Cancelled FSC 2840 NSNs
| Cancelled NSN | Replacement NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840-00-001-8370 000018370 | 2840-00-508-9137 | No Item Name Available | III End Item Identification: Engine, aircraft, turbofan, model TF39-GE1A | General Electric Company (07482) | |
| 2840-00-003-0831 000030831 | 2840-01-215-3554 | No Item Name Available | III End Item Identification: Acft eng J85-GE-21 Criticality Code Justification: AGAV | General Electric Company (99207) | |
| 2840-00-003-9568 000039568 | 2840-01-103-5056 | No Item Name Available | III End Item Identification: Acft eng J85 Special Features: 1.465 min 1.47 max in. lg; 0.221 in. w; 0.06 min 0.07 max in. dia of two places Material: Steel overall | General Electric Company (99207) Sterling Machine Company Inc. (03983) White Engineering Surfaces (2M223) | |
| 2840-00-004-4111 000044111 | 2840-00-808-3885 | No Item Name Available | III End Item Identification: UH-1 turbine engine (T-53) III Part Name Assigned By Controlling Agency: Diffuser assembly exhaust | Akron Tent and Awning Co. (91457) Honeywell International Inc. (99193) | |
| 2840-00-006-1077 000061077 | 2840-00-208-3347 | No Item Name Available | III End Item Identification: Engine model TF41 General Characteristics Item Description: Cres, ams 5512, 0.043-0.053 in. thk bra cket material, cres, AMS5646 spacer material, 1.3093 in. overall W, 45 deg angle, 0.640 in. holecenter one end to hole center other end III Fsc Application Data: Aircraft jet engine | Allison Transmission Inc. (73342) | |
| 2840-00-006-4381 000064381 | 2840-01-120-1965 | No Item Name Available | III End Item Identification: Acft eng TF41 Criticality Code Justification: AGAV Engine Section Location: High pressure compressor | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-006-5096 000065096 | 2840-00-181-0280 | No Item Name Available | III End Item Identification: J-85 aircraft engine General Characteristics Item Description: Steel, B50T1181, general electric co, 125 aa microinch surfacefinish rating | General Electric Company (99207) | |
| 2840-00-006-5101 000065101 | 2840-01-216-4769 | No Item Name Available | III End Item Identification: Acft eng J85-GE-21 Criticality Code Justification: Matt and feat and agav Special Features: Matl ams 5608 | Barlow Metal Stamping Inc. (9M944) Berkshire Manufactured Products Inc. (02653) Bristol Aerospace LTD (35951) General Electric Company (99207) | |
| 2840-00-006-5121 000065121 | 2840-01-090-7312 | No Item Name Available | Criticality Code Justification: AGAV End Item Identification: Acft eng J85-GE-21A Diameter: 15.480 inches nominal | General Electric Company (99207) | |
| 2840-00-006-5855 000065855 | 4810-00-906-2326 | No Item Name Available | Reference Number Differentiating Characteristics: As differentiated by source control dwg no. 1-300-194 Style Designator: A1 straight thru Voltage in Volts and Current Type: 18.0 dc and 30.0 dc | Hamilton Sundstrand Corporation (55820,99167) Honeywell International Inc. (99193) Whittaker Controls Inc. (79318) | |
| 2840-00-008-6438 000086438 | 2840-01-120-1965 | No Item Name Available | III End Item Identification: Acft eng TF41 Criticality Code Justification: AGAV Engine Section Location: High pressure compressor | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-008-8524 000088524 | 1560-00-954-7752 | No Item Name Available | III End Item Identification: Aircraft model F-4C III Supplementary Features: Functional description:bleed air duct, manifold | Boeing Company, The (76301) Senior Operations LLC (98769) | |
| 2840-00-009-0680 000090680 | 2840-01-019-8131 | No Item Name Available | III End Item Identification: Engine, acft, turbofan, model no. TF39-GE-1A General Characteristics Item Description: Cres ams 5510, 2.658 in. min, 0.766 in. max lg, 0.057 in. min, 0.069 in. max thk, 0.098 in. min, 0.102 in. max dia 4 mtg holes | General Electric Company (07482) | |
| 2840-00-009-9412 000099412 | 2840-00-551-6677 | No Item Name Available | III End Item Identification: TF39GE1A Criticality Code Justification: AGAV Engine Section Location: Compressor | General Electric Company (07482) | |
| 2840-00-009-9421 000099421 | 2840-01-218-0210 | No Item Name Available | III End Item Identification: Acft eng TF39-GE-1C Criticality Code Justification: AGAV Engine Section Location: Compressor | General Electric Company (07482) | |
| 2840-00-011-0679 000110679 | 2840-00-962-2550 | No Item Name Available | III End Item Identification: T-56 aircraft engine Criticality Code Justification: CZCJ Engine Section Location: Compressor | Allison Transmission Inc. (73342) General Motors Corp. (24617) Rolls-Royce Corporation (63005) | |
| 2840-00-011-0684 000110684 | 2840-01-142-5637 | No Item Name Available | Criticality Code Justification: AGAV Engine Section Location: Accessory gearbox Material: Steel overall | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-011-0691 000110691 | 2840-00-910-9160 | No Item Name Available | III End Item Identification: T-56 aircraft engine Criticality Code Justification: AGAV | Allison Transmission Inc. (73342) Rolls-Royce Corporation (63005) | |
| 2840-00-012-3268 000123268 | 5365-00-134-4871 | No Item Name Available | III Part Name Assigned By Controlling Agency: Ring, retaining | Honeywell International Inc. (99193) | |
| 2840-00-012-7145 000127145 | 2840-00-869-1830 | No Item Name Available | Criticality Code Justification: RDAL End Item Identification: Acft eng J85 Reference Data and Literature: T.O. 2J-J85-64, fig 10, ind 23 | General Electric Company (99207) Kerns Manufacturing Corp. (93596) |