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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 C77001 thru G22001

Owner Main P/N Aero Info P/N End Item All P/N Title
Boeing C77001 77-B37-1311 -14 1311 Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.
Boeing C77001 77-B37-1311 -18 1311 Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.
Boeing C77001 77-B37-1311 -25 1311 Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.
Boeing C77001 77-B37-1311 -28 1311 Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.
Boeing C77001 77-B37-1311 -31 1311 Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.
Boeing C77002 77-B37-1252 -1 1252 Test Box - Tachometer System. Used to simulate N1 & N2 tachometer output during engine tachometer system test, Autothrottle System test, & Stall Warning System tests per Maintenance Manuals.
Boeing C77002 77-B37-1252 -20 1252 Test Box - Tachometer System. Used to simulate N1 & N2 tachometer output during engine tachometer system test, Autothrottle System test, & Stall Warning System tests per Maintenance Manuals.
Boeing C77003 77-B37-1312 -1 1312 Test Box - P.C. Cards, Engine Accessory Unit. Used to test Engine Accessory Unit printed circuit assemblies.
Boeing C77004 77-MUL-1512 -1 1512 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.
Boeing C77004 77-MUL-1512 -10 1512 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.
Boeing F70210 71-B07-1417 -1 1417 Breakout Box Assy - Outflow Valve Conn. To provide test points between wiring and outflow valve for measuring proper electrical values and as an aid in troubleshooting.
Boeing F70211 31-B07-1418 -* 1418 Breakout Box Assy - Connector. The assy is installed, for troubleshooting, between system components and airplane wiring.
Boeing F70212 31-B07-1419 -1 1419 Breakout Box Assy - Connector. This is installed between system components and the A/P wiring to aid in troubleshooting.
Boeing F70213 26-B07-1420 -1 1420 Breakout Box - Control Unit Fire Detect. To check and adjust fire detection systems installed on the airplane.
Boeing F70215 28-B07-1421 -1 1421 Test Harness - Fuel Dump Chute Actuator. Harness is used to conduct continuity and voltage tests of either the actuator or A/P wiring from a location exterior to the chute location.
Boeing F70216 30-B07-1422 -1 1422 Breakout Box - Control Unit, Window Heat . To provide access to electrical components of the Window Heat Control Unit for measurement and adjustment.
Boeing F70259 22-B07-1423 -1 1423 Breakout Box Assy. Used to test speed command accessory unit (M4226).
Boeing F70287 22-B07-1424 -1 1424 Test Box - Speed Command Module. Used to test the functions of the Speed Command Accessory Unit, M4226, 65-87688 (ref).
Boeing F70289 70-B07-1602 -1 1602 Coverplate - Auxiliary Fuel Vent System. Used to provide a means of plugging the auxiliary vent duct assy 65-69946 during fuel leakage test.
Boeing F70303 31-MUL-1226 -1 1226 Tachometer - Engine Trim, Remote. Connects to the N2 Tachometer System Test Receptacle in the control cabin. This places remote tach in parallel with selected eng tach ind to check accuracy.
Boeing F70303 31-MUL-1226 -2 1226 Tachometer - Engine Trim, Remote. Connects to the N2 Tachometer System Test Receptacle in the control cabin. This places remote tach in parallel with selected eng tach ind to check accuracy.
Boeing F70303 31-MUL-1226 -3 1226 Tachometer - Engine Trim, Remote. Connects to the N2 Tachometer System Test Receptacle in the control cabin. This places remote tach in parallel with selected eng tach ind to check accuracy.
Boeing F70316 28-MUL-1338 -1 1338 Auxiliary Defueling External Power Control Unit. Used to defuel an aircraft using an external ground power source.
Boeing F70316 28-MUL-1338 -140 1338 Auxiliary Defueling External Power Control Unit. Used to defuel an aircraft using an external ground power source.
Boeing F70318 70-B07-1640 -1 1640 Test Harness - APU Inlet & Exhaust Doors. Used during APU door adjustment and test to energize the door open and closed from the door location.
Boeing F70328 70-MUL-1601 -1 1601 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.
Boeing F71375 27-B07-1424 -* 1424 Mach Trim System Analyzer. The Mach Trim System Analyzer is used in place of the Mach Trim Coupler to analyze the rest of the system.
Boeing F71420 71-B07-1633 -* 1633 Test Set & Adapter Assy - HF Comm Sys. Used as a portable monitoring device designed for rapid location of a malfunction within the HF Communication System. Limited usage.
Boeing F72731 28-MUL-1243 -81 1243 Adapter Assy & Fuel & Oil Qty Test Sets. Used to isolate faulty fuel & oil quantity indicating system components. Note: See current drawing for dash number applicability.
Boeing F72731 28-MUL-1243 -82 1243 Adapter Assy & Fuel & Oil Qty Test Sets. Used to isolate faulty fuel & oil quantity indicating system components. Note: See current drawing for dash number applicability.
Boeing F72785 24-MUL-1187 -551 1187 Test Set - Elevator, Rudder, Aileron PCU. Used to test the elevator, rudder and aileron power control units. See drawing for additional test cables required.
Boeing F72785 24-MUL-1187 -573 1187 Test Set - Elevator, Rudder, Aileron PCU. Used to test the elevator, rudder and aileron power control units. See drawing for additional test cables required.
Boeing F72786 22-MUL-1289 1289 Test Set - Stall Warning Components. Used to test the stall warning system components either on the bench or installed on the airplane. See fab drawing F72855,56,57,58 and 59.
Boeing F72891 49-MUL-1290 -1 1290 Indicator - APU RPM, Test Set. Provides a means of observing the APU speed during troubleshooting situations at Auxiliary Power Unit locations.
Boeing F72891 49-MUL-1290 -20 1290 Indicator - APU RPM, Test Set. Provides a means of observing the APU speed during troubleshooting situations at Auxiliary Power Unit locations.
Boeing F72911 77-B27-1291 -6 1291 Auto Pack Trip - Engine Fail Simulator Assy. To change 28VDC from one pine to another during system adj/test. Trip position simulates engine press below 90 PSIG, normal pos simulates eng press above 120PSIG.
Boeing F72917 29-MUL-1255 -1 1255 Test Equipment - Ground Fault Protection System, Hydraulic System B., Abex Pumps. To provide for functional testing of the hydraulic system B pump motor ground fault protection system.
Boeing F72917 29-MUL-1255 -19 1255 Test Equipment - Ground Fault Protection System, Hydraulic System B., Abex Pumps. To provide for functional testing of the hydraulic system B pump motor ground fault protection system.
Boeing F72947 49-B27-1293 -163 1293 Test Fixture Set - Power Control Unit, Flight Spoiler. Used for complete functional test of Power Control Unit.
Boeing F72970 22-B27-1256 -1 1256 Breakout Box - SP50 & SP150 Single Pitch Channel. Used for various adjustments & tests to the autopilot, when connected to the appropriate test plugs in the E3 Electronics Rack. See MM, Section 22.
Boeing F72971 22-B27-1257 -1 1257 Breakout Box - SP150 Autopilot Test, Roll and Dual Pitch Computers. The test equipment plugs into the E3 Electronics Rack and is used for various adjustments and tests.
Boeing F72989 34-MUL-1258 -1 1258 Cable - Directional Gyro Extension. Used to connect the Sperry Directional Gyro (2588302-4) to A/P wiring when mounted on the tilt/rotational table for directional reference system testing.
Boeing F72998 77-MUL-1294 -1 1294 Adapter Cable - N1 Simulator. Used to connect tachometer tester in place of the N1 tach transmitters to simulate N1 signals for testing full flight regime autothrottle systems.
Boeing F72998 77-MUL-1294 -15 1294 Adapter Cable - N1 Simulator. Used to connect tachometer tester in place of the N1 tach transmitters to simulate N1 signals for testing full flight regime autothrottle systems.
Boeing F73007 27-B27-1295 -1 1295 Electronic Test Equipment - Elevator Feel and Centering Unit. Used in conjunction with F73008 Test Fixture to functionally test the Elevator Feel and Centering Unit.
Boeing F73015 31-MUL-1259 -1 1259 Test Box - Stall Warning Module. Used to test the Stall Warning Module per OHM 31-15-01 and 31-15-02.
Boeing F73015 31-MUL-1259 -20 1259 Test Box - Stall Warning Module. Used to test the Stall Warning Module per OHM 31-15-01 and 31-15-02.
Boeing F80129 32-B37-1208 -1 1208 Antiskid - Auto Brake - Auto Speed Brake Tester. Used to check out the skid control and auto brake system.
Boeing F80129 32-B37-1208 -100 1208 Antiskid - Auto Brake - Auto Speed Brake Tester. Used to check out the skid control and auto brake system.
Boeing F80135 29-MUL-1296 -1 1296 Cable Assembly - Hydraulic Leakage Check. To determine hydraulic leakage by measuring the current draw of the electric motor driven hydraulic pump.
Boeing F80135 29-MUL-1296 -10 1296 Cable Assembly - Hydraulic Leakage Check. To determine hydraulic leakage by measuring the current draw of the electric motor driven hydraulic pump.
Boeing F80138 34-MUL-1251 -1 1251 Extension Cable - Vertical Gyro. Connects the Tilt Table with A/P wiring for reference system testing. For A/P equipped with Bendix vertical gyro.
Boeing F80139 34-MUL-1198 -1 1198 Extension Cable - Vertical Gyro. Used to connect vertical gyro on the Tilt Table with A/P wiring for attitude reference system testing, Sperry Gyro.
Boeing F80165 80-B37-1629 -1 1629 Test Set - Door Proximity Sensor/Actuator Gap. Used on Door Warning System to check that actuator-to-sensor gap is correctly adjusted & to verify integrity of sensor-to-switch module wiring.
Boeing F80165 80-B37-1629 -42 1629 Test Set - Door Proximity Sensor/Actuator Gap. Used on Door Warning System to check that actuator-to-sensor gap is correctly adjusted & to verify integrity of sensor-to-switch module wiring.
Boeing F80206 24-B37-1262 -1 1262 Breakout Box - Cabin Pressure Control Unit. Used to check voltages from test connector on cabin pressure controller on P/N 763810-1 & -2.
Boeing F80208 32-B37-1499 -1 1499 Tester - Anti-skid/Autospeed Brake. Used to check wheel speed transducers with anti-skid system functional test. Simulates input signal to anti-skid control from wheel speed transducers.
Boeing F80217 22-B37-1265 -1 1265 Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.
Boeing F80217 22-B37-1265 -101 1265 Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.
Boeing F80217 22-B37-1265 -103 1265 Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.
Boeing F80217 22-B37-1265 -122 1265 Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.
Boeing F80217 22-B37-1265 -125 1265 Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.
Boeing F80217 22-B37-1265 -139 1265 Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.
Boeing F80218 27-B37-1313 -1 1313 Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.
Boeing F80218 27-B37-1313 -31 1313 Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.
Boeing F80218 27-B37-1313 -38 1313 Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.
Boeing F80218 27-B37-1313 -40 1313 Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.
Boeing F80218 27-B37-1313 -41 1313 Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.
Boeing F80218 27-B37-1313 -42 1313 Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.
Boeing F80221 80-B37-1263 -1 1263 Test Set - Proximity Sensors T/R. Used to supply 28VDC power to the T/R upper and lower door lock prox sensors. Provides the proper proximity sensor indication during T/R operation.
Boeing F80223 34-MUL-1264 -1 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80223 34-MUL-1264 -123 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set. Applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80223 34-MUL-1264 -140 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set. Applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80223 34-MUL-1264 -147 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set. Applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80223 34-MUL-1264 -148 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set. Applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80223 34-MUL-1264 -2 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set. Applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80223 34-MUL-1264 -3 1264 Radio Altitude Signal Simulator. Used to provide dual low range radio altimeter data to the autopilot system using only one test set. Applicable to any aircraft using two LRRA receiver-transmitters to ARINC 552A application with dual autopilot system.
Boeing F80224 80-B37-1605 -58 1605 Test Eqpt - Flight Spoiler Power Control Unit. Used to conduct functional test after overhaul of Flight Spoiler Power Control Units.
Boeing F80224 80-B37-1605 -60 1605 Test Eqpt - Flight Spoiler Power Control Unit. Used to conduct functional test after overhaul of Flight Spoiler Power Control Units.
Boeing F80225 22-B37-1521 -1 1521 SP177 Dual Channel FCC Test Equipment. Used to check the SP177 Dual Channel Autopilot Computers.
Boeing F80225 22-B37-1521 -19 1521 SP177 Dual Channel FCC Test Equipment. Used to check the SP177 Dual Channel Autopilot Computers.
Boeing F80227 80-B37-1577 -1 1577 Test Cable - N1 Simulation. Adapts a signal generator to aircraft test receptacle D556 to simulate N1 tach generator signal for testing full range autothrottle system.
Boeing F80228 80-B37-1578 -1 1578 Adapter Cable - N1 Simulator. Used to connect tach tester in place of the N1 tachometer transmitter to simulate N1 signals for testing full flight autothrottle system per MM.
Boeing F80228 80-B37-1578 -15 1578 Adapter Cable - N1 Simulator. Used to connect tach tester in place of the N1 tachometer transmitter to simulate N1 signals for testing full flight autothrottle system per MM.
Boeing F80229 26-MUL-1297 1297 Tester - Fire Extinguishing System. Used to test the electrical wiring continuity of the engine and APU fire extinguishing systems.
Boeing F80237 31-B37-1314 -1 1314 Test Set Equipment Cooling System Performance. Used for the adjustment and test of the equipment cooling system.
Boeing F80237 31-B37-1314 -13 1314 Test Set Equipment Cooling System Performance. Used for the adjustment and test of the equipment cooling system.
Boeing G21001 21-B47-1547 -1 1547 Lockout - Test Switch, N2 Engine Speed Discrete PCA. Used to hold the CH1 or CH2 switch of the N2 engine speed discrete PCA's in the test position to simulate engines on condition during test of the equipment cooling system.
Boeing G21001 21-B47-1547 -11 1547 Lockout - Test Switch, N2 Engine Speed Discrete PCA. Used to hold the CH1 or CH2 switch of the N2 engine speed discrete PCA's in the test position to simulate engines on condition during test of the equipment cooling system.
Boeing G21002 21-B47-1548 -1 1548 Test Equip - PRSRZ Outflow Valve Alt. Simulation. Used to test altitude pressure switch by simulating 11,000 ft cabin altitude pressure ICU (Sta 2210,WL182.RBL/LBL 77)
Boeing G21002 21-B47-1548 -17 1548 Test Equip - PRSRZ Outflow Valve Alt. Simulation. Used to test altitude pressure switch by simulating 11,000 ft cabin altitude pressure ICU (Sta 2210,WL182.RBL/LBL 77)
Boeing G21002 21-B47-1548 -26 1548 Test Equip - PRSRZ Outflow Valve Alt. Simulation. Used to test altitude pressure switch by simulating 11,000 ft cabin altitude pressure ICU (Sta 2210,WL182.RBL/LBL 77)
Boeing G21002 21-B47-1548 -30 1548 Test Equip - PRSRZ Outflow Valve Alt. Simulation. Used to test altitude pressure switch by simulating 11,000 ft cabin altitude pressure ICU (Sta 2210,WL182.RBL/LBL 77)
Boeing G22001 34-B47-1340 -119 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -120 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -122 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -123 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -139 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -140 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -147 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.
Boeing G22001 34-B47-1340 -148 1340 Test Equip - Low Range Radio Altimeter System. Used to test low range radio altimeter system.

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