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AMES > INFORMATION - Completed Projects - Minor Repairs
No. Project Number Aircraft Model Certification Basis Documentation
1 M04400107.15092006 Airbus A320-232 JAR 25 AMES / 24.10.2006
Project Description
EASA Validation of Jet Blue Engineering Order 5300233 demanding a structural repair related to the Live TV system on specified aircraft.


No. Project Number Aircraft Model Certification Basis Documentation
2 M04400108.15092006 Airbus A320-232 JAR 25 AMES / 13.10.2006
Project Description
EASA Validation of Jet Blue Engineering Order 5300234 demanding a structural repair / modification related to the Live TV system on specified aircraft.


No. Project Number Aircraft Model Certification Basis Documentation
3 M04400109.15092006 Airbus A320-232 JAR 25 AMES / 24.10.2006
Project Description
EASA Validation of Jet Blue Engineering Order 5300238 providing instructions for repair / reworking of the doubler installation under the Live TV antenna clevis fittings at Frame C50, stringer 4L and 4R.


No. Project Number Aircraft Model Certification Basis Documentation
4 M04400110.15092006 Airbus A320-232 JAR 25 AMES / 11.10.2006
Project Description
EASA Validation of Jet Blue Engineering Order 5300507 providing instructions for permanent repair of the fuselage skin dent damage in the area of the standby static port.


No. Project Number Aircraft Model Certification Basis Documentation
5 M04400111.15092006 Airbus A320-232 JAR 25 AMES / 13.10.2006
Project Description
EASA Validation of Jet Blue Engineering Order 5301068 providing instructions for structural repair at the aft section of the fuselage between frame C61 and C62 and stringer P40 and P43.


No. Project Number Aircraft Model Certification Basis Documentation
6 M04400131.24042008 Airbus A320-232 JAR 25 AMES / 25.05.2008
Project Description
This AMES Minor Repair provides the validation for a repair performed by JetBlue referenced in EO 5302145.
During installation of Live TV at MCO, Frame 50 Inner Flange was damaged. The damage is detailed in Fig.1 A & 1D of EO 5302145. The Frame part number is D53470511200 and the material is 2024 T42 and thickness 0.047