01-272-3084
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3085
Structural Aircraft Panel
Used on c-5 aircraft. trim panel, matl nomex phenolic honeycomb core
01-272-3086
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3087
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3088
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3089
Structural Aircraft Panel
Matl honeycomb core STM28-108
01-272-3090
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl honeycomb core STM28-106
01-272-3091
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3092
Structural Aircraft Panel
Used on c-5 aircraft. material nomex phenolic honeycomb core
01-272-3093
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3094
Structural Aircraft Panel
Used on c-5 aircraft. trim panel; matl nomex phenolic honeycomb core
01-272-3101
Aircraft Former
Used on C-141. matl size LS60261-1X34; opp -102
01-272-3102
Aircraft Former
Used on C-141. matl size LS60261-1X90
01-272-3387
Structural Component Air Support
5.000" overall length 0.050" material thickness
01-272-4361
Access Aircraft Cover
Used on a-10 aircraft. adf antenna
01-272-4415
Structural Aircraft Plate
Used on B-52. c/o 1 fitting, 1 ball fitting, 1 packing, 1 nut; nha 413-10423
01-272-4416
Structural Aircraft Plate
Used on acft model b-1b.
01-272-4932
Structural Component Air Support
4.500" overall length 0.050" material thickness
01-272-4933
Structural Component Air Support
0.050" material thickness
01-272-4934
Structural Component Air Support
3.938" overall length
01-272-4937
Airfoil Rib
Used on aircraft,f-14. 0.032" material thickness
01-272-4938
Airfoil Rib
Used on aircraft,f-14. 0.032" material thickness
01-272-4939
Aircraft Skin
Aluminum alloy, qq-a-250/5 2024-T3; 0.025 in. material thickness
01-272-4940
Aircraft Skin
Jskin material aluminum alloy, qq-a-250/5, alloy 2024-T3 clad; 0.045 in. thk stock; stringers material, aluminum alloy, qq-a-250/12, alloy 7075-T6; acrylic lacquer, gloss, insignia white, 17375 grumman aircraft GSS4407
01-272-4941
Center Wing Section
Steel, mil-s-25043, 17-7ph; primer, epoxy polyamide, mil-p-23377, ty 1; 12.120 in.lg; 0.032 in.thk;
01-272-5584
Structural Component Air Support
2.000" overall width
01-272-5585
Structural Component Air Support
01-272-5586
Structural Component Air Support
0.063" material thickness
01-272-5587
Structural Component Air Support
01-272-5588
Structural Component Air Support
01-272-5596
Airfoil Rib
Used on aircraft,f-14. 0.032" material thickness
01-272-5597
Airfoil Rib
Used on aircraft,f-14. 0.032" material thickness
01-272-5598
Airfoil Rib
0.050" material thickness primer epoxy-polyamide surface treated
01-272-5599
Airfoil Rib
Used on f-14 tomcat airplane.... 0.040" material thickness heat treat per T62, other material; primer, epoxy polyamide primer epoxy-polyamide surface treated
01-272-5600
Aircraft Skin
Aluminum alloy, qq-a-250/5 2024-0; 0.040 in. thk
01-272-5864
Access Aircraft Door
Used on acft model b-52. opposite p/n -5; located les 1027.28 to les 1049.73; used on leading edge gap cover installation
01-272-5965
Aircraft Former
16.500" overall length 7.560" overall width 0.063" material thickness 6al-4v
01-272-6394
Structural Component Air Fitting
Used on b-52 se agmbrl. drive fitting mfg name fitting drive
01-272-6530
Structural Component Air Support
01-272-6624
Structural Aircraft Plate
Used on s-3 viking airplane.... 0.050" material thickness
01-272-6625
Aircraft Fairing
0.020" material thickness
01-272-6626
Aircraft Skin
01-272-6627
Aircraft Fairing
01-272-6628
Aircraft Fairing
01-272-6629
Aircraft Fairing
01-272-6630
Structural Component Air Support
01-272-6631
Structural Component Air Support
0.125" material thickness
01-272-6632
Structural Component Air Support
14.000" overall length
01-272-6636
Aircraft Former
Used on aircraft,tomcat f-14. 0.040" material thickness
01-272-6637
Aircraft Former
Used on aircraft,tomcat f-14. 0.040" material thickness
