Airframe Structural Components: 3-74244-3, 3-74271-1, 374314-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3-74244-3 3742443 | 1560-00-977-9808 | Arm, Operating | General Characteristics Item Description: Steel, 1.2415 in. lg, 0.563 in. O/a W, 0.650 in. H, mtg hole 0.203 in.dia | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74245-1 3742451 | 1560-00-977-9809 | Arm Assembly, Flap | General Characteristics Item Description: Aluminum alloy, QQ-A-250/12 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74245-2 3742452 | 1560-00-977-9810 | Arm Assembly, Flap | General Characteristics Item Description: Aluminum alloy, QQ-A-250/2 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74262-3 3742623 | 1560-00-326-7787 | Arm, Flap Position | Special Features: This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition General Characteristics Item Description: Aluminum alloy, QQ-A-200/11, 7075-T73511, 1.810 in. lg, 1.150 in. W, 0.540 in. H, s shaped Criticality Code Justification: FEAT | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 37-4265-1L 3742651L | 1560-01-313-8721 | Bracket, Structural Component, Air | Side for Which Designed: Left side Aircraft Location: Main landing gear wheel well beam Aircraft Mission Design Series: C-130 | A and M Aerospace Inc. (6Z800) | |
| 374266-1 3742661 | 1560-00-626-9630 | Box Assembly, Junction | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
| 374267-2 3742672 | 1560-00-626-9629 | Cover Assembly, Junction box | III End Item Identification: Aircraft model C-130 | Lockheed Martin Corporation (98897) | |
| 37427 | 1560-01-212-9532 | Body, Transfer Modul | III End Item Identification: UH-60, rotary wing aircraft | Eaton Corporation (99643) | |
| 3-74271-1 3742711 | 1560-00-987-6115 | Support, Stroke Limiter | III End Item Identification: Acft model T38 General Characteristics Item Description: Aluminum alloy, QQ-A-250/11 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 374291-1 3742911 | 1560-01-446-2319 | Support, Structural Component, Air | III End Item Identification: C130 hercules aircraft Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 374297-3 3742973 | 1560-01-393-6167 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Aluminum alloy 2024 Aircraft Location: Cockpit; co-pilots side | Lockheed Martin Corporation (98897) | |
| 374298-2 3742982 | 1560-00-672-6483 | Cap, Receptacle Outlet | III End Item Identification: Aircraft model C-130 General Characteristics Item Description: 3.320 in. lg | Lockheed Martin Corporation (98897) | |
| 3-74301-5 3743015 | 1560-00-868-2118 | Bracket, Travel Limiter | III End Item Identification: T38A aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74303-1 3743031 | 1560-00-961-6770 | Bracket, Pulley | General Characteristics Item Description: Magnesium alloy AZ91C, QQ-M-56 T6 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74304-1 3743041 | 1560-00-967-2411 | Pulley Assembly, Rudder | General Characteristics Item Description: Aluminum alloy 2024-0, QQ-A-250/5, 0.040 in. material thk, 3.430 in. lg, 2.068 in. W, 2.500 in. deep | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74305-3 3743053 | 1560-00-966-5271 | Pulley Assembly, Rudder | General Characteristics Item Description: Aluminum alloy 2024-0, QQ-A-250/5, 0.063 in. material thk, 77.0 deg bracket angle | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74309-1 3743091 | 1560-00-987-6158 | Tube, Guide, Spring | General Characteristics Item Description: Cres, MIL-T-6845, 3.140 in. O/a lg | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74312-3 3743123 | 1560-01-038-5001 | Arm-Trunnion | III End Item Identification: Next assy no. 18-74001, F5F acft General Characteristics Item Description: Keyway per MS35756-2 at 10 deg 30MIN, to improve clearance between travel limiter crank arm and housing | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-74312-5 3743125 | 1560-01-038-5001 | Arm-Trunnion | III End Item Identification: Next assy no. 18-74001, F5F acft General Characteristics Item Description: Keyway per MS35756-2 at 10 deg 30MIN, to improve clearance between travel limiter crank arm and housing | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 374314-1 3743141 | 1560-00-626-9627 | Panel Assy, Ice Dete | Lockheed Martin Corporation (98897) |