01-227-8079
Structural Aircraft Panel
Used on c-5 aircraft. c/o: fwd panel (1) , bracket (2) ; part of -102d door assembly-slat actuator 1b
01-227-8090
Aircraft Stringer
Part of fan cowl
01-227-8487
Fuel Aircraft Tank
Shape: cylindrical
01-227-8808
Aircraft Skin
Used on c-5b aircraft. matl 7075-T6 alclad per qq-a-250/13; matl size .040X33.0X98.0; skin, lower-trailing edge, wing tip; opposite -105a; nha 4J20100-102a
01-227-8812
Thermal Special Purpo Insulation
Acft c-5; 13 sq ft matl; used on -101a sound absorbig/thermal door
01-227-8846
Thermal Special Purpo Insulation
Fuel resistant
01-227-8847
Thermal Special Purpo Insulation
Fuel resistant
01-228-0801
Aircraft Former
01-228-1477
Structural Component Air Support
01-228-1478
Structural Component Air Support
2.760" overall length 1.810" overall width
01-228-3386
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 plate, 2 grommet; located at sta yan 25.93 to yan 81.50
01-228-3601
Access Aircraft Door
Used on c-5b aircraft.
01-228-3602
Access Aircraft Door
Used on c-5 aircraft.
01-228-3713
Structural Aircraft Plate
Cover diverter lower-left hand
01-228-3714
Structural Component Air Fitting
Used on c-5b aircraft. 14.000" overall length 0.188 " material thickness matl/size LS3531-3X14; opposite-102a; NHA4F55602
01-228-3715
Structural Component Air Fitting
Used on c-5b aircraft. 14.000" overall length 0.188" material thickness matl/size LS3531-3X14 opposite-101a; NHA4F55602
01-228-3716
Structural Component Air Fitting
Used on c-5b aircraft. matl/size 0.375X3.0X3.0; 7075-T651 alum alloy per qq-a-250/12; nha 4F55602
01-228-3717
Structural Component Air Support
Used on c-5b aircraft. clevis assembly-upper spt, strut, windshield post no 1, fus sta 338.50; c/o: -113a clevis (1) , bushing (2) ; opposite -112a; nha 4F11932
01-228-3721
Structural Component Air Fitting
C/o 1 carriage fitting, 4 bushing; opposite -101a; nha 4J41309
01-228-3722
Structural Component Air Support
Used on c-5b aircraft. carriage fitting assembly-front, outbd, flap no 2; c/o: -104a carriage ftg (1) , bushing (4) ; opposite -101a; nha 4J41213
01-228-3725
Structural Component Air Support
Used on c-5b aircraft. fitting, bumper-ctr section, wheel well, sta 1418.16 & 1488.16 mlg fairing; c/o: -603a fitting (1) , nut plate (4)
01-228-3726
Structural Component Air Support
Used on c-5b aircraft. carriage fitting assembly-front, outbd, flap no 1; c/o: -104b carriage ftg (1) , bushing (4) ; opposite -101b; nha 4J41113
01-228-3727
Structural Component Air Support
Used on c-5b aircraft. carriage fitting assembly-front, outbd, flap no 1; c/o: -103b carriage ftg (1) , bushing (4) ; opposite -102b; nha 4J41113
01-228-3728
Structural Component Air Support
Used on f-5 aircraft. support-bracket, mlg alt rel crank
01-228-3729
Structural Component Air Support
Used on acft model f-16c/d. made from aluminum alloy casting per AMS4218-T6
01-228-3730
Structural Component Air Support
Used on acft model e-3a.
01-228-3732
Structural Component Air Support
Used on c-141 acft. p/o frame, aft, cowl; power plant station 147.95
01-228-3733
Structural Component Air Support
Used on f-15 acft.
01-228-3742
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-upper, slat 5, outerwing; opposite -176a
01-228-3743
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-upper, slat 5, outerwing; opposite -175a
01-228-3744
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-upper, slat 6, outerwing; opposite -168a
01-228-3745
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-upper, slat 6, outerwing; opposite -167a
01-228-3746
Structural Aircraft Panel
Used on c-5b aircraft. panel assembly-upper, slat 7, outerwing; opposite -168a
01-228-3748
Structural Aircraft Panel
Used on c-5 aircraft. c/o: -117a panal (1) , -119a panal (1) ; used on -113 door assembly-lox service fwd whl well fairing
01-228-3749
Structural Aircraft Panel
Used on acft model e-3a. consists of 3 facesheet; 4 bottom panel, 2 inbd panel, 1 doubler, 1 shroud assy, 2 grommet, misc hardware; located at sta 460 l.h.; nha 204-40501
01-228-3750
Structural Aircraft Panel
01-228-3751
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 skin, 1 beaded doubler, 2 lower doubler; opp -2; nha 65-3495; located at sta 235.98 to WL532
01-228-3752
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upr doubler; opp -2; nha 65-3495; located at sta 169.08 to 191.38
01-228-3753
Structural Aircraft Panel
Used on acft model e-3a. consist of 10 beaded doubler, 10 skin, 10 lwr doubler, 10 upr doubler, 1 skin assy, 1 doubler, 1 access door; nha 65-3495; opp -1; located at station 70.97 to 93.26
01-228-3754
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upr doubler; opp -2; nha 65-3495; located at station 70.97 to 93.26
01-228-3766
Aircraft Former
5.000" overall length 3.750" overall width 0.040" material thickness
01-228-3767
Aircraft Former
31.500" overall length 5.000" overall width 0.080" material thickness
01-228-3768
Aircraft Former
43.500" overall length
01-228-3769
Aircraft Former
48.000" overall length
01-228-3770
Aircraft Former
65.000" overall length
01-228-3771
Aircraft Former
75.000" overall length
01-228-3772
Aircraft Former
44.000" overall length
01-228-3773
Aircraft Former
01-228-3774
Aircraft Former
62.000" overall length
