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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.

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Part #'s G22001 thru J26004

Owner Main P/N Aero Info P/N End Item All P/N Title
Boeing G22001 34-B47-1340 -154 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -155 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -79 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22003 22-MUL-1545 -1 1545 Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches.
Boeing G22003 22-MUL-1545 -2 1545 Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches.
Boeing G22003 22-MUL-1545 -50 1545 Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches.
Boeing G22003 22-MUL-1545 -51 1545 Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches.
Boeing G22003 22-MUL-1545 -83 1545 Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches.
Boeing G22003 22-MUL-1545 -84 1545 Test Equip - Autothrottle Clutch. Used to run in and acceptance test autothrottle clutches.
Boeing G22004 22-B47-1531 -1 1531 Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max.
Boeing G22004 22-B47-1531 -2 1531 Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max.
Boeing G22004 22-B47-1531 -3 1531 Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max.
Boeing G22004 22-B47-1531 -4 1531 Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max.
Boeing G22004 22-B47-1531 -5 1531 Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max.
Boeing G22004 22-B47-1531 -6 1531 Access Pad - Electronic Circuit Connector. Used to provide access to electrical contacts on connectors 100 pins max.
Boeing G23001 23-MUL-1546 -1 1546 Test Box - RCP Processor Card. Used for testing and troubleshooting the Radio Communications Panel Processor.
Boeing G23001 23-MUL-1546 -23 1546 Test Box - RCP Processor Card. Used for testing and troubleshooting the Radio Communications Panel Processor.
Boeing G23001 23-MUL-1546 -32 1546 Test Box - RCP Processor Card. Used for testing and troubleshooting the Radio Communications Panel Processor.
Boeing G24003 24-B47-1549 -1 1549 Test Box - Lightning Protector. Used to test lightning protector.
Boeing G25007 25-B47-1609 -1 1609 Test Eqpt - Cargo PDU Limit Switch Assy. Used to verify both the mounting position (measured in degrees CW/CCW degrees from 0") and the electric-mechanical actuation of steerable PDU.
Boeing G26001 26-B47-1278 -105 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -36 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -37 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -39 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -4 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -5 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -50 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -51 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -52 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -57 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -58 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -6 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -60 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -61 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -67 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -69 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -7 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -70 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -71 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -72 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -73 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -74 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -90 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -91 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -92 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -93 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 -94 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26001 26-B47-1278 1278 Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests.
Boeing G26003 26-B47-1551 -1 1551 Breakout Box - DA-15P Connector. Used to test 285U0291CA11/Smoke Door Indicator Module or any component having a DA-15P type connector.
Boeing G26004 31-MUL-1497 -1 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G26004 31-MUL-1497 -10 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G26004 31-MUL-1497 -23 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G26004 31-MUL-1497 -39 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G26004 31-MUL-1497 -40 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G26004 31-MUL-1497 -49 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G26004 31-MUL-1497 -55 1497 Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors.
Boeing G27009 27-B47-1277 -19 1277 Test Box - Alternate Drive Motor L/E Flap. Used to verify three phase electrical power availability to the LE flap alternate drive motor.
Boeing G27021 27-B47-1552 -1 1552 Breakout Box - ARINC/Filter/Fuse PCA. Used in conjunction with A27039 breakout box to test the ARINC/Filter/Fuse PCA card.
Boeing G27025 27-B47-1553 -1 1553 Test Equip - T.E. Flap Alternate Drive Motor Current. Used to verify three phase electrical power availability to T.E. Flap Inboard/Outboard Alternate Drive Motor.
Boeing G27027 27-B47-1554 -1 1554 Control Box Equip - Power Pack, TE Flap Drive. Used to test the operation of the Power Pack Drive Unit of the TE Flap.
Boeing G27033 27-MUL-1555 -1 1555 Adapter Cable - Outboard Aileron Lockout. Used to allow the outboard aileron lockout actuator to be driven to the retracted (locked) position.
Boeing G27033 27-MUL-1555 -2 1555 Adapter Cable - Outboard Aileron Lockout. Used to allow the outboard aileron lockout actuator to be driven to the retracted (locked) position.
Boeing G28002 28-B47-1556 -34 1556 Test Equip - Volumetric Top-Off Calibration. Used to test Volumetric Shutoff Control Unit.
Boeing G28002 28-B47-1556 -38 1556 Test Equip - Volumetric Top-Off Calibration. Used to test Volumetric Shutoff Control Unit.
Boeing G28002 28-B47-1556 -48 1556 Test Equip - Volumetric Top-Off Calibration. Used to test Volumetric Shutoff Control Unit.
Boeing G28006 28-B47-1557 -1 1557 Adapter Equipment - Calibration, Fuel Quantity Totalizer. Used to calibrate fuel quantity totalizer with fuel in tanks. Applicable to airplanes with ten fuel tanks.
Boeing G28007 28-B47-1558 -1 1558 Test Box - Fuel Quantity Indicating System. Used during test of the Fuel Quantity Indicating System (FQIS) to further isolate faults after BITE analysis.
Boeing G28007 28-B47-1558 -15 1558 Test Box - Fuel Quantity Indicating System. Used during test of the Fuel Quantity Indicating System (FQIS) to further isolate faults after BITE analysis.
Boeing G28013 28-B47-1524 -1 1524 Test Equip - Override Jettison Fuel Pump, Fault Current Detector. Used in place of Override Jettison Pump to provide dummy load & current detector during operational test of Fault Current Detector System.
Boeing G28013 28-B47-1524 -16 1524 Test Equip - Override Jettison Fuel Pump, Fault Current Detector. Used in place of Override Jettison Pump to provide dummy load & current detector during operational test of Fault Current Detector System.
Boeing G32006 32-B47-1559 -1 1559 Breakout Box - Control Lever, Landing Gear Actuator Module Assy. Used to test Control Lever Gear Actuator Module Assy.
Boeing G32014 32-B47-1560 -20 1560 Test Equip - Torque Sensor, Brake Control. Used to test Brake Control Unit response to variations in torque sensor input.
Boeing G32016 32-B47-1561 -1 1561 Breakout Box- Landing Gear Control Lever Module. Used to test the 257U0002 Landing Gear Control Lever Module per CMM 32-31-01.
Boeing G32018 32-B47-1562 1562 Test Equipment - Hard Ground Jumper. Used to simulate activation of Air/Ground (GCU) at P414 & P415 panel per chapters MM 73-00-00 & MM 32-09-02.
Boeing G36035 36-MUL-1619 -1 1619 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.
Boeing G36035 36-MUL-1619 -2 1619 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.
Boeing G38001 38-B47-1564 -1 1564 Test Box - Potable Water Module/PC Assy. Used to test Potable Water Module/Printed Circuit Assy's per MM 38-14-03 and MM 38-14-05.
Boeing G38001 38-B47-1564 -21 1564 Test Box - Potable Water Module/PC Assy. Used to test Potable Water Module/Printed Circuit Assy's per MM 38-14-03 and MM 38-14-05.
Boeing G77001 77-B47-1268 -1 1268 Test Box - Low N1 Test. Used to provide electrical connection for a signal generator and electronic counter to N1 transmitter plug or N1 engine disconnect panel plug during low N1 indication test.(-1/JT9D) (-2/RB211) (-3/CF6)
Boeing G77001 77-B47-1268 -2 1268 Test Box - Low N1 Test. Used to provide electrical connection for a signal generator and electronic counter to N1 transmitter plug or N1 engine disconnect panel plug during low N1 indication test.(-1/JT9D) (-2/RB211) (-3/CF6)
Boeing G77001 77-B47-1268 -3 1268 Test Box - Low N1 Test. Used to provide electrical connection for a signal generator and electronic counter to N1 transmitter plug or N1 engine disconnect panel plug during low N1 indication test.(-1/JT9D) (-2/RB211) (-3/CF6)
Boeing G77003 77-B47-1565 -1 1565 Test Box - PIMU. Used to perform manual test of the Propulsion Interface Monitor Unit module per CMM 77-51-01.
Boeing J22004 22-MUL-1614 -1 1614 Test Eqpt - Autothrottle Gearbox, Brake. Used in the run-in and Acceptance Test Procedures for Autothrottle Brake (254W4101), Rudder Control Brake (253W3349), and Autothrottle Gearbox Brake (254W140) Assemblies. The J22004-1, -54 are for 50 Hz Power Syste
Boeing J22004 22-MUL-1614 -2 1614 Test Eqpt - Autothrottle Gearbox, Brake. Used in the run-in and Acceptance Test Procedures for Autothrottle Brake (254W4101), Rudder Control Brake (253W3349), and Autothrottle Gearbox Brake (254W140) Assemblies. The J22004-1, -54 are for 50 Hz Power Syste
Boeing J22004 22-MUL-1614 -54 1614 Test Eqpt - Autothrottle Gearbox, Brake. Used in the run-in and Acceptance Test Procedures for Autothrottle Brake (254W4101), Rudder Control Brake (253W3349), and Autothrottle Gearbox Brake (254W140) Assemblies. The J22004-1, -54 are for 50 Hz Power Syste
Boeing J22004 22-MUL-1614 -55 1614 Test Eqpt - Autothrottle Gearbox, Brake. Used in the run-in and Acceptance Test Procedures for Autothrottle Brake (254W4101), Rudder Control Brake (253W3349), and Autothrottle Gearbox Brake (254W140) Assemblies. The J22004-1, -54 are for 50 Hz Power Syste
Boeing J25004 25-B77-1615 -23 1615 Test Eqpt - Cargo Stop/Lock Assemblies. Functionally test the 451W1330, 451W1360, 451W460, 451W14470 Cargo Lock Assemblies.
Boeing J26002 26-B77-1621 -1 1621 Used to monitor and troubleshoot the airplane wiring and cardfile backplane integrity by providing pin access to connectors. The -1 consists of a -4 extender card assembly and a -7 storage box assy.
Boeing J26002 26-B77-1621 -2 1621 Used to monitor and troubleshoot the airplane wiring and cardfile backplane integrity by providing pin access to connectors. The -2 consists of a -5 extender card assembly and a -8 storage box assy.
Boeing J26002 26-B77-1621 -3 1621 Used to monitor and troubleshoot the airplane wiring and cardfile backplane integrity by providing pin access to connectors. The -3 consists of a -6 extender card assembly and a -9 storage box assy.
Boeing J26003 26-B77-1584 -12 1584 Test Box - Time Delay, Cargo Fire Extinguishing Bottle. Used to record the elapsed time between the initial and secondary squib firings of the cargo fire extinguishing bottles.
Boeing J26004 26-B77-1585 -2 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -24 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -25 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -26 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -27 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -28 1585 Storage Box, Test Equipment - Squib, Fire Extinguishing System.
Boeing J26004 26-B77-1585 -3 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -4 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -43 1585 Cable Assy - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.
Boeing J26004 26-B77-1585 -5 1585 Test Equipment - Squib, Fire Extinguishing System. Used to verify the required voltage at the appropriate squib connector upon discharge.

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<<Part #'s C77001 thru G22001