Qualification
- Composite
- Aluminum H/T
Composite Qualifications
Customer | Process | Process detail | Project | Remark |
---|---|---|---|---|
Boeing | BAC5980 | NDT | B777FLE | Chukdong Plant |
BAC5317-2 BAC5317-3 |
Sandwich Panel Laminate |
B777 FLE B737 Emp/Max B767 Sex.48 |
Chukdong Plant | |
Bombardier | BAPS260-001 BAPS260-002 BAPS151-001 BAPS157-027 BAPS157-028 BAPS160-040 |
Laminate Laminate Rivet and Nut-plates Install Sealing Sealing Alodine and Paint touch-up |
CRJ | Chukdong Plant |
KAI (R.O.K.G) | A88MP0007 A88MP0028 A88MP0030 A88MP0031 |
Sandwich + Laminate | KUH | Chukdong · TP Plant |
KPMP200002 KPMP200003 KPMP200009 |
Sandwich + Laminate | KT-100 | Chukdong · TP Plant | |
KDS85MP0009 KDS85MP0010 KDS85MP0326 |
Laminate | FA-50 | Chukdong · TP Plant |
Aluminum Heat Treatment Qualifications
Customers In Korea | Customer | Process Specification | Detail Process | Project |
---|---|---|---|---|
DAaQ (Defense Agency for Technology and Quality) |
IFC-10-244-01 MD | Heat Treatment of 7010-T74 Quenched in Water without Additive |
T-50 FA-50 |
|
IFC-10-241-11 MD | Heat Treatment of the Aluminum Alloys 7075-T73 and 7175-T73 Quenched in Aqueous Solution P.A.G |
|||
KARI (KOREA Aerospace Research Institute) |
WPS-102 | Heat Treatment of Aluminum Alloy Parts | KUH | |
SeAH Aerospace & Defense | AMS2772 | Heat Treatment for Aluminum Alloy Solution Heat treatment Aging Heat treatment Annealing Heat treatment |
||
Stretcher process "S/T" | ||||
Cutting process | ||||
Straightening process | ||||
Customers overseas | Boeing | BAC5602 | Heat Treat of Aluminum Alloys | B787 |
Collins Aerospace (Hamilton Sundstrand) |
AMS2770 | Heat Treat of Aluminum Alloy Parts | B787 | |
HS 454 | Heat Treatment of the Aluminum Alloys | |||
SAFRAN SAFRAN (Messier-Dowty) |
IFC-10-244-01 MD | Heat Treatment of 7010-T74 Quenched in Water without Additive |
A320 A340 A350 A380 |
|
IFC-10-241-11 MD | Heat Treatment of the Aluminum Alloys 7075-T73 and 7175-T73 Quenched in Aqueous Solution P.A.G |