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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 B71034 thru C77001

Owner Main P/N Aero Info P/N End Item All P/N Title
Boeing B71034 71-MUL-1395 -29 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 -40 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 -48 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 -63 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 B73002 73-B57-1396 -1 1396 Test Box - Power Supply, Propulsion Discrete Interface Unit (PDIU). Used to test Propulsion Discrete Interface Unit (PDIU) power supply assy.
Boeing B78009 78-B37-1569 -21 1569 Lock Equipment - Thrust Reverser Maintenance. Used to energize thrust reverser arm solenoid to positively prevent deploy command to directional control valve.
Boeing B78009 78-B37-1569 -26 1569 Lock Equipment - Thrust Reverser Maintenance. Used to energize thrust reverser arm solenoid to positively prevent deploy command to directional control valve.
Boeing C21001 21-B37-1513 -1 1513 Test Set - Equipment Cooling System Performance. Used for adjustment and test of the equipment cooling system.
Boeing C21001 21-B37-1513 -12 1513 Test Set - Equipment Cooling System Performance. Used for adjustment and test of the equipment cooling system.
Boeing C21001 21-B37-1513 -16 1513 Test Set - Equipment Cooling System Performance. Used for adjustment and test of the equipment cooling system.
Boeing C21001 21-B37-1513 -19 1513 Test Set - Equipment Cooling System Performance. Used for adjustment and test of the equipment cooling system.
Boeing C22001 22-B37-1254 -1 1254 Test Box - IRS Master Caution Module. Used to test the IRS Master Caution Module.
Boeing C22001 22-B37-1254 -13 1254 Test Box - IRS Master Caution Module. Used to test the IRS Master Caution Module.
Boeing C22001 22-B37-1254 -18 1254 Test Box - IRS Master Caution Module. Used to test the IRS Master Caution Module.
Boeing C22001 22-B37-1254 -21 1254 Test Box - IRS Master Caution Module. Used to test the IRS Master Caution Module.
Boeing C22003 22-B37-1287 -1 1287 Test Box - Mach Trim Actuator. Used to test Mach Trim Actuator.
Boeing C22003 22-B37-1287 -18 1287 Test Box - Mach Trim Actuator. Used to test Mach Trim Actuator.
Boeing C22003 22-B37-1287 -22 1287 Test Box - Mach Trim Actuator. Used to test Mach Trim Actuator.
Boeing C22004 22-B37-1570 -1 1570 Breakout Box - IFSAU (65-52820). Used to access the pins when testing and troubleshooting the IFSAU (Integrated Flight System Accessory Unit).
Boeing C22005 22-B37-1632 -1 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -22 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -25 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -4 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -5 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -6 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -7 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C22005 22-B37-1632 -8 1632 Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors.
Boeing C23001 23-B37-1622 -13 1622 Test Box - Attendant Handset/IHC PWA. Used for manual bench testing of flight attendant handsets and Integrated Handset Controller (IHC) PWA per the CMM (Handset - Component Maintenance Manual Chapter 23-42-15).
Boeing C23001 23-B37-1622 -15 1622 Test Box - Attendant Handset/IHC PWA. Used for manual bench testing of flight attendant handsets and Integrated Handset Controller (IHC) PWA per the CMM (Handset - Component Maintenance Manual Chapter 23-42-15).
Boeing C24005 24-B37-1623 -1 1623 Test Box - P5-4 AC System Generator APU. Used in conjunction with CMM 31-37-71 to test and troubleshoot the P5-4 Module Assembly.
Boeing C24006 24-B37-1624 -1 1624 Test Box - P5-5 Generator Drive and Standby Power. Used in conjunction with CMM 31-10-41 to test and troubleshoot the P5-5 Module Assembly.
Boeing C26001 26-B37-1625 -1 1625 Test Equipment - Fire Extinguishing System. Used to test the Fire Bottle Squib circuitry for 737-300 per MM 26-21-00.
Boeing C26001 26-B37-1625 -20 1625 Test Equipment - Fire Extinguishing System. Used to test the Fire Bottle Squib circuitry for 737-300 per MM 26-21-00.
Boeing C26001 26-B37-1625 1625 Test Equipment - Fire Extinguishing System. Used to test the Fire Bottle Squib circuitry for 737-300 per MM 26-21-00.
Boeing C26002 26-B37-1510 -1 1510 Test Equipment - Engine/APU Fire Detection System (Walter Kidde).
Boeing C26002 26-B37-1510 -21 1510 Test Equipment - Engine/APU Fire Detection System (Walter Kidde).
Boeing C26005 26-B37-1630 -1 1630 Test Box - APU/Engine Fire Detection System. Used to manually test the installed engine and APU fire detection system (Whittaker) by simulating fire, over-heat, and ground fault conditions; tester acts like an additional detector element connected in para
Boeing C26006 26-MUL-1626 -1 1626 Test Box - Cargo Fire Extinguishing System. Used to test the airplane electrical wiring to the forward cargo and aft squibs on the bottle(s).
Boeing C26006 26-MUL-1626 -29 1626 Test Box - Cargo Fire Extinguishing System. Used to test the airplane electrical wiring to the forward cargo and aft squibs on the bottle(s).
Boeing C26006 26-MUL-1626 -30 1626 Test Box - Cargo Fire Extinguishing System. Used to test the airplane electrical wiring to the forward cargo and aft squibs on the bottle(s).
Boeing C27006 27-B37-1301 -12 1301 Test Equip - Cutout Switch, Stab Trim Control (Component Maintenance). Used to perform functional test on cutout switch assy.
Boeing C27006 27-B37-1301 -22 1301 Test Equip - Cutout Switch, Stab Trim Control (Component Maintenance). Used to perform functional test on cutout switch assy.
Boeing C27006 27-B37-1301 -34 1301 Test Equip - Cutout Switch, Stab Trim Control (Component Maintenance). Used to perform functional test on cutout switch assy.
Boeing C27007 27-B37-1302 -1 1302 Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement.
Boeing C27007 27-B37-1302 -14 1302 Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement.
Boeing C27007 27-B37-1302 -17 1302 Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement.
Boeing C27007 27-B37-1302 -21 1302 Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement.
Boeing C27007 27-B37-1302 -26 1302 Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement.
Boeing C27007 27-B37-1302 -31 1302 Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement.
Boeing C27009 27-B37-1303 -1 1303 Test Box - Digital Stall Warning Computer. Used to test Digital Stall Warning Computer Unit.
Boeing C27009 27-B37-1303 -13 1303 Test Box - Digital Stall Warning Computer. Used to test Digital Stall Warning Computer Unit.
Boeing C27009 27-B37-1303 -15 1304 Test Box - Digital Stall Warning Computer. Used to test Digital Stall Warning Computer Unit.
Boeing C27009 27-B37-1303 -22 1303 Test Box - Digital Stall Warning Computer. Used to test Digital Stall Warning Computer Unit.
Boeing C27010 27-B37-1582 -1 1582 Test Box - Autoslat Computer. Use to test Autoslat Computer Assy.
Boeing C27010 27-B37-1582 -19 1582 Test Box - Autoslat Computer. Use to test Autoslat Computer Assy.
Boeing C27010 27-B37-1582 -21 1582 Test Box - Autoslat Computer. Use to test Autoslat Computer Assy.
Boeing C27011 27-B37-1304 -1 1304 Test Box - Printed Circuit Cards, Autoslat Computer. Used to test Autoslat Computer printed circuit cards.
Boeing C27011 27-B37-1304 -12 1304 Test Box - Printed Circuit Cards, Autoslat Computer. Used to test Autoslat Computer printed circuit cards.
Boeing C27011 27-B37-1304 -16 1304 Test Box - Printed Circuit Cards, Autoslat Computer. Used to test Autoslat Computer printed circuit cards.
Boeing C27013 27-B37-1579 -1 1579 Test Box - Auxiliary PCA, DSWC. Used to test Digital Stall Warning Computer Auxiliary PCA.
Boeing C27013 27-B37-1579 -11 1579 Test Box - Auxiliary PCA, DSWC. Used to test Digital Stall Warning Computer Auxiliary PCA.
Boeing C27014 27-B37-1305 -1 1305 Test Box - Discrete Input/Output PCA, DSWC. Used to test Digital Stall Warning Computer discrete input/output printed circuit assy.
Boeing C27014 27-B37-1305 -11 1305 Test Box - Discrete Input/Output PCA, DSWC. Used to test Digital Stall Warning Computer discrete input/output printed circuit assy.
Boeing C27014 27-B37-1305 -21 1305 Test Box - Discrete Input/Output PCA, DSWC. Used to test Digital Stall Warning Computer discrete input/output printed circuit assy.
Boeing C27016 27-B37-1306 -1 1306 Test Box - Central Processing Unit PCA Card. Used to test Central Processing Unit printed circuit assembly card.
Boeing C27016 27-B37-1306 -11 1306 Test Box - Central Processing Unit PCA Card. Used to test Central Processing Unit printed circuit assembly card.
Boeing C29002 29-B37-1631 -1 1631 Test Box - Rudder Power Control Unit. Used to permit the operation of the yaw damper system within the Rudder Power Control Unit in order to facilitate the internal leakage check of the rudder PCU per Airplane Maintenance Manual procedure 29-00-00.
Boeing C29002 29-B37-1631 -17 1631 Test Box - Rudder Power Control Unit. Used to permit the operation of the yaw damper system within the Rudder Power Control Unit in order to facilitate the internal leakage check of the rudder PCU per Airplane Maintenance Manual procedure 29-00-00.
Boeing C30001 30-B37-1627 -1 1627 Test Box - P5-9, Window and Pitot Heat Module. Used to bench test the P5-9 Window and Pitot Heat Module.
Boeing C30001 30-B37-1627 -21 1627 Test Box - P5-9, Window and Pitot Heat Module. Used to bench test the P5-9 Window and Pitot Heat Module.
Boeing C31001 31-B37-1307 -1 1307 Test Box - Printed Circuit Card Window & Pitot Heat. Used to test window and pitot heat printed circuit assembly.
Boeing C31001 31-B37-1307 -13 1307 Test Box - Printed Circuit Card Window & Pitot Heat. Used to test window and pitot heat printed circuit assembly.
Boeing C31003 31-B37-1571 -1 1571 Test Box - EIS Data Retrieval. Used to provide user interface between ARINC 429 transmitter/receiver (customer furnished) and the Engine Instrument System (EIS) Primary Display Unit. Used for EIS data retrieval and then to clear EIS memory.
Boeing C32001 32-B37-1308 -1 1308 Test Box - Engine Speed Detector and Landing Gear Transfer Valve Control Cards. Used to test Engine Speed Detector and Landing Gear Transfer Valve Control Cards.
Boeing C32004 27-B37-1518 -1 1518 Test Equipment - Proximity System. Used to test Proximity System Sensor & Solid State Switch. Test per MM32-09-200-3, MM32-61-00, MM32-61-11, MM32-61-21, MM32-61-31, MM32-6141, MM32-61-51.
Boeing C32004 27-B37-1518 -35 1518 Test Equipment - Proximity System. Used to test Proximity System Sensor & Solid State Switch. Test per MM32-09-200-3, MM32-61-00, MM32-61-11, MM32-61-21, MM32-61-31, MM32-6141, MM32-61-51.
Boeing C32004 27-B37-1518 -47 1518 Test Equipment - Proximity System. Used to test Proximity System Sensor & Solid State Switch. Test per MM32-09-200-3, MM32-61-00, MM32-61-11, MM32-61-21, MM32-61-31, MM32-6141, MM32-61-51.
Boeing C32004 27-B37-1518 -52 1518 Test Equipment - Proximity System. Used to test Proximity System Sensor & Solid State Switch. Test per MM32-09-200-3, MM32-61-00, MM32-61-11, MM32-61-21, MM32-61-31, MM32-6141, MM32-61-51.
Boeing C32004 27-B37-1518 -58 1518 Test Equipment - Proximity System. Used to test Proximity System Sensor & Solid State Switch. Test per MM32-09-200-3, MM32-61-00, MM32-61-11, MM32-61-21, MM32-61-31, MM32-6141, MM32-61-51.
Boeing C34001 34-B37-1309 -1 1309 Adapter Assy LSI FMC/COU, ATS. Used to provide test capability for the Lear-Siegler FMC/CDU on the Boeing ATS-182.
Boeing C34004 34-B37-1572 -1 1572 Circuit Board Assy - Detector, ARINC 429 - Label FF. Used to provide test capability for the Smiths (LSI) FMC/CDU on the Boeing ATS-182.
Boeing C34005 34-MUL-1608 -1 1608 Extended Box - Radio Altimeter Receiver Transmitter. Used in place of Radio Altimeter (RA) Receiver - Transmitter (RT) primarily AlliedSignal Model ALA-52B RA RT.
Boeing C34006 34-MUL-1607 -1 1607 Adapter, Tray - EFIS Symbol Generator Software Loading. Used to load software into the S242T404 EFIS symbol generator.
Boeing C34006 34-MUL-1607 -53 1607 Adapter, Tray - EFIS Symbol Generator Software Loading. Used to load software into the S242T404 EFIS symbol generator.
Boeing C34006 34-MUL-1607 -57 1607 Adapter, Tray - EFIS Symbol Generator Software Loading. Used to load software into the S242T404 EFIS symbol generator.
Boeing C34011 34-B37-1573 -1 1573 Adapter Assy - Honeywell MCP/FCC ATS. Used to provide test capability for the Honeywell MCP/FCC on the Boeing ATS-182.
Boeing C34011 34-B37-1573 -11 1573 Adapter Assy - Honeywell MCP/FCC ATS. Used to provide test capability for the Honeywell MCP/FCC on the Boeing ATS-182.
Boeing C34011 34-B37-1573 -12 1573 Adapter Assy - Honeywell MCP/FCC ATS. Used to provide test capability for the Honeywell MCP/FCC on the Boeing ATS-182.
Boeing C34012 34-B37-1511 -1 1511 Test Box - Total Air Temperature Probe, Air Data System. Used during test of the Air Data System to connect decade resistance box in place to total air temperature probe per Maintenance Manual Chapter 34-12-00.
Boeing C34012 34-B37-1511 -2 1511 Test Box - Total Air Temperature Probe, Air Data System. Used during test of the Air Data System to connect decade resistance box in place to total air temperature probe per Maintenance Manual Chapter 34-12-00.
Boeing C34012 34-B37-1511 -21 1511 Test Box - Total Air Temperature Probe, Air Data System. Used during test of the Air Data System to connect decade resistance box in place to total air temperature probe per Maintenance Manual Chapter 34-12-00.
Boeing C49002 49-B37-1574 -1 1574 Test Box - APU Control Unit. Used to perform LRU (Line Replaceable Unit) functional test and SRU (Shop Repairable Unit) troubleshooting for the APU Control Unit.
Boeing C71012 71-B37-1310 -1 1310 Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.
Boeing C71012 71-B37-1310 -21 1310 Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.
Boeing C71012 71-B37-1310 -28 1310 Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.
Boeing C71012 71-B37-1310 -35 1310 Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.
Boeing C71012 71-B37-1310 -47 1310 Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.
Boeing C72001 72-B37-1575 -1 1575 Indicator Overlay Set - Airborne Vibration Monitoring. Used to improve readability of the Airborne Vibration Monitoring System Indicator during engine trim operations.
Boeing C73002 73-B37-1628 -1 1628 Test Box - P5-68 Power Management Control Module. Used to bench test the P5-68 Module.
Boeing C75001 75-B37-1576 -1 1576 Switch, Patent - System Test. Used to hold the Air-Gnd-Nose sensing pushbutton switches in the depressed position during functional testing.
Boeing C77001 77-B37-1311 -1 1311 Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.

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<<Part #'s A31007 thru B71034