| SPCL |
SPECIAL TEST FEATURES |
PROOF & LEAK TEST AT 113 PSIG |
| ABHP |
OVERALL LENGTH |
33.790 INCHES NOMINAL |
| ABMK |
OVERALL WIDTH |
7.250 INCHES NOMINAL |
| CZDJ |
AIRCRAFT LOCATION |
WING, LEADING EDGE |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
DMS 1563 MFR REF SINGLE MATERIAL RESPONSE |
| BWJF |
SIDE FOR WHICH DESIGNED |
LEFT SIDE |
| ABPX |
MATERIAL THICKNESS |
0.016 INCHES MINIMUM |
| SUPP |
SUPPLEMENTARY FEATURES |
MAX OPERATING PRESSURE 48 PSIG; MAX TEMPERATURE 450 DEG F |
| MATT |
MATERIAL |
STEEL CORROSION RESISTING |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
C-17A |
| FEAT |
SPECIAL FEATURES |
DUCT ASSY,FLEXIBLE,ANTI-ICING, LEADING EDGE; C/O -20 WELD ASSY, 8 SQ FT -5 SILICONE BOUND FIBER GLASS BATTING, 5 SQ FT -7 SILICONE COATED GLASS CLOTH COVER & 2 FT X 1" -11 GLASS FABRIC PRESSURE SENSITIVE TAPE; -20 WELD ASSY INCLUDES -3, -15 & -17 DUCTS, -13 & -23 GUSSETS, -21 DOUBLER,2 EA 17P8N1021-1 BUSHINGS, 2 EA 10252-266 FLEXIBLE JOINTS, 7D0072-300FSC & 7D0072-300MSC FLANGES; NHA 17N6N0691 |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE |