01-229-1042
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 plate, 4 grommet; located at yan 25.93 - yan 81.50
01-229-1043
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 3 grommet, 1 plate; located at yan 25.93-yan 81.50
01-229-1044
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 foil, 1 batt blanket, 1 plate, 58 grommet, 2 edge closure, staples a/r; located at yan 25.93 to yan 81.50
01-229-1045
Thermal Special Purpo Insulation
Consist of 1 foil; 1 facesheet; 1 batt blanket; 7 grommet; 1 plate
01-229-1183
Aircraft Window Panel
01-229-2446
Aircraft Fairing
Used on aircraft model f-18.
01-229-2447
Aircraft Fairing
Used on aircraft model f-18.
01-229-2448
Aircraft Fairing
Used on aircraft model f-18.
01-229-2450
Aircraft Fairing
Used on aircraft model f-18. laminated kevlar 49 per mms-525, type 2
01-229-2451
Aircraft Fairing
Used on aircraft model f-18. laminated levlar 49 per mms-525, type 2
01-229-2452
Aircraft Fairing
Used on aircraft model f-18. laminated kevlar 49 per mms-525, type 2
01-229-2459
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/13, cond o
01-229-2460
Horizontal Stabilizer
Used on aircraft model av-8.
01-229-3280
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 foil, 1 batt blanket, 1 plate, 9 grommet; located at yan 25.93 to yan 81.50
01-229-3281
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 foil, 1 batt blanket, 1 plate, 5 grommet; located at yan 25.93 to yan 81.50
01-229-3703
Structural Aircraft Panel
Used on acft model e-3a. consist of 10 beaded doubler, 10 skin, 10 lwr doubler, 10 upper doubler, 1 skin assy, 1 doubler, 1 access door, misc hardware; opposite p/n -1; nha 65-3495; located at station 146.78 to 169-08
01-229-3704
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upper doubler; finish srf-12.915; nha 65-3495; located at sta 48.67 to 70.97
01-229-3705
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 skin assy, 2 beaded doubler, 2 doubler, 2 angle stiffener, 2 skin; nha 65-3495; located at sta 93.26 to 102.18
01-229-3706
Structural Aircraft Panel
Used on acft model e-3a. consist of 1o beaded doubler, 10 skin, 10 lwr doubler, 10 upper doubler, 1 bonded panel assy, 1 doubler, 1 door; finish srf-12.915; opposite p/n -1; nha 65-3495; located at sta 48.67 to 70.97
01-229-3726
Thermal Special Purpo Insulation
01-229-3727
Thermal Special Purpo Insulation
01-229-3728
Thermal Special Purpo Insulation
01-229-4106
Structural Component Air Support
01-229-4559
Aircraft Skin
01-229-4562
Aircraft Stiffener
28.000" overall length engine access door
01-229-4563
Aircraft Skin
01-229-5754
Structural Aircraft Plate
6.800" overall length 4.500" overall width 0.125" material thickness 6al-6v-2sn per MM1203; nha 68A333001
01-229-5755
Structural Aircraft Plate
6.800" overall length 2.600" overall width 0.140" material thickness 6al-6v-2sn per mms-1203; nha 68A333001
01-229-5756
Structural Aircraft Plate
6.800" overall length 2.600" overall width 0.140" material thickness 6al-6v-2sn per mms-1203; nha 680333001
01-229-5761
Structural Component Air Support
Used on f-15 acft. 6al-4v per mil-t-9046 type 3, comp c; 21.50 in. lg, 6.00 in. wd, 1.375 in. thk; opposite p/n -2007; nha 68A331013; located on lower longeron fs 684.100 support
01-229-5762
Structural Component Air Support
Used on f-15 acft. 6al-4v per mil-t-9046 type 3, comp c; 21.50 in. lg, 6.00 in. wd, 1.375 in. thk; opposite p/n -2008; nha 68A331013; located on lwr longeron fs 684.100 support
01-229-5763
Structural Component Air Support
Used on f-15 acft. 7075-T7351 per MMS159, cond T7351; 10.25 in. lg, 3.00 in. wd, 0.125 in. thk; opposite p/n -2003; nha 68A318018; located on fs 408.340
01-229-5775
Aircraft Former
01-229-5776
Aircraft Former
01-229-5778
Aircraft Skin
65.000" overall length 40.000" overall width
01-229-5779
Aircraft Skin
Used on F-15.
01-229-5780
Aircraft Skin
Used on F-15.
01-229-5781
Aircraft Skin
Used on F-15.
01-229-5782
Aircraft Skin
Used on f-15 acft. 6al-4v per mil-t-9046 type iii, comp c anl; 7.65 in. lg, 6.83 in. wd, 0.071 in. thk; opposite p/n -2004; same as -2001; located on fs 572.160 to fs 565.330
01-229-5783
Aircraft Skin
Used on F-15. 24.000" overall length 7.000" overall width nha 68A314022 & 68T060138
01-229-5784
Aircraft Skin
Used on F-15. 12.000" overall length 8.000" overall width nha 68A314022 & 68T060138
01-229-8375
Aircraft Skin
Aluminum alloy
01-229-8798
Structural Component Air Support
Used on acft model b-1b.
01-229-8822
Thermal Special Purpo Insulation
01-229-8823
Thermal Special Purpo Insulation
01-229-8825
Thermal Special Purpo Insulation
01-229-8826
Thermal Special Purpo Insulation
Consist of 20 grommet, outer facesheet, 1 inner facesheet, 1 retainer, 1 blanket, 1 id plate; located on yn 216.5 to yn 265.25; used as nac insulation blanket assy
01-229-8827
Thermal Special Purpo Insulation
Consist of 1 inner facesheet, 1 outer facesheet, 1 retainer, 1 blanket, 1 id plate, 5 grommet; located on yn 216.5 to yn 265.25; used on nac insulation blanket assy
