BOEING 76 Search Results

BACC63 Series

Abstract: BACC63 BACC10GH BOEING bacc63 BACC45FT BACC63BP bacc10 BACC10JS BACC45FN BACC45
Contextual Info: CYLINDRICAL C48 Series/MIL-C-26500 Accessories & Application Tooling Boeing: BACC45 / BACC63 Series MIL-C-26500 C48 Series Introduction • Qualified to MIL-C-26500. ■ Styles qualified to Boeing BACC45 Series. FEATURES ■ Styles qualified to Boeing BACC63 Series.

vor antenna

Abstract: DM N56-1 Antenna VOR aircraft VHF receiver VOR Antenna design Boeing 787 N56-1 aircraft part number
Contextual Info: NAVIGATION DM N56-1 VOR ANTENNA The DM N56-1, designed for the Boeing 757 and 767 aircraft, provides a concept that can be incorporated in many aircraft designs to provide integral VHF navigation systems performance. The DM N56-1 free standing, balanced-loop array

BACC63BP

Abstract: BACC63BPXX bacc63BV BACC63B MIL-C-26500 pyle
Contextual Info: MIL-C-26500/Boeing BACC63BP/BV aluminum/stainless steel ratchet lock plug, mating flange receptacle RATCHET LOCK PLUG Stainless Steel/Aluminum Pyle ZZY-RC/AC-12XX* Seríes BACC63BPXX* M THREAD .310 MIN MATING FLANGE MOUNTED, THREADED RECEPTACLE Stainless Steel/Aluminum

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

ms90362-3

Abstract: BACC47 en3545 BACC65 bacc10 ms3459 backshell BACC63BP BACC66 ms24266r ms90362
Contextual Info: AUTHORIZED DISTRIBUTOR AND/OR ASSEMBLY FACILITY FOR BOEING FQIS HARNESSES B-707/B-727/B-737 10-60479 B-727 10-61757 B-737 10-61827 B-747 60B40037 B-747 60B40147 B-747-NG S283A202 B-757/B-767 S283T025 B-747-400 S283U007 Series Series Series Series Series Series

CN0966

Abstract: MS24266 BACC45FN MS24266R22 MS24265 "1.6 - 20 UNEF-2A BACC45FT mil-c-26500 C0909 1.062-18
Contextual Info: MIL-C-26500 C48 Series Introduction GENERAL DESCRIPTION The C48 Series describes a family of connectors qualified to MIL-C-26500. While maintaining the MIL-C-26500 mating interface, this product has also been expanded to include qualifications to numerous Boeing specifications

protectron

Contextual Info: 1553 TYPE DATA BUS HARNESSES AND JUMPER CABLES G G G G G G BOEING qualified Available with or without connectors Up to 4 stubs per coupler Complete harnesses any type and cable length Production 100 % tested for electrical performance Can be supplied with or without

protectron

Abstract: radiall 600 STD1553
Contextual Info: 1553 TYPE DATA BUS HARNESSES AND JUMPER CABLES q BOEING qualified q Available with or without connectors q Up to 4 stubs per coupler q Complete harnesses any type and cable length q Production 100 % tested for electrical performance q Can be supplied with or without

125-92-9

Abstract: kings 125-92-9 1-761-11MA9
Contextual Info: GSD REVISIONS CHANGES hO cm I o 1.79 1.73 CO ho •{§D. 3 HOLES NOTES: 1. FOR USE WITH BOEING S280W503-5 k ADAMS RUSSELL FC38Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE DIE KTH=2213. 4. INTERFACE PER MIL-STD-348, FIG. 313=1. 5. CENTER CONTACT (1-761-11MA9) SUPPLIED UNASSEMBLED.

Contextual Info: NOTES: 1. FOR USE WITH BOEING S280W503-1 k 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. 310=1. 5. CENTER CONTACT 1 - 1 027-4MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 875=92=3

875-91-3

Contextual Info: 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-2207. 4. INTERFACE PER MIL-STD-348, FIG. 310=1. 5. CENTER CONTACT 1 - 1 027-2MA9 SUPPLIED UNASSEMBLED. 6. MARK PACKAGE: KINGS 875=91=3

FC20Z

Contextual Info: DASH NO. M CODE MADE FROM NOTES: 1. FOR USE WITH BOEING S280W503-3 & ADAMS RUSSELL FC20Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-546-1 3. FOR CRIMPING USE DIE SIZE KTH-2216. 4. INTERFACE PER MIL-STD-348 FIG. 313-1. 5. CENTER CONTACT 1-569-35MA9 SUPPLIED UNASSEMBLED.

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

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.

1-7443-1MA9

Contextual Info: DASH NO. U CODE MADE FROM GSD REVISIONS CHANGES ER 35985 CO ME 12/12/94 cn I I CO CO NOTES: 1. FOR USE WITH BOEING S280W503-6 à ADAMS RUSSELL FC48Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3=546=2. 3. FOR CRIMPING USE DIE KTH=2229. 4. CENTER CONTACT, 1-7443-1MA9, SUPPLIED UNASSEMBLED.

2971-7-16

Contextual Info: MARK: KINGS 2 9 7 1 - 7 - * DATE CODE SEE SHEET 2 FOR USE WITH BOEING BM S13-65 OH & ADAMS RUSSELL FC28Z CABLES. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . FOR CRIMPING USE DIE KTH-2212. INTERFACE PER M IL-STD-348, FIG. 304-2. FOR USE WITH .075 MAX. PANEL.

KTH-2212

Abstract: S280W503-4
Contextual Info: DASH NO. M CODE MADE FROM REVISIONS GSD ER NJ 35794 MJB 09/20/94 CT> I CN 38250 C BDH 03/14/01 O "-~ J I CD NOTES: 1. FOR USE WITH BOEING S280W503-4 AND ADAMS RUSSELL FC28Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3-5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2212.

FC28Z

Contextual Info: DASH NO. M CODE MADE FROM {£ D. 3 HOLES STAMP: KINGS 2 9 7 5 -6 - * NOTES: 1. FOR USE WITH BOEING S280W503-4 & ADAMS RUSSELL FC28Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2212. 4. INTERFACE PER MIL-STD-348, FIG. 304-1 (EX. KEYING).

MIL-STD-348 301-1

Contextual Info: GSD REVISIONS CHANGES ER 35913 MJB 11/29/94 en œ CN 37743 B TML 12/11/98 I œ I co NOTES: 1. FOR USE WITH BOEING S280W503-2 it 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.

Contextual Info: REVISIONS REVISED AND REDRAWN PER ER8354 RMS 05/29/08 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. INTERFACE PER MIL-STO-348, FIG. 301-1. 5. CENTER CONTACT 1 -5 6 9 -2 1 MA9 SUPPLIED UNASSEMBLED.

S280W503-2

Abstract: 2-1539-1M27
Contextual Info: DASH NO. M CODE MADE FROM GSD REVISIONS ER KH oo 34036 08/03/92 ^1 CD I CD -F ^ I O vl 2—1539—1M27 STAMP: KINGS 8 7 6 -6 4 -3 NOTES: 1. FOR USE WITH BOEING S280W503-2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3-5 4 6 -1 . 3. FOR CRIMPING USE DIE KTH-2207.

126-58-9

Contextual Info: REVISIONS CHANGES GSD ho CD I cn 34030 07/30/92 CN KH 33566 E 10/20/92 CN 34481 C JCA 06/07/93 QQ I CO CN 37743 B TML 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 SIZE KTH-2161.

Contextual Info: GSD REVISIONS oo ho cr> ER KH 35656 08/29/94 I co I CD NOTES: 1. FOR USE WITH BOEING S280W503-4 & ADAMS RUSSELL FC28Z CABLES. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 -2 . 3. FOR CRIMPING USE DIE KTH-2212. 4. INTERFACE PER MIL-STD-348. FIG. 309-1. 5. CENTER CONTACT 1-534-93MA9 SUPPLIED UNASSEMBLED.

126-58-9

Abstract: MAX511
Contextual Info: OASH NO. y COOE MADE FROM REVISIONS “O > ^3 REVISED ANO REDRAWN PER ER 8354 RMS 05/29/06 to CD I cn CO I CO STAMP: KINGS 126-58-9 3 HOLES 5 5 WIDE (3 GROOVES) NOTES: 1. FOR USE WITH BOEING S280W503- 2 & ADAMS RUSSELL FC14Z CABLE. 2. FOR CABLING INSTRUCTIONS SEE 3 -5 4 6 - 1.