| Number | 
                            2025-0240 | 
                        
                        
                            | Issued by | 
                               Europe | 
                        
                        
                            | Issue date | 
                            2025-10-27 | 
                        
                                                
                            | Effective date | 
                            2025-11-10 | 
                        
                                                
                            | EASA approval number | 
                             | 
                        
                        
                            | ATA Chapter | 
                            05 | 
                        
                        
                            Approval Holder  / Type Designation | 
                            
                                
                                    - 
                                        FOKKER SERVICES
                                        
                                            - 
                                                F27
                                                
                                                    - 
                                                        MARK050
                                                    
 
                                                    - 
                                                        MARK0502
                                                    
 
                                                    - 
                                                        MARK0604
                                                    
 
                                                 
                                             
                                         
                                     
                                 
                             | 
                        
                        
                            | Revision | 
                            
                                Not applicable
    			              | 
                        
                        
                            | Correction | 
                            
                                Not applicable
    			              | 
                        
                        
                            | Supersedure | 
                            
                                This AD supersedes EASA AD 2025-0085 dated 14 April 2025.
                             | 
                        
                        
                            | Publication(s) and related information | 
                            FS "Airworthiness Limitations Section Part 2, Fokker 50/60 Airworthiness Limitation Items (ALI's) and Safe Life Items (SLI's)", Report SE-622, Issue 17 dated 01 August 2025.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. | 
                        
                        
                            | PAD number | 
                            25-152 | 
                        
                        
                            | Remarks | 
                            
                                1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 September 2025 as PAD 25-152 for consultation until 24 October 2025. No comments were received during the consultation period.
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.
                             |