Airframe Structural Components: 1203821-113, 1203927-109, 1204069-151
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1203821-113 1203821113 | 1560-00-262-0023 | Duct Assembly, Compartment | General Characteristics Item Description: Fiberglass, polyester, 23.120 in. lg | Lockheed Martin Corporation (98897) | |
| 1203821-119 1203821119 | 1560-00-262-0023 | Duct Assembly, Compartment | General Characteristics Item Description: Fiberglass, polyester, 23.120 in. lg | Lockheed Martin Corporation (98897) | |
| 1203822-101 1203822101 | 1560-00-262-0024 | Duct Assembly, Compartment | General Characteristics Item Description: Fiberglass, polyester, 18.250 in. lg | Lockheed Martin Corporation (98897) | |
| 1203823-101 1203823101 | 1560-00-262-0025 | Duct, Nonmetallic | General Characteristics Item Description: Fiberglass, polyester, 20.500 in. lg | Lockheed Martin Corporation (98897) | |
| 1203877-101 1203877101 | 1560-00-276-3752 | Duct, Nonmetallic | General Characteristics Item Description: Polyester, glass fabric | Lockheed Martin Corporation (98897) | |
| 1203878-101 1203878101 | 1560-00-262-0026 | Duct Assembly, Copilot | General Characteristics Item Description: Fiberglass, polyester | Lockheed Martin Corporation (98897) | |
| 1203879-101 1203879101 | 1560-00-263-7050 | Duct Assembly, Branched | III End Item Identification: Aircraft model S3A General Characteristics Item Description: Glass fabric, polyester | Lockheed Martin Corporation (98897) | |
| 1203881-101 1203881101 | 1560-00-284-1808 | Duct Assembly, Nonmetallic | III End Item Identification: Aircraft model S-3A General Characteristics Item Description: Glass fabric, polyester, 12.200 in. lg | Lockheed Martin Corporation (98897) | |
| 1203927-105 1203927105 | 1560-00-274-7064 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 alloy 2024 temp T3 fed spec single material response Mounting Opening Shape Style: 1 unthreaded hole | Lockheed Martin Corporation (98897) | |
| 1203927-109 1203927109 | 1560-00-274-7066 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-25014 alloy 2024 T6 fed spec single material response End Item Identification: S-3 aircraft | Lockheed Martin Corporation (98897) | |
| 1203959 | 1560-00-191-7551 | Channel, Aircraft | Aircraft Mission Design Series: C-47 Special Features: U/a: starter brace channel Overall Length: 7.969 inches nominal | Boeing Company, The (18355,88277) | |
| 1203976-101 1203976101 | 1560-00-292-5096 | Manifold, Duct | III End Item Identification: Aircraft model S3A General Characteristics Item Description: Glass fabric polyester | Lockheed Martin Corporation (98897) | |
| 1203979-103 1203979103 | 1560-00-279-8919 | Elbow Assembly, Exhaust | Lockheed Martin Corporation (98897) | ||
| 1203979-105 1203979105 | 1560-01-026-2417 | Duct Assembly, Air Conditioning-H | END Item Identification: Aircraft model S-3A | Lockheed Martin Corporation (98897) | |
| 1203982-101 1203982101 | 1560-00-279-8920 | Adapter, Duct | General Characteristics Item Description: Aluminum alloy | Lockheed Martin Corporation (98897) | |
| 120400-1 1204001 | 1560-00-943-5003 | Windshield Panel, Aircraft | III End Item Identification: Windshield, cockpit CANOPY;CH-53E, MH-53E, 2H53DIIN, S-80M-1, YCH-53E. Aircraft Mission Design Series: H-53 Special Features: Abrasion resistant coating (pilkington arc SS-6590) is to be applied to entire outer surface of outer panel and to be applied to entire inner surface of inner panel; windshield shall be capable of withstanding high temperature setting of 110 degrees f; windshield shall be capable of operating at an ambient air temperature of -56 degrees F. | Sierracin Corporation (12035) | |
| 120400-2 1204002 | 1560-00-943-5004 | Windshield Panel, Aircraft | III End Item Identification: Windsheild panel AIRCRAFT;CH-53E, MH-53E, 2H53DIIN, YCH-53E, S-80M-1 helicopter Aircraft Mission Design Series: H-53 Special Features: Abrision resistant coating (pilkington arc SS-6590) is to be applied to the entire outer and inner surface of the outer and inner panel.windsheild shall be capable of withstanding hih temperature settings of 110 degrees F and capable of operating at ambient temperatures of -65 degrees F. | Sierracin Corporation (12035) | |
| 1204069-149 1204069149 | 1560-00-283-1346 | Step, Fuselage, Aircraft | III End Item Identification: Aircraft model S-3A General Characteristics Item Description: Titanium alloy, MIL-T-9046, comp 6 | Lockheed Martin Corporation (98897) | |
| 1204069-150 1204069150 | 1560-00-283-1347 | Step, Fuselage, Aircraft | III End Item Identification: Aircraft model S-3A General Characteristics Item Description: Titanium alloy, MIL-T-9046, comp 6 | Lockheed Martin Corporation (98897) | |
| 1204069-151 1204069151 | 1560-00-285-8519 | Step, Fuselage, Aircraft | III End Item Identification: Aircraft model S-3A General Characteristics Item Description: Titanium alloy, MIL-T-9046, comp 6 | Lockheed Martin Corporation (98897) |