01-160-2685
Access Aircraft Door
Used on T-33.
01-160-2686
Access Aircraft Door
Used on T-33.
01-160-2885
Access Aircraft Door
Used on f-16 aircraft. for access to quick disconnect
01-160-2886
Access Aircraft Door
01-160-3008
Structural Aircraft Plate
Used on B-52. alter BAC1512-202 x .60
01-160-3009
Structural Aircraft Plate
2.900" overall length 1.500" overall width 0.040" material thickness commercially pure
01-160-3011
Structural Component Air Support
01-160-3013
Structural Aircraft Panel
Used on B-52. 12.600" overall length 5.500" overall width
01-160-3014
Structural Component Air Support
Used on b-52 aircraft. used on rear spar, inboard; make from p/n 25-2669-1 forging, 4335 mod. steel per spec ams 6428 forge per mil-f-7190 grade a
01-160-3022
Structural Component Air Support
C/o web, 2; doubler, 2; shear tie; bracket; stiffener, 2; mid chord spar; miscellaneous hardware
01-160-3077
Structural Aircraft Panel
Used on c/kc-135. 11.500" overall length 9.600" overall width finish f-2.115
01-160-3078
Structural Aircraft Plate
20.000" overall length 20.000" overall width 0.025" material thickness used as doubler; opposite pn 25-2304-15
01-160-3079
Structural Aircraft Plate
7.000" overall length 7.000" overall width 0.063" material thickness used as doubler
01-160-3080
Structural Aircraft Plate
7.000" overall length 7.000" overall width 0.063" material thickness used as doubler; opposite pn 25-2304-17
01-160-3081
Structural Aircraft Plate
6.500" overall length 5.500" overall width 0.050" material thickness used as end plate; opposite pn 25-2668-807
01-160-3082
Structural Aircraft Plate
20.000" overall length 20.000" overall width 0.025" material thickness used as doubler
01-160-3083
Structural Aircraft Plate
10.200" overall length 9.900" overall width 0.090" material thickness used as doubler
01-160-3084
Structural Aircraft Plate
55.300" overall length 17.200" overall width 0.050" material thickness used as web
01-160-3085
Structural Aircraft Plate
55.000" overall length 17.200" overall width 0.050" material thickness used as web; opposite pn 25-2354-52
01-160-3086
Structural Aircraft Plate
6.000" overall length 0.063" material thickness opposite p/n 25-2354-524; used as doubler
01-160-3087
Structural Aircraft Plate
6.000" overall length 2.500" overall width 0.063" material thickness opposite p/n 25-2354-523; used as doubler
01-160-3088
Structural Aircraft Plate
22.000" overall length 1.150" overall width 0.125" material thickness comp 4335
01-160-3089
Structural Aircraft Plate
50.500" overall length 0.050" material thickness 6al-4v
01-160-3090
Structural Aircraft Plate
7.300" overall length 7.100" overall width 0.071" material thickness 6al-4v
01-160-3091
Structural Aircraft Plate
41.600" overall length 10.700" overall width 0.050" material thickness 6al-4v
01-160-3092
Structural Aircraft Plate
10.900" overall length 5.900" overall width 0.050" material thickness 6al-4v
01-160-3093
Structural Aircraft Plate
11.200" overall length 1.000" overall width 0.020" material thickness 6al-4v
01-160-3094
Structural Aircraft Plate
21.000" overall length 1.250" overall width 0.250" material thickness opposite pn 25-2355-44
01-160-3095
Structural Aircraft Plate
Used on B-52. stock size
01-160-3096
Structural Aircraft Plate
41.000" overall length 11.000" overall width 0.050" material thickness 6al-4v
01-160-3097
Structural Aircraft Plate
11.000" overall length 11.000" overall width 0.050" material thickness 6al-4v
01-160-3098
Structural Aircraft Plate
6.200" overall length 1.150" overall width 0.032" material thickness
01-160-3099
Structural Aircraft Plate
15.300" overall length 1.300" overall width 0.063" material thickness 6al-4v
01-160-3100
Structural Aircraft Plate
Stock size
01-160-3101
Structural Aircraft Plate
33.100" overall length 10.600" overall width 0.100" material thickness
01-160-3102
Structural Aircraft Plate
49.500" overall length 2.600" overall width 0.020" material thickness
01-160-3103
Structural Aircraft Plate
33.100" overall length
01-160-3104
Structural Aircraft Plate
Used on b-52 aircraft. rused as doubler on tail fairing installation right hand inboard strut; matl-corrosion resistant steel sheet type aisi 301 1/4 hard mil-s-5059 comp 301 surface cond 2d; dimensions-8.000 in. lg, 2.300 in. w, 0.025 in. thk
01-160-3105
Structural Aircraft Plate
Used on b-52 aircraft. used as doubler on tail fairing installation right hand inboard strut; matl-corrosion resistant steel sheet type aisi 301 1/4 hard mil-s-5059 comp 301 surface condition 2d; dimensions-8.100 in. lg, 1.700 in. w, 0.025 in. thk
01-160-3106
Structural Aircraft Plate
Used on b-52 aircraft. nused as web on tail fairing installation right hand inboard strut; matl-corrosion resistant steel sheet aisi 302 m-s-5059 comp 302 annealed surface condition 2d; dimensions-30.000 in. lg, 30.000 in. w, 0.025 in. thk
01-160-3107
Structural Aircraft Plate
Used on acft model b52. cres steel aisi 301 per mil-s-5059 1/4 hard cond 2d, 0.025 in.thk, 5.750 in.w, 7.600 in.lg, used on tail fairing, outboard strut
01-160-3108
Structural Aircraft Plate
Used on acft model b52. cres steel aisi 301 per mil-s-5059 comp d annealed cond 2d, 0.028 in.thk, 1.400 in.w, 15.500 in.lg, used on tail fairing, outboard strut
01-160-3109
Structural Aircraft Plate
Used on acft model b52. cres steel aisi 301 per mil-s-5059 comp d annealed cond 2d, 0.020 in.thk, 1.400 in.w, 12.300 in.lg, used on tail fairing, outboard strut
01-160-3110
Structural Aircraft Plate
Used on acft model b52. cres steel aisi 301 per mil-s-5059 comp d annealed, 0.020 in.thk, 1.400 in.thk, 15.500 in.lg, used on tail fairing, outboard strut, right hand
01-160-3111
Structural Aircraft Plate
Used on B-52.
01-160-3112
Structural Aircraft Plate
Used on B-52.
01-160-3114
Aircraft Fairing
01-160-3115
Aircraft Fairing
01-160-3118
Structural Component Air Support
9.100" overall length 6.100" overall width 0.040" material thickness
