01-111-8818
Cutter Cable Blade
01-111-9517
Access Aircraft Door
01-111-9712
Structural Aircraft Panel
19.250" overall length 6.750" overall width
01-111-9917
Structural Component Air Fitting
01-112-0025
Structural Aircraft Panel
Used on c-5a aircraft. 79.750" overall length
01-112-2011
Aircraft Former
3.750" overall length 2.410" overall width 0.032" material thickness sill, door, engine access
01-112-2026
Structural Aircraft Panel
01-112-2034
Aircraft Fairing
01-112-2052
Structural Aircraft Panel
Used on F-4.
01-112-2054
Structural Aircraft Plate
Used on acft model f4. sheet steel 301 per mil-s-5059 comp 301, cond 1/2 hard, 0.010 in.thk, 3.500 in.w, 4.700 in.lg, left hand, used on center section fwd, torque box
01-112-2061
Aircraft Skin
Used on C-135.
01-112-2661
Aircraft Fairing
01-112-2670
Structural Aircraft Plate
Used on acft model f4. age harden per p.s.15922, used on door assy number 5 engine access located from fs 447.05 to fs 493.00, lh
01-112-2675
Structural Component Air Support
Used on acft model f-16. c/o support p/n 16P1888-15, support p/n 16P1888-17, as required rivets
01-112-2676
Structural Component Air Support
Used on acft model f4. al alloy 7178-0 per qq-a-250/15 cond 0, 0.063 in.thk, 5.000 in.w, 9.000 in.lg, left hand, used on frame assembly located at fs 264.50
01-112-2689
Aircraft Former
6.100" overall length 2.180" overall width 0.100" material thickness
01-112-2690
Aircraft Former
9.950" overall length 1.700" overall width 0.040" material thickness
01-112-2695
Aircraft Pylon
01-112-2707
Thermal Special Purpo Insulation
Used on main landing gear pod, lh fuselage station 818.0 to 878.0; end item identification:aircraft, model c-141
01-112-3657
Access Aircraft Door
Used on aircraft model rf-4b.
01-112-3658
Access Aircraft Door
Used on aircraft model rf-4b.
01-112-3659
Access Aircraft Door
Used on aircraft model rf-4b.
01-112-3781
Aircraft Skin
37.000" overall length 29.000" overall width nha pn 16B416-811; eff on 62-00779999; superseded p/n 16B4620-37 ni per ecn 6A963
01-112-5616
Aircraft Fairing
01-112-6854
Aircraft Strut
01-112-6865
Aircraft Strut
25.450" overall length
01-112-6866
Aircraft Strut
01-112-6870
Structural Component Air Support
01-112-6993
Structural Aircraft Plate
2.930" overall length 2.370" overall width
01-112-6995
Structural Component Air Support
Used on t-38 trainer aircraft. c/o 1 panel assembly
01-112-6996
Structural Component Air Support
Used on acft model f-16. c/o 2 ea. bracket p/n 16B1876-7, washer p/n AN960-10l, pin p/n MS20392-2C29, pin p/n MS24665-1012
01-112-6997
Structural Component Air Support
Used on f-15, eagle aircraft.
01-112-7009
Airfoil Rib
Used on F-15.
01-112-7010
Airfoil Rib
Used on F-15.
01-112-7013
Aircraft Skin
Used on a-10 airplane.. 22.250" overall length 9.690" overall width heat treat per T6
01-112-7015
Aircraft Stringer
01-112-8837
Aircraft Channel
Used on f-15a/tf-15a acft. 7.870" overall length 4.430" overall width 0.056" material thickness function-rib to main spar, lower forward; matl-6al-4v stk per mil-t-9046 type iii comp-c, cond-annealed
01-112-8838
Aircraft Channel
Used on f-15a/tf-15a acft. 7.870" overall length 4.430" overall width 0.056" material thickness function-spar to rib-main spar, lower forward; matl-6al-4v stk per mil-t-9046 type iii comp-c, cond-annealed
01-112-8839
Aircraft Channel
Used on f-15a/tf-15a. 9.000" overall length 4.430" overall width 0.056" material thickness function-spar to rib-intermediate, lower aft; matl-6al-4v per mil-t-9046 type iii comp-c, cond-annealed
01-112-8840
Aircraft Strut
10.400" overall length 1.300" overall width 0.500" material thickness
01-112-8841
Aircraft Strut
10.400" overall length 1.300" overall width 0.500" material thickness
01-112-8842
Aircraft Strut
10.400" overall length 1.300" overall width 0.500" material thickness
01-112-9382
Structural Component Air Support
Used on c-5a acft.
01-112-9388
Aircraft Skin
Used on F-111.
01-112-9389
Aircraft Spar
65.000" overall length 4.000" overall width 0.080" material thickness
01-112-9391
Aircraft Spar
77.000" overall length 4.000" overall width 0.080" material thickness
01-113-0201
Structural Component Air Support
Used on EH-60A.
