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747 ELECTRONIC TEST EQUIPMENT
747 PRODUCTS AS LISTED IN BOEING, DOUGLAS
PRODUCTS DIVISION, SUPPORT EQUIPMENT SUMMARY
(ALPHA-NUMERIC BY MAIN P/N)
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Next Page |
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| Main P/N |
A23002 |
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| End Item |
-14 |
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| Aero Info P/N |
23-MUL-1403 |
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| Title |
Test Box Assy - TV Antenna Coupler. Used to aid in the measurement of DC and RF parameters of the TV antenna coupler module assy. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-200B
747-200C
747-200F
747-300
747-400
747-COMB
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A23002-1
A23002-1
A23002-1
A23002-1
A23002-1
A23002-1 |
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| Main P/N |
A26002 |
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| End Item |
-54 |
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| Aero Info P/N |
26-MUL-1405 |
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| Title |
Test Box - Time Delay, Cargo Fire Extinguisher Bottle 2A. Used to record the length of time between initiation & subsequent engagement of the cargo fire extinguisher bottle 2A time delay relay. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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A26002-51
A26002-51 |
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| Main P/N |
A27030 |
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| End Item |
-51 |
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| Aero Info P/N |
27-MUL-1354 |
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| Title |
Test Box - Power Supply, CSEU. Used for functional test of the control system electronic unit power supply assembly. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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A27030-48
A27030-48 |
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| Main P/N |
A27038 |
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| End Item |
-1 |
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| Aero Info P/N |
27-MUL-1355 |
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| Title |
Breakout Box - Printed Circuit Card. Used to test printed circuit cards having common connectors. |
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| Notes |
Used with 66 pin connectors |
Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
A27038 |
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| End Item |
-10 |
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| Aero Info P/N |
27-MUL-1355 |
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| Title |
Breakout Box - Printed Circuit Card. Used to test printed circuit cards having common connectors. |
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| Notes |
Used with 41 pin connectors |
Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
A27038 |
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| End Item |
-6 |
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| Aero Info P/N |
27-MUL-1355 |
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| Title |
Breakout Box - Printed Circuit Card. Used to test printed circuit cards having common connectors. |
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| Notes |
Used with 114 pin connectors |
Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
A27039 |
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| End Item |
-1 |
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| Aero Info P/N |
27-MUL-1356 |
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| Title |
Breakout Box - ARINC 600, Bench Test. Used to bench test components having ARINC 600 connectors. |
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| Notes |
Used for ARINC 600 size 2 connectors |
Applicability
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Supersedes
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Replaces
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747-400
700-400F
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| Main P/N |
A27039 |
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| End Item |
-19 |
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| Aero Info P/N |
27-MUL-1356 |
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| Title |
Breakout Box - ARINC 600, Bench Test. Used to bench test components having ARINC 600 connectors. |
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| Notes |
Used for ARINC 600 size 1 connectors |
Applicability
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Supersedes
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Replaces
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747-400
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A27039-9 |
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| Main P/N |
A27044 |
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| End Item |
-53 |
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| Aero Info P/N |
27-MUL-1357 |
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| Title |
Test Box - Converter CSEU Power Supply. Used to test the CSEU power supply filter/chopper/regulator and converter assemblies. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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A27044-44
A27044-44 |
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| Main P/N |
A27045 |
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| End Item |
-16 |
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| Aero Info P/N |
27-MUL-1358 |
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| Title |
Test Box - Noise, CSEU Power Supply. Used to test noise in the control systems electronic unit power supply assy P/N 287T0017. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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A27045-1
A27045-1 |
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| Main P/N |
A27052 |
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| End Item |
-1 |
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| Aero Info P/N |
27-MUL-1359 |
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| Title |
Test Box - Regulator, CSEU Power Supply. Used to test regulator card of CSEU power supply. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
A27053 |
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| End Item |
-29 |
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| Aero Info P/N |
27-MUL-1360 |
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| Title |
Test Box - Monitor, CSEU Power Supply. Used to test CSEU monitor PWA PC card. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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A27053-26
A27053-26 |
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| Main P/N |
A27059 |
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| End Item |
-1 |
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| Aero Info P/N |
27-MUL-1361 |
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| Title |
Breakout Box - Chopper/Regulator Power Supply, CSEU. Used with B27018 FSEU/CSEU power supply breakout box to test 285T0485 chopper/regulator PWA. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
A27115 |
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| End Item |
-1 |
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| Aero Info P/N |
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| Title |
Test Equip - Outboard Aileron Lockout Actuator. Used to test outboard aileron lockout actuators. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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| Main P/N |
A31003 |
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| End Item |
-33 |
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| Aero Info P/N |
31-MUL-1398 |
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| Title |
Test Box - Power Supply, Warning Electronic Unit (WEU). Used to test Warning Electronic Unit power supply and monitor assembly. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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A31003-1, -25 |
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| Main P/N |
A31003 |
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| End Item |
-34 |
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| Aero Info P/N |
31-MUL-1398 |
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| Title |
Test Box - Power Supply, Warning Electronic Unit (WEU). Used to test Warning Electronic Unit power supply and monitor assembly. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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A31003-1, -29 |
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| Main P/N |
A31004 |
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| End Item |
-1 |
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| Aero Info P/N |
31-MUL-1399 |
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| Title |
Breakout Box - Power Supply & Monitor, WEU. Used to continuity test the Warning Electronic Unit power supply and Monitor Assembly Unit. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
A31005 |
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| End Item |
-14 |
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| Aero Info P/N |
31-MUL-1400 |
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| Title |
Test Box - Noise, WEU Power Supply. Used to perform noise test on Warning Electronic Unit power supply assembly. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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A31005-1
A31005-1 |
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| Main P/N |
A31008 |
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| End Item |
-1 |
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| Aero Info P/N |
31-MUL-1402 |
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| Title |
Test Cable - WEU Power Supply. Used to reconnect WEU Power Supply after disassembly for testing. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
A33003 |
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| End Item |
-359 |
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| Aero Info P/N |
33-MUL-1371 |
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| Title |
Breakout Box - Multipurpose. Used for component testing of panel assemblies. |
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| Notes |
See drawing for applicable cable assemblies. |
Applicability
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Supersedes
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Replaces
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747-400
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A33003-1 |
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| Main P/N |
A34011 |
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| End Item |
-1 |
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| Aero Info P/N |
34-MUL-1380 |
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| Title |
Breakout Box Equipment - ARINC 600, Line Maintenance. Used to probe ARINC 600 airplane connectors for continuity checking and interfacing the ARINC 429 digital data bus analyzer with airplane wiring. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
A34011 |
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| End Item |
-112 |
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| Aero Info P/N |
34-MUL-1380 |
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| Title |
Breakout Box Equipment - ARINC 600, Line Maintenance. Used to probe ARINC 600 airplane connectors for continuity checking and interfacing the ARINC 429 digital data bus analyzer with airplane wiring. |
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| Notes |
-112 Connector Kit consists of assorted connectors and a storage box. |
Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
A34015 |
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| End Item |
-27 |
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| Aero Info P/N |
34-MUL-1383 |
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| Title |
Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
747-COMB
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A34015-23
A34015-23
A34015-23 |
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| Main P/N |
ADMIT |
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| End Item |
-1 |
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| Aero Info P/N |
03-B47-1600 |
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| Title |
Aircraft Digital Maintenance Information Terminal (ADMIT). Provides remote access to the Central Maintenance Computer (CMC) via a portable VXI mainframe computer attached to the CMC by a 75 foot long cable. Two touch-screen computer monitors are attached to the ADMIT also with one-hundred foot long. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
B20005 |
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| End Item |
-41 |
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| Aero Info P/N |
20-MUL-1300 |
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| Title |
Test Equipment - Velocity/Position Transducer. Used in conjunction with functional test stands to interface with X-Y plotter and oscilloscope where velocity/position measurements are required. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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B20005-12
B20005-12
B20005-12
B20005-12
B20005-12
B20005-12
B20005-12
B20005-12
B20005-12
B20005-12 |
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1 |
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| Main P/N |
B20005 |
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| End Item |
-52 |
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| Aero Info P/N |
20-MUL-1300 |
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| Title |
Test Equipment - Velocity/Position Transducer. Used in conjunction with functional test stands to interface with X-Y plotter and oscilloscope where velocity/position measurements are required. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1
B20005-1 |
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| Main P/N |
B20005 |
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| End Item |
-68 |
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| Aero Info P/N |
20-MUL-1300 |
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| Title |
Test Equipment - Velocity/Position Transducer. Used in conjunction with functional test stands to interface with X-Y plotter and oscilloscope where velocity/position measurements are required. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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B20005-51
B20005-51
B20005-51
B20005-51
B20005-51
B20005-51
B20005-51
B20005-51
B20005-51
B20005-51 |
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| Main P/N |
B27018 |
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| End Item |
-19 |
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| Aero Info P/N |
27-MUL-1392 |
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| Title |
Breakout Box - Power Supply, FSEU, CSEU. Used with A27038 for 757 fleet to test FSEU Pwr Supply/FSEU Power Supply Printed Wiring Assembly and FSEU Input Power Supply. For 757/767 fleet use with A27059 to test CSEU Chopper Regulator Wiring Assembly. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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B27018-1
B27018-1 |
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| Main P/N |
B34001 |
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| End Item |
-1 |
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| Aero Info P/N |
34-MUL-1544 |
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| Title |
Test Fixture - Power Supply Cards/Cont Panel Assy. Used to support the ILS, VOR, ATC, ADF & Dual ADF Power Supply Cards while troubleshooting per CMM 34-31-61, CMM 34-51-61, CMM 34-53-61, CMM 34-57-61 & CMM 34-57-62. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
B71034 |
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| End Item |
-40 |
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| Aero Info P/N |
71-MUL-1395 |
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| Title |
Test Equipment - Engine Pressure Monitoring. Used to monitor engine pressure during Test Procedure No. 9 PW4000 (767) Test Procedure No. 12 JT9D (767) |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
C34005 |
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| End Item |
-1 |
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| Aero Info P/N |
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| Title |
Extended Box - Radio Altimeter Receiver Transmitter. Used in place of Radio Altimeter (RA) Receiver - Transmitter (RT) primarily AlliedSignal Model ALA-52B RA RT. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
C77004 |
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| End Item |
-10 |
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| Aero Info P/N |
77-MUL-1512 |
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| Title |
Test Box - Generic AVM Interface. Used to provide user interface between ARINC 429 transmitter/receiver (customer furnished) and the generic airborne vibration monitor, for acquiring fault and flight history. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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C77004-1
C77004-1 |
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| Main P/N |
F70316 |
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| End Item |
-140 |
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| Aero Info P/N |
28-MUL-1338 |
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| Title |
Auxiliary Defueling External Power Control Unit. Used to defuel an aircraft using an external ground power source. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
747-SP
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F70316-1
F70316-1
F70316-1
F70316-1
F70316-1
F70316-1
F70316-1
F70316-1
F70316-1 |
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| Main P/N |
F70328 |
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| End Item |
-1 |
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| Aero Info P/N |
70-MUL-1601 |
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| Title |
Probe - Film Resistance Measuring. Used with multimeter to measure resistance of electrical bond between conductive coating on non-conductive plastic sheet and the grounding fasteners. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
747-SP
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| Main P/N |
F72785 |
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| End Item |
-573 |
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| Aero Info P/N |
24-MUL-1187 |
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| Title |
Test Set - Elevator, Rudder, Aileron PCU. Used to test the elevator, rudder and aileron power control units. See drawing for additional test cables required. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
747-SP
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F72785-551
F72785-551
F72785-551
F72785-551
F72785-551
F72785-551
F72785-551
F72785-551
F72785-551 |
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| Main P/N |
F80138 |
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| End Item |
-1 |
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| Aero Info P/N |
34-MUL-1251 |
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| Title |
Extension Cable - Vertical Gyro. Connects the Tilt Table with A/P wiring for reference system testing. For A/P equipped with Bendix vertical gyro. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
747-SP
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| Main P/N |
F80139 |
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| End Item |
-1 |
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| Aero Info P/N |
34-MUL-1198 |
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| Title |
Extension Cable - Vertical Gyro. Used to connect vertical gyro on the Tilt Table with A/P wiring for attitude reference system testing, Sperry Gyro. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
747-SP
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| Main P/N |
G21001 |
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| End Item |
-11 |
|
|
|
| Aero Info P/N |
21-B47-1547 |
|
|
|
| Title |
Lockout - Test Switch, N2 Engine Speed Discrete PCA. Used to hold the CH1 or CH2 switch of the N2 engine speed discrete PCA's in the test position to simulate engines on condition during test of the equipment cooling system. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-400
747-400F
|
G21001-1
G21001-1 |
|
|
|
| Main P/N |
G21002 |
|
|
|
| End Item |
-30 |
|
|
|
| Aero Info P/N |
21-B47-1548 |
|
|
|
| Title |
Test Equip - PRSRZ Outflow Valve Alt. Simulation. Used to test altitude pressure switch by simulating 11,000 ft cabin altitude pressure ICU
(Sta 2210,WL182.RBL/LBL 77) |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-400
747-400F
|
G21002-1,-17, -26
G21002-1,-17, -26
|
|
|
|
| Main P/N |
G22001 |
|
|
|
| End Item |
-148 |
|
|
|
| Aero Info P/N |
34-B47-1340 |
|
|
|
| Title |
Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
G22001-122
G22001-122
G22001-122
G22001-122
G22001-122
G22001-122
G22001-122
G22001-122 |
F80223-1, -2, -3
F80223-1, -2, -3
F80223-1, -2, -3
F80223-1, -2, -3
F80223-1, -2, -3
F80223-1, -2, -3
F80223-1, -2, -3
F80223-1, -2, -3 |
|
|
| Main P/N |
G22001 |
|
|
|
| End Item |
-154 |
|
|
|
| Aero Info P/N |
34-B47-1340 |
|
|
|
| Title |
Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
G22001-147
G22001-147
G22001-147
G22001-147
G22001-147
G22001-147
G22001-147
G22001-147 |
|
|
|
| Main P/N |
G22001 |
|
|
|
| End Item |
-155 |
|
|
|
| Aero Info P/N |
34-B47-1340 |
|
|
|
| Title |
Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
G22001-123
G22001-123
G22001-123
G22001-123
G22001-123
G22001-123
G22001-123
G22001-123 |
|
|
|
| Main P/N |
G22003 |
|
|
|
| End Item |
-83 |
|
|
|
| Aero Info P/N |
22-MUL-1545 |
|
|
|
| Title |
Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-400
747-400F
|
|
G22003-50, -39
G22003-50, -39 |
|
|
| Main P/N |
G22003 |
|
|
|
| End Item |
-84 |
|
|
|
| Aero Info P/N |
22-MUL-1545 |
|
|
|
| Title |
Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-400
747-SP
|
|
G22003-51, -39
G22003-51, -39 |
|
|
| Main P/N |
G22004 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
22-B47-1531 |
|
|
|
| Title |
Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
G22004 |
|
|
|
| End Item |
-2 |
|
|
|
| Aero Info P/N |
22-B47-1531 |
|
|
|
| Title |
Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
G22004 |
|
|
|
| End Item |
-3 |
|
|
|
| Aero Info P/N |
22-B47-1531 |
|
|
|
| Title |
Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
G22004 |
|
|
|
| End Item |
-4 |
|
|
|
| Aero Info P/N |
22-B47-1531 |
|
|
|
| Title |
Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
G22004 |
|
|
|
| End Item |
-5 |
|
|
|
| Aero Info P/N |
22-B47-1531 |
|
|
|
| Title |
Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
G22004 |
|
|
|
| End Item |
-6 |
|
|
|
| Aero Info P/N |
22-B47-1531 |
|
|
|
| Title |
Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
G23001 |
|
|
|
| End Item |
-32 |
|
|
|
| Aero Info P/N |
23-MUL-1546 |
|
|
|
| Title |
Test Box - RCP Processor Card. Used for testing and troubleshooting the Radio Communications Panel Processor. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-400
747-400F
|
G23001-23
G23001-23 |
|
|
|
| Main P/N |
G24003 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
24-B47-1549 |
|
|
|
| Title |
Test Box - Lightning Protector. Used to test lightning protector. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-200B
747-300
747-S
|
|
|
|
|
| Main P/N |
G25007 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
|
|
|
|
| Title |
Test Eqpt - Cargo PDU Limit Switch Assy. Used to verify both the mounting position (measured in degrees CW/CCW degrees from 0") and the electric-mechanical actuation of steerable PDU. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-400F
|
|
|
|
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| Previous Page |
Next Page |
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21115 Longeway Road, #A, Sonora, CA 95370
Tel: 209-533-2868 / Fax: 209-536-0497 / E-mail: Sales@AeroInfoInc.com
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