Airframe Structural Components: GS13AC5, GS517F2, GSR602-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| GS13AC5 | 1560-00-067-8376 | Sealing Strip, Cabin | III End Item Identification: OV-1B, OV-1C, OV-1D, RV-1D acft | Northrop Grumman Systems Corporation (26512) | |
| GS15693-2 GS156932 | 1560-01-522-0443 | Rod Assembly, Cover, Aircraft | III Supplementary Features: Dmwr 55-2915-340, B-24 29 | Hamilton Sundstrand Corporation (73030) | |
| GS18422 | 1560-00-611-9354 | Panel, Structural, Aircraft | Overall Length: 28.120 inches nominal Overall Width: 19.649 inches nominal | Lucent Technologies Inc. (06KW9) | |
| GS2100-060-0750-SC-50 GS21000600750SC50 | 1560-01-528-0319 | Seal GS2100-060-0750-SC-50, Aircr | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| GS2100-060-2000-SC-50 GS21000602000SC50 | 1560-01-528-0321 | Shielding Gasket, Aircraft | III End Item Identification: UH1 aircraft Criticality Code Justification: AGAV | Bell Helicopter Textron Inc. (97499) | |
| GS24594-1 GS245941 | 1560-01-530-3660 | Oil Fill, Drain set | III End Item Identification: E2C hawkeye aircraft | Hamilton Sundstrand Corporation (73030) | |
| GS25D1 | 1560-00-006-4657 | Support, Mount | III End Item Identification: Aircraft model F-14 | Northrop Grumman Systems Corporation (26512) | |
| GS25D2 | 1560-00-006-4658 | Support, Mount | III End Item Identification: A-6 aircraft General Characteristics Item Description: 2.186 in. lg, 0.500 in. W, 0.255 in. H | Northrop Grumman Systems Corporation (26512) | |
| GS25E1 | 1560-00-004-3065 | Support, Harness | III End Item Identification: F-15 aircraft General Characteristics Item Description: Polyamide GM4104BFA fscm 26512, 0.750 in. lg, 0.938 in. W, 0.500 in. thk | Northrop Grumman Systems Corporation (26512) | |
| GS25E3 | 1560-00-004-3066 | Support, Harness | III End Item Identification: F-14 aircraft General Characteristics Item Description: Polyamide GM4104BFA fscm 26512, 0.750 in. lg, 0.938 in. W, 0.500 in. thk | Northrop Grumman Systems Corporation (26512) | |
| GS25E5 | 1560-00-004-3067 | Support, Harness | III End Item Identification: F-14 aircraft General Characteristics Item Description: Polyamide GM4104BFA fscm 26512, 1.125 in. lg, 0.938 in. W, 0.500 in. thk | Northrop Grumman Systems Corporation (26512) | |
| GS25E7 | 1560-00-005-8088 | Support, Harness | General Characteristics Item Description: Polyamide GM4104BFA fscm 26512, 0.500 in. lg, 0.938 in. W, 0.500 in. thk | Northrop Grumman Systems Corporation (26512) | |
| GS25E9 | 1560-00-004-3068 | Support, Harness | III End Item Identification: F-14 aircraft General Characteristics Item Description: Polyamide GM4104BFA fscm 26512, 1.750 in. lg, 0.938 in. W, 0.500 in. thk | Northrop Grumman Systems Corporation (26512) | |
| GS517F2 | 1560-01-283-2495 | Fire Shield, Coupling | General Characteristics Item Description: Reinforced fiberglass cloth, thermo-chem 6-88, johns-manville; truncated conical shape; 5.240 in. major dia; 2.650 in. minor dia; 4.000 in. h; expansion slits on small end 1.250 in. lg; accomodates 3.000 in. dia tube; constant operating temperature range 204.0 deg centigrade | Northrop Grumman Systems Corporation (26512) | |
| GS875Y2 | 1560-01-223-0013 | Strip, Lighting | Northrop Grumman Systems Corporation (26512) | ||
| GS875Y3 | 1560-01-223-3128 | Strip, Lighting | Northrop Grumman Systems Corporation (26512) | ||
| GSR435-12BP GSR43512BP | 1560-00-181-3447 | Panel, Structural, Aircraft | Northrop Grumman Systems Corporation (26512) | ||
| GSR451-14 GSR45114 | 1560-00-348-7025 | Parts kit, Aircraft Engine Build- | End Item Identification: Aircraft model HU16 | Northrop Grumman Systems Corporation (26512) | |
| GSR455-3 GSR4553 | 1560-00-564-4794 | Pylon, Aircraft | Aircraft Mission Design Series: HU-16 | Northrop Grumman Systems Corporation (26512) | |
| GSR602-11 GSR60211 | 1560-00-523-4613 | Wing, Assy | Northrop Grumman Systems Corporation (26512) |