BOEING Search Results

KTH-2161

Abstract: S280W503-2 FC14Z KTH-2161 die JCA34 122-37-9 ASTM-B140 adams russell
Contextual Info: 1. 2. 3. 4. 5. 6. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLES. FOR CABLING INSTRUCTIONS SEE 3-546-1. FOR CRIMPING USE DIE KTH-2161. INTERFACE PER MIL-STD-348, FIG. 313-2. CENTER CONTACT 1-3999-4MA9 SUPPLIED UNASSEMBLED. MARK PACKAGE: KINGS 122-37-9

BACC47

Abstract: EN3545 bacc10 ms24266r BACC63BP BACC45FT Boeing bacc10 Boeing souriau 8522 BACC63CB
Contextual Info: AUTHORIZED DISTRIBUTOR AND/OR ASSEMBLY FACILITY FOR BOEING FQIS HARNESSES B-707/B-727/B-737 B-727 B-737 B-747 B-747 B-747-NG B-757/B-767 B-747-400 B757/B767 10-60479 10-61757 10-61827 60B40037 60B40147 S283A202 S283T025 S283U007 S345T002 Series Series Series

Contextual Info: R E V IS IO N S ISSUE OO 1.2 6 CHANGES ER KH 0 3 1.20 REVISED PER D M F304 E R 35 768 K PL 1 1 /1 0 /1 1 B 0 3 -F3- 1.0 7 1.0 3 34036 0 8 /0 3 /9 2 k O J c=j c o r^ ro to Cvl tD I— t o 2 - 1 5 3 9 - 1 M 27 CUSTOMER NOTES: 1. FOR USE WITH BOEING B M S 1 3 -6 5 OF k ADAMS RUSSELL FC14Z CABLE.

Contextual Info: NOTES: 1. FOR USE WITH BOEING B M S 1 3 -6 5 OE & ADAMS RUSSELL FC 11Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 - 5 4 6 - 1 . 3. FOR CRIMPING USE DIE K T H -2 2 1 4 . 4. INTERFACE PER M IL -S T D -3 4 8 , FIG. 3 1 0 - 1 . 5. CENTER CONTACT 1 - 1 0 2 7 - 4 M A 9 SUPPLIED UNASSEMBLED.

Contextual Info: GSD 34197 1 0 /1 2 /9 2 _ JC A 2977 4:1 sc a le APPROX su r fa c e AREA WAS: E - 1 7 7 2 3 USED ON REF; BOEING JACK, PANEL, BNC GSD JCA 0 8 /0 6 /9 2 d e s ig n jt 0 8 /0 7 /9 2 *• V IS § MAY 2007 - THIS DRAWING BECAME THE PROPERTY OF WINCHESTER ELECTRONICS CORPORATION, WALLINGFORD, CT 06492

Contextual Info: 5 /1 6 -3 2 U N E F -2 A THREAD 2 - 1 5 3 9 -1 M 2 7 _ l _ / ll \ MARK: KINGS 8 9 2 - 3 - 9 DATE CODE NOTES: 1. FOR USE WITH BOEING B M S 1 3 -6 5 OF & ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 - 5 4 6 - 3 .

Contextual Info: NOTES: 1. FOR USE WITH BOEING B M S 1 3 -6 5 OF & ADAMS RUSSELL FC14Z CABLES. 2 . FOR CABLING INSTRUCTIONS SEE 3 - 5 4 6 - 1 . 3 . FOR CRIMPING USE DIE K T H -2 2 0 7 . 4 . INTERFACE PER M IL -S T D -3 4 8 , FIG. 3 1 0 - 2 . 5 . CENTER CONTACT 1 - 1 0 2 9 - 2 M A 9 SUPPLIED UNASSEMBLED.

Contextual Info: REVISIONS ISSUE 1206 2 2 -9 2.21 2 .1 5 - 1.8 2 1.7 6 .66 — * .6 4 CHANGES ER 35256 JC A 1 2 /1 6 /9 3 CN 1 35739 A M JB CN 2 0 8 /1 0 /9 4 38322 TM L REVISED PE R D M F 3 0 4 & ER34270 D CY T NOTES: 1. FOR USE WITH BOEING B M S 1 3 -6 5 OH & ADAMS RUSSELL FC 28Z CABLES.

Contextual Info: honeyüjell/ s s e c 3ÛE D • 4-S S I 0 7 5 □ Q nQ b‘13 7 ■ I H0N3 VDTDemod Preliminary VARIABLE DIFFERENTIAL TRANSFORMER DEMODULATOR This is a Boeing owned design manufactured by Honeywell FEATURES OTHER Programmable electronic interface between a LVDT

126-71-9

Contextual Info: DASH NO. M CODE REVISIONS MADE FROM ER 35795 KH 09/19/94 NJ cn I CN 38250 C BDH 03/14/01 I CO CN 38538 C JPK 04/09/02 STAMP: KINGS 126-71-9 YRWK DATE CODE DEEP X WIDE (3 GROOVES) NOTES: 1. FOR USE WITH BOEING S280W503-3 & ADAMS RUSSELL FC20Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-1.

KTH-2229

Contextual Info: GSD REVISIONS ch an ges ER 35534 KH 04/15/94 ISO O CT CN 35776 E KH 02/24/95 I Osl o CN 38323 E TML 06/18/01 I CO NOTES: 1. 2. 3. 4. 5. 6. FOR USE WITH BOEING S280W503-6 & ADAMS RUSSELL FC48Z CABLES. FOR CABLING INSTRUCTIONS SEE 3-546-2. FOR CRIMPING USE DIE KTH-2229.

Contextual Info: REVISIONS GSD 1.585 1.525 CHANGES ER KH KD 33861 04/20/92 O cn 2—1543—1M27 I .02 4^ 3 HOLES OO I CO NOTES: 1. FOR USE WITH BOEING S280W503-4 & ADAMS RUSSELL FC28Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE DIE KTH-2212. 4. INTERFACE PER MlL-STD-348, FIG. 304=1.

755-78-9

Contextual Info: DASH NO. U CODE M ADE FROM NOTES: 1. FOR USE WITH BOEING S280W503-2 à ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3=546=1. 3. FOR CRIMPING USE DIE KTH-2161. 4. INTERFACE PER MIL-STD-348, FIG. 301 =1. 5. CENTER CONTACT 1-569-21MA9 SUPPLIED UNASSEMBLED.

Contextual Info: DASH NO. U CODE MADE FROM GSD REVISIONS CHANGES KD ER O KVH 11/04/94 35891 OsJ I KD I CO NOTES: 1. FOR USE WITH BOEING S2 8 0 1 5 0 3 -6 k ADAMS RUSSELL FC48Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE KTH-2229. 4. INTERFACE PER MIL=STD=348t FIG. 304=2.

Contextual Info: REVISIONS = o GSD CHANGES ER KH 34043 08/17/92 cm O ' I -o O I CO \ — 2—1545—1M27 NOTES: 1. FOR USE WITH BOEING S280W503-1 & ADAMS RUSSELL FC11Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3-546-1. 3. FOR CRIMPING USE DIE KTH-2214. 4. INTERFACE PER MIL-STD-348, FIG. 301-1.

Contextual Info: REVISIONS CHANGES ER KH 34067 08/1292 INJ I 4^ O I CO 4 PLACES NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3=546=1. 3. FOR CRIMPING USE DIE KTH-2161. 4. INTERFACE PER MIL-STD-348, FIG. 313=2. 5. CENTER CONTACT (1-507-38MA9) SUPPLIED UNASSEMBLED.

CO 824

Contextual Info: SD 1.79 , 1.73 R E V IS IO N S ch an ges ER KH ro o O si CN 37507 A I 1.47 1.43 34035 08/10/92 VLS cn 11/26/97 I CO - -U 2—1539—1M27 STAMP: KINGS 1203-15-9 YRWK DATE CODE 5/8-24 UNEF-2A TH'D NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE.

1-569-35MA9

Abstract: KTH-2216
Contextual Info: 1.17 1.11 NOTES: 1. FOR USE WITH BOEING S280W503-3 à ADAMS RUSSELL FC20Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3=546=1. 3. FOR CRIMPING USE DIE KTH=2216. 4. INTERFACE PER MIL=STD=348, FIG. 301 = 1. 5. CENTER CONTACT 1-569-35MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 755=93=9

123-22-5

Contextual Info: o 1.19 1.15 YRWK DATE CODE NOTES: 1. FOR USE WITH BOEING S280W503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=1. 3. FOR CRIMPING USE DIE KTH-2161. 4. INTERFACE PER MIL-STD-348, FIG. 313=2. 5. MARK PACKAGE: KINGS 123-22-5 YRWK (DATE CODE)

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-3 k ADAMS RUSSELL FC20Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=1. 3. FOR CRIMPING USE DIE KTH-2216. 4. INTERFACE PER MIL-STD-348, FIG. 313=2. 5. FOR USE WITH .140 MAX. PANEL. 6. CENTER CONTACT 1-507-40MA9 SUPPLIED UNASSEMBLED.

121-44-9

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W 503-2 k ADAMS RUSSELL FC14Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=1. 3. FOR CRIMPING USE DIE KTH-2161. 4. INTERFACE PER MIL-STD-348, FIG. 313=2. 5. FOR USE WITH .140 MAX. PANEL. 6. CENTER CONTACT 1-507-38M A 9 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.

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W 503-6 à ADAMS RUSSELL FC48Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE DIE KTH=2229. 4. INTERFACE PER MIL-STD-348, FIG. 304=2. 5. CONTACT 1 -7 3 1 1-1MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 1 2 0 1 -2 1 -9

S280W503-2

Abstract: MIL-STD-348 301-1
Contextual Info: GSD REVISIONS ER 35913 MJB 11/29/94 en CD CN 37743 B I TML 12/11/98 CD I CO NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-1. 3. FOR CRIMPING USE DIE KTH-2161. 4. CENTER CONTACT 1-504-35MA9 SUPPLIED UNASSEMBLED.