01-318-5580
Aircraft Bulkhead
01-318-7257
Aircraft Fairing
01-318-7302
Structural Component Air Support
01-318-7557
Structural Aircraft Plate
1.590" overall length 1.300" overall width 0.063" material thickness
01-318-7561
Structural Aircraft Panel
Used on pacer special. 47.000" overall length 11.000" overall width nuclear hardness critical item & smoothness critical item; core material; nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -001
01-318-7562
Structural Aircraft Panel
Used on pacer special. 42.000" overall length 11.000" overall width nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -006
01-318-7563
Structural Aircraft Panel
Used on pacer special. 42.000" overall length 11.000" overall width nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -005
01-318-7564
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -016
01-318-7565
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -015
01-318-7566
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -016
01-318-7567
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -015
01-318-7568
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -002
01-318-7569
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb; opposite -001
01-318-7572
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; opp -002; matl: nomex honeycomb core per bms 8-124 cl iv, ty v, gr 5 thickness tolerance plus or minus .006; c/o: core (-005)
01-318-7573
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; opp -001; matl: nomex honeycomb core per bms 8-124 cl iv, ty v, gr 5, thickness tolerance plus of minus .006; c/o: core (-006)
01-318-7574
Structural Aircraft Panel
Used on pacer special. 40.500" overall length 26.000" overall width nuclear hardness critical item; core material: nomex honeycomb per BMS8-124, class iv, type v, gr 3, thk tolerance plus or minus .006; opposite -008
01-318-7575
Structural Aircraft Panel
Used on pacer special. 45.500" overall length 26.000" overall width gnuclear hardness critical item & smoothness critical item; core material: nomex honeycomp per BMS8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opp -007; dimensions listed are stock size
01-318-7576
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critial item; core material: nomex honeycomb iaw BMS8-124, cl iv, ty v, gr 5, thk tolerance plus or minus .006; opposite -010
01-318-7578
Structural Aircraft Panel
Used on pacer special. 27.500" overall length 34.500" overall width nuclear hardness critiacal item & smoothness critical item; core material: nomex honeycomb per BMS8-124, cl iv, ty v, gr 5, thk tolerance plus or minus .006; opposite -008; fin f-25.01
01-318-7579
Structural Aircraft Panel
Used on pacer special. 27.500" overall length 34.500" overall width nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb per BMS8-124, cl iv, ty v, gr, thk tolerance plus or minus .006; fin f-25.01; opposite -007
01-318-7580
Structural Aircraft Panel
Used on pacer special. 30.000" overall length 21.000" overall width gnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124 cl iv, ty v, gr 5, thk tolerance plus or minus .006; opposite -002; dimensions listed are stock size
01-318-7581
Structural Aircraft Panel
Used on pacer special. 30.000" overall length 21.000" overall width gnuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124 cl iv, ty v, gr 5, thk tolerance plus or minus .006; opposite -001; dimensions listed are stock size
01-318-7582
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smootness critical item; core matl: nomex honeycomb per BMS8-124 cl iv, ty v, gr 3, thk tolerance plus or minus .006 opposite -012
01-318-7583
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS4-128 cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -011
01-318-7584
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124 cl iv, ty v, gr 5, thk tolerance plus or minus .006; opposite -036
01-318-7585
Structural Aircraft Panel
Nuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb per BMS8-124 cl iv, ty v, gr 5, thk tolerance plus or minus .006; opposite -035
01-318-7586
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb; opposite -008
01-318-7587
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothess critical item; core matl: nomex honeycomb; opposite -008
01-318-7588
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb; opposite -014
01-318-7589
Structural Aircraft Panel
Used on pacer special. nuclear hardness critical item & smoothness critical item; core matl: nomex honeycomb; opposite -013
01-318-7590
Structural Aircraft Panel
C/o 1 core; nha DAA3132B700; opposite -006; finish f-14.67 plus f-19.62; nuclear hardness critical item, smoothness critical item
01-318-7591
Structural Aircraft Panel
C/o 1 core; nha DAA3132B700; opposite -005; finish f-14.67 plus f-19.62; nuclear hardness critical item, smoothness critical item
01-318-7592
Structural Aircraft Panel
Nuclear hardness critical item & smoothness critical item; c/o: panel & baffle
01-318-7593
Structural Aircraft Panel
Opposite -005; finish f-25.01; nuclear hardness critical item/smoothness critical item; nha DAA3132B800; c/o 1 panel
01-318-7594
Structural Aircraft Panel
C/o 2 panels; nha DAA3132B800; opposite -004; finish f-25.01; nuclear hardness critical item; smoothness critical item
01-318-7595
Structural Aircraft Panel
C/o 2 panels; nha DAA3132B800; nuclear hardness critical item; smoothness critical item; opposite -003; finish f-25.01
01-318-7597
Aircraft Skin
01-318-7598
Structural Component Air Support
01-318-7599
Structural Component Air Support
01-318-7600
Structural Component Air Support
01-318-7634
Longeron Repair Kit
Used on C-141.
01-318-8555
Structural Aircraft Plate
Used on 1520-01-106-9519.
01-318-8569
Eye Rotating Shaft Bracket
Used on 1520-01-106-9519.
01-318-8744
Access Aircraft Door
Used on mh-53e acft.
01-318-8827
Aircraft Fairing
Used on acft mh-53e.
01-318-8828
Structural Aircraft Panel
Used on sh-60b acft.
