Airframe Structural Components: 12W8683-808, 12W8688-3, 12W8691-801
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
12W8683-808 12W8683808 | 1560-00-998-8888 | Cover, Access, Aircraft | End Item Identification: Aircraft, model F111 | Lockheed Martin Corporation (81755) | |
12W8684-7 12W86847 | 1560-00-949-6869 | Stop, Track, Translating | General Characteristics Item Description: Steel, 1.500 in. lg, 1.150 in. W, 0.800 in. H III FSC Application Data: Flap, wing, airframe | Lockheed Martin Corporation (81755) | |
12W8685-13 12W868513 | 1560-00-466-3149 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.120 in. thk, 0.530 in. W 1 end, 0.880IN. W opposite end, 4.180 in. lg, 2 holes drilled thru 0.196 in. min, 0.204MAX dia in line 0.310 in. from side, 0.310 in. from each end | Lockheed Martin Corporation (81755) | |
12W8685-14 12W868514 | 1560-00-466-3150 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.120 in. thk, 0.530 in. W 1 end, 0.880IN. W opposite end, 4.180 in. lg, 2 holes drilled thru 0.196 in. min, 0.204MAX dia in line 0.310 in. from side, 0.310 in. from each end | Lockheed Martin Corporation (81755) | |
12W8685-21 12W868521 | 1560-00-990-5922 | Plate, Guide, Track NO. 3 | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.130 in. thk, 0.560 in. W, 1.570 in. lg, 2HOLES drilled thru 0.196 in. min, 0.196 max dia in line 0.180 in. from SIDE0.410 in. from each end | Lockheed Martin Corporation (81755) | |
12W8685-25 12W868525 | 1560-00-975-4602 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Special Features: U/a:plate, guide, track NO.3;MATL: alum bronze, 0.811IN wd 1 end, 1.740IN wd opposite end, 4 holes drilled thru on 31.069IN radius 0.191IN min, 0.196 max dia equally spaced 0.380 in. from side Material Document and Classification: QQ-C-450 fed spec single material response | Lockheed Martin Corporation (81755) | |
12W8685-26 12W868526 | 1560-00-975-4603 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Special Features: U/a:plate, guide, track NO.3;MATL: alum bronze, 0.811IN wd 1 end, 1.740IN wd opposite end, 4 holes drilled thru max dia equally spaced 0.380 in. from side Material Document and Classification: QQ-C-450 fed spec single material response | Lockheed Martin Corporation (81755) | |
12W8685-27 12W868527 | 1560-00-934-1071 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Special Features: U/a:plate, guide, track NO.3;MATL: alum bronze;c/o: 2 holes drilled thru 0.191IN min, 0.199IN max dia, in line 0.380IN from end Material Document and Classification: QQ-C-450 fed spec single material response | Lockheed Martin Corporation (81755) | |
12W8685-29 12W868529 | 1560-00-074-3894 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-A-450, 0.100 in. thk, 0.800 in. W, 3.400 in. lg, 2HOLES drilled thru 0.196 in. min, 0.204 max dia, 0.380 in. from side | Lockheed Martin Corporation (81755) | |
12W8685-30 12W868530 | 1560-00-074-3895 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.100 in. thk, 0.800 in. W, 3.400 in. lg, 2HOLES drilled thru in line 0.380 in. from side | Lockheed Martin Corporation (81755) | |
12W8685-31 12W868531 | 1560-00-074-3898 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.100 in. thk, 0.811 in. W 1 end, 1.740 in.W opposite end, 4 holes drilled thru, 0.191 in. min, 0.196 max dia equallyspaced on a 30.469 in. radius 0.380 in. from side, 1 hole drilled thru 0.380IN. dia 0.880 in. from end and 0.680 in. from side | Lockheed Martin Corporation (81755) | |
12W8685-32 12W868532 | 1560-00-074-3900 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-A-450, 0.100 in. thk, 0.811 in. W 1 end, 1.740 in.W opposite end, 4 holes drilled thru 0.191 in. min, 0.196 max dia equallyspaced on a 30.469 in. radius 0.380 in. from side, 1 hole drilled thru 0.380IN. dia 0.880 in. from end and 0.680 in. from side | Lockheed Martin Corporation (81755) | |
12W8685-40 12W868540 | 1560-00-998-8890 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.100 in. thk, 0.940 in. W 1 end, 1.500 in.W opposite end, 4.220 in. lg, 2 holes drilled thru 0.250 in. dia, 0.250 in.from side | Lockheed Martin Corporation (81755) | |
12W8685-41 12W868541 | 1560-00-131-8881 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.180 in. thk 1 side, 0.270 in. thk oppositeside, serrations 0.500 in. W on 1 side, 0.830 in. O/a W, 1.570 in. lg, 2HOLES drilled thru 0.312 in. min. 0.320 max dia, 0.750 in.apart in LINE0.530 in. from side beginning 0.410 in. from end | Lockheed Martin Corporation (81755) | |
12W8685-43 12W868543 | 1560-00-131-8881 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.180 in. thk 1 side, 0.270 in. thk oppositeside, serrations 0.500 in. W on 1 side, 0.830 in. O/a W, 1.570 in. lg, 2HOLES drilled thru 0.312 in. min. 0.320 max dia, 0.750 in.apart in LINE0.530 in. from side beginning 0.410 in. from end | Lockheed Martin Corporation (81755) | |
12W8685-45 12W868545 | 1560-00-466-3149 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.120 in. thk, 0.530 in. W 1 end, 0.880IN. W opposite end, 4.180 in. lg, 2 holes drilled thru 0.196 in. min, 0.204MAX dia in line 0.310 in. from side, 0.310 in. from each end | Lockheed Martin Corporation (81755) | |
12W8685-46 12W868546 | 1560-00-466-3150 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.120 in. thk, 0.530 in. W 1 end, 0.880IN. W opposite end, 4.180 in. lg, 2 holes drilled thru 0.196 in. min, 0.204MAX dia in line 0.310 in. from side, 0.310 in. from each end | Lockheed Martin Corporation (81755) | |
12W8688-3 12W86883 | 1560-00-835-1126 | Bracket, Expansion Hinge, Outboard | General Characteristics Item Description: Aluminum alloy, 2024-T851, QQ-A-250/4 | Lockheed Martin Corporation (81755) | |
12W8688-4 12W86884 | 1560-00-081-2632 | Bracket, Expansion Hinge, Outboard | General Characteristics Item Description: Aluminum alloy, 2024-T851, QQ-A-250/4 | Lockheed Martin Corporation (81755) | |
12W8691-801 12W8691801 | 1560-00-949-6883 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Steel, 2.550 in. lg, 2.280 in. W, 1.760 in. H, 2 holes 0.313 in. min, 0.315 in. max dia in line in two places | Lockheed Martin Corporation (81755) |