Cancelled FSC 1650 NSNs
| Cancelled NSN | Replacement NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1650-00-000-0128 000000128 | 1650-01-065-7768 | No Item Name Available | III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems Special Features: Used on model 3U3151-5E servoactuator; T.O.9H2-5-261-4 Design Characteristics: Double acting single cylinder | Boeing Company, The (76301) GE Aviation Systems LLC (60029) | |
| 1650-00-001-1735 000011735 | 1650-00-570-0216 | No Item Name Available | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: 0.431 in. min, 0.435 in. max od | Eaton Aerospace LLC () | |
| 1650-00-001-1742 000011742 | 1650-00-570-0215 | No Item Name Available | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: 1.500 in. min, 1.502 in.max od, 0.0673 in. min, 0.0677 in.max O/a H | Eaton Aerospace LLC (62983) | |
| 1650-00-003-1482 000031482 | 1650-00-467-6155 | No Item Name Available | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, comp 2024, temper T351, 4.880 in. min, 4.890 in. max od | Northrop Grumman Systems Corporation (26512,61174,79RG9) | |
| 1650-00-003-1489 000031489 | 1650-00-922-1439 | No Item Name Available | III End Item Identification: Grumman model F-14A aircraft General Characteristics Item Description: Cres, irregular SHAPE;4.576 in.O/a LG;1.125 in.bore | Kell-Strom Tool International Inc. (75245) Northrop Grumman Systems Corporation (26512,61174,79RG9) | |
| 1650-00-003-3714 000033714 | 1650-01-253-5836 | No Item Name Available | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Allied-Signal Inc. (77068) Honeywell International Inc. (59364) Moog Inc. (0ZWK8) Northrop Grumman Systems Corporation (26512,61174,79RG9) | |
| 1650-00-004-2878 000042878 | 1650-00-433-8797 | No Item Name Available | III End Item Identification: Acft model F-14A General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, comp 2024, temper T351, 3.818 in. min, 3.828 in. max od | Northrop Grumman Systems Corporation (26512,61174,79RG9) | |
| 1650-00-004-3739 000043739 | 1650-00-181-9344 | No Item Name Available | III Fsc Application Data: Hydraulic system, acft Material: Plastic filtering medium plastic seal Design Type: Nonreusable | Pall Aeropower Corporation (18350) Pall GMBH (C0202) PTI Technologies Inc. (05228) | |
| 1650-00-004-9776 000049776 | 1650-01-050-8682 | No Item Name Available | III End Item Identification: TA-4J aircraft | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-004-9777 000049777 | 1650-01-047-7250 | No Item Name Available | III End Item Identification: TA-4J aircraft | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-004-9778 000049778 | 1650-01-052-7023 | No Item Name Available | III End Item Identification: Aircraft model A-4 | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-004-9779 000049779 | 1650-01-047-7248 | No Item Name Available | III End Item Identification: TA-4J aircraft | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-004-9780 000049780 | 1650-01-047-7249 | No Item Name Available | III End Item Identification: TA-4J aircraft | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-004-9781 000049781 | 1650-01-047-7251 | No Item Name Available | III End Item Identification: TA-4J aircraft | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-005-3695 000053695 | 1650-01-154-1596 | No Item Name Available | III End Item Identification: Aircraft model F-4 | Hamilton Sundstrand Corporation (99167) | |
| 1650-00-006-1019 000061019 | 1650-00-434-0666 | No Item Name Available | III End Item Identification: C-5 a/b main landing gear Special Features: Steel MIL-S-6709, comp a, cadmium plate external surface QQ-P-416, ty 1, class 2, heat treat MIL-H-6875 case depth of 0.013 in.to 0.018 in.case hardness 92 min.on rockwell 15N scale, 4 mtg holes MS33649-8, tap drill 29/32 in. deep, 3/4-16 unjf 3B thrd;reference data LITERATURE:T.O.9H10-3-48-3;FSC application data:aircraft hydraulic, vacuum, deicing system | Parker-Hannifin Corporation (59211,93835) | |
| 1650-00-006-7933 000067933 | 1650-01-063-0562 | No Item Name Available | III End Item Identification: Aircraft model F-14A | Northrop Grumman Systems Corporation (26512,61174,79RG9) | |
| 1650-00-008-5435 000085435 | 1650-00-476-9483 | No Item Name Available | III End Item Identification: Acft model F-14A General Characteristics Item Description: Cres, AMS5659, 1.477 in. O/a lg, 1.188 in. od | Northrop Grumman Systems Corporation (26512,61174,79RG9) | |
| 1650-00-008-6454 000086454 | 1650-01-027-0237 | No Item Name Available | III End Item Identification: Acft model T-39 | Sabreliner Corp. (32184) Sabreliner Corporation (0ESK8) | |
| 1650-00-010-0395 000100395 | 1650-00-133-6270 | No Item Name Available | Design Characteristics: Single acting twin cylinder Bore Diameter: 1.6865 inches minimum 1.6877 inches maximum Extended Length: 39.750 inches nominal | The Boeing Company (77272) |