FSC 1680 Miscellaneous Aircraft Accessories and Components: 1680-01-038-8286, 1680-01-038-8359, 1680-01-039-0815
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1680-01-038-8286 1680010388286 | 18-62106-1 85720106-601A | Control unit, Aircraft | III End Item Identification: Aircraft model F5F | Northrop Grumman Corp. (22915) Northrop Grumman Systems Corporation (76823) Wyvern Technologies (0C8D3) | |
| 1680-01-038-8314 1680010388314 | 14-70200-505 | Seat, Aircraft Ejection | III Fsc Application Data: Aircraft model F5E Adjustability: Adjustable Adjustment Type: Horizontal and vertical | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 1680-01-038-8359 1680010388359 | 14-50833-501 | Control Assembly, Quadrant | Aircraft Mission Design Series: F-5 | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1680-01-038-8366 1680010388366 | 18-50827-1 | Control Assembly, Quadrant | Aircraft Mission Design Series: F-5 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 1680-01-038-8374 1680010388374 | 18-62103-501 | Control unit, Weapon | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | ||
| 1680-01-038-8389 1680010388389 | 14-50833-1 | Control Assembly, Quadrant | Special Features: Quadrant assembly, throttle control Aircraft Mission Design Series: F-5A/B | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1680-01-038-9004 1680010389004 | 13239 | Swivel, Aircraft Container Valve | III End Item Identification: Aircraft model A10 General Characteristics Item Description: Aluminum alloy, anodize finish, 3.683 in. lg, 2.250 in. W, 1.694 in. min to 1.697 in. max H, as noted machined surfaces 32.0 microinch finish | Pacific Scientific Company (45402, 05167) | |
| 1680-01-038-9005 1680010389005 | 28108 28108-1 | Guide | III End Item Identification: Aircraft model A10 General Characteristics Item Description: Aluminum alloy QQ-A-225/8 comp 6061 cond T6, anodize finish MIL-A-8625 ty 3 cl 1, 1.800 in. O/a lg, 1.738 in.min to 1.740 in. max od, bore 0.896 india 1.675 in. dp, mtg facilities 2 holes 0.188 in. dp tapped 6-32 UNC-3B thdmin dpth 0.125 in. | Rogerson ATS (04192) | |
| 1680-01-038-9006 1680010389006 | 42132-619 42132E619 | Sling, Winch | III End Item Identification: Acft C5A General Characteristics Item Description: Used to position cargo winch P/N 42132R505 fscm 82402 in aircraft | Goodrich Corporation (3HRL4, 00462) Triumph Gear Systems Inc. (82402) | |
| 1680-01-038-9007 1680010389007 | 177529-2 | Bracket | III End Item Identification: Actuator assembly, a/C model C-5A | Curtiss-Wright Controls Inc. (71791) | |
| 1680-01-038-9010 1680010389010 | 178207 | Spring, Gear box | III End Item Identification: Gear box assy a/C model C-5A | Curtiss-Wright Controls Inc. (71791) | |
| 1680-01-038-9012 1680010389012 | 178255 | Carrier, Actuator, Aircraft | III End Item Identification: Aircraft model C5A | Curtiss-Wright Controls Inc. (71791) | |
| 1680-01-038-9014 1680010389014 | 178277 | Carrier, Actuator, Aircraft | III End Item Identification: Aircraft model C5A | Curtiss-Wright Controls Inc. (71791) | |
| 1680-01-038-9088 1680010389088 | 18-70044-1 | Curtain, Blind Flying | III End Item Identification: F-5F acft | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 1680-01-038-9876 1680010389876 | 4F59183-101A | Control Assembly | III End Item Identification: Auxiliary ramp locks General Characteristics Item Description: 4F59183-101A control assy. is made from 42022-13 fscm 78710 | Lockheed Martin Corporation (98897) | |
| 1680-01-038-9877 1680010389877 | 4F59183-102A | Control Assembly | III End Item Identification: Auxiliary ramp locks General Characteristics Item Description: P/N 4F59183-102A control assy. is made from 42022-14 fscm 78710 | Lockheed Martin Corporation (98897) | |
| 1680-01-038-9883 1680010389883 | 69-22496-1 | Sprocket-Brake, Stab. Trim System | III End Item Identification: Next higher part 65-27762 applicable to the E-3A aircraft General Characteristics Item Description: Steel MIL-S-25043 or ams 5644, 25 tooth sprocket W/ american std. chain no. 35 per A.S.A.-B29.1-1957 W/ 3/8 pitch W/ 0.200 roller dia. type 1 or 2, spline pitch dia. 0.8125 csk 120 plus or minus one deg. X 0.88 plus or MINUS0.01 dia., 0.440-0.445 in. W, 8 holes equally spaced 0.50-0.52 dia., 3.19 in. lg, 125 aa microinch fin. on tooth profile, 65 aa microinch fin. on spline tooth surfaces, all other machined surfacesw/ 250 aa microinch fin., sprocket pitch dia. 2.992 | The Boeing Company (81205) | |
| 1680-01-039-0813 1680010390813 | A51K56539-16 A51K56539-11 | Handle, Safety | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy MIL-A-21180, class 2, grade C, type A356, 6.906 in. lg O/a, 0.984 in. H | Northrop Grumman Systems Corporation (61174, 26512) | |
| 1680-01-039-0814 1680010390814 | A51K56539-12 | Handle, Safety Device | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy MIL-A-21180, class 2, grade C, type A356, 6.906 in. lg O/a, 0.984 in. H | Northrop Grumman Systems Corporation (26512, 61174) | |
| 1680-01-039-0815 1680010390815 | A51K56527-11 | Spring Retainer, Female | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy QQ-A-225/6, type 2024, temper 351, 0.940 in. dia, 2.560 in. lg O/a | Northrop Grumman Systems Corporation (61174, 26512) |