| MRC |
Requirement Statement |
Characteristics |
| AGAV |
III END ITEM IDENTIFICATION |
FUEL NOZZLE ASSY FOR TF33-7/-100 AIRCRAFT ENGINE |
| MATT |
MATERIAL |
STEEL CORROSION RESISTING |
| SUPP |
III SUPPLEMENTARY FEATURES |
0.836 - 0.846 IN. LG 0.158 - 0.159 IN. OD ONE END,0.308 - 0.310 IN. OD OTHER END 0.1545 IN. DP |
| AXMY |
SHOCK/SPRING MOUNTING METHOD |
HELICAL SPRING,P/N 267627,SEATS IN COUNTERBORE 0.220 - 0.225 IN.,0.035 - 0.045 IN. DP AT END OF SUPPORT |
| AXMX |
SUPPORTING OBJECT/SURFACE ATTACHMENT METHOD |
INTEGRAL PART OF NOZZLE SET ATTACHED TO FUEL MANIFOLD ASSY |
