Airbus C-295

72 parts applicable to this airframe — military_transport

Part NumberStatus
08-19348unknown
103860-1PMA
130544-1PMA
2119924-1PMA
21213050OEM
212224089OEM
2122320016OEM
212234004OEM
212241001OEM
21246100151OEM
212462221OEM
2243500-21PMA
29S-7D5154-11P29S-7D5154-11OEM
29S-7D5154-12P29S-7D5154-12OEM
29S-7D5154-13P29S-7D5154-13OEM
29S-7D5154-14P29S-7D5154-14OEM
29S-7D5154-19P29S-7D5154-19OEM
29S-7D5154-21P29S-7D5154-21OEM
29S-7D5154-22P29S-7D5154-22OEM
29S-7D5154-27P29S-7D5154-27OEM
54OEM
7-44766-12PMA
AC780011OEM
AC780023OEM
AC811000OEM
AC911016OEM
AG247000-04PMA
AG728000-18PMA
AG728000-46PMA
AG822000-03PMA
AG843000-15PMA
FRAME18RIBOEM
LN93614C46L4347OEM
LN93614C46L4635OEM
LN93614C46L4653OEM
LN93614C4L4347OEM
M2030AC-4PMA
SMR5154-11PMA
SMR5154-12PMA
SMR5154-13PMA
SMR5154-14PMA
SMR5154-19PMA
SMR5154-21PMA
SMR5154-22PMA
SMR5154-27PMA
ST00342BOOEM
ST02131LAOEM
ST03776NYOEM
ST04177ATOEM
ST04211ATOEM

Airworthiness Directive activity

FAA / EASA public regulatory data

2airworthiness directives affecting this fleet — recurring compliance demand for the parts and shops that serve it
Most recent
  • FAA AD 2024-24-04effective Jan 13, 2025Mixed actions

    The FAA is superseding Airworthiness Directive (AD) 2018-18- 09, which applied to all Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes; and certain Model C- 295 airplanes. AD 2018-18-09 required a detailed inspection of the upper and lower lugs of each horizontal stabilizer-to-fuselage rear attachment fitting, repair if necessary, and a report of findings. This AD was prompted by reports of new occurrences of cracking. This AD requires repetitive inspections, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also revises the applicability. The FAA is issuing this AD to address the unsafe condition on these products.

  • FAA AD 2023-25-11effective Feb 7, 2024Mixed actions

    The FAA is superseding Airworthiness Directive (AD) 2021-02- 18, which applied to all Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes and Model C-295 airplanes. AD 2021-02-18 required repetitive inspections for cracking or broken rivets of certain left- and right-hand stringers and surrounding structure, and repair if necessary. This AD was prompted by a modification that was developed to reinforce the structure in the affected area, providing terminating action for the repetitive inspections required by AD 2021-02-18. This AD continues to require certain actions in AD 2021-02-18 and requires the new terminating action for the repetitive inspections, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

Directives linked to this airframe family in the FAA / EASA regulatory corpus we have processed — not a complete historical AD list. An AD is a compliance requirement that drives scheduled work (inspections, replacements, modifications) across the fleet; inspection directives are not replacement directives, and none of this is a prediction that any part will fail.