Airframe Structural Components: 3-12331-77B, 3-12392-6, 3-12392-9
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3-12331-77B 31233177B | 1560-00-905-4456 | Firewall, Fuselage | III End Item Identification: Aircraft model F5 General Characteristics Item Description: Nickel-chromium alloy, AMS5542 cond a | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12331-8 3123318 | 1560-00-891-3590 | Firewall, Fuselage | III End Item Identification: Aircraft model F5 General Characteristics Item Description: Titanium, AMS4901 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 312358 | 1560-00-047-5064 | Fitting, Accessory Drain | General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, 1.840 in. lg, 0.438-20 unf 3A thd one end, 0.196 in. min, 0.203 in. max dia hole thru flange 4 places | Lockheed Martin Corporation (98897) | |
| 3-12364-1 3123641 | 1560-00-715-3115 | Blanket Assembly, Firewall | III End Item Identification: Aircraft model T38 General Characteristics Item Description: Steel, MIL-S-6721 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12364-2 3123642 | 1560-00-897-7185 | Blanket Assembly, Firewall | III End Item Identification: Aircraft model T38 General Characteristics Item Description: Steel, MIL-S-6721 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12387-1 3123871 | 1560-00-964-0843 | Beam, Horizontal Stabilizer | III End Item Identification: Aircraft model T38 General Characteristics Item Description: Magnesium alloy, QQ-M-56 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12389-2 3123892 | 1560-01-333-7332 | Fitting, Structural Component, Air | Aircraft Mission Design Series: T-38 Material: Aluminum Aircraft Location: Upper longeron | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12389-3 3123893 | 1560-01-337-3468 | Fitting, Structural Component, Air | Aircraft Mission Design Series: T-38 Special Features: T.O. 1T-38A-4-11 Material: Aluminum alloy | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12389-4 3123894 | 1560-01-335-9666 | Fitting, Structural Component, Air | Aircraft Mission Design Series: T-38 Material: Aluminum alloy Aircraft Location: Upper longeron | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12391-1 3123911 | 1560-00-908-1798 | Ejector, Aft Fuselage | General Characteristics Item Description: Cres, AMS5536 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12391-3 3123913 | 1560-00-829-4327 | Fuselage Section | Aircraft Mission Design Series: T-38 Special Features: Manufacture suggested name: ejector-aft fuselage; sheet hastelloy; C/o: -5 stiffeners and -13 shroud Material: Nickel alloy | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12391-4 3123914 | 1560-01-486-6677 | Fuselage Section | Aircraft Mission Design Series: T-38 Special Features: Manufactured suggest name: (ejector-aft fuselage); sheet hastealloy; same as -3 except where ecn 01A0449 is applied using 3 seperate -21 shroud components; C/O -5 stiffeners and -21 shroud Material: Nickel alloy | Aerometals Inc. (32664) Aeroparts Manufacturing & Repair Inc. (15992) Intertrade Aviation Corp. (8T729) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392 312392 | 1560-00-966-9870 | Former, Aircraft | Aircraft Mission Design Series: T-38 Special Features: This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition Material Thickness: 0.025 inches nominal | Derco Aerospace Inc. (8X044) | |
| 3-12392-11 31239211 | 1560-00-966-9866 | Doubler, Former, Acft | General Characteristics Item Description: Steel, AMS5536, 23.000 in. lg, 15.000 in. W, 0.025 in. matl thk | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392-13 31239213 | 1560-00-966-9862 | Doubler, Former, Acft | General Characteristics Item Description: Steel, AMS5536, 16.000 in. lg, 8.000 in. W, 0.025 in. matl thk | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392-5 3123925 | 1560-00-966-9869 | Former, Aircraft | Aircraft Mission Design Series: T-38 Material Thickness: 0.025 inches nominal | Derco Aerospace Inc. (8X044) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392-6 3123926 | 1560-00-966-9870 | Former, Aircraft | Aircraft Mission Design Series: T-38 Special Features: This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition Material Thickness: 0.025 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392-7 3123927 | 1560-00-966-9867 | Doubler, Former, Acft | General Characteristics Item Description: Steel, AMS5536, 23.000 in. lg, 13.000 in. W, 0.025 in. matl thk | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392-8 3123928 | 1560-00-966-9868 | Doubler, Former, Acft | General Characteristics Item Description: Steel, AMS5536, 23.000 in. lg, 13.000 in. W, 0.025 in. matl thk | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-12392-9 3123929 | 1560-00-966-9861 | Plate, Structural, Aircraft | Aircraft Mission Design Series: T-38 Special Features: Matl-sht hastelloy X-nickel base steel Aircraft Location: Former installatin, cant fuselage | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |