EASA Regulations for Piper Aircraft PA-28 (Dakota)

5 airworthiness directives and regulations affecting Piper Aircraft PA-28 (Dakota).

EASA AD US-2024-14-03

Auto Flight - Garmin GFC 500 Autopilot System - Software Update

The Federal Aviation Administration's Airworthiness Directive 2024-14-03 addresses various airplanes equipped with the Garmin GFC 500 Autopilot System installed under Supplemental Type Certificate No. SA01866WI. This directive mandates a software update to the Garmin GFC 500 Autopilot System to prevent un-commanded automatic pitch trim runaway events. The affected aircraft include all models specified in the directive that have the optional GSA 28 pitch trim servo installed.

Jul 22, 2024

Airworthiness DirectiveMaintenanceSafety MgmtCommander (Cpac, Inc.) 112Commander (Cpac, Inc.) 114Daher Aerospace TBMooney International Corporation M20Piper Aircraft PA-24 (Comanche)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 Aircraft PA-30 (Twin Comanche)Piper Aircraft PA-32 (Cherokee Six)Piper Aircraft PA-32 (Piper 6X)Piper Aircraft PA-32 (Saratoga)Piper Aircraft PA-32R (Lance)Piper Aircraft PA-39 (Twin Comanche)Textron Aviation 172 (Skyhawk)Textron Aviation 172RGTextron Aviation 177 (Cardinal)Textron Aviation 177RG (Cardinal RG)Textron Aviation 182 (Skylane)Textron Aviation 19Textron Aviation 206Textron Aviation U206 (Super Skywagon)Textron Aviation 206H (Stationair)Textron Aviation 210 (Centurion)Textron Aviation 23 (Musketeer)Textron Aviation 24 (Sierra)Textron Aviation 33 (Bonanza)Textron Aviation 35 (Bonanza)Textron Aviation 36 (Bonanza)Textron Aviation F172Textron Aviation F177RGTextron Aviation F182Textron Aviation FR172 (Reims Rocket)Textron Aviation P172DTextron Aviation P206Textron Aviation TP206 (Super Skylane)Textron Aviation R172 (Hawk XP)

EASA SIB SAIB-2022-20

Wing Lower Spar Cap Bolt Holes

The FAA Special Airworthiness Information Bulletin SAIB: 2022-20 provides information regarding fatigue cracks found in the lower spar cap bolt holes of Piper Aircraft, Inc. PA-28 and PA-32 airplanes. This bulletin follows a fatal 2018 accident involving a Piper PA-28R-201 airplane and the subsequent Airworthiness Directive AD 2020-26-16, which mandated inspections of certain lower spar cap bolt holes. The bulletin highlights inspection findings of numerous cracks and hole-quality issues across the fleet and discusses ongoing analysis to develop further corrective actions.

Oct 20, 2022

Safety Information BulletinMaintenanceSafety MgmtPiper 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 Aircraft PA-32 (Cherokee Six)Piper Aircraft PA-32 (Piper 6X)Piper Aircraft PA-32 (Saratoga)Piper Aircraft PA-32R (Lance)

EASA SIB AIR-21-10

Forward Wing Spar to Fuselage Attachment Fittings - Visual Inspection

The Special Airworthiness Information Bulletin SAIB: AIR-21-10 is an FAA advisory concerning potential corrosion in the forward wing spar to fuselage attachment fittings on certain Piper Aircraft, Inc. models including PA-28, PA-32, PA-34, and PA-44 series airplanes. It highlights the risk of galvanic corrosion between steel fittings and aluminum spars in areas that may be difficult to inspect visually. This bulletin provides information to owners and operators but does not mandate regulatory action.

Jul 19, 2021

EASA AD US-2018-07-03

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.

Apr 9, 2018

Airworthiness DirectiveFlight OpsSafety MgmtPiper 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-28-140Piper PA-28-150Piper PA-28-151Piper PA-28-160Piper PA-28-161Piper PA-28-180Piper PA-28-181Piper PA-28-236Piper PA-28-201TPiper PA-28R-180Piper PA-28R-200Piper PA-28R-201Piper PA-28R-201TPiper PA-28RT-201Piper PA-28RT-201T

EASA AD US-2018-02-05

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.

Jan 24, 2018

Airworthiness DirectiveMaintenanceSafety MgmtPiper 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-28-140Piper PA-28-150Piper PA-28-151Piper PA-28-160Piper PA-28-161Piper PA-28-180Piper PA-28-181Piper PA-28-236Piper PA-28-201TPiper PA-28R-180Piper PA-28R-200Piper PA-28R-201Piper PA-28R-201TPiper PA-28RT-201Piper PA-28RT-201T