01-113-0213
Structural Component Air Support
Used on uh-60a helicopter.
01-113-0230
Structural Component Air Support
Used on uh-60a helicopter.
01-113-0448
Aircraft Fairing
Used on 1520010350266 and 1520010820686. 0.625" material thickness
01-113-1412
Structural Component Air Support
01-113-1413
Aircraft Channel
Used on f-15a/tf-15a. 7.920" overall length 4.430" overall width 0.056" material thickness function-spar to rib-rear lower forward; matl-6al-4v per mil-t-9046 type iii cmpsn-c cond-annealed
01-113-1414
Aircraft Former
7.920" overall length 4.430" overall width 0.056" material thickness function-spar to rib-rear lower forward
01-113-1465
Structural Aircraft Plate
81.000" overall length 19.000" overall width 1.250" material thickness mmx-149
01-113-1466
Structural Aircraft Plate
Function-splice plate, inner-lower XW155.024; matl-al alloy 2124 T851 qq-a-250/4 T851 mms-149; dim.-81.000 in. lg, 19.000 in. w, 1.250 in. thk
01-113-1467
Structural Aircraft Plate
82.000" overall length 8.000" overall width 1.250" material thickness mms-149
01-113-1468
Structural Aircraft Plate
82.000" overall length 8.000" overall width 1.750" material thickness function-splice plate; mms-149
01-113-1469
Structural Aircraft Plate
82.000" overall length 8.000" overall width 1.750" material thickness function-splice plate; mms-149
01-113-1927
Structural Aircraft Panel
Used on c-5a acft. c/o panel p/n 4W54010-109a; retainer p/n 4W54010-117a; matl glass fabric, mil-c-9084, type 8b; used from wing to fuselage fairing, wing station 120.361
01-113-1928
Structural Aircraft Panel
Used on c-5a acft. matl glass fabric, mil-c-9084, type 8b; used on wing to fuselage fairing, wing station 120.361
01-113-1929
Structural Aircraft Panel
Used on c-5a acft. matl glass fabric mil-c-9084, type 8b; used on wing to fuselage fairing, wing station 120.361
01-113-1930
Structural Aircraft Panel
Used on C-5A. matl glass fabric mil-c-9084, type 8b; used on wing to fuselage fairing, wing station 120.361
01-113-1931
Structural Aircraft Panel
With fabric
01-113-1932
Structural Aircraft Panel
Used on c-5a acft. matl glass fabric mil-c-9084, type 8b; used on wing to fuselage fairing, wing station 120.361
01-113-1933
Structural Aircraft Panel
Used on c-5a acft. matl glass fabric mil-c-9084, type 8b; used on wing to fuselage fairing, wing station 120.361
01-113-1934
Structural Aircraft Panel
With fabric
01-113-1935
Structural Aircraft Plate
Used on c-5a acft.
01-113-1936
Structural Aircraft Plate
Used on c-5a acft.
01-113-1937
Structural Aircraft Plate
Used on c-5a acft. c/o plate p/n 4P11049-117b; inserts 2, p/n MS21209F1-20p; used on deflector vent end seal, aspiscrub system
01-113-2400
Aircraft Bulkhead
Main landing gear well, fwd
01-113-2402
Aircraft Fairing
01-113-2403
Aircraft Fairing
01-113-2406
Structural Component Air Fitting
Matl: saum forging; temper T73
01-113-2408
Structural Component Air Fitting
Matl: steel forging AMS6526
01-113-2409
Structural Component Air Fitting
Matl: alum forging; temper T73
01-113-3092
Aircraft Bulkhead
Fwd equipment bay assembly
01-113-3093
Aircraft Frame
4.520" overall length 3.630" overall width 0.050" material thickness
01-113-3103
Structural Component Air Support
Used on b52/cmi. 356-T6 per AMS4260; finish f-2.20 plus f-12.37 plus f-12.101
01-113-3130
Aircraft Channel
Used on f-15a/tf-15a. 6.440" overall length 4.370" overall width 0.056" material thickness function-spar to rib-main upper aft; matl-6al-4v
01-113-3131
Aircraft Channel
Used on f-15a/tf-15a. 6.440" overall length 4.370" overall width 0.056" material thickness function-spar to rib-main, upper aft; matl-6al-4v per mil-t-9046 type iii comp-c cond-annealed
01-113-3132
Aircraft Channel
Used on f-15a/tf-15a acft. 7.400" overall length 4.600" overall width 0.063" material thickness function-spar to rib-rear, upper forward; matl-6al-4v per mil-t-9046 type iii comp-c cond-annealed
01-113-3233
Structural Aircraft Plate
01-113-3393
Bell Crank
Right hand
01-113-4452
Vertical Stabilizer
Used on aircraft model f-14.
01-113-6073
Structural Component Air Support
2.500" overall width retainer-restrictor support tube, nlg
01-113-6481
Structural Aircraft Panel
Used on f-4 aircraft.
01-113-6488
Aircraft Former
Do not use cadmium plated tools on this item
01-113-6489
Aircraft Former
24.500" overall length
01-113-6490
Aircraft Former
7.050" overall length 2.750" overall width 0.063" material thickness
01-113-6493
Aircraft Pylon
01-113-6494
Aircraft Pylon
01-113-6958
Aircraft Door
C/o 1 door assy, misc hardware
01-113-6960
Aircraft Door
C/o 1 door assy, misc hardware
01-113-6961
Aircraft Door
C/o 1 door assy, misc hardware
01-113-6962
Aircraft Door
C/o 1 door assy, misc hardware
