01-148-0642
Aircraft Former
31.000" overall length 1.800" overall width 0.020" material thickness commercially pure
01-148-0643
Aircraft Former
27.900" overall length 1.700" overall width 0.020" material thickness commercially pure
01-148-0644
Aircraft Former
11.200" overall length 1.800" overall width 0.030" material thickness commercially pure
01-148-0645
Aircraft Former
11.200" overall length 1.800" overall width 0.030" material thickness commercially pure
01-148-0646
Aircraft Former
1.200" overall length 1.400" overall width 0.020" material thickness commercially pure
01-148-0647
Aircraft Former
26.500" overall length 1.300" overall width 0.020" material thickness commercially pure
01-148-0649
Aircraft Former
5.100" overall length 1.300" overall width 0.020" material thickness
01-148-0650
Aircraft Former
26.500" overall length 1.300" overall width 0.020" material thickness
01-148-0651
Aircraft Former
2.500" overall length 1.400" overall width 0.040" material thickness
01-148-0652
Aircraft Former
35.500" overall length 2.100" overall width 0.020" material thickness opp 25-2307-501
01-148-0653
Aircraft Former
1.000" overall length 1.000" overall width 0.125" material thickness finish f-8.05
01-148-0654
Aircraft Former
6.000" overall length 2.000" overall width 0.063" material thickness ht tr to 180, 000 to 200, 000 psi; AL350
01-148-0655
Aircraft Former
6.600" overall length 3.300" overall width 0.040" material thickness compliance with boeing spec 5300
01-148-0656
Aircraft Former
01-148-0658
Aircraft Former
25.300" overall length made from GA3065, alcoa 9802 or 67580
01-148-0659
Aircraft Former
16.500" overall length material-GA3065, alcoa 9802 or 67580
01-148-0660
Aircraft Former
17.100" overall length material-made from GA3065, alcoa 9802 or 67580
01-148-0661
Aircraft Former
14.300" overall length function-tee
01-148-0662
Aircraft Former
14.300" overall length function-tee
01-148-0665
Longeron
64.200" overall length 7.000" overall width 0.040" material thickness
01-148-0666
Longeron
35.900" overall length 5.500" overall width 0.040" material thickness
01-148-0667
Longeron
64.200" overall length 7.000" overall width 0.040" material thickness
01-148-0669
Aircraft Skin
Used on acft model b52. titanium per ams 4901, 0.025 in.thk, 5.700 in.w, 9.700 in.lg, rh
01-148-0671
Aircraft Skin
Used on acft model b52. titanium per ams 4901, 0.025 in.thk, 9.700 in.w, 57.000 in.lg, left hand
01-148-0673
Aircraft Skin
Used on b-52 aircraft. material-al clad 2024-0 per qq-a-250/5, heat treated to T4; location -tail fairing installation, outboard strut; wing
01-148-0674
Aircraft Skin
Used on b-52 aircraft. material-cres steel sheet aisi 302 mil-s-5059 comp d annealed, surface cond 2d; left hand; location-tail fairing installation, outboard strut, pp station 245.00
01-148-0675
Aircraft Skin
Used on B-52. 95.000" overall length 22.000" overall width 6A1-4v per bms 7-39; finish f 10.10; opposite p/n -12
01-148-0676
Aircraft Skin
Used on B-52. 18.000" overall length 12.000" overall width 6A1-4v, bms 7-39; finish f 10.10; opposite p/n -12
01-148-0677
Aircraft Skin
Used on B-52. 18.000" overall length 12.000" overall width 6A1-4v, bms 7-39; finish f 10.10; opposite p/n -11
01-148-0678
Aircraft Skin
Used on b-52 aircraft. location-tail fairing installation-outboard strut, right hand; material-cres steel sheet aisi 302 mil-s-5059, comp d annealed, surf cond 2d; pp 245.00 station
01-148-1330
Structural Aircraft Panel
Used on aircraft model f-18.
01-148-1386
Stabilizer Aircraft Fairing
Used on aircraft model ch-53e. cognizant service:navy;
01-148-1387
Aircraft Fairing
Used on aircraft model ch53e.
01-148-1729
Access Aircraft Door
Used on t-39 aircraft. provides access to oxygen equipment, lh
01-148-1971
Access Aircraft Cover
Used on b-1b acft. same as -011 except change exterior coating; nha L3005999; used on fuslg side tailcone radome
01-148-1972
Access Aircraft Cover
Used on b-1b acft.
01-148-2008
Aircraft Wing Assembly
Wing box assy
01-148-2018
Stiffener Aircraft Rib
01-148-2019
Aircraft Stiffener
01-148-2020
Aircraft Stiffener
01-148-2021
Aircraft Stiffener
01-148-2022
Stiffener Aircraft Rib
01-148-2047
Structural Aircraft Panel
Used on EF-111. radar absorbing
01-148-2049
Structural Aircraft Panel
Used on EF-111. radar absorbing
01-148-2050
Structural Aircraft Plate
20.100" overall length 18.500" overall width 0.090" material thickness used as doubler
01-148-2051
Structural Aircraft Plate
20.100" overall length 18.500" overall width 0.090" material thickness opposite p/n 25-2353-511; used as doubler
01-148-2052
Structural Aircraft Plate
5.900" overall length 2.900" overall width 0.063" material thickness opposite p/n 25-2353-5/4; used as doubler
01-148-2053
Structural Aircraft Plate
5.900" overall length 2.900" overall width 0.063" material thickness opposite p/n 25-2353-5/3; used as doubler
01-148-2054
Structural Aircraft Plate
Function-web assembly
01-148-2055
Structural Aircraft Plate
Function-web assembly
