KTH-2211 DIE Search Results

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 304-2. 5. FOR USE WITH .22 MAX PANEL. 6. CENTER CONTACT 1-534-89MA9 SUPPLIED UNASSEMBLED.

MC 3041

Abstract: FC14Z 1205-47-9 KTH-2211 die KTH-2211 S280W503-2
Contextual Info: 1.53 1.47 •JJ 0. 3 HOLES — NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348. FIG. 304-1. 5. CENTER CONTACT (1 -547-47MA9) SUPPLIED UNASSEMBLED.

1-534-89MA9

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 304-2. 5. FOR USE WITH .22 MAX PANEL. 6. CENTER CONTACT 1-534-89MA9 SUPPLIED UNASSEMBLED.

MIL-45204

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 304=2. 5. FOR USE WITH .22 MAX PANEL. 6. CENTER CONTACT 1-534-89MA9 SUPPLIED UNASSEMBLED.

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348. FIG. 309-2. 5. FOR USE WITH .075 MAX. PANEL. 6. CENTER CONTACT 1-5917-2MA9 SUPPLIED UNASSEMBLED.

Contextual Info: 2. 3. 4. 6. 7. 8. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . FOR CRIMPING USE DIE KTH-2211. INTERFACE PER MIL-STD-348, FIG. 304-2. FOR USE WITH .075 MAX. PANEL. CENTER CONTACT 1-534-96MA9 SUPPLIED UNASSEMBLED. MARK PACKAGE: KINGS 2 9 7 1 - 8 - * - = — v

S280W503-2

Contextual Info: 1.655 1.595 NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 309-1. 5. CENTER CONTACT 1-903-22MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 825-10-9

KTH-2211

Contextual Info: 1.94 1.86 STAMP: KINGS 2975-4- * YRWK DATE CODE NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG). 304-1 (EX. KEYING). 5. CENTER CONTACT (1-547-47MA9) SUPPLIED UNASSEMBLED.

Contextual Info: 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. FOR CABLING INSTRUCTIONS SEE 3-546-2. FOR CRIMPING USE DIE KTH-2211. FOR USE WITH .188 MAX. PANEL. CENTER CONTACT 1-842-23MA9 SUPPLIED UNASSEMBLED. INTERFACE PER MIL-STD-348. FIG. 302-2.

S280W503-2

Contextual Info: SD REVISIONS ER JCA <LO CT 33875 04/16/92 CN 37437 A I VLS 09/08/98 cn I co NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348 FIG. 302-1.

S280W

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W 503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 304=2. 5. FOR USE WITH .22 MAX PANEL. 6. CENTER CONTACT 1-534-89M A 9 SUPPLIED UNASSEMBLED.

1-547-47MA9

Contextual Info: 1.53 NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 304-1. 5. CENTER CONTACT 1-547-47MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 120 5-4 7-9

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348 FIG. 302-1. 5. CENTER CONTACT 1-534-91MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 7 9 6 -1 5 -9

Contextual Info: DASH NO. M CODE MADE FROM NOTES: 1. FOR USE WITH BOEING S280W 503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 3 0 2 -1 . 5. CENTER CONTACT 1 - 9 0 3 -2 2 SUPPLIED UNASSEMBLED.

FC14Z

Abstract: KTH-2211 die S280W503-2 KTH-2211 1-534-91MA9
Contextual Info: REVISIONS ER 35655 KH 08/29/94 oo IS J CT CN 37437 A I VLS 09/08/98 OO I CO NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 309-1.

S280

Abstract: S280W503-2
Contextual Info: SD REVISIONS OMMGCS ER JCA CO CD 33875 04/16/92 CN 37437 A VLS 09/08/98 I cn I co NOTES: 1. FOR USE WITH BOEING S280W503-2 ft ADAMS RUSSELL FC142 CABLES. 2. FOR CABUNG INSTRUCTIONS SEE 3-546-2. 3. FOR CRMPMG USE DIE KTH-2211. 4. WTERFACE PER »«.-STD-348 FIG. 302-1.

S280W503-2

Contextual Info: SD REVISIONS ER JCA hO o 33876 04/14/92 OJ CN 37437 A I VLS 09/10/98 -Fa. I CO FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. FOR CABLING INSTRUCTIONS SEE 3-546-2. FOR CRIMPING USE DIE KTH-2211. INTERFACE PER MIL-STD-348. FIG. 304-2. CENTER CONTACT 1-534-89MA9 SUPPLIED UNASSEMBLED.

S280W503-2

Contextual Info: 2.14 -O 2.22 \ V o .010 DEEP x -j 5 WIDE 2 GROOVES .020 I / o / > .04 D. (3 HOLES) • .02 NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 309-1 (EX. KEYING).

s280w503-2

Contextual Info: REVISIONS SD .73 TYP. .71 ISSUE CHANGES ER 33873 KH 04/14/92 I CN 37437 A VLS 09/09/98 1 I CO NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211. 4. INTERFACE PER MIL-STD-348, FIG. 304-2.

Contextual Info: 1.53 1.47 O •j£ D. 3 HOLES — £. 3. 4. 5. 6. ru n lA D L IN U IIPIIOmUL-IIIIUinilO O LL J= JW fO = Z . FOR CRIMPING USE DIE KTH-2211. INTERFACE PER MIL-STD-348, FIG. 304=1. CENTER CONTACT (1-547-47M A 9) SUPPLIED UNASSEMBLED. MARK PACKAGE: KINGS 1 2 0 5 -4 7 -9

mc 17410

Contextual Info: SD REVISIONS ER JCA ro o 33876 04/14/92 CN 37437 A C jn J I VLS 09/10/98 I CO FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. FOR CABLING INSTRUCTIONS SEE 3-546-2. FOR CRIMPING USE DIE KTH-2211. INTERFACE PER MIL-STD-348, FIG. 304-2. CENTER CONTACT 1-534-89MA9 SUPPLIED UNASSEMBLED.

1206-21-9

Abstract: 1-534-91MA9
Contextual Info: REVISIONS CHANGES ER 34034 KH 08/06/92 ISO cn> O CN 34086 E MJB 08/19/92 I ro CN 37437 A VLS 09/09/98 I CN 38324 E TUL 06/19/01 CO NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3-546-2. 3. FOR CRIMPING USE DIE KTH-2211.

S280W503-2

Abstract: kings kv19-19
Contextual Info: REVISIONS NO ER KH 34034 08/06/92 O cn CN 34086 E MJB 08/19/92 I ho CN 37437 A VLS 09/09/98 I CN 38324 E TML 06/19/01 to NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2211.

Contextual Info: SD REVISIONS CHANGES ER JCA ND O 33876 04/14/92 CN I VLS 37437 A 09/10/98 4^ I CO FOR USE WITH BOEING S280W 503-2 k ADAMS RUSSELL FC14Z CABLES. FOR CABLING INSTRUCTIONS SEE 3=546=2. FOR CRIMPING USE DIE KTH-2211. INTERFACE PER MlL=STD=348, FIG. 304=2. CENTER CONTACT 1-534-89M A 9 SUPPLIED UNASSEMBLED.