CAP,PROTECTIVE,DUST AND MOISTURE
Hardware, Commercial
Application: W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); TRIDENT HULL STRUCTURE; AIRCRAFT, C-2A (REPROCURED); AIRCRAFT, SOF (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); SUBMARINE AUXILLARY AND MISCELLANEOUS SYSTEMS; HELICOPTER LANDING SYSTEM, LAMPS MK III; MISSILE, TOMAHAWK; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D)
Technical characteristics
8 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| APGF | DESIGN TYPE | THREADED |
| BZMQ | INSIDE DIAMETER LENGTH | INCHES NOMINAL 0.500 |
| ADAV | OVERALL DIAMETER | INCHES NOMINAL 0.625 |
| MATT | MATERIAL | PLASTIC |
| THDS | THREAD SIZE AND SERIES/TYPE DESIGNATOR | UNF 9 TO 16-18 |
| AAJD | THREAD CLASS | 1B |
| BZMX | ROUND CAP OUTSIDE SURFACE CONDITION | KNURLED |
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); TRIDENT HULL STRUCTURE; AIRCRAFT, C-2A (REPROCURED); AIRCRAFT, SOF (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); SUBMARINE AUXILLARY AND MISCELLANEOUS SYSTEMS; HELICOPTER LANDING SYSTEM, LAMPS MK III; MISSILE, TOMAHAWK; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D) |
Cross-references
11 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| A7208-403 | 55806 |
| NAS832-6 | 80205 |
| NAS832 | 80205 |
| M5501/11-F6 | 81349 |
| MIL-C-5501/11 | 81349 |
| 5340PL0845484 | 9009H |
| CD6 | 95760 |
| CD6 | F2521 |
| CD-6 | D9182 |
| M5501/11F6 | D9182 |
| NAS832-6 | 050R4 |
Supersedes
This item replaces cancelled NIINs 007274775 · 011858603 · 012348459. An older drawing citing one of those numbers resolves here.