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    tca 321 Datasheets

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    tca 321 datasheet (14)

    Part ECAD Model Manufacturer Description Type PDF
    TCA321 Unknown Shortform Data and Cross References (Misc Datasheets) Scan PDF
    TCA321 Unknown Shortform IC and Component Datasheets (Plus Cross Reference Data) Scan PDF
    TCA321 Unknown IC Datasheets - Shortform Scan PDF
    TCA321A Unknown Shortform Data and Cross References (Misc Datasheets) Scan PDF
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    TCA321G Unknown Shortform Data and Cross References (Misc Datasheets) Scan PDF
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    TCA321G Siemens Components for Surface Mounting 1983/4 Scan PDF
    TCA321GG Unknown Shortform Data and Cross References (Misc Datasheets) Scan PDF
    TCA321GG Unknown Shortform IC and Component Datasheets (Plus Cross Reference Data) Scan PDF
    TCA321W Unknown Shortform Data and Cross References (Misc Datasheets) Scan PDF
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    information applikation

    Abstract: information applikation mikroelektronik Mikroelektronik Information Applikation applikation heft A109D mikroelektronik DDR a 109 opv VEB mikroelektronik schaltungen 861 TAA 761 A
    Text: , B 765 D, B 861 D, B B 2761 D, B 2765 D, B 4761 D,B 4765 Typen der Fa. Siemens äquivalent» TCA 311 A, TCA 315 A, TCA 321 A, TCA 325 A, TCA 331 A, TCA 335 A, TAA 761 A, TAA 765 A, TAA 861 A, TAA 665 A, TAA , Richtwert E2 ^ 20 El . 3.2. 3.2.1 . Eilterschaltungen Tiefpaßschaltungen zeigt die Schaltung eines , , wie sie Bild 3.21 zeigt. Ur»r 5,6V A Dz L S M 16 7d3 U s1k V 5,6V 1k ! , Betriebsspannungsabhängigkeit zu verringern, kann eine Stromquelle entsprechend Bild 3.21 eingesetzt werden. ß'iLd. 3.23


    OCR Scan     		PDF

    05-E0537

    Abstract: e0537 FORM0357 TVAXX00X0XS
    Text: OUTLINE DRAWING REQUIREMENTS. 3.2 SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3 , CALCULATE, USING LINEAR REGRESSION, THE SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. 3.3 INSPECTION IN , (XX), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD


    Original     		PDF TVAXX00X0XS QA0006 FORM0357 MIL-STD-130. MC0023. 05-E0537 05-E0537 e0537 TVAXX00X0XS

    2010 - Not Available

    Abstract: No abstract text available
    Text: TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 QUALITY ASSURANCE: 3.1 , 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE RANGE -55°C TO +125°C. 3.2.1.1 CALCULATE, USING LINEAR REGRESSION, THE SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. 3.3


    Original     		PDF TVAXX00X0XS 824W170 824F036 755W002. 423F006

    2010 - Not Available

    Abstract: No abstract text available
    Text: ), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 , (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE , CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER


    Original     		PDF TVAXX00X0XW3 824W160 824F036 755W002. 10-E0600

    2007 - FORM0357

    Abstract: No abstract text available
    Text: (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE , CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS , . 4.0 PACKAGING: DB VALUE (XX), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND


    Original     		PDF TVAXX00X0XG QA0006 FORM0357 MIL-STD-130. MC0023. 05-E0716

    2004 - FORM0357

    Abstract: No abstract text available
    Text: SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20 , THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. DB VALUE (XX), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X).


    Original     		PDF TVAXX00X0XF MIL-STD-130. QA0006 FORM0357 MC0023. 04-E191

    2007 - Not Available

    Abstract: No abstract text available
    Text: VALUE (X), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD , . 3.2 SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA , SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25


    Original     		PDF TVAXX00X0XW3S QA0006 FORM0357 MC0023. 07-E0068

    2001 - Not Available

    Abstract: No abstract text available
    Text: ), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 , (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE , CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER


    Original     		PDF TVAXX00X0XW3S QA0006 FORM0357 MC0023.

    2010 - 755w002

    Abstract: No abstract text available
    Text: ), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 , (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE , CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER


    Original     		PDF TVAXX00X0XW3S 824W170 824F036 755W002. 755w002

    2001 - Not Available

    Abstract: No abstract text available
    Text: TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. QUALITY ASSURANCE: 3.1 SAMPLE INSPECT PER , (DESTRUCTIVE TESTING): 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE , CALCULATE TCA USING THE FOLLOWING FORMULA TCA = SLOPE ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER


    Original     		PDF TVAXX00X0XHW3 MC0023.

    2007 - Not Available

    Abstract: No abstract text available
    Text: VALUE (X), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD , . 3.2 SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA , SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25


    Original     		PDF TVAXX00X0XW3S QA0006 FORM0357 MC0023. 07-E0989

    2006 - E0718

    Abstract: FORM0357
    Text: SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20 , THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. DB VALUE (X), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X).


    Original     		PDF TVAXX00X0XW3 MIL-STD-130. QA0006 FORM0357 MC0023. 06-E0718 E0718

    2011 - Not Available

    Abstract: No abstract text available
    Text: CONTROL: PER MIL-STD-1686. UNIT MARKING: DB VALUE (XX), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). , CONFORMANCE TO OUTLINE DRAWING REQUIREMENTS. 3.2 SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE , CALCULATE, USING LINEAR REGRESSION, THE SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. 3.3 3.4 INSPECTION IN


    Original     		PDF TVAXX00X0X 824W170 755W002. 423F006

    2001 - TVAXX00X0X

    Abstract: FORM0357
    Text: SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20 , THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. DB VALUE (XX), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X).


    Original     		PDF TVAXX00X0X MIL-STD-130. QA0006 FORM0357 MC0023. TVAXX00X0X

    2001 - Not Available

    Abstract: No abstract text available
    Text: TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 QUALITY ASSURANCE: 3.1 , 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE RANGE -55°C TO +125°C. 3.2.1.1 CALCULATE, USING LINEAR REGRESSION, THE SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. 3.3


    Original     		PDF TVAXX00X0XS QA0006 FORM0357 MC0023.

    2010 - Not Available

    Abstract: No abstract text available
    Text: SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 QUALITY , TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE RANGE , TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7


    Original     		PDF TVAXX00X0XW3F 824W170 824F036 755W002.

    2010 - Not Available

    Abstract: No abstract text available
    Text: ), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 , (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20°C OVER THE TEMPERATURE , CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER


    Original     		PDF TVAXX00X0XF 824W170 824F036 755W002.

    2009 - 09-E0767

    Abstract: No abstract text available
    Text: REQUIREMENTS. 3.2 SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND , REGRESSION, THE SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . , OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. STANDARD PACK PER 755W002


    Original     		PDF TVAXX00X0XW3S 824W170 824F036 MIL-STD-130. 755W002. 09-E0767 09-E0767

    FORM0357

    Abstract: No abstract text available
    Text: SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20 , THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.2.1.3 ACCEPTANCE LIMITS: PER 1.1.7. DB VALUE (X), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X).


    Original     		PDF TVAXX00X0XW3F MIL-STD-130. QA0006 FORM0357 MC0023. 05-E0190

    2003 - Not Available

    Abstract: No abstract text available
    Text: VALUE (X), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD , SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA EVERY 20 , THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25°C 3.2.1.3


    Original     		PDF TVAXX00X0XW3 QA0006 FORM0357 MC0023.

    2001 - Not Available

    Abstract: No abstract text available
    Text: VALUE (XX), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD , . 3.2 SAMPLE INSPECTION (DESTRUCTIVE TESTING). 3.2.1 SELECT THREE (3) UNITS FROM LOT AND MEASURE DCA , SLOPE OF THE CURVE. 3.2.1.2 CALCULATE TCA USING THE FOLLOWING FORMULA: TCA = SLOPE . ATTENUATION @ 25


    Original     		PDF TVAXX00X0XG QA0006 FORM0357 MC0023.

    2004 - Not Available

    Abstract: No abstract text available
    Text: CONTROL: PER MIL-STD-1686. UNIT MARKING: DB VALUE (X), DIRECTION OF SHIFT (N OR P) AND TCA SHIFT (X). , TP-8965. 3.2.1 GROUP A TESTING 3.2.1.1 VISUAL AND MECHNICAL INSPECTION PER SHEET 3. 3.2.1.2 INITIAL , INPUT POWER SEE 1.1.6. 3.2.1.6 SUB-GROUP 1 (3 SAMPLES) 3.2.1.6.1 TCA MEASUREMENT - MEASURE AND RECORD , 1009765000 - 1 OF 3 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.3.1.7.3 ACCEPTANCE LIMITS: NOMINAL TCA +/-0.001 dB/dB/°C. 3.2.2 GROUP B TESTING (7 SAMPLES APPROVED


    Original     		PDF TP-8965. MC0023. 04-E033

    2004 - Not Available

    Abstract: No abstract text available
    Text: TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. QUALITY ASSURANCE: 3.1 VERIFY 100% VISUAL , NUMBER PER TP-8965. 3.2.1 GROUP A TESTING 3.2.1.1 VISUAL AND MECHNICAL INSPECTION PER SHEET 3. 3.2.1.2 , 168 HRS AT INPUT POWER SEE 1.1.6. 3.2.1.6 SUB-GROUP 1 (3 SAMPLES) 3.2.1.6.1 TCA MEASUREMENT - MEASURE , -E033 DWG # REV LVL SHEET 1009705000 - 1 OF 3 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.3.1.7.3 ACCEPTANCE LIMITS: NOMINAL TCA +/-0.001 dB/dB/°C. 3.2.2


    Original     		PDF TP-8965. MC0023. 04-E033

    2004 - Not Available

    Abstract: No abstract text available
    Text: ), DIRECTION OF SHIFT (N) AND TCA SHIFT (X). LEGIBILITY AND PERMANENCY PER MIL-STD-130. 2.0 3.0 , AND/OR C TESTING AS INDICATED BY THE PART NUMBER PER TP-8965. 3.2.1 GROUP A TESTING 3.2.1.1 VISUAL AND , TCA MEASUREMENT - MEASURE AND RECORD ATTENUATION AT DC EVERY 20°C FROM -55°C TO +125°C PER 2.5.1 OF TP , 04-E033 DWG # REV LVL SHEET 1009785000 - 1 OF 3 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.3.1.6.3 ACCEPTANCE LIMITS: NOMINAL TCA +/-0.001 dB/dB/°C.


    Original     		PDF TP-8965. MC0023.

    2004 - Not Available

    Abstract: No abstract text available
    Text: DISCHARGE CONTROL: PER MIL-STD-1686. UNIT MARKING: DB VALUE (X), DIRECTION OF SHIFT (N) AND TCA SHIFT (X). , TP-8965. 3.2.1 GROUP A TESTING 3.2.1.1 VISUAL AND MECHNICAL INSPECTION PER SHEET 3. 3.2.1.2 INITIAL , INPUT POWER SEE 1.1.6. 3.2.1.6 SUB-GROUP 1 (3 SAMPLES) 3.2.1.6.1 TCA MEASUREMENT - MEASURE AND RECORD , 1009835000 - 1 OF 3 CALCULATE TCA USING THE FOLLOWING FORMULA: SLOPE . TCA = ATTENUATION @ 25°C 3.3.1.6.3 ACCEPTANCE LIMITS: NOMINAL TCA +/-0.001 dB/dB/°C. 3.2.2 GROUP B TESTING (7 SAMPLES APPROVED


    Original     		PDF TP-8965. MC0023. 04-E033
    ...

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