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767 ELECTRONIC TEST EQUIPMENT
767 Products as listed in Boeing, Douglas Products Division, Support Equipment Summary
(ALPHA-NUMERIC BY MAIN P/N)
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Aero Info, Inc.
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| Previous page |
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Next page |
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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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767-200
767-200ER
767-300
767-300ER
767-300F
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A31003-1, -29
A31003-1, -29
A31003-1, -29
A31003-1, -29
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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767-200
767-200ER
767-300
767-300ER
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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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767-200
767-200ER
767-300
767-300ER
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A31005-1
A31005-1
A31005-1
A31005-1
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| Main P/N |
A31006 |
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| End Item |
-17 |
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| Aero Info P/N |
31-MUL-1401 |
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| Title |
Shorting Module - Master Warning Printed Circuit Assy. Used to simulate power supply faults on the Warning Electronics Unit (WEU). |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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A31006-5
A31006-5
A31006-5
A31006-5
A31006-5
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| Main P/N |
A31007 |
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| End Item |
-1 |
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| Aero Info P/N |
31-MUL-1285 |
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| Title |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector. |
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| Notes |
Used with Teledyne Tester 2222786, 2227295, 2225302 |
Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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| Main P/N |
A31007 |
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| End Item |
-34 |
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| Aero Info P/N |
31-MUL-1285 |
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| Title |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Sundstrand tester to the appropriate digital flight recorder system test connector. |
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| Notes |
Used with Sundstrand Tester 981-6301-002 |
Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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A31007-30
A31007-30
A31007-30
A31007-30
A31007-30
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| Main P/N |
A31007 |
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| End Item |
-49 |
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| Aero Info P/N |
31-MUL-1285 |
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| Title |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Sundstrand tester to the appropriate digital flight recorder system test connector. |
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| Notes |
Used with Sundstrand Tester 981-6301-002 |
Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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A31007-30
A31007-30
A31007-30
A31007-30
A31007-30
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| Main P/N |
A31007 |
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| End Item |
-59 |
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| Aero Info P/N |
31-MUL-1285 |
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| Title |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector. |
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| Notes |
Used with Teledyne Tester 2229738 |
Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
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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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767-200
767-200ER
767-300
767-300ER
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| Main P/N |
A31010 |
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| End Item |
-1 |
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| Aero Info P/N |
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| Title |
Breakout Box - Power Supply Unit, WEU |
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| Notes |
Line 669 &Up. |
Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
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| Main P/N |
A32074 |
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| End Item |
-1 |
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| Aero Info P/N |
32-MUL-1367 |
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| Title |
Breakout Box - Relay System, Air/Ground. Used for continuity and voltage check of air ground relay system. (May use TE65B40719) |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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| Main P/N |
A33001 |
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| End Item |
-1 |
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| Aero Info P/N |
33-MUL-1369 |
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| Title |
Test Box - Master Dim & Test P.C. Card. Used for testing & troubleshooting of the Master Dim and Test Ground Seeking Printed Circuit Assembly P/N 285T0097. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
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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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767-200
767-200ER
767-300
767-300ER
767-300F
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A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
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| Main P/N |
A33004 |
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| End Item |
-1 |
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| Aero Info P/N |
33-MUL-1587 |
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| Title |
Test Box - Autobright Sensor. Used to test
Autobright Sensor 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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767-200
767-200ER
767-300
767-300ER
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A33002-36
A33002-36
A33002-36
A33002-36
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| Main P/N |
A34003 |
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| End Item |
-46 |
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| Aero Info P/N |
34-MUL-1372 |
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| Title |
Test Box - Rear Module and Control Panel ATC. Used to test ATC Control Panel and ATC rear 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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767-200
767-200ER
767-300
767-300ER
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A34003-43
A34003-43
A34003-43
A34003-43
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| Main P/N |
A34004 |
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| End Item |
-30 |
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| Aero Info P/N |
34-MUL-1373 |
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| Title |
Test Box - Front Module, ATC (Air Traffic Control). Used for functional test of ATC front module. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
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A34004-27
A34004-27
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| Main P/N |
A34005 |
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| End Item |
-1 |
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| Aero Info P/N |
34-MUL-1374 |
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| Title |
Test Box - ADF Front Module Assembly. Used for component testing of the Automatic Direction Finder (ADF) front module 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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767-200
767-200ER
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| Main P/N |
A34006 |
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| End Item |
-21 |
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| Aero Info P/N |
34-MUL-1375 |
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| Title |
Test Box - ADF Control Panel and Rear Module. Used to test the ADF control panel and rear module. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
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A34006-1
A34006-1
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| Main P/N |
A34007 |
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| End Item |
-36 |
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| Aero Info P/N |
34-MUL-1376 |
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| Title |
Test Box - Rear Module and Control Panel, ILS. Used to test ILS control panel and ILS rear module 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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767-200
767-200ER
767-300
767-300ER
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A34007-33
A34007-33
A34007-33
A34007-33
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| Main P/N |
A34008 |
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| End Item |
-1 |
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| Aero Info P/N |
34-MUL-1377 |
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| Title |
Test Box - Front Module, ILS. Used to test the ILS front module. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
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| Main P/N |
A34009 |
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| End Item |
-29 |
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| Aero Info P/N |
34-MUL-1378 |
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| Title |
Test Box - Rear Module & Control Panel,
VOR/DME rear module and control panel. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
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A34009-26
A34009-26
A34009-26
A34009-26
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| Main P/N |
A34010 |
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| End Item |
-21 |
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| Aero Info P/N |
34-MUL-1379 |
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| Title |
Test Box - Front Module, VOR/DME. Used to test the VOR/DME front module. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
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A34010-1
A34010-1
A34010-1
A34010-1
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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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767-200
767-200ER
767-300
767-300ER
767-300F
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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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767-200
767-200ER
767-300
767-300ER
767-300F
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| Main P/N |
A34011 |
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| End Item |
-119 |
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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 |
-119 Adapter Cable consists of two adapter cables and a storage box. |
Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-300F
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| Main P/N |
A34013 |
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| End Item |
-18 |
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| Aero Info P/N |
34-MUL-1381 |
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| Title |
Test Box - Power Supply, Control Panel. Used to test control panel power supply units. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
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A34013-1
A34013-1
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| Main P/N |
A34014 |
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| End Item |
-14 |
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| Aero Info P/N |
34-MUL-1382 |
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| Title |
Test Box - Power Supply, Control Panel. Used to test control panel 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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767-200
767-200ER
767-300
767-300ER
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A34014-1
A34014-1
A34014-1
A34014-1
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| Main P/N |
A34015 |
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| End Item |
-26 |
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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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767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
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A34015-20
A34015-20
A34015-20
A34015-20
A34015-20
A34015-20
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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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767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
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A34015-23
A34015-23
A34015-23
A34015-23
A34015-23
A34015-23
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| Main P/N |
A38002 |
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| End Item |
-1 |
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| Aero Info P/N |
38-B67-1410 |
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| Title |
Test Box - Signal Unit PCA, Potable Water. Used to test the potable water signal 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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767-200
767-200ER
767-300
767-300ER
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| Main P/N |
A38010 |
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| End Item |
-11 |
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| Aero Info P/N |
38-MUL-1583 |
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| Title |
Test Cable - Potable Water Quantity Xmtr. Used to provide electrical access to water tank quantity transmitter for calibration. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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767-200
767-200ER
767-300
767-300ER
767-400ER
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A38010-1
A38010-1
A38010-1
A38010-1
A38010-1
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| Main P/N |
A73001 |
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| End Item |
-1 |
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| Aero Info P/N |
73-B67-1413 |
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| Title |
Test Cable - Electronic Engine Control
JT9D-7R4D. Used to connect E.E.C. to Sorenson QRD40-2M22 External Power Supply during airplane system testing of EEC and thrust management system. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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767-200
767-200ER
767-300
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| Main P/N |
A77001 |
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| End Item |
-1 |
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| Aero Info P/N |
77-MUL-1384 |
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| Title |
Test Box - Power Supply, EECM. Used to test the Power Supply Assy - Electronic Engine Control Monitor Module Assembly. |
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| Notes |
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Applicability
|
Supersedes
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Replaces
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767-200
767-200ER
767-300
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| Main P/N |
A77002 |
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| End Item |
-1 |
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| Aero Info P/N |
77-B67-1414 |
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| Title |
Test Box - Display Board, EECM. Used to test EECM Display Board. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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767-200
767-200ER
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| Main P/N |
A77003 |
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| End Item |
-18 |
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| Aero Info P/N |
77-MUL-1299 |
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| Title |
Test Box - Indicating System, Exhaust Gas
Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W |
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| Notes |
Used on JT9D-7R4 engines. |
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
|
A77003-15
A77003-15
A77003-15
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| Main P/N |
A77004 |
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| End Item |
-18 |
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| Aero Info P/N |
77-B67-1415 |
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| Title |
Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D). |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
|
A77004-1
A77004-1
A77004-1
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| Main P/N |
A77004 |
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| End Item |
-19 |
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| Aero Info P/N |
77-B67-1415 |
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| Title |
Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D). |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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|
|
767-200
767-200ER
767-300
|
A77004-2
A77004-2
A77004-2
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| Main P/N |
A77005 |
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| End Item |
-58 |
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| Aero Info P/N |
77-B67-1416 |
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| Title |
Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801). |
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| Notes |
Use on A/P with CF6-80A & CF6-80A2 engines. |
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
|
A77005-1
A77005-1
A77005-1
|
|
|
|
| Main P/N |
A77005 |
|
|
|
| End Item |
-59 |
|
|
|
| Aero Info P/N |
77-B67-1416 |
|
|
|
| Title |
Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801). |
|
|
|
| Notes |
Use on A/P with CF6-80C2 engines. |
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
|
A77005-24
A77005-24
A77005-24
A77005-24
A77005-24
A77005-24
|
|
|
|
| Main P/N |
A77005 |
|
|
|
| End Item |
-60 |
|
|
|
| Aero Info P/N |
77-B67-1416 |
|
|
|
| Title |
Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801). |
|
|
|
| Notes |
Use on A/P with CF6-80C2 & CF6-80C2 |
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
|
A77005-37
A77005-37
A77005-37
A77005-37
A77005-37
A77005-37
|
|
|
|
| Main P/N |
A77005 |
|
|
|
| End Item |
-61 |
|
|
|
| Aero Info P/N |
77-B67-1416 |
|
|
|
| Title |
Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801). |
|
|
|
| Notes |
Use on A/P with CF6-80C2 (FADEC) only. |
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
|
A77005-52
A77005-52
A77005-52
A77005-52
A77005-52
A77005-52
|
|
|
|
| Main P/N |
B23001 |
|
|
|
| End Item |
-6 |
|
|
|
| Aero Info P/N |
23-MUL-1387 |
|
|
|
| Title |
Extender Board - Audio Accessory Unit Assembly. Used in conjunction with A23006 during test of Audio Accessory Unit Assy. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
|
|
B23001-1
B23001-1
B23001-1
B23001-1
|
|
|
| Main P/N |
B27018 |
|
|
|
| End Item |
-19 |
|
|
|
| Aero Info P/N |
27-MUL-1392 |
|
|
|
| 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. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
|
B27018-1
B27018-1
B27018-1
B27018-1
|
|
|
|
| Main P/N |
B34001 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
34-MUL-1544 |
|
|
|
| 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. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
|
|
|
|
|
| Main P/N |
B71034 |
|
|
|
| End Item |
-29 |
|
|
|
| Aero Info P/N |
71-MUL-1395 |
|
|
|
| Title |
Test Equipment - Engine Pressure Monitoring. Used to monitor engine pressure during Test Procedure No. 9 PW4000 (767) Test Procedure No. 12 JT9D (767) |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200ER
767-300
767-300ER
767-300F
|
|
|
|
|
| Main P/N |
B71034 |
|
|
|
| End Item |
-40 |
|
|
|
| Aero Info P/N |
71-MUL-1395 |
|
|
|
| Title |
Test Equipment - Engine Pressure Monitoring. Used to monitor engine pressure during Test Procedure No. 9 PW4000 (767) Test Procedure No. 12 JT9D (767) |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200ER
767-300
767-300ER
767-300F
|
|
|
|
|
| Main P/N |
B71034 |
|
|
|
| End Item |
-48 |
|
|
|
| Aero Info P/N |
71-MUL-1395 |
|
|
|
| Title |
Test Equipment - Engine Pressure Monitoring. Used to monitor engine pressure during Test Procedure No. 9 PW4000 (767) Test Procedure No. 12 JT9D (767) |
|
|
|
| Notes |
Has longer hoses required for use on the 767-300 |
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200ER
767-300
767-300ER
767-300F
|
|
B71034-13
B71034-13
B71034-13
B71034-13
|
|
|
| Main P/N |
C34005 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
71-MUL-1395 |
|
|
|
| Title |
Extended Box - Radio Altimeter Receiver
Transmitter. Used in place of Radio Altimeter (RA) Receiver - Transmitter (RT) primarily AlliedSignal Model ALA-52B RA RT. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
|
|
|
|
| Main P/N |
C34006 |
|
|
|
| End Item |
-57 |
|
|
|
| Aero Info P/N |
34-MUL-1607 |
|
|
|
| Title |
Adapter, Tray - EFIS Symbol Generator Software Loading. Used to load software into the S242T404 EFIS symbol generator. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
|
C34006-53
C34006-53
C34006-53
C34006-53
C34006-53
|
|
|
| Main P/N |
C77004 |
|
|
|
| End Item |
-10 |
|
|
|
| Aero Info P/N |
77-MUL-1512 |
|
|
|
| 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. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
C77004-1
C77004-1
C77004-1
C77004-1
C77004-1
|
|
|
|
| Main P/N |
F70328 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
70-MUL-1601 |
|
|
|
| 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. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
|
|
|
|
| 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
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
G22003-50
G22003-50
G22003-50
G22003-50
G22003-50
|
|
|
|
| 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
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
G22003-51
G22003-51
G22003-51
G22003-51
G22003-51
|
|
|
|
| Main P/N |
G26004 |
|
|
|
| End Item |
-39 |
|
|
|
| Aero Info P/N |
31-MUL-1497 |
|
|
|
| Title |
Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
G26004-1, -10
G26004-1, -10
G26004-1, -10
G26004-1, -10
G26004-1, -10
|
|
|
|
| Main P/N |
G26004 |
|
|
|
| End Item |
-40 |
|
|
|
| Aero Info P/N |
31-MUL-1497 |
|
|
|
| Title |
Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
G26004-23
G26004-23
G26004-23
G26004-23
G26004-23
|
|
|
|
| Main P/N |
G27033 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
27-MUL-1555 |
|
|
|
| Title |
Adapter Cable - Outboard Aileron Lockout. Used to allow the outboard aileron lockout actuator to be driven to the retracted (locked) position. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
|
|
|
|
|
| Main P/N |
G27033 |
|
|
|
| End Item |
-2 |
|
|
|
| Aero Info P/N |
27-MUL-1555 |
|
|
|
| Title |
Adapter Cable - Outboard Aileron Lockout. Used to allow the outboard aileron lockout actuator to be driven to the retracted (locked) position. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
|
|
|
|
|
| Main P/N |
G36035 |
|
|
|
| End Item |
-1 |
|
|
|
| Aero Info P/N |
|
|
|
|
| Title |
Test Eqpt - Pneumatic System Health Check. Test equipment is used to perform the Pneumatic System Health Check on 747-400 and 767 airplanes with Pratt & Whitney and GE engines. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
|
|
|
|
|
| Main P/N |
G36035 |
|
|
|
| End Item |
-2 |
|
|
|
| Aero Info P/N |
|
|
|
|
| Title |
Test Eqpt - Pneumatic System Health Check. Test equipment is used to perform the Pneumatic System Health Check on 747-400 and 767 airplanes with Pratt & Whitney and GE engines. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
|
|
|
|
|
| Main P/N |
J32001 |
|
|
|
| End Item |
-43 |
|
|
|
| Aero Info P/N |
32-MUL-1539 |
|
|
|
| Title |
Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
J32001-39
J32001-39
J32001-39
J32001-39
J32001-39
|
|
|
|
| Main P/N |
J32001 |
|
|
|
| End Item |
-46 |
|
|
|
| Aero Info P/N |
32-MUL-1539 |
|
|
|
| Title |
Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
767-200
767-200ER
767-300
767-300ER
767-300F
|
|
J32001-43
J32001-43
J32001-43
J32001-43
J32001-43
|
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| Previous 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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