01-216-7722
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/14 to; matl 0.040 in. thk by 2.800 in. w by 5.200 in. lg; u cross section; right appl
01-216-7723
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/14 to; matl 0.040 in. thk by 2.800 in. w by 5.200 in. lg; u cross section; left appl
01-216-7724
Structural Component Air Support
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5 T3; matl 0.040 in. thk by 8.578 in. w by 8.641 in. lg
01-216-7725
Structural Component Air Support
Used on 1560-00-891-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.040 in. thk by 2.062 in. w by 3.453 in. lg
01-216-7922
Access Aircraft Door
Used on aircraft model f-14.
01-216-8105
Wing Landing Flap
01-216-8106
Wing Landing Flap
01-216-8107
Aircraft Leading Edge
Used on aircraft model c-2a.
01-216-8108
Aircraft Leading Edge
Used on aircraft model c-2a.
01-216-8109
Structural Aircraft Panel
01-216-8364
Structural Aircraft Plate
Used on acft model kc-135.
01-216-8365
Structural Component Air Support
Used on c-5 aircraft. fitting assembly-rear bm, elev actuator, outbd, sta 250.756; c/o: -703a fitting (1) , bushing (2) ; opposite -702a; nha 4T30123
01-216-8366
Structural Component Air Support
Used on c-5 aircraft. fitting assembly-rear bm, elev actuator, outbd, sta 250.756; c/o: -704a fitting (1) , bushing (2) ; opposite -701a; nha 4T31023
01-216-8377
Thermal Special Purpo Insulation
01-216-9156
Structural Component Air Support
01-216-9509
Observation Window
01-216-9766
Structural Component Air Support
01-216-9970
Access Aircraft Cover
Used on acft model b-1b. consists of 1 door, 1 cover, 1 tab; nha L8700151
01-216-9972
Access Aircraft Door
Used on acft model f-16c/d usaf. nha 16B6506-15; eff on 5c 0178, 0180, 0182, 0188, 0190, 0192, 0194, 0202, 0204, 0206, 0208, 0212, 0214, 0216, 0218, 0220, 0222, 0224, 0226, 0228, 0233 on, 5d 31, 33, 35, 39 on; supersededby 16B6578-1 ni per ecn 9K252; located at fs 392 to 398
01-216-9973
Access Aircraft Door
Used on acft model b-1b. consists of 2 base, 2 fitting, 4 shim, 1 pad, 1 door assy, misc hardware; nha L3400302
01-217-0126
Structural Component Air Bracket
14.510" overall length 0.500" overall width canopy mounted body positioning hfeatgandle
01-217-0145
Structural Aircraft Plate
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13 to; matl 0.032 in. thk by 4.516 in. w by 4.750 in. lg
01-217-0152
Structural Component Air Support
C/o 1 fitting, 1 plate, adhesive a/r; opp -19; superseded 16W262.16 ow PERECN8H462; eff 5c 0001 9999; nha 16W050-808
01-217-0153
Structural Component Air Support
Used on acft model b-1b. 6al-4v titanium per mil-t-9046, type iii, comp c, cond a; 3.38 in. long, 1.65 in. wide, 0.080 in. thk; nha L3207040
01-217-0180
Thermal Special Purpo Insulation
01-217-0181
Thermal Special Purpo Insulation
01-217-0182
Thermal Special Purpo Insulation
01-217-0969
Structural Component Air Support
14.500" overall length 9.380" overall width
01-217-1373
Structural Component Air Support
C/o 1 fitting, 1 plate, adhesive a/r; opp -20; superseded 16W262-15 ow PERECN8H462; eff 5c 0001 9999; nha 16W050-807
01-217-1374
Structural Component Air Support
C/o 1 fitting, 1 plate, adhesive a/r; opp -20; nha 16W050-807; superseded 16W263-15 ow per ECN8H467; eff 5c 0001 9999
01-217-1375
Structural Component Air Support
C/o 1 fitting, 1 plate, adhesive a/r; opp -19; nha 16W050-808; superseded 16W263-16 ow per ecn 8H467; eff 5c 0001 9999
01-217-1376
Structural Component Air Fitting
17.000" overall length 10.000" overall width
01-217-1377
Structural Component Air Fitting
01-217-1378
Structural Component Air Support
Superseded 16W265-16 ow per ECN8H482; eff 5c 0001 9999; nha 16W050-808
01-217-2279
Structural Component Air Support
Steel, aisi 1095; heat treated, mil-h-6875, rockwell scale c, 46.0 min, 49.0 max; magnetic particle inspected, mil-i-6868; cadmium
01-217-2280
Structural Component Air Support
Used on e-2 aircraft. 5.000" overall length 2.000" overall width 0.036" material thickness
01-217-2281
Structural Component Air Support
Used on e-2 aircraft. 5.000" overall length 2.000" overall width 0.036" material thickness bracket part number 123AV60762-3; clamp assembly 123P60832-7; 2 bolts AV4-12a; 4 washers AN960-416l; 2 nuts MS21042L4
01-217-2527
Structural Component Air Support
01-217-3045
Structural Component Air Support
Steel, aisi 1095 or 4130 or 4140 or 4340 or 6150 or 8630 or 8740, normalized, mil-h-6875; magnetic particle inspected, mil-i-6868; cadmium, qq-p-416, class 2, type 2; primer, epoxy polyamide; paint, acrylic lacquer, gloss, insignia white; flat one side, 2 half clamps, opposite side
01-217-3153
Aircraft Door
01-217-3164
Structural Component Air Support
Used on acft model b-52g/h. opposite p/n -2
01-217-3165
Structural Component Air Support
4.600" overall length 1.400" overall width 0.063" material thickness opp -2; nha 4013561
01-217-3168
Structural Aircraft Panel
Used on f-5e aircraft. matl abs copolymer rigid sheet per mil-p-19904; .047in thick; part of -501 panel assembly-lh, console removable
01-217-3629
Structural Aircraft Plate
01-217-4176
Structural Component Air Support
Steel, mil-s-18729, alloy aisi 4130; bracket part number 123AV60763-11
01-217-4915
Structural Aircraft Plate
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.040 in. thk by 3.891 in. w by 10.250 in. lg
