The Panel,armor,seat,shoulder, cataloged under National Stock Number 1680-00-975-0200, is classified within Federal Supply Class 1680 (Miscellaneous Aircraft Accessories and Components) of the Aircraft Components and Accessories group. Government technical data includes 1 specification, cited from the U.S. Government catalog. 1 additional reference document (drawings, advisory and superseded references) is recorded in the U.S. Government catalog. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 1680-00-975-0200 |
| Item Name | Panel,armor,seat,shoulder |
| FSC / FSG | 1680 / 16 — Miscellaneous Aircraft Accessories and Components |
| Status | ACTIVE |
| General Characteristics Item Description | ALUMINUM ALLOY QQ-A-250/4 COMP 2024 COMP O,TILE,CERAMIC,HIGH STRENGTHCOMMERCIAL GRADE,CLOTH,NYLON,BALLISTICMIL-C-12369,DIM.,16.600 IN. NOM LG,5.771 IN. NOM O/A W,5.000 IN. NOM W PANEL,1.090 IN. LEFT SIDE WIDTH BENT UPWARD AT 45 DEG ANGLE,TOP AND BOTTOM WIDTH TAPERED 9.0 DEG TOWARD RIGHT,0.735 IN. MAX O/A THICK,0.485 IN. NOM TILE THICKNESS,0.250 IN. NOM ALUMINUM THICKNESS,7 HOLES 0.301 IN. NOM DIA EQUALLY SPACED ON LEFT SIDE 45 DEG ANGLE 0.500 IN. FROM EDGE,NEOPRENE CHANNEL 0.500 IN. DEEP,0.700 IN. INSIDE WIDTH ATTACHED TO TOP,BOTTOM AND RIGHT SIDE,ALUMINUM AND TILE BONDED W/PROSEAL 890B1/2,COMPOSITEE ARMOR WEIGHT 10.5 PSF MAX,USED ON INBOARD SHOULDER PLATE CO-PILOT UH-1B,UH-D IN |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL D — Destroy Item |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | X |
| Reference | Meaning |
|---|---|
| 178042-1 | 3/2 Design control — primary reference U.S. Government activity |
NSN 1680-00-975-0200 is a Panel,armor,seat,shoulder, classified under FSC 1680, Miscellaneous Aircraft Accessories and Components. Status: active.
Key specifications for 1680-00-975-0200: General Characteristics Item Description: ALUMINUM ALLOY QQ-A-250/4 COMP 2024 COMP O,TILE,CERAMIC,HIGH STRENGTHCOMMERCIAL GRADE,CLOTH,NYLON,BALLISTICMIL-C-12369,DIM.,16.600 IN. NOM LG,5.771 IN. NOM O/A W,5.000 IN. NOM W PANEL,1.090 IN. LEFT SIDE WIDTH BENT UPWARD AT 45 DEG ANGLE,TOP AND BOTTOM WIDTH TAPERED 9.0 DEG TOWARD RIGHT,0.735 IN. MAX O/A THICK,0.485 IN. NOM TILE THICKNESS,0.250 IN. NOM ALUMINUM THICKNESS,7 HOLES 0.301 IN. NOM DIA EQUALLY SPACED ON LEFT SIDE 45 DEG ANGLE 0.500 IN. FROM EDGE,NEOPRENE CHANNEL 0.500 IN. DEEP,0.700 IN. INSIDE WIDTH ATTACHED TO TOP,BOTTOM AND RIGHT SIDE,ALUMINUM AND TILE BONDED W/PROSEAL 890B1/2,COMPOSITEE ARMOR WEIGHT 10.5 PSF MAX,USED ON INBOARD SHOULDER PLATE CO-PILOT UH-1B,UH-D IN. 1 specification is documented in the U.S. Government catalog.
No hazard code in the DLA record (HMIC N). Hazard information on this page is shown exactly as it appears in the DLA record.
NSN 1680-00-975-0200 has DEMIL Code D. Demilitarization may be required before disposal or transfer to non-military entities.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-16.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.