Engine Components » Valve Caps

02-15245
0215245

2915-00-831-6933

008316933

04050
04050

2995-01-252-9498

012529498

1211-517986
1211517986

2915-00-700-7545

007007545

1411-587681
1411587681

2915-00-671-0274

006710274

Used on 29156211675.

1411-587682
1411587682

2915-00-671-0276

006710276

Used on 29156211675.

1422-566842
1422566842

2915-00-787-1201

007871201

anodize per mil-a-8625 type 2; irregular shape

158667-1
1586671

2915-01-296-8825

012968825

Used on aircraft model hu25a oil/fuel heater system. aluminum alloy, 1.250 in.lg; width 1.781 in.; includes three drilled mounting holes 0.219 in.dia.

16BS100C2
16BS100C2

2915-00-963-9505

009639505

18249
18249

2995-00-909-9937

009099937

18971
18971

2915-00-909-9117

009099117

Used on ab spraybar assy,ge 5014t67,5019t91 and 5040t18,t19,for j85 acft engine. cres per AMS5353; end cap seats on valve subassy

20600
20600

2995-00-909-1211

009091211

23008236
23008236

2995-01-323-5672

013235672

steel, corrosion resisting, ams 5651; 2.154 in. lg; 1.380 in. w; threaded 0.4375-20 unjf 3a; two holes 0.217 in. min

232-36956-2
232369562

2995-01-126-5007

011265007

Used on mhu-159/e. plug assembly, alignment; c/o p/n 232-36952-1

2650634
2650634

2915-01-234-8597

012348597

Used on aug fuel control,p/n 441418,for f100-pw-220 acft eng. functional description:part of segment cutoff valve assy; cognizant service:air force; alum alloy 1.87 in.od x 0.36 in.h, boss 0.68 in.h, 0.50 in.od at end; bore 0.1562 in.dia drill thru, 0.2969 in.dia flat bottom drill 0.385 in.max dp; external seal groove 1.71 in.dia 0.41 in.w;

2663995
2663995

2915-01-224-2193

012242193

Used on enc control assy,p/n 441290-5,for f100-pw-220 acft eng.

2664284
2664284

2915-01-221-0052

012210052

Used on aug fuel control,p/n 441418,for f100-pw-220 acft eng. alum alloy; 2.250 in. l by 1.420 in. dia by 0.34 in. thk w/hole thru each end 0.23 in. dia; body 0.18 in. h, 1.12 in. od, 1.05 in. max id 0.24 in. dp, cen bore 0.44 in. dia 0.06 in. dp

2664371
2664371

2915-01-222-3814

012223814

Used on main fuel control,p/n 441396,for f100-pw-220 acft eng.

2671413
2671413

2915-01-220-6850

012206850

2712491
2712491

2915-01-326-8588

013268588

Used on f-15a aircraft. used on automatic crossfeed checkvalve

2721436
2721436

2915-01-202-3228

012023228

Used on pilot valve,2710738m3,b-1b aircraft fuel system. alum alloy 6061-T651 per qq-a-225/8, anodize; 0.46 in. h, 0.70 in. od w/0.838 in. dia flange 0.060 in. thk, 0.625 in. id; hole thru top cen 0.135 in. dia, 4 holes thru wall eq sp 0.12 in. dia

3174546-1
31745461

2995-01-325-5065

013255065

3175093-1
31750931

2995-01-316-9248

013169248

Used on uh-60l/ah-64a engine (t701c). o/a width 4.425 in. min, 4.445 in. max; o/a height 1.485 in. min, 1.505 in. max; contains 5 holes 0.218 in. min, 0.226 in. max diameter thru flange

3201-16364-20-1
320116364201

2915-01-266-5326

012665326

320410
320410

2995-01-212-9845

012129845

321218
321218

2995-01-212-9846

012129846

321428
321428

2995-01-212-9847

012129847

4061T38P01
4061T38P01

2915-01-144-4261

011444261

Used on aircraft engine f404-ge-400. cres ams 5637, 0.600 in. min, 0.620 in. max lg.

40A669
40A669

2995-01-287-7430

012877430

456021
456021

2995-00-755-7434

007557434

steel, ams 6322 comp 8740; 1.610 in. min

5007650
5007650

2915-01-205-1274

012051274

Used on augm fuel pump,p/n 9338m20p05,for f110 acft eng. body 1.125 in. h, 0.890 in. min id; 2 mtg tabs flush w/top 0.188 in. thk, port cen top 0.562 in. max dia

5008434
5008434

2915-01-262-2641

012622641

Used on for f101eng. matl wrought aluminum per ams 4117; 1.308 in.long; 1st end threaded, 1.3125-12 unj-3a; 1.197 in.groove od; 1.625 in.flange od; 2nd end hex head 0.875 in.across with one hole 0.096 in. dia thru

512266
512266

2915-00-723-7477

007237477

acft engine fuel control; alum alloy ams 4120 or HS145 class 3, grade c; anodized per ams 24780; 0.240 in. lg

524502
524502

2915-00-719-8688

007198688

543548
543548

2915-00-738-9208

007389208

1.360" overall length 0.809" outside diameter alum alloy qq-a-200/8a, T6 or ams 4150; rockwell hardness rating 49, 5r 30t min; heat treated per mil-h-6088 united aircraft spec no. HS454

543553
543553

2915-00-962-9026

009629026

544-0200-00-0
5440200000

2915-01-322-3597

013223597

2.252 in. min, 2.258 in. max lg from flange to end of rod; item c/o valve cover p/n 044-1190-00-0; set screw p/n 018-1102-72-0; piercing rod p/n 012-1080-00-0

576765
576765

2915-00-976-3493

009763493

696654
696654

2995-00-863-1098

008631098

727121
727121

2995-01-151-0819

011510819

Used on aircraft engine f404-ge-400. 1.423" overall length

74A650085-2001
74A6500852001

2915-01-246-3168

012463168

755291-1
7552911

2915-01-066-8838

010668838

Used on jfc110 f100 engine. acft engine fuel systems components

764953-1
7649531

2915-01-083-6805

010836805

Used on t700-ge series turbine engine.

776779-1
7767791

2915-01-174-8126

011748126

Used on ch-47 turbine engine, rotary wing aircraft.

786168-1
7861681

2915-01-326-8589

013268589

Used on valve fuel shutoff.

790089-2
7900892

2915-01-323-1112

013231112

792004-1
7920041

2915-01-326-5081

013265081

792368-2
7923682

2915-01-323-1113

013231113

RD37106-1
RD371061

2995-01-319-8817

013198817

Used on nha lube and scavenge pump assy,r/n rr37170d.

U520192
U520192

2935-00-858-0756

008580756

U524701
U524701

2915-00-719-7340

007197340

Valve Caps. 213 part numbers in this category