Approvals / Certificates |
The exceptional quality requirements of the aerospace industry, to ensure optimal product quality and reproducibility, has necessitated that the supplying companies be extensively approved. The approvals take place at national level, the EN 9100 and Nadcap approvals for instance, and are reinforced by the individual company approvals. In most cases the company approvals, which primarily evaluate the quality management systems, are supported by the material qualification programmes in which the ultimate quality of the individual material grades is accessed.
A list of some of the major quality approvals which are held by the Deutsche Edelstahlwerke can be seen as below |
• Airbus Germany |
• Airbus UK |
• EADF Aerospatiale Matra Airbus |
• Rolls Royce |
• Eurocopter |
• Pfalzflugzeugwerke |
• Turbomeca |
• Singapore Technology Centre |
• Bombardier / Shorts |
• Pratt & Whitney |
• Lord Aerospace |
• Westland Helicopter |
• Hawker Beechcraft |
• BAE Systems |
• Messier Dowty |
• Liebherr |
• GKN Aerospace |
• SKF Aerospace |
• Premium Aerotech |
• Aircelle* |
• Goodrich* |
• Nadcap (AS7102) |
• ISO 9001:2000 |
• EN 9100:2003 |
• DIN EN ISO/IEC 17025:2005 |
|
* Material approval |
|
|
|
Our product range for aerospace grades (steel)
Chemical composition
Material No. |
Short Name |
Nat. |
Specification |
Designation |
1.3505 |
100 Cr6 |
USA |
AMS 6440 |
|
1.4006 |
X12Cr13 |
D |
DIN/EN 10088-3 |
|
|
|
AISI 410 |
|
|
USA |
AMS 5613 |
|
1.4014 |
X20Cr13 |
D |
LW 1.4014 |
|
1.4044 |
|
GB |
BS 3S62 |
S 62 |
|
|
WL. 1.4044 Part 1 |
|
X22CrNi17 |
D |
DIN 65038 |
1.4044; 1.4044 |
1.4418 |
|
F |
AIR 9160/9161 |
Z15CN17.03 |
|
|
BS 7S80 |
7S80 |
|
GB |
BS 5S100/1993 |
|
X4CrNiMo16-5-1 |
F |
AIR 9160/9161 |
Z8CND 17.04 |
1.4542 |
X5CrNiCuNb16-4 |
USA |
AMS 5643 |
AMS 5643 |
1.4544 |
|
F |
AIR 9160 |
|
1.4545 |
X5CrNiCuNb15-5 |
D |
WL. 1.4545 Part 1 |
1.4545 |
1.4546 |
|
USA |
AMS 5659 Type I |
AMS 5659 |
|
USA |
AMS 5659 Type II |
AMS 5659 |
X5CrNiNb18-10 |
D |
WL. 1.4546 Part 1 |
1.4546 |
1.4548 |
|
|
BS 2S130 |
|
|
GB |
BS 5S100/1993 |
2S130 |
|
USA |
AMS S5646 |
AMS S5646 |
X5CrNiCuNb17-4-4 |
D |
WL. 1.4548 Part 1 |
1.4548 |
1.4939 |
|
USA |
AMS 5622 |
AMS 5622 |
|
X12CrNiMoV12-3 |
D |
WL. 1.4939 |
1.4939 |
1.5815 |
|
F |
AIR 9160 |
|
|
GB |
|
S151 |
|
USA |
AMS 5719 |
Jethete M 152 |
36CrNi6-4 |
F |
AIR 9160/9161 |
35NC6 |
1.6562 |
40NiCrMo8-4 |
USA |
AISI 4340 |
AMS 6414 |
1.6657 |
14NiCrMo13-4 |
F |
AIR 9160/9161 |
16NCD13 |
1.6722/23 |
|
USA |
SAE 9310 |
|
|
USA |
AMS 6265 |
|
|
F |
16 NCD 17 |
|
|
|
D |
ZFNL9207 |
|
|
GB |
BS S156/S82 |
|
32NiCrMo13-4 |
GB |
BS 2S97+ S154+S140 |
2S97/S154/S140 |
1.6745 |
|
|
BS 5S100/1993 |
|
40NiMoCr10-5 |
GB |
BS 2S98+5S99 |
2S98/5S99 |
1.6747 |
|
|
BS 5S100/1993 |
|
30NiCrMo16-6 |
F |
AIR 9160/9161 |
30NCD16, 35NCD16 |
1.6928 |
41SiNiCrMoV7-3 |
USA |
AMS 6419 |
300 M |
1.7220 |
34CrMo4 |
F |
AIR 9160/9161 |
35CD4 |
1.7223 |
41CrMo4 |
D |
SEL 7223 |
|
1.7734 |
|
USA |
SAE 4120 (AMS 6382) |
|
15CrMoV6-9 |
D |
WL 1.7734 |
1.7734 |
1.7765 |
|
F |
AIR 9160/9161 |
15CDV6 |
32CrMoV12-10 |
D |
WL 1.7765 |
|
1.8515 |
|
F |
AIR 9160 Bl. 89 |
32CDV13 |
|
31CrMo12 |
D |
SEL 8515 |
|
1.8523 |
|
GB |
BS 4S106 |
BS 4S106 |
|
39CrMoV13-9 |
D |
SEL 8523 |
|
|
|
F |
|
40CDV12 |
|
|
GB |
BS 3S132 |
3S132 |
back to top |
Several common aerospace grades are available from stock (steel)
Diameterin mm |
1.4044.6 (S80) |
1.4546.9 (S130) |
1.4545.4
15-5PH (H1025) |
1.4548.4
17-4PH (H1025) |
1.4542.9
17-4PH Cond. A |
6 |
|
|
Ο |
Ο |
|
8 |
|
Ο |
Ο |
Ο |
|
12.7 |
|
Ο |
|
|
|
16 |
|
Ο |
Ο |
Ο |
Ο |
20 |
Ο |
+ |
Ο |
Ο |
|
22 |
|
+ |
Ο |
Ο |
|
22.23 |
Ο |
|
|
|
|
25 |
Ο |
+ |
Ο |
Ο |
+ |
28 |
|
+ |
|
|
|
30 |
|
+ |
Ο |
Ο |
+ |
32 |
Ο |
+ |
Ο |
Ο |
|
35 |
|
|
|
|
+ |
36 |
Ο |
|
Ο |
Ο |
|
40 |
Ο |
+ |
Ο |
Ο |
+ |
44.45 |
|
+ |
|
|
|
45 |
|
+ |
Ο |
Ο |
+ |
47.63 |
|
+ |
|
|
|
50 |
Ο |
+ |
Ο |
Ο |
+ |
55 |
|
+ |
+ |
+ |
+ |
60 |
Ο |
+ |
+ |
+ |
+ |
65 |
|
|
Ο |
Ο |
|
70 |
Ο |
+ |
Ο |
Ο |
+ |
76.2 |
|
+ |
|
|
|
80 |
|
+ |
Ο |
Ο |
+ |
82.55 |
+ |
+ |
|
|
|
85 |
|
|
+ |
+ |
|
88.9 |
+ |
+ |
|
|
|
90 |
|
|
Ο |
Ο |
+ |
95 |
|
|
+ |
+ |
|
95.25 |
+ |
+ |
|
|
|
100 |
|
+ |
Ο |
Ο |
+ |
101.6 |
+ |
+ |
|
|
|
105 |
|
|
+ |
+ |
|
107.95 |
+ |
+ |
|
|
|
110 |
|
|
+ |
+ |
+ |
114.3 |
+ |
+ |
|
|
|
115 |
|
|
+ |
+ |
|
120 |
|
|
+ |
+ |
+ |
120.7 |
+ |
+ |
|
|
|
125 |
|
+ |
|
|
|
130 |
|
|
+ |
+ |
+ |
140 |
|
|
+ |
+ |
+ |
150 |
|
|
|
|
+ |
155 |
|
|
+ |
+ |
|
160 |
|
|
+ |
+ |
+ |
170 |
|
|
+ |
+ |
|
180 |
|
|
|
|
+ |
190 |
|
|
+ |
+ |
|
200 |
|
|
+ |
+ |
+ |
|
o = peeled/drawn bright bar LN 668 + = LN 1013 rough peeled |
back to top |
|
Sheets thickness < 7 mm |
Plates(thickness ≤ 7 mm) |
Grade |
2024 |
5086 |
2024 |
2618 A |
7010 |
7175 |
Temper |
T 3 |
T 3 Clad |
H 111 |
T 351 |
T 851 |
T 7451 |
T 7351 |
Specification |
|
AIR
ASNA
QQA
WL
DAN
CR
AIMS |
9048
3010
250 / 4
-
-
-
- |
9048
3012
250 / 5
-
-
-
- |
9048
3044
-
-
-
-
- |
9048
3011
250 / 4
3.1354
422
1.1.0.36
03.02.004.02 |
9048
3355
-
-
-
-
- |
-
3098
-
-
-
-
- |
9048
3050
250 / 12
3.4364
422
-
- |