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Boeing Tools have arrived direct from the manufacturer and is available for immediate delivery. Our online inventory will be updated regularly until sold. To obtain a price quotation or to request availability, please check the item(s) and click on "submit" below the tables on each page.

If you can't locate your part number, please use our Tool Locator Request Form.

Part #'s A31007 thru B71034

Owner Main P/N Aero Info P/N End Item All P/N Title
Boeing A31007 31-MUL-1285 -59 1285 Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system  test connector.
Boeing A31008 31-MUL-1402 -1 1402 Test Cable - WEU Power Supply. Used to reconnect WEU Power Supply after disassembly for testing.
Boeing A31010 31-MUL-1620 -1 1620 Breakout Box - Power Supply Unit, WEU
Boeing A32074 32-MUL-1367 -1 1367 Breakout Box - Relay System, Air/Ground. Used for continuity and voltage check of air ground relay system. (Breakout box TE65B40719 may be used if available).
Boeing A33001 33-MUL-1369 -1 1369 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.
Boeing A33002 33-MUL-1370 -36 1370 Test Box - Autobright Sensor. Used to test Autobright Sensor Unit.
Boeing A33003 33-MUL-1371 -1 1371 Breakout Box - Multipurpose. Used for component testing of panel assemblies.
Boeing A33003 33-MUL-1371 -359 1371 Breakout Box - Multipurpose. Used for component testing of panel assemblies.
Boeing A33004 33-MUL-1587 -1 1587 Test Box - Autobright Sensor. Used to test Autobright Sensor Unit.
Boeing A34003 34-MUL-1372 -1 1372 Test Box - Rear Module and Control Panel ATC. Used to test ATC Control Panel and ATC rear module assy.
Boeing A34003 34-MUL-1372 -43 1372 Test Box - Rear Module and Control Panel ATC. Used to test ATC Control Panel and ATC rear module assy.
Boeing A34003 34-MUL-1372 -46 1372 Test Box - Rear Module and Control Panel ATC. Used to test ATC Control Panel and ATC rear module assy.
Boeing A34004 34-MUL-1373 -1 1373 Test Box - Front Module, ATC (Air Traffic Control). Used for functional test of ATC front module.
Boeing A34004 34-MUL-1373 -24 1373 Test Box - Front Module, ATC (Air Traffic Control). Used for functional test of ATC front module.
Boeing A34004 34-MUL-1373 -27 1373 Test Box - Front Module, ATC (Air Traffic Control). Used for functional test of ATC front module.
Boeing A34004 34-MUL-1373 -30 1373 Test Box - Front Module, ATC (Air Traffic Control). Used for functional test of ATC front module.
Boeing A34005 34-MUL-1374 -1 1374 Test Box - ADF Front Module Assembly. Used for component testing of the Automatic Direction Finder (ADF) front module assembly.
Boeing A34006 34-MUL-1375 -1 1375 Test Box - ADF Control Panel and Rear Module. Used to test the ADF control panel and rear module.
Boeing A34006 34-MUL-1375 -21 1375 Test Box - ADF Control Panel and Rear Module. Used to test the ADF control panel and rear module.
Boeing A34007 34-MUL-1376 -1 1376 Test Box - Rear Module and Control Panel, ILS. Used to test ILS control panel and ILS rear module assembly.
Boeing A34007 34-MUL-1376 -33 1376 Test Box - Rear Module and Control Panel, ILS. Used to test ILS control panel and ILS rear module assembly.
Boeing A34007 34-MUL-1376 -36 1376 Test Box - Rear Module and Control Panel, ILS. Used to test ILS control panel and ILS rear module assembly.
Boeing A34008 34-MUL-1377 -1 1377 Test Box - Front Module, ILS. Used to test the ILS front module.
Boeing A34009 34-MUL-1378 -1 1378 Test Box - Rear Module & Control Panel, VOR/DME rear module and control panel.
Boeing A34009 34-MUL-1378 -22 1378 Test Box - Rear Module & Control Panel, VOR/DME rear module and control panel.
Boeing A34009 34-MUL-1378 -24 1378 Test Box - Rear Module & Control Panel, VOR/DME rear module and control panel.
Boeing A34009 34-MUL-1378 -26 1378 Test Box - Rear Module & Control Panel, VOR/DME rear module and control panel.
Boeing A34009 34-MUL-1378 -29 1378 Test Box - Rear Module & Control Panel, VOR/DME rear module and control panel.
Boeing A34010 34-MUL-1379 -1 1379 Test Box - Front Module, VOR/DME. Used to test the VOR/DME front module.
Boeing A34010 34-MUL-1379 -21 1379 Test Box - Front Module, VOR/DME. Used to test the VOR/DME front module.
Boeing A34011 34-MUL-1380 -1 1380 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.
Boeing A34011 34-MUL-1380 -112 1380 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.
Boeing A34011 34-MUL-1380 -119 1380 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.
Boeing A34013 34-MUL-1381 -1 1381 Test Box - Power Supply, Control Panel. Used to test control panel power supply units.
Boeing A34013 34-MUL-1381 -18 1381 Test Box - Power Supply, Control Panel. Used to test control panel power supply units.
Boeing A34014 34-MUL-1382 -1 1382 Test Box - Power Supply Control Panel. Used to test control panel power supply assembly.
Boeing A34014 34-MUL-1382 -1 1382 Test Box - Power Supply Control Panel. Used to test control panel power supply assembly.
Boeing A34014 34-MUL-1382 -14 1382 Test Box - Power Supply Control Panel. Used to test control panel power supply assembly.
Boeing A34015 34-MUL-1383 -1 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -10 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -13 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -16 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -20 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -23 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -26 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A34015 34-MUL-1383 -27 1383 Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels.
Boeing A38002 38-B67-1410 -1 1410 Test Box - Signal Unit PCA, Potable Water. Used to test the potable water signal unit.
Boeing A38010 38-MUL-1583 -1 1583 Test Cable - Potable Water Quantity Xmtr. Used to provide electrical access to water tank quantity transmitter for calibration.
Boeing A38010 38-MUL-1583 -11 1583 Test Cable - Potable Water Quantity Xmtr. Used to provide electrical access to water tank quantity transmitter for calibration.
Boeing A73001 73-B67-1413 -1 1413 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.
Boeing A77001 77-MUL-1384 -1 1384 Test Box - Power Supply, EECM. Used to test the Power Supply Assy - Electronic Engine Control Monitor Module Assembly.
Boeing A77002 77-B67-1414 -1 1414 Test Box - Display Board, EECM. Used to test EECM Display Board.
Boeing A77003 77-MUL-1299 -1 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77003 77-MUL-1299 -10 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77003 77-MUL-1299 -15 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77003 77-MUL-1299 -18 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77003 77-MUL-1299 -28 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77003 77-MUL-1299 -34 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77003 77-MUL-1299 -38 1299 Test Box - Indicating System, Exhaust Gas Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W Engines).
Boeing A77004 77-B67-1415 -1 1415 Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D).
Boeing A77004 77-B67-1415 -18 1415 Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D).
Boeing A77004 77-B67-1415 -19 1415 Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D).
Boeing A77004 77-B67-1415 -2 1415 Test Box - Tachometer System. Used during test of the N1 tachometer systems (CF6-80A) and N1/N2 tachometer systems (JT9D-7R4D).
Boeing A77005 77-B67-1416 -1 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -24 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -37 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -52 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -58 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -59 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -60 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing A77005 77-B67-1416 -61 1416 Test Equip - AVM System N1 & N2 Interface. Used to provide A/P interface with Vibration Monitoring Systems Test Set (UT-801).
Boeing B20005 20-MUL-1300 -11 1300 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.
Boeing B20005 20-MUL-1300 -12 1300 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.
Boeing B20005 20-MUL-1300 -13 1300 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.
Boeing B20005 20-MUL-1300 -35 1300 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.
Boeing B20005 20-MUL-1300 -40 1300 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.
Boeing B20005 20-MUL-1300 -41 1300 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.
Boeing B20005 20-MUL-1300 -42 1300 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.
Boeing B20005 20-MUL-1300 -51 1300 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.
Boeing B20005 20-MUL-1300 -52 1300 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.
Boeing B20005 20-MUL-1300 -68 1300 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.
Boeing B21003 21-B57-1385 -1 1385 Jumper Test Wire - Engine Speed Card (Engine Run Simulation). Used to simulate a running engine.
Boeing B22002 22-B57-1386 -1 1386 Breakout Box - Yaw Damper EMI Filter. Used to test the yaw damper EMI filter assy P/N 285T0374.
Boeing B23001 23-MUL-1387 -1 1387 Extender Board - Audio Accessory Unit Assembly. Used in conjunction with A23006 during test of Audio Accessory Unit Assy.
Boeing B23001 23-MUL-1387 -6 1387 Extender Board - Audio Accessory Unit Assembly. Used in conjunction with A23006 during test of Audio Accessory Unit Assy.
Boeing B24002 24-B57-1388 -1 1388 Test Box - Time Delay Relay, 10 Second Dropout. Used to test 10 second dropout time delay relay.
Boeing B25001 25-B57-1389 -1 1389 Test Box - Off-Wing Escape System. Used during functional test of off-wing escape system.
Boeing B26001 26-B57-1390 -1 1390 Test Equip - Engine and APU Fire Detection System (Graviner). Used to simulate a fire condition to the fire detection system control cards during engine and APU fire detection system test.
Boeing B26004 26-B57-1611 -1 1611 Test Box - AFOLTS PCA. Used to bench test A285N0028 AFOLTS PCA.
Boeing B27017 27-B57-1391 -1 1391 Test Box - Power Supply, FSEU. Used to test the FSEU power supply.
Boeing B27018 27-MUL-1392 -1 1392 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.
Boeing B27018 27-MUL-1392 -19 1392 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.
Boeing B27061 27-B57-1393 -1 1393 Test Box - Rudder/Elevator PCU Monitor. Used to simulate PCU monitor sensors during test of the rudder/elevator PCU monitor system.
Boeing B27071 27-B57-1426 -1 1426 Test Box - Elevator Hardover Test. Used to bypass the autopilot system and activate the appropriate autopilot servo valve used during elevator hardover test. See MM 27-31-00.
Boeing B27071 27-B57-1426 -18 1426 Test Box - Elevator Hardover Test. Used to bypass the autopilot system and activate the appropriate autopilot servo valve used during elevator hardover test. See MM 27-31-00.
Boeing B27071 27-B57-1426 -34 1426 Test Box - Elevator Hardover Test. Used to bypass the autopilot system and activate the appropriate autopilot servo valve used during elevator hardover test. See MM 27-31-00.
Boeing B29005 29-B57-1394 -17 1394 Simulator - Yaw Damper Module. Used in place of yaw damper modules when performing test requiring yaw damper servo input for rudder displacement.
Boeing B31001 31-B57-1525 -1 1525 Cable Adapter, Bus Analyzer, ARINC 429. Used to adapt 429 bus analyzer to D761 757 Digital Flight Data Recorder System test connector.
Boeing B34001 34-MUL-1544 -1 1544 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.
Boeing B71034 71-MUL-1395 -1 1395 Test Equipment - Engine Pressure Monitoring. Used to monitor engine pressure during Test Procedure No. 9 PW4000 (767) Test Procedure No. 12 JT9D (767)
Boeing B71034 71-MUL-1395 -13 1395 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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<<Part #'s A26001 thru A31007