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2021-0107R2 : Wings – Lower Main Wing Spar Caps – Inspection

Number 2021-0107R2
Issued by Europe  Europe
Issue date 2022-05-20
Effective date 2022-05-27
EASA approval number
ATA Chapter 57
Approval Holder
/ Type Designation
  • PIPER AIRCRAFT INC.
    • PA-28 (Archer)
      • PA-28-181 (Archer II)
      • PA-28-181 (Archer III)
    • PA-28 (Cadet)
      • PA-28-161
    • PA-28 (Cherokee)
      • PA-28-235 (Pathfinder)
    • PA-28 (Warrior)
      • PA-28-151 (Warrior)
      • PA-28-161 (Warrior II)
      • PA-28-161 (Warrior III)
    • PA-28R (Arrow)
      • PA-28R-180
      • PA-28R-200
      • PA-28R-200 (Arrow II)
      • PA-28R-201 (Arrow III)
      • PA-28R-201T (Turbo Arrow III)
      • PA-28RT-201 (Arrow IV)
      • PA-28RT-201T (Turbo Arrow IV)
    • PA-32 (Cherokee Six)
      • PA-32-260
      • PA-32-300
    • PA-32R (Lance)
      • PA-32R-300
      • PA-32RT-300 (Lance II)
      • PA-32RT-300T (Turbo Lance II)
Revision This AD revises EASA AD 2021-0107R1 dated 13 May 2021.
Correction Not applicable
Supersedure For affected aeroplanes operated under EU regulation, the original issue of this AD replaced FAA State of Design AD 2020-26-16, which was not adopted by EASA.
Publication(s) and related information Piper SB 1345 dated 27 March 2020. Piper SL 997 dated 14 May 1987.
PAD number 21-041
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The original issue of this AD was posted on 10 March 2021 as PAD 21-041 for consultation until 07 April 2021. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.