piper PA-28, PA-32, PA-34 and PA-44 series - Horizontal Stabilator Turnbuckle

The Special Airworthiness Information Bulletin SAIB: CE-11-01 is an FAA informational bulletin addressing a potential airworthiness concern involving the horizontal stabilator turnbuckle and control cable assembly on Piper PA-28, PA-32, PA-34, and PA-44 series airplanes. The issue involves stress corrosion cracking that could lead to failure of the turnbuckle/control cable assembly and loss of pitch control. This bulletin applies to all serial numbers of the specified Piper models.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34
  • Piper PA-44

EASA SIB CE-10-17

May 28, 2010

Piper PA-28 and PA-32 Main Landing Gear Torque Link Inspection Interval

The Special Airworthiness Information Bulletin (SAIB) CE-10-17 is an FAA informational bulletin addressing the inspection interval for the main landing gear torque link on Piper PA-28 and PA-32 aircraft models. It specifically concerns certain serial numbers of PA-28-140, PA-28-150/-160/-180, PA-28-235, PA-32-260, and PA-32-300 aircraft. The bulletin recommends incorporating Piper Service Bulletin 1199 to enhance inspection frequency and replacement times for the main landing gear torque link assemblies.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32

EASA SIB CE-09-23

Apr 15, 2009

Fuel Starvation due to a Blocked Fuel Tank Outlet

Special Airworthiness Information Bulletin SAIB: CE-09-23 is an FAA informational bulletin addressing fuel starvation risks in Piper PA-28, PA-32, and PA-34 series airplanes. It highlights concerns about environmental deterioration of a sloshing compound previously used to repair leaking fuel tanks, which can peel and block fuel tank outlets, potentially starving the engine of fuel.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32
  • Piper PA-34