Airbus C-295
72 parts applicable to this airframe — military_transport
| Part Number | Status |
|---|---|
| 08-19348 | unknown |
| 103860-1 | PMA |
| 130544-1 | PMA |
| 2119924-1 | PMA |
| 21213050 | OEM |
| 212224089 | OEM |
| 2122320016 | OEM |
| 212234004 | OEM |
| 212241001 | OEM |
| 21246100151 | OEM |
| 212462221 | OEM |
| 2243500-21 | PMA |
| 29S-7D5154-11P29S-7D5154-11 | OEM |
| 29S-7D5154-12P29S-7D5154-12 | OEM |
| 29S-7D5154-13P29S-7D5154-13 | OEM |
| 29S-7D5154-14P29S-7D5154-14 | OEM |
| 29S-7D5154-19P29S-7D5154-19 | OEM |
| 29S-7D5154-21P29S-7D5154-21 | OEM |
| 29S-7D5154-22P29S-7D5154-22 | OEM |
| 29S-7D5154-27P29S-7D5154-27 | OEM |
| 54 | OEM |
| 7-44766-12 | PMA |
| AC780011 | OEM |
| AC780023 | OEM |
| AC811000 | OEM |
| AC911016 | OEM |
| AG247000-04 | PMA |
| AG728000-18 | PMA |
| AG728000-46 | PMA |
| AG822000-03 | PMA |
| AG843000-15 | PMA |
| FRAME18RIB | OEM |
| LN93614C46L4347 | OEM |
| LN93614C46L4635 | OEM |
| LN93614C46L4653 | OEM |
| LN93614C4L4347 | OEM |
| M2030AC-4 | PMA |
| SMR5154-11 | PMA |
| SMR5154-12 | PMA |
| SMR5154-13 | PMA |
| SMR5154-14 | PMA |
| SMR5154-19 | PMA |
| SMR5154-21 | PMA |
| SMR5154-22 | PMA |
| SMR5154-27 | PMA |
| ST00342BO | OEM |
| ST02131LA | OEM |
| ST03776NY | OEM |
| ST04177AT | OEM |
| ST04211AT | OEM |
Airworthiness Directive activity
FAA / EASA public regulatory data
- 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.