Airframe Structural Components: 3P34804-101, 3P40024-115, 3P40024-121
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P34804-101 3P34804101 | 1560-00-075-8994 | Bracket, Pulley Support Engine Co | General Characteristics Item Description: Steel, AMS5355B, 2.810 in. H | Aero Components Inc. (59213) Falcon Manufacturing Corp. (0HM72) Lockheed Martin Corporation (98897) | |
| 3P35003-101 3P35003101 | 1560-01-345-3333 | Funnel, Drain | III End Item Identification: Acft C-141 General Characteristics Item Description: C/O 1 funnel, 1PLATE;NHA 3P21702 | Lockheed Martin Corporation (98897) | |
| 3P35004-101 3P35004101 | 1560-00-553-6430 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: U/a:bracket, drain & vent instl | Lockheed Martin Corporation (98897) | |
| 3P35005-101 3P35005101 | 1560-00-553-6432 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: U/a:bracket, drain & vent instl | Lockheed Martin Corporation (98897) | |
| 3P35005-107 3P35005107 | 1560-00-553-6474 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P35008-115 3P35008115 | 1560-00-050-1015 | Collector, Drain and Vent | III End Item Identification: Aircraft, model C141 | Lockheed Martin Corporation (98897) | |
| 3P35017-101 3P35017101 | 1560-00-868-5328 | Fitting, Drain, Pylon | General Characteristics Item Description: Aluminum alloy, QQ-A-225-8, 1.125 in. lg | Lockheed Martin Corporation (98897) | |
| 3P35018-101 3P35018101 | 1560-00-789-4667 | Coupling, Drain, Aft Beam | General Characteristics Item Description: Synthetic rubber, lac 23-926, fscm 98897, flared 1 end 1.380 in. dia, 0.500 in. id opposite end | Lockheed Martin Corporation (98897) | |
| 3P35019-101 3P35019101 | 1560-01-145-5057 | Pan, Outboard Pylon | III End Item Identification: C-141A/B acft General Characteristics Item Description: C/O tube, 1; flange, 1; pan, 1; pan and flange matl al alloy, QQ-A-327, 6061-0; tube matl al alloy tubing, WW-T-789, 6061-0; 8.740 in. lg; 5.390 in. w; 1.870 in. lg tube W/flange; used as pan, drain-aft upper beam | Lockheed Martin Corporation (98897) | |
| 3P35020-131 3P35020131 | 1560-00-246-8356 | Funnel Assembly, Mast Drain | III End Item Identification: Acft model C-141 General Characteristics Item Description: Aluminum alloy, 6061-T4, QQ-A-250/11, and 2024-T3, QQ-A-250/5 | Lockheed Martin Corporation (98897) | |
| 3P35021-101 3P35021101 | 1560-00-780-8025 | Bracket Assembly, Duct | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Titanium alloy, AMS4901 annealed, 5.310 in. O/a lg, 1.600 in. O/a W, 1.450 in. O/a H | Lockheed Martin Corporation (98897) | |
| 3P35022-101 3P35022101 | 1560-01-135-3673 | Pan Assembly, Drain | III End Item Identification: C-141A/B General Characteristics Item Description: Used on inboard pylon; C/O-pan, tube, flange | Lockheed Martin Corporation (98897) | |
| 3P35446-101 3P35446101 | 1560-00-753-6844 | Lever, Control, Thrust Reverser | General Characteristics Item Description: Aluminum alloy, 356-T6, ams 4260 | Lockheed Martin Corporation (98897) | |
| 3P35502-101 3P35502101 | 1560-01-135-8945 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Matl: al aly clad; 5 holes 0.220 in dia; U/a: support, elect wiring Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P38901-107 3P38901107 | 1560-00-944-9161 | Shield, Screen and s | Lockheed Martin Corporation (98897) | ||
| 3P38902-103 3P38902103 | 1560-01-146-0760 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141A/B Special Features: C/O:2 holes, 0.385IN dia;distance from C to C 2.900 in; 2 holes, 0.322IN dia;temper T4;OPP to P/N 3P38902-104; U/a: spacer Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P38902-104 3P38902104 | 1560-01-146-0759 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141A/B Special Features: C/O:2 holes, 0.385IN dia;distance from C to C 2.900 in; 2 holes, 0.322IN dia;temper T4;OPP to P/N 3P38902-103; U/a: spacer Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P40024-115 3P40024115 | 1560-00-075-8995 | Vane Assembly, Louver | General Characteristics Item Description: Cres, MIL-S-6721 | Lockheed Martin Corporation (98897) | |
| 3P40024-117 3P40024117 | 1560-00-072-7835 | Vane Assembly, Louver | General Characteristics Item Description: Cres, MIL-S-6721 | Lockheed Martin Corporation (98897) | |
| 3P40024-121 3P40024121 | 1560-00-072-7837 | Vane Assembly, Louver | General Characteristics Item Description: Cres, MIL-S-6721 | Lockheed Martin Corporation (98897) |