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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 J26006 thru TSJSPZ1-4

Owner Main P/N Aero Info P/N End Item All P/N Title
Boeing J26006 26-B77-1616 -1 1616 Controller - Power Supply, E/E Cooling Fans. Used for facilitating the operation of the Electrical/Electronic Cooling Fans (Vent and Left Supply Fan) during a normal disabler test. Consists of -2 controller assy and -3 storage box assy.
Boeing J26007 26-MUL-1610 -1 1610 Test Box, Cargo Smoke Heater Test Plug. Used to simulate Heater Sensor Circuit and measure voltage output of the Cargo Smoke Detection System Heater Controllers. (Applicable to 777-200; 767 GMF; 747-400 All except freighters).
Boeing J27056 27-MUL-1634 -1 1634 Test Eqpt-Run In, Variable Drive. Used in conjunction with customer furnished component test fixtures to accomplish run-in tests.
Boeing J27056 27-MUL-1634 -2 1634 Test Eqpt-Run In, Variable Drive. Used in conjunction with customer furnished component test fixtures to accomplish run-in tests.
Boeing J27056 27-MUL-1634 -38 1634 Test Eqpt-Run In, Variable Drive. Used in conjunction with customer furnished component test fixtures to accomplish run-in tests.
Boeing J27056 27-MUL-1634 -39 1634 Test Eqpt-Run In, Variable Drive. Used in conjunction with customer furnished component test fixtures to accomplish run-in tests.
Boeing J32001 32-MUL-1539 -1 1539 Measuring Equip - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals.
Boeing J32001 32-MUL-1539 -31 1539 Measuring Equip - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals.
Boeing J32001 32-MUL-1539 -39 1539 Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals.
Boeing J32001 32-MUL-1539 -43 1539 Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals.
Boeing J32001 32-MUL-1539 -46 1539 Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals.
Boeing J34001 34-B77-1586 -17 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -18 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -19 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -20 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -23 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -24 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -25 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -26 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -27 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -28 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -50 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -51 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -52 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -53 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -54 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -55 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -56 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -57 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -58 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J34001 34-B77-1586 -59 1586 Breakout Box - Line Maintenance. Used to provide pin access for LRU rack connectors.
Boeing J52027 52-B77-1617 -1 1617 Test Box - Connector, Squib. Used to aid in measuring continuity and battery pack voltage at the EPAS Reservoir Squib Connector (DM52109).
Boeing J52029 52-B77-1618 -1 1618 Test Eqpt - Squib, Overwing Exit. Used to verify Squib firing current on Escape Slide, EPAS (Emergency Power Assist System).
Boeing MIT69B62284 12-B47-1280 -* 1280 By-Pass Jumper Plug - Retractable PDU, Cargo Handling to simulate A/P actuated positions of S1, S2 & S3 PDU Limit Switches to permit operation of side cargo door powered loading system if drive unit fails.
Boeing ST895A-3 70-MUL-1603 -1 1603 Probe - Surface Resistivity Measurement. Used to measure surface resistivity of flat panels, fairings and radomes.
Boeing TE60B00019 77-B47-1317 -1 1317 Adapter Harness - Oil Qty Ind. Calib. Used to permit Connecting a variable capacitance test set to the airplane wiring for calibration of the oil qty indicator. Selection required.
Boeing TE60B00019 77-B47-1317 -101 1317 Adapter Harness - Oil Qty Ind. Calib. Used to permit Connecting a variable capacitance test set to the airplane wiring for calibration of the oil qty indicator. Selection required.
Boeing TE60B00019 77-B47-1317 -51 1317 Adapter Harness - Oil Qty Ind. Calib. Used to permit Connecting a variable capacitance test set to the airplane wiring for calibration of the oil qty indicator. Selection required.
Boeing TE60B40037-1 28-B47-1244 -* 1244 Test Adapter - Fuel Qty Gage. Used to connect variable capacitance test set to front spar connector for testing individual fuel qty probes.
Boeing TE60B40108 28-B47-1276 1276 Test Equipment - Override/Jettison Fuel Pump, Fault Current Detector. Used to provide a dummy load for testing.
Boeing TE60B40147 28-B47-1566 -* 1566 Test Adapter - TRW Cinch Fuel Qty Probe. To connect variable capacitance test set to front spar connector for testing of individual fuel quantity probes. (Applies to Apls Mfg after June, 1981)
Boeing TE60B80099 22-B47-1320 -* 1320 Test Set - Autothrottle System TAT/EPRL. Eliminates req for PNEU pressure source to test EPR mode of full flight regime autothrottle system on A/P with TAT/EPR limit controlled engines.
Boeing TE65B00776 28-MUL-1188 -1 1188 Harness - Cal Adapt, Fuel Qty Indicator. Used to connect test set to A/P for calib of fuel qty inds. & tank units. (wing & ctr tanks on -100 & SP, wing only on others).
Boeing TE65B00776 28-MUL-1188 -101 1188 Harness - Cal Adapt, Fuel Qty Indicator. Used to connect test set to A/P for calib of fuel qty inds. & tank units. (wing & ctr tanks on -100 & SP, wing only on others).
Boeing TE65B00776 28-MUL-1188 -51 1188 Harness - Cal Adapt, Fuel Qty Indicator. Used to connect test set to A/P for calib of fuel qty inds. & tank units. (wing & ctr tanks on -100 & SP, wing only on others).
Boeing TE65B40719 24-MUL-1274 -* 1274 Breakout Box - Ground Safety Relay. Used to probe ground safety relays while functioning.
Boeing TE65B40861 32-B47-1326 -* 1326 Test Equipment, Warning Switches MLG. Used to deactivate electric switches per functional test document D6-13200 Sec. 02.4100, Rev. B.
Boeing TE65B40880 22-B47-1197 -* 1197 Test Equip. Adapter Cables MHRS No. 1 & 2. These cables are required to adapt the magnetic heading reference system synchro transmitter output to a synchro repeater.
Boeing TE65B42891 52-B47-1200 -* 1200 Breakout Box - Side Cargo Door Module. Used to test 747 side cargo door module assembly.
Boeing TE65B83189 27-B47-1639 -* 1639 Test Unit - Rudder Ratio Control System. Used to detect defective units in the Rudder Ratio Control System
Boeing TE65B84683 52-B47-1335 -* 1335 Test Tool - Pressure Vessel Cartridge, Type "A" Door. Used to check the pressure vessel electrical firing system for type "A" door - stretched upper deck.
Boeing TE65B88745 26-B47-1636 -* 1636 Test Set - Flowmeter Hyd Sys Leakage. Provides means of monitoring internal leakage rate in each hydraulic system with Arkwin Flowmeter installed on airplane.
Boeing TE65B90115 71-B47-1269 -* 1269 Adapter Cable - Engine Oil Qty, A/P Wiring. Used to check engine oil qty airplane wiring for capacitance. Applicable to JT9D-3 and -7 engines only.
Boeing TE65B91156 71-B47-1270 -* 1270 Cable - Oil Tank Probe, Engine. Used to check the engine oil tank probe for capacitance. Applicable to JT9D-3 and -7 engines only.
Boeing TE69B48251 30-MUL-1638 -* 1638 Used to verify that lightning protectors will dissipate lightning surge.
Boeing TSJ60B00002-2 34-B47-1273 -* 1273 Autothrottle Adapter Attitude Sim. Table. To mount the autothrottle computer for simultaneous tilting operations during functional test.
Boeing TSJ60B80099 77-B47-1323 -* 1323 Test Cable & B/O Box, Auto Throttle Comp. To allow testing of full flight regime autothrottle computer when removed from A/P and to provide access to individual wires of input cable.
Boeing TSJSPZ1-1 22-B47-1183 -* 1183 Test Jig - Pitch and Roll Computer Test. Test box to gain access to test connector terminals of autopilot pitch & roll computers.
Boeing TSJSPZ1-2 22-B47-1184 -* 1184 Test Jig - Monitor Logic and Auto. Stab. Test box to gain access to test connector terminals of autopilot monitor and logic unit, plus auto-stabilizer trim unit.
Boeing TSJSPZ1-3 22-B47-1185 -* 1185 Test Jig - Accessory Box, Test Point Box. Used to gain access to test connector terminals of autopilot accessory boxes 1 & 2, plus stabilizer trim accessory box.
Boeing TSJSPZ1-4 22-B47-1186 -* 1186 Test Jig - Landing Control and Logic Unit. To gain access to the test connector terminals of the autopilot landing control and logic unit on those A/P equipped with Sperry Rand landing control.

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


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