01-047-9616
Structural Aircraft Plate
13.000" overall length internal heat shield
01-047-9617
Structural Aircraft Plate
17.000" overall length shield, internal heat
01-047-9644
Structural Aircraft Plate
Used on acf model f-16. located from fuselage station 375.48 to fs 381.78
01-047-9645
Structural Component Air Support
Used on acft model f-16.
01-047-9648
Longeron
Used on acft model f-16. located from lower center station 279.40 to 341.80;
01-047-9649
Longeron
Used on acft model f-16. located from lower center station 279.40 to 341.80;
01-047-9652
Aircraft Skin
Used on acft model f-16. 96.000" overall length 18.000" overall width
01-048-0331
Aircraft Pylon
01-048-0693
Thermal Special Purpo Insulation
End item identification:aircraft, model f-4e
01-048-1270
Structural Aircraft Plate
Aluminum alloy-4.030 in. long, 2.800 in. wide, 0.050 in. thick
01-048-1433
Wing Aircraft Fairing
01-048-1775
Structural Component Air Support
1.200" overall length 0.090" overall width
01-048-1786
Aircraft Windshield Panel
01-048-1795
Aircraft Skin
Used on acft f-16. matl per gen dyn spec P6102-1, 22.400 in. oa lg, 3.800 in. w first end, 4.560 in. wide second end, used on tail hook fitting fairing
01-048-1798
Structural Component Air Fitting
7.000" overall length access door hinge connection
01-048-1802
Structural Component Air Support
2.100" overall length 2.250" overall width frame attachment fitting
01-048-1934
Access Aircraft Cover
Used on acft model f-16a.
01-048-1986
Airfoil Rib
21.200" overall length 5.300" overall width 0.050" material thickness
01-048-1987
Airfoil Rib
12.500" overall length 10.300" overall width 0.032" material thickness
01-048-1988
Aircraft Skin
Used on acft model f4-a/c. aluminum alloy qq-a-28 cond T6, 11.47 in. w, 21.17 in. lg, .040 in. thk.
01-048-1989
Aircraft Skin
Used on F-16. 55.000" overall length 15.000" overall width
01-048-2687
Access Aircraft Door
Eff 0004 on; nha 16B003-1; located fs 446.10 to fs 453.20; acft f-16
01-048-2869
Structural Component Air Bracket
01-048-2872
Structural Aircraft Plate
01-048-2873
Structural Aircraft Plate
01-048-2887
Aircraft Former
Superseded p/n 16B5802-18 ow ecn 54896; nha p/n 16B5250-815; eff 0007-0032
01-048-2894
Wing Landing Flap
Used as: flap assembly
01-048-2898
Structural Aircraft Panel
01-048-2908
Structural Component Air Support
Used on acft model f-16. alum.alloy per qq-a-362, comp 6061-T6, located on sill upper longeron, fs 236.00
01-048-2909
Structural Component Air Support
Used on acft model f-16. alum.alloy per qq-a-362, comp 6061-T6, located at upper sill longeron, fs 236.00
01-048-2917
Aircraft Skin
Used on acft model f-16a. 54.000" overall length 41.000" overall width located lower left hand from FS189 to FS243, nha 16B1933-3; eff 0007-on; superseded p/n 16B1313-31 ni ecn 45173
01-048-2918
Aircraft Skin
Used on acft model f-16. 55.000" overall length 17.000" overall width located on lower right hand from fuselage station 189.06 to 243
01-048-3043
Bell Crank
0.3745" bore diameter
01-048-3100
Structural Component Air Support
Used on t-2b aircraft. steel, mil-t-6736, comp 4130, cond n tube matl
01-048-3386
Access Aircraft Door
Used on f-16a/b. rh fire access FS361 to FS369
01-048-3388
Structural Component Air Support
Used on acft model f-16a/b usaf. alum.alloy 7075-T73, per qq-a-367, comp 7075, located at fuselage station 344.24; eff 0007-on; nha 16B560-1
01-048-4535
Structural Component Air Support
Used on acft model f-16. located at fuselage stations 196, 203
01-048-4536
Structural Component Air Support
Used on acft model f-16. located at fuselage stations 196, 203
01-048-4537
Structural Component Air Support
Used on acft model f-16. located on right hand upper side at fuselage stations 196, 203
01-048-4551
Aircraft Skin
Used on F-16. 22.000" overall length 3.000" overall width
01-048-4552
Aircraft Skin
Used on F-16. 32.000" overall length 3.000" overall width
01-048-5032
Access Aircraft Door
01-048-5087
Aircraft Frame
18.000" overall length 7.000" overall width 0.063" material thickness
01-048-5089
Aircraft Frame
30.000" overall length 10.000" overall width 0.050" material thickness
01-048-5090
Aircraft Bulkhead
Split canted fuel
01-048-5096
Aircraft Bulkhead
Fixed canopy
01-048-5101
Access Aircraft Door
Used on F-16. 13th stage connector lh access
01-048-5105
Access Aircraft Door
Used on f-16a and f-16b. used on 7th stage connector, lh door
01-048-5167
Structural Component Air Support
Used on acft model f-16. located at fuselage station 229.68
01-048-5168
Structural Component Air Support
Used on acft model f-16. located at fuselage station 229.68
