01-090-4038
Aircraft Skin
01-090-4039
Aircraft Skin
01-090-5022
Aileron Balance Weight
Used on acft c135. 32.300 in. lg, 1.900 in. w, 0.060 in. th. 6 percent antimony lead comp per l-16. finish f-12.206
01-090-5709
Structural Aircraft Plate
Used on acft model f4c. alum alloy 7178-0 per qq-a-250/15 cond 0, 0.050 in.thk, 2.100 in.w, 3.640 in.lg, right hand
01-090-5719
Aircraft Fairing
C/o 1 inlet ring, 1 skin instl, 1 former instl, 1 latch back-up, 1 skin instl, 1 bracket
01-090-5737
Aircraft Fairing
9.500" overall length 7.500" overall width 0.040" material thickness
01-090-5742
Airfoil Rib
5.540" overall length 4.700" overall width 0.040" material thickness
01-090-6610
Aircraft Window Panel
Used on boeing acft model 727. outer pane passenger window
01-090-6951
Structural Component Air Support
4.360 in.lg; 4.000 in.w; 0.800 in.h;
01-090-7413
Aircraft Fairing
7.600" overall length 0.100" material thickness rudder seal, panel nbr 4449
01-090-7414
Aircraft Fairing
25.530" overall length 0.100" material thickness rudder seal, panel nbr 4445
01-090-7416
Aircraft Fairing
25.520" overall length 0.100" material thickness rudder seal, panel nbr 4446
01-090-7417
Aircraft Fairing
27.500" overall length 0.100" material thickness rudder seal, panel nbr 4444
01-090-7446
Aircraft Door
C/o 1 door assy, 4 retainer, 2 strap, 23 stud bolts, 24 retaining ringsrivets as required
01-090-7458
Structural Aircraft Plate
Used on acft model f4e. do not use cadmium plated tools on this item, titanium alloy ams 4908, 8mn per mil-t-9046 type 3 comp a annealed, 0.040 in.thk, 0.800 in.w, 2.300 in.lg; left hand;
01-090-7459
Structural Aircraft Plate
Used on acft model f4c. do not use cadmium plated tools on this item, titanium alloy ams 4908, stock size 0.032 in.thk, 10.040 in.w, 12.080 in.lg, used on seal assembly panel fuselage section 362.00;
01-090-7469
Aircraft Skin
33.500" overall length 18.300" overall width cond 0, heat treat per mac p.s. 15529
01-090-8106
Structural Aircraft Panel
Used on aircraft model f-14.
01-090-8107
Structural Aircraft Panel
Used on aircraft model f-14.
01-090-8108
Structural Component Air Support
Used on aircraft model f-14.
01-090-8115
Aircraft Skin
Used on aircraft model f-14.
01-090-8116
Aircraft Skin
Used on aircraft model f-14.
01-090-8813
Airfoil Rib
8.000" overall length 5.300" overall width 0.040" material thickness
01-090-9200
Structural Component Air Bracket
C/o 1 bracket, 1 strap, 4 nutplate
01-091-0433
Structural Aircraft Plate
C/o plate, pad, sealant
01-091-0497
Thermal Special Purpo Insulation
3matl:119 trim cloth, vinyl coated fiberglass nonporous lusterless gray 3815, 300 fiberglass batt superfine pf insulation code a-81, fireproof treated cotton muslin backing, cemented construction, left hand; end item identification:aircraft, model F4g
01-091-1477
Structural Aircraft Plate
1.950" overall length 1.300" overall width 0.032" material thickness lefthane
01-091-1478
Structural Aircraft Plate
Used on acft model f4c. alum alloy 7075-T6 per qq-a-250/12 cond T6, 0.250 in.thk, 2.000 in.w, 6.140 in.lg, right hand
01-091-1479
Structural Aircraft Plate
01-091-2138
Structural Component Air Bracket
01-091-2792
Access Aircraft Door
Used on EA6B.
01-091-4112
Structural Component Aircraf Web
20.900" overall length 6.600" overall width 0.025" material thickness
01-091-4129
Access Aircraft Door
Used on acft e3a. used on wing tip cap assembly
01-091-4130
Aircraft Fairing
01-091-4131
Access Aircraft Door
Used on acft e3a. used on wing tip; 23.600 in lg, 14.600 in wd, 0.080 in thk; finish srf-2132; used on left hand
01-091-4165
Aircraft Skin
01-091-4166
Aircraft Skin
60.000" overall length 35.000" overall width
01-091-4230
Bell Crank
0.748" bore diameter
01-091-4784
Aircraft Spar
01-091-4785
Aircraft Spar
01-091-4786
Aircraft Spar
01-091-4787
Aircraft Spar
01-091-4788
Aircraft Spar
01-091-4811
Structural Aircraft Plate
Used on acft model f4c. do not use cadmium plated tools on this item, titanium 6al-4v ams-4911 annealed per mil-t-9046 type 3, 0.437 in.thk, 4.860 in.w, 4.950 in.lg, right hand;
01-091-4823
Thermal Special Purpo Insulation
Matl:119 trim cloth, vinyl coated fiberglass, nonporous lusterless gray 3815, 300 fiberglass batt superfine df insulation code a-81, fireproof treated; end item identification:aircraft, model F4
01-091-7075
Aircraft Channel
01-091-7516
Longeron
Used on acft model f-16a usaf. aluminum alloy per fms-3002-T851; located fs 88.00 to fs 189.00; eff 61 0007 0261; superseded p/n 16B1103-18 ow per ecn 59359; nha 16B1931-6;
01-091-7517
Longeron
Used on f-16 acft. alum alloy per fms-3002-T851; located fs 88.00 to fs 189.00;
