Owner
Main P/N
Aero Info P/N
End Item
All P/N
Title
Boeing
03-B47-1600
03-B47-1600
-1
1600
Aircraft Digital Maintenance Information Terminal (ADMIT). Provides remote access to the Central Maintenance Computer (CMC) via a portable VXI mainframe computer attached to the CMC by a 75 foot long cable. Two touch-screen computer monitors are attached
Boeing
10-61959
28-MUL-1604
-*
1604
Specification - Test Set, Fuel Qty Gage. Test set specification for a variable capacitance fuel quantity gage test set. Used to check out and calibrate fuel gages and tank probes on aircraft.
Boeing
2ME65B94600
07-B47-1637
-*
1637
Aftermount Adapter - Lift Fixture, CF6. This replaces the G.E. Aft Mount Adapter on the G.E. Lift Fixture to allow engine pickup with the aft engine mount assy attached.
Boeing
2MIT65B80430
24-B47-1333
-*
1333
Box - Dual Outlet Rectifier. Used to rectify airplane electrical power (400 Hz AC) to DC utility electrical power for alternate means of opening nose cargo door when A/P system is inoperative.
Boeing
2TE60B00010
24-B47-1281
-*
1281
Breakout Box - Circuit Breaker, AC Generating System. Used to check continuity of auxiliary contacts of 60B00010-3, -10, -20, -25 split system circuit breaker; airplane with two external power systems.
Boeing
2TE60B40037-1
28-B47-1242
-*
1242
Adapter Cable. Used to adapt test tool TE60B40037-1 to front spar connector for testing individual TRW/Cinch fuel qty probes for airplanes Line No. 540 and on.
Boeing
2TE60B80099
22-B47-1321
-*
1321
Test Set - Autothrottle System TAT/EPRL. Eliminates req for PNEU pressure source to test EPR mode of full flight regime autothrottle sys on A/P with TAT/EPR limit controlled engines.
Boeing
2TE65B00713
30-B47-1635
-*
1635
Indicator - Beta Angle, Engine Trim. Used to enable use of AIDS installation for beta angle indication during engine trimming.
Boeing
2TE65B00776
28-MUL-1189
-1
1189
Harness - Cal Adapter, Fuel Qty Indicator. Used to connect variable capacitance test set to airplane wiring for calibration of fuel qty indicator.
Boeing
2TE65B00776
28-MUL-1189
-101
1189
Harness - Cal Adapter, Fuel Qty Indicator. Used to connect variable capacitance test set to airplane wiring for calibration of fuel qty indicator.
Boeing
2TE65B00776
28-MUL-1189
-51
1189
Harness - Cal Adapter, Fuel Qty Indicator. Used to connect variable capacitance test set to airplane wiring for calibration of fuel qty indicator.
Boeing
2TE65B46006
34-B47-1327
-*
1327
Test Cable, Flight Data Entry Panel. Test Cable will permit remote operation of flight data entry panel. Limited to KSS A/P with Hamilton Standard Aid System.
Boeing
2TE65B57053
12-B47-1328
-*
1328
Jumper Cable Set - Water Qty Xmtr Calibration. To check calib of water qty xmtr per chapter 38-14-00 of the Maintenance Manual.
Boeing
2TE65B63076
32-B47-1330
-*
1330
Test Equipment Simulator - Steerable PDU. Used to check mechanical and electrical functions of the Steerable Power Drive Units. (PDU 2, 3, 4R and 4L).
Boeing
2TSJ60B80099
22-B47-1324
-*
1324
Test Jig - Autothrottle Test Point Box. Facilitates testing of full flight regime autothrottle computer through computer test terminals.
Boeing
2TSJ65B40700
34-B47-1325
-*
1325
Adapter - Test Cable, Data Signal Display. Used as a test cable to connect the Data Signal Display Unit to the F.D.A.U.
Boeing
3MIT65B94600
72-B47-1199
-*
1199
Trim Kit - CF6-50E Engine. Allows adjustment of the main fuel control & monitoring of the VSV & VBV with the engine operating and cowl doors closed.
Boeing
3TE60B40147
28-B47-1318
-*
1318
Adapter Cable - Used to test tool TE60B40147-1 Front Spar Connector for testing individual Amphenol fuel qty probes for airplanes with firing order 1 - 589.
Boeing
3TE60B80099
22-B47-1321
-*
1321
Test Set - Autothrottle System TAT/EPRL. Eliminates req for PNEU pressure source to test EPR modeof full flight regime autothrottle sys on A/P with TAT/EPR limit controlled by RB211 series engines.
Boeing
3TE65B00776
28-MUL-1190
-1
1190
Harness - Cal Adapt, Fuel Qty Indicator. Used to connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator.
Boeing
3TE65B00776
28-MUL-1190
-101
1190
Harness - Cal Adapt, Fuel Qty Indicator. Used to connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator.
Boeing
3TE65B00776
28-MUL-1190
-51
1190
Harness - Cal Adapt, Fuel Qty Indicator. Used to connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator.
Boeing
3TE65B40880
34-B47-1272
-*
1272
Test Equipment Adapter Cables MHRS No. 1 & 2. Required to adapt the Magnetic Heading Reference System Synchro Transmitter output to a synchro repeater, North Atlantic Industries, Series 8300.
Boeing
3TE65B63076
34-B47-1330
-*
1330
Test Equipment - Simulator - Steerable PDU. Used to test operation of Power Drive Unit Steering Actuator limit switches. (for PDU's 6L, 6R, 7L & 7R)
Boeing
4TE60B00002
34-B47-1315
-*
1315
Cable, INS Attitude Simulator - Track Heading Systems. Used in place of -4 cable assy on the 4TSJ60B00002 INS Attitude Simulator. The cable/simulator tests INS ext program control configurations w/track heading.
Boeing
4TE60B80099
22-B47-1322
-*
1322
Test Set - Autothrottle System TAT/EPRL. Eliminates req for PNEU pressure source to test EPR modeof full flight regime autothrottle sys on A/P with TAT/EPR limit controlled by RB211 series engines.
Boeing
4TE65B63076
32-B47-1279
-*
1279
Test Equip - Simulator/Monitor, Steerable PDU 23R & 24. Used to simulate/monitor elect inputs to Steerable Power Units 23R & 24 during cargo handling functional test.
Boeing
5TE65B00776
28-MUL-1193
-1
1193
Harness - Cal Adapt, Fuel Qty. Used to connect test set to A/P for calibration of fuel qty inds & tank units. (ctr tanks on -200B,C,F & SR).
Boeing
5TE65B00776
28-MUL-1193
-101
1193
Harness - Cal Adapt, Fuel Qty. Used to connect test set to A/P for calibration of fuel qty inds & tank units. (ctr tanks on -200B,C,F & SR).
Boeing
5TE65B00776
28-MUL-1193
-51
1193
Harness - Cal Adapt, Fuel Qty. Used to connect test set to A/P for calibration of fuel qty inds & tank units. (ctr tanks on -200B,C,F & SR).
Boeing
5TE65B63076
32-B47-1331
-*
1331
Test Equip - Simulator - Steerable PDU. To check mechanical and electrical functions of the steerable power drive units. (PDU 23R & 24).
Boeing
5TSJ60B00002
34-B47-1195
1195
Simulator - Attitude I.N.S. Used in place of the INS Nav Unit to simulate airplane attitudes for the testing of autoflight, flight controls, and navigation systems.
Boeing
6TE65B00776
28-B47-1192
-*
1192
Harness - Calibration Adapter, Fuel Qty Totalizer. Used to calibrate fuel qty totalizer with fuel in the tanks.
Boeing
6TE65B63076
32-B47-1332
-*
1332
Test Equip - Simulator - Steerable/Retractable PDU. To provide dummy cams & elect monitor dev for posit adj of steerable, retractable PDU limit switches cargo loading system.
Boeing
6TSJ60B00002
34-B47-1568
1568
Simulator - Attitude, I.N.S. Used in place of the INS Nav Unit to simulate airplane attitudes for the testing of auto flight, flight controls, and navigation systems.
Boeing
7TE65B00776
28-B47-1298
-1
1298
Harness - Calib Adapt Fuel Qty Indicator. To connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator. For details of usage see 747 Maintenance Manual.
Boeing
7TE65B00776
28-B47-1298
-101
1298
Harness - Calib Adapt Fuel Qty Indicator. To connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator. For details of usage see 747 Maintenance Manual.
Boeing
7TE65B00776
28-B47-1298
-51
1298
Harness - Calib Adapt Fuel Qty Indicator. To connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator. For details of usage see 747 Maintenance Manual.
Boeing
8TE65B00776
28-B47-1246
-*
1246
Harness - Calibration Adapter, Fuel Qty Totalizer (9 Tanks). Used to calibrate fuel qty totalizer with fuel in tanks. At empty setting, with all inputs removed, input lines grounded, totalizer should read same as indicator.
Boeing
A21004
21-MUL-1341
-1
1341
Test Box - Current Sensor, Fan, Environmental Control System. Used to test the current sensor assy, P/N 285T0177, on the ECS fan.
Boeing
A22001
22-MUL-1342
-15
1342
Control Unit - Remote, Maintenance Control Display Panel. Enables remote operation of the MCDP and the display of its data on flight deck instruments.
Boeing
A22001
22-MUL-1342
-22
1342
Control Unit - Remote, Maintenance Control Display Panel. Enables remote operation of the MCDP and the display of its data on flight deck instruments.
Boeing
A22005
22-MUL-1343
-1
1343
Breakout Box - ATS Loadboard Yaw Damper Monitor Receiver, PCA. Used to test the yaw damper monitor receiver PCA.
Boeing
A22005
22-MUL-1343
-9
1343
Breakout Box - ATS Loadboard Yaw Damper Monitor Receiver, PCA. Used to test the yaw damper monitor receiver PCA.
Boeing
A22006
22-B67-1540
-1
1540
Breakout Box - Fault Display PCA, Yaw Damper. Used to test yaw damper unit module fault display.
Boeing
A22007
22-MUL-1541
-1
1541
Breakout Box - ARINC/Filter/Fuse PCA, Yaw Damper. Used in conjunction with A27039 Test Yaw Damper Unit Module ARINC/Filter/Fuse PCA Card. Per MM 22-21-35.
Boeing
A23001
23-MUL-1344
-1
1344
Acoustic Coupler - Attendants Handset. Used in conjunction with A23004 Flight Attendant Interphone Test Box to test 285T0038 Interphone Assy.
Boeing
A23001
23-MUL-1344
-4
1344
Acoustic Coupler - Attendants Handset. Used in conjunction with A23004 Flight Attendant Interphone Test Box to test 285T0038 Interphone Assy.
Boeing
A23001
23-MUL-1344
-8
1344
Acoustic Coupler - Attendants Handset. Used in conjunction with A23004 Flight Attendant Interphone Test Box to test 285T0038 Interphone Assy.
Boeing
A23001
23-MUL-1344
-8
1344
Acoustic
Boeing
A23001
23-MUL-1344
-9
1344
Acoustic Coupler - Attendants Handset. Used in conjunction with A23004 Flight Attendant Interphone Test Box to test 285T0038 Interphone Assy.
Boeing
A23001
23-MUL-1344
-9
1344
Acoustic
Boeing
A23002
23-MUL-1403
-1
1403
Test Box Assy - TV Antenna Coupler. Used to aid in the measurement of DC and RF parameters of the TV antenna coupler module assy.
Boeing
A23002
23-MUL-1403
-14
1403
Test Box Assy - TV Antenna Coupler. Used to aid in the measurement of DC and RF parameters of the TV antenna coupler module assy.
Boeing
A23003
23-MUL-1345
-15
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-17
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-20
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-23
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-24
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-29
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-30
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23003
23-MUL-1345
-34
1345
Test Box - Printed Circuit Cards, Audio Accessory Unit. Used to test cards in the audio accessory unit.
Boeing
A23004
23-MUL-1346
-1
1346
Test Box - Interphone, Flight Attendant. Used to test flight attendant interphone assembly (handset) P/N 285T0038.
Boeing
A23006
23-MUL-1347
-1
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-16
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-22
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-23
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-26
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-27
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-34
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-39
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-45
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-46
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23006
23-MUL-1347
-47
1347
Test Box - Audio Accessory Unit. Used to perform functional test on audio accessory unit.
Boeing
A23009
23-MUL-1348
-14
1348
Test Box - Audio Selector Panel. Used to functionally test 285T0022 audio selector panel, 285T0226 printed circuit card and 285T0227 printed circuit card.
Boeing
A23009
23-MUL-1348
-20
1348
Test Box - Audio Selector Panel. Used to functionally test 285T0022 audio selector panel, 285T0226 printed circuit card and 285T0227 printed circuit card.
Boeing
A23009
23-MUL-1348
-25
1348
Test Box - Audio Selector Panel. Used to functionally test 285T0022 audio selector panel, 285T0226 printed circuit card and 285T0227 printed circuit card.
Boeing
A23011
23-MUL-1349
-1
1349
Test Box - Power Supply, Audio Accessory Unit. Used to the the audio accessory unit (AAU) power supply assy, P/N 285T0387.
Boeing
A24004
24-MUL-1350
-1
1350
Test Relay - Isolation Request, Power Distribution System. Used to test AC power system switching in autoland mode.
Boeing
A24004
24-MUL-1350
-2
1350
Test Relay - Isolation Request, Power Distribution System. Used to test AC power system switching in autoland mode.
Boeing
A24005
24-MUL-1351
-1
1351
Load Bank - DC Generation System. Used to load the transformer rectifier unit during test of the DC generation system.
Boeing
A24008
24-MUL-1352
-1
1352
Test Box - Hydraulic Motor Driven GCU. Used to simulate hydraulic motor generator GCU operation.
Boeing
A24008
24-MUL-1352
-19
1352
Test Box - Hydraulic Motor Driven GCU. Used to simulate hydraulic motor generator GCU operation.
Boeing
A24008
24-MUL-1352
-27
1352
Test Box - Hydraulic Motor Driven GCU. Used to simulate hydraulic motor generator GCU operation.
Boeing
A25012
25-B67-1404
-1
1404
Electrical Test Equipment - Off Wing Escape Slide System. Used to simulate the door latch opening actuator and the spoiler override actuator squibs during off-wing escape slide system tests.
Boeing
A25012
25-B67-1404
-19
1404
Electrical Test Equipment - Off Wing Escape Slide System. Used to simulate the door latch opening actuator and the spoiler override actuator squibs during off-wing escape slide system tests.
Boeing
A25022
25-B67-1612
-1
1612
Test Equipment - PDU, Guide and Rollout Stops. Provides a means of breaking out wiring for testing and troubleshooting of the guides, rollout stops, and self-erecting PDU's in the general market freighters.
Boeing
A26001
26-MUL-1353
-1
1353
Electrical Test Equipment - Bottle Squib, Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib for voltage measurement during engine, APU & cargo compartment fire extinguishing system tests.
Boeing
A26001
26-MUL-1353
-101
1353
Electrical Test Equipment - Bottle Squib, Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib for voltage measurement during engine, APU & cargo compartment fire extinguishing system tests.
Boeing
A26001
26-MUL-1353
-102
1353
Electrical Test Equipment - Bottle Squib, Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib for voltage measurement during engine, APU & cargo compartment fire extinguishing system tests.
Boeing
A26001
26-MUL-1353
-106
1353
Electrical Test Equipment - Bottle Squib, Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib for voltage measurement during engine, APU & cargo compartment fire extinguishing system tests.
Boeing
A26001
26-MUL-1353
-131
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-132
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-133
1353
Electrical Test Equipment - Bottle Squib, Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib for voltage measurement during engine, APU & cargo compartment fire extinguishing system tests.
Boeing
A26001
26-MUL-1353
-134
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-135
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-136
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-137
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-138
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-139
1353
Adapter Cable Assy
Boeing
A26001
26-MUL-1353
-144
1353
Adapter Cable Assy