A300 B2-202 A1 AIRBUS Airbus A300 basic model (GE CF6) Up to and including C* checks X X A300 B4-102 A1 AIRBUS A300 C4-203 Airbus A300 basic model (GE CF6) Daily /weekly / defect rectification X A1 AIRBUS A300 B2-320 Airbus A300 basic model (PW JT9D) Daily/Weekly/defect rectifications X Up to C checks* excluding C4C, S4C and A1 The BOEING COMPANY Boeing 767-200 BOEING 767-200 (PW 4000) X X multiples PC-12 A2 PILATUS AIRCRAFT PC-2/45 Pilatus PC 12 (PW PT6) Up to and including weekly checks X PC-12/47E LAVIA ARGENTINA S.A. A2 - Piper PA-25 (Lycoming) Up to and including 100H/Annual checks* X (LAVIASA) AS355 E AS355 F1 A3 EUROCOPTER Eurocopter AS 355 (RR Corp 250) Defect rectification, Daily X AS355 F2 A4 NIL Should be mentioned in this table for each approved site: - in columns TC holder and limitation: the information from the column 1 and 3 of the table in Appendix I to AMC to Part-66 respectively, as specified in ED DECISION 2011/003/R and its successive issues, except that the should be deleted. The limitation must include the engine type. word “Series” - in column Aircraft Model: the data from column 2 or from the same Appendix I “Aeroplane Model” „Helicopter Model” - in column Maintenance level: the scope of maintenance activity at each location or station as agreed by the ICETRA. - in case of group rating, each aircraft composing the group should be listed. *: The limitation relative to the maintenance checks/tasks should be addressed as referenced in TC Holder data (i.e. MRB/MPD). **In case of unforeseen maintenance such as but not limited to major repairs and modifications that is not already described within this chapter, the AMO shall contact the competent authority. Engine maintenance Example: Rating ENGINE/APU MODEL Limitation Maintenance level B1 TFE 731-20 TFE 731- 20AR Modules turbine exchange
A1 AIRBUS A300 B2-202 A300 B4-102 Airbus A300 basic model (GE CF6) Up to and including C* checks X X A1 AIRBUS A300 C4-203 Airbus A300 basic model (GE CF6) Daily /weekly / defect rectification X A1 AIRBUS A300 B2-320 Airbus A300 basic model (PW JT9D) Daily/Weekly/defect rectifications X A1 The BOEING COMPANY Boeing 767-200 BOEING 767-200 (PW 4000) Up to C checks* excluding C4C, S4C and multiples X X A2 PILATUS AIRCRAFT PC-12 PC-2/45 PC-12/47E Pilatus PC 12 (PW PT6) Up to and including weekly checks X A2 LAVIA ARGENTINA S.A. (LAVIASA) - Piper PA-25 (Lycoming) Up to and including 100H/Annual checks* X A3 EUROCOPTER AS355 E AS355 F1 AS355 F2 Eurocopter AS 355 (RR Corp 250) Defect rectification, Daily X A4 NIL Should be mentioned in this table for each approved site: - in columns TC holder and limitation: the information from the column 1 and 3 of the table in Appendix I to AMC to Part-66 respectively, as specified in ED DECISION 2011/003/R and its successive issues, except that the word “Series” should be deleted. The limitation must include the engine type. - in column Aircraft Model: the data from column 2 “Aeroplane Model” or „Helicopter Model” from the same Appendix I - in column Maintenance level: the scope of maintenance activity at each location or station as agreed by the ICETRA. - in case of group rating, each aircraft composing the group should be listed. *: The limitation relative to the maintenance checks/tasks should be addressed as referenced in TC Holder data (i.e. MRB/MPD). **In case of unforeseen maintenance such as but not limited to major repairs and modifications that is not already described within this chapter, the AMO shall contact the competent authority. Engine maintenance Example: Rating ENGINE/APU MODEL Limitation Maintenance level B1 TFE 731-20 TFE 731- 20AR Modules turbine exchange