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ground support equipment

767 ELECTRONIC TEST EQUIPMENT

767 Products Support Equipment Summary
(ALPHA-NUMERIC BY MAIN P/N)

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Main P/N A31003


End Item -34


Aero Info P/N 31-MUL-1398


Title Test Box - Power Supply, Warning Electronic Unit (WEU). Used to test Warning Electronic Unit power supply and monitor assembly.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
A31003-1, -29
A31003-1, -29
A31003-1, -29
A31003-1, -29
A31003-1, -29

Main P/N A31004


End Item -1


Aero Info P/N 31-MUL-1399


Title Breakout Box - Power Supply & Monitor, WEU. Used to continuity test the Warning Electronic Unit power supply and Monitor Assembly Unit.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER


Main P/N A31005


End Item -14


Aero Info P/N 31-MUL-1400


Title Test Box - Noise, WEU Power Supply. Used to perform noise test on Warning Electronic Unit power supply assembly.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER

A31005-1
A31005-1
A31005-1
A31005-1
Main P/N A31006


End Item -17


Aero Info P/N 31-MUL-1401


Title Shorting Module - Master Warning Printed Circuit Assy. Used to simulate power supply faults on the Warning Electronics Unit (WEU).


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
A31006-5
A31006-5
A31006-5
A31006-5
A31006-5

Main P/N A31007


End Item -1


Aero Info P/N 31-MUL-1285


Title Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector.


Notes Used with Teledyne Tester 2222786, 2227295, 2225302
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F


Main P/N A31007


End Item -34


Aero Info P/N 31-MUL-1285


Title Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Sundstrand tester to the appropriate digital flight recorder system test connector.


Notes Used with Sundstrand Tester 981-6301-002
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F

A31007-30
A31007-30
A31007-30
A31007-30
A31007-30
Main P/N A31007


End Item -49


Aero Info P/N 31-MUL-1285


Title Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Sundstrand tester to the appropriate digital flight recorder system test connector.


Notes Used with Sundstrand Tester 981-6301-002
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F

A31007-30
A31007-30
A31007-30
A31007-30
A31007-30
Main P/N A31007


End Item -59


Aero Info P/N 31-MUL-1285


Title Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector.


Notes Used with Teledyne Tester 2229738
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11

Main P/N A31008


End Item -1


Aero Info P/N 31-MUL-1402


Title Test Cable - WEU Power Supply. Used to
reconnect WEU Power Supply after disassembly for testing.



Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER


Main P/N A31010


End Item -1


Aero Info P/N



Title Breakout Box - Power Supply Unit, WEU


Notes Line 669 &Up.
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER


Main P/N A32074


End Item -1


Aero Info P/N 32-MUL-1367


Title Breakout Box - Relay System, Air/Ground. Used for continuity and voltage check of air ground relay system. (May use TE65B40719)


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F


Main P/N A33001


End Item -1


Aero Info P/N 33-MUL-1369


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.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300


Main P/N A33003


End Item -359


Aero Info P/N 33-MUL-1371


Title Breakout Box - Multipurpose. Used for component testing of panel assemblies.


Notes See drawing for applicable cable assemblies.
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1

Main P/N A33004


End Item -1


Aero Info P/N 33-MUL-1587


Title Test Box - Autobright Sensor. Used to test
Autobright Sensor Unit.



Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
A33002-36
A33002-36
A33002-36
A33002-36

Main P/N A34003


End Item -46


Aero Info P/N 34-MUL-1372


Title Test Box - Rear Module and Control Panel ATC. Used to test ATC Control Panel and ATC rear module assy.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER

A34003-43
A34003-43
A34003-43
A34003-43
Main P/N A34004


End Item -30


Aero Info P/N 34-MUL-1373


Title Test Box - Front Module, ATC (Air Traffic Control). Used for functional test of ATC front module.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER

A34004-27
A34004-27
Main P/N A34005


End Item -1


Aero Info P/N 34-MUL-1374


Title Test Box - ADF Front Module Assembly. Used for component testing of the Automatic Direction Finder (ADF) front module assembly.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER


Main P/N A34006


End Item -21


Aero Info P/N 34-MUL-1375


Title Test Box - ADF Control Panel and Rear Module. Used to test the ADF control panel and rear module.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER

A34006-1
A34006-1
Main P/N A34007


End Item -36


Aero Info P/N 34-MUL-1376


Title Test Box - Rear Module and Control Panel, ILS. Used to test ILS control panel and ILS rear module assembly.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER

A34007-33
A34007-33
A34007-33
A34007-33
Main P/N A34008


End Item -1


Aero Info P/N 34-MUL-1377


Title Test Box - Front Module, ILS. Used to test the ILS front module.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER

Main P/N A34009


End Item -29


Aero Info P/N 34-MUL-1378


Title Test Box - Rear Module & Control Panel,
VOR/DME rear module and control panel.



Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
A34009-26
A34009-26
A34009-26
A34009-26


Main P/N A34010


End Item -21


Aero Info P/N 34-MUL-1379


Title Test Box - Front Module, VOR/DME. Used to test the VOR/DME front module.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
A34010-1
A34010-1
A34010-1
A34010-1


Main P/N A34011


End Item -1


Aero Info P/N 34-MUL-1380


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.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F


Main P/N A34011


End Item -112


Aero Info P/N 34-MUL-1380


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.


Notes -112 Connector Kit consists of assorted connectors and a storage box.
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F


Main P/N A34011


End Item -119


Aero Info P/N 34-MUL-1380


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.


Notes -119 Adapter Cable consists of two adapter cables and a storage box.
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F


Main P/N A34013


End Item -18


Aero Info P/N 34-MUL-1381


Title Test Box - Power Supply, Control Panel. Used to test control panel power supply units.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER

A34013-1
A34013-1

Main P/N A34014


End Item -14


Aero Info P/N 34-MUL-1382


Title Test Box - Power Supply, Control Panel. Used to test control panel power supply assembly.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
A34014-1
A34014-1
A34014-1
A34014-1


Main P/N A34015


End Item -26


Aero Info P/N 34-MUL-1383


Title Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
A34015-20
A34015-20
A34015-20
A34015-20
A34015-20
A34015-20


Main P/N A34015


End Item -27


Aero Info P/N 34-MUL-1383


Title Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-300F
767-400ER
A34015-23
A34015-23
A34015-23
A34015-23
A34015-23
A34015-23


Main P/N A38002


End Item -1


Aero Info P/N 38-B67-1410


Title Test Box - Signal Unit PCA, Potable Water. Used to test the potable water signal unit.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER


Main P/N A38010


End Item -11


Aero Info P/N 38-MUL-1583


Title Test Cable - Potable Water Quantity Xmtr. Used to provide electrical access to water tank quantity transmitter for calibration.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
767-300ER
767-400ER

A38010-1
A38010-1
A38010-1
A38010-1
A38010-1

Main P/N A73001


End Item -1


Aero Info P/N 73-B67-1413


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.



Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300


Main P/N A77001


End Item -1


Aero Info P/N 77-MUL-1384


Title Test Box - Power Supply, EECM. Used to test the Power Supply Assy - Electronic Engine Control Monitor Module Assembly.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300


Main P/N A77002


End Item -1


Aero Info P/N 77-B67-1414


Title Test Box - Display Board, EECM. Used to test EECM Display Board.


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER


Main P/N A77003


End Item -18


Aero Info P/N 77-MUL-1299


Title Test Box - Indicating System, Exhaust Gas
Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W



Notes Used on JT9D-7R4 engines.
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
A77003-15
A77003-15
A77003-15


Main P/N A77004


End Item -18


Aero Info P/N 77-B67-1415


Title Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D).


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
A77004-1
A77004-1
A77004-1


Main P/N A77004


End Item -19


Aero Info P/N 77-B67-1415


Title Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D).


Notes
Applicability
Supersedes
Replaces


767-200
767-200ER
767-300
A77004-2
A77004-2
A77004-2


Main P/N A77005


End Item -58


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 CF6-80A & 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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