|
Main P/N
|
End Item
|
Title
|
Aero Info P/N
|
Applicability
|
Supersedes
|
Replaces
|
| 906-10246-3 |
|
Loop Resistance Tester |
|
737-NG |
|
|
| PTTS-892B |
|
Position Transmitter Test Set |
|
737-ALL |
|
|
| 10-61959 |
-* |
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. |
28-MUL-1604 |
737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| 2TE65B00776 |
-1 |
Harness - Cal Adapter, Fuel Qty Indicator. Used to connect variable capacitance test set to airplane wiring for calibration of fuel qty indicator. |
28-MUL-1189 |
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| 2TE65B00776 |
-101 |
Harness - Cal Adapter, Fuel Qty Indicator. Used to connect variable capacitance test set to airplane wiring for calibration of fuel qty indicator. |
28-MUL-1189 |
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| 2TE65B00776 |
-51 |
Harness - Cal Adapter, Fuel Qty Indicator. Used to connect variable capacitance test set to airplane wiring for calibration of fuel qty indicator. |
28-MUL-1189 |
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
|
|
|
|
|
|
|
| 3TE65B00776 |
-1 |
Harness - Cal Adapt, Fuel Qty Indicator. Used to connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator. |
28-MUL-1190 |
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| 3TE65B00776 |
-101 |
Harness - Cal Adapt, Fuel Qty Indicator. Used to connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator. |
28-MUL-1190 |
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| 3TE65B00776 |
-51 |
Harness - Cal Adapt, Fuel Qty Indicator. Used to connect variable capacitance test set to A/P wiring for calibration of fuel qty indicator. |
28-MUL-1190 |
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| A27036 |
-22 |
Test Box - Power Supply, Flap Slat Electronic Unit (FSEU). Power Supply Assy P/N 285T0286. |
27-B67-1406 |
737-400
737-400
|
A27036-1, -16
A27036-1, -16
|
|
| A27081 |
-1 |
Readout And Control Equipment - Functional Test Stands. Used to test the elevator feel & centering unit, TE flaps rotary actuator, TE flaps power drive unit, inboard & outboard LE slats power drive
unit, & the ovhd. Pass. Center balance gearbox |
27-MUL-1362 |
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
737-ADV
737-CQC
|
|
|
| A31007 |
-1 |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector.
Notes: Used with Teledyne Tester 2222786, 2227295, 2225302
|
31-MUL-1285 |
737-200
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| A31007 |
-34 |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Sundstrand tester to the appropriate digital flight recorder system test connector.
Notes: Used with Sundstrand Tester 981-6301-002
|
31-MUL-1285 |
737-300
737-400
737-500
737-ADV
|
|
A31007-30
A31007-30
A31007-30
A31007-30
|
| A31007 |
-39 |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector.
Notes: Used with Teledyne Tester
|
31-MUL-1285 |
737-200
737-300
737-400
737-500
737-ADV
737-CQC
|
|
|
| A31007 |
-49 |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Sundstrand tester to the appropriate digital flight recorder system test connector.
Notes: Used with Sundstrand Tester 981-6301-002
|
31-MUL-1285 |
737-200
737-300
737-400
737-500
737-ADV
737-CQC
|
|
A31007-30
A31007-30
A31007-30
A31007-30
A31007-30
A31007-30 |
| A31007 |
-59 |
Adapter Cable - Tester, Digital Flight Recorder System. Used to adapt Teledyne tester to the appropriate digital flight recorder system test connector.
Notes: Used with Teledyne Tester 2229738
|
31-MUL-1285 |
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
737-ADV
737-CQC
|
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11
A31007-11 |
|
| A33003 |
-359 |
Breakout Box - Multipurpose. Used for component testing of panel assemblies.
Notes: See drawing for applicable cable assemblies.
|
33-MUL-1371 |
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
737-ADV
737-CQC
|
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1
A33003-1 |
|
| A34011 |
-1 |
Breakout Box Equipment - ARINC 600, Line Maintenance. Used to probe ARINC 600 airplane connectors for continuity checking and interfacing the ARINC 429 digital data bus analyzer with airplane wiring. |
34-MUL-1380 |
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
737-ADV
737-CQC
|
|
|
| A34011 |
-112 |
Breakout Box Equipment - ARINC 600, Line Maintenance. Used to probe ARINC 600 airplane connectors for continuity checking and interfacing the ARINC 429 digital data bus analyzer with airplane wiring.
Notes: -112 Connector Kit consists of assorted connectors and a storage box.
|
34-MUL-1380 |
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
737-ADV
737-CQC
|
|
|
| A34015 |
-27 |
Test Box - Power Interrupt, ILS/VOR Control Panel. Used in conjunction with A33003 during test of ILS and VOR control panels. |
34-MUL-1383 |
737-300
737-400
737-500
737-600
737-700
737-800
737-900
|
A34015-23
A34015-23
A34015-23
A34015-23
A34015-23
A34015-23
A34015-23 |
|
| A38010 |
-11 |
Test Cable - Potable Water Quantity Xmtr. Used to provide electrical access to water tank quantity transmitter for calibration. |
38-MUL-1583 |
737-600
737-700
737-800
737-900
|
A38010-1
A38010-1
A38010-1
A38010-1 |
|
| A77003 |
-38 |
Test Box - Indicating System, Exhaust Gas
Temperature (EGT). Used during test of the exhaust gas temperature indicating system. (P&W) |
77-MUL-1299 |
737-300
737-400
737-500
|
A77003-10,-28,-3
A77003-10,-28,-3
A77003-10,-28,-3
|
|
| B20005 |
-52 |
Test Equipment - Velocity/Position Transducer. Used in conjunction with functional test stands to interface with X-Y plotter and oscilloscope where velocity/position measurements are required. |
20-MUL-1300 |
737-300
737-400
737-500
|
B20005-1
B20005-1
B20005-1 |
|
| B78009 |
-21 |
Lock Equipment - Thrust Reverser Maintenance. Used to energize thrust reverser arm solenoid to positively prevent deploy command to directional control valve. |
737-300
737-400
737-500 |
|
|
|
| B78009 |
-26 |
Lock Equipment - Thrust Reverser Maintenance. Used to energize thrust reverser arm solenoid to positively prevent deploy command to directional control valve. |
78-B37-1569 |
737-300
737-400
737-500
737-600
737-700
737-800
737-900
|
|
|
| C21001 |
-18 |
Test Box - IRS Master Caution Module. Used to test the IRS Master Caution Module.
Notes: Used on IRS P/N's 69-37399-1,-7,-9; 69-73636 & 69-51813-9.
|
22-B37-1254 |
737-300
737-400
737-500
|
C22001-13
C22001-13
C22001-13 |
|
| C21001 |
-21 |
Test Box - IRS Master Caution Module. Used to test the IRS Master Caution Module.
Notes: Used on IRS P/N's 69-37399-8,-10,-12
|
22-B37-1254 |
|
|
|
| C22003 |
-22 |
Test Box - Mach Trim Actuator. Used to test Mach Trim Actuator. |
22-B37-1287 |
737-300
737-400
737-500
|
C22003-18
C22003-18
C22003-18
|
|
| C22004 |
-1 |
Breakout Box - IFSAU (65-52820). Used to access the pins when testing and troubleshooting the IFSAU (Integrated Flight System Accessory Unit). |
22-B37-1570 |
|
|
|
| C22005 |
-22 |
Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors. |
|
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
|
|
C22005-1
C22005-1
C22005-1
C22005-1
C22005-1
C22005-1
C22005-1
C22005-1
C22005-1 |
| C22005 |
-4 |
Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors. |
|
737-600
737-700
737-800
737-900
|
|
|
| C22005 |
-5 |
Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors. |
|
737-600
737-700
737-800
737-900
|
|
|
| C22005 |
-6 |
Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors. |
|
737-600
737-700
737-800
737-900
|
|
|
| C22005 |
-7 |
Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors. |
|
737-600
737-700
737-800
737-900
|
|
|
| C22005 |
-8 |
Breakout Box - Multipurpose, 100 Pin. Used for testing components and/or systems. It is also used to access (breakout) contacts of connectors. |
|
737-600
737-700
737-800
737-900
|
|
|
| C23001 |
-15 |
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). |
|
737-100
737-600
737-700
737-800
737-900
|
|
C23001-13
C23001-13
C23001-13
C23001-13
C23001-13 |
| C24005 |
-1 |
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. |
|
737-600
737-700
737-800
737-900
|
|
|
| C24006 |
-1 |
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. |
|
737-600
737-700
737-800
737-900 |
|
|
| C26002 |
-21 |
Test Equipment - Engine/APU Fire Detection System (Walter Kidde). |
|
737-300
737-400
737-500
|
C26002-1
C26002-1
C26002-1
|
|
| C26005 |
-1 |
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 parallel. |
|
737-600
737-700
737-800
737-900
|
|
|
| C26006 |
-1 |
Test Box - Cargo Fire Extinguishing System. Used to test the airplane electrical wiring to the forward cargo and aft squibs on the bottle(s). |
|
737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-900
737-ADV
737-CQC
|
|
|
| C27006 |
-34 |
Test Equip - Cutout Switch, Stab Trim Control (Component Maintenance). Used to perform functional test on cutout switch assy. |
27-B37-1301 |
737-300
737-400
737-500
|
|
C27006-12, -22
C27006-12, -22
C27006-12, -22 |
| C27007 |
-31 |
Test Box - Cutout Switch, Stab Trim Control (Line Maintenance). Used to test stabilizer trim cutout system in conjunction with rapid control column movement. |
27-B37-1302 |
737-300
737-400
737-500
737-600
737-700
737-800
737-900
|
|
C27007-26
C27007-26
C27007-26
C27007-26
C27007-26
C27007-26
C27007-26 |
| 27009 |
-13 |
Test Box - Digital Stall Warning Computer. Used to test Digital Stall Warning Computer Unit.
Notes: C27009-13 is used on Boeing 65-52819-3 & -10 Digital Stall Warning Computers only. C27009-15 is used on all others.
|
27-B37-1303 |
737-300 |
|
C27009-1 |
| C27009 |
-22 |
Test Box - Digital Stall Warning Computer. Used to test Digital Stall Warning Computer Unit. |
27-B37-1303 |
737-100
737-200
737-CQC
737-ADV
737-500
737-600
737-700
737-800
737-900
|
|
C27009-15
C27009-15
C27009-15
C27009-15
C27009-15
C27009-15
C27009-15
C27009-15
C27009-15 |
| C27010 |
-21 |
Test Box - Autoslat Computer. Use to test Autoslat Computer Assy. |
27-B37-1582 |
737-300
737-400
|
C27010-19
C27010-19
|
|
| C27011 |
-16 |
Test Box - Auxiliary PCA, DSWC. Used to test Digital Stall Warning Computer Auxiliary PCA. |
27-B37-1304 |
737-300
737-400 |
C27011-1, -12
C27011-1, -12
|
|
| C27013 |
-1 |
Test Box - Auxiliary PCA, DSWC. Used to test Digital Stall Warning Computer Auxiliary PCA.
Notes: Used on DSWC P/N's 65-52819-3. C27013-11 is used on all other DSWC's.
|
27-B37-1579 |
737-300 |
|
|
| C27013 |
-11 |
Test Box - Auxiliary PCA, DSWC. Used to test Digital Stall Warning Computer Auxiliary PCA.
Notes: Used on DSWC P/N's 65-52819-3. C27013-11 is used on all other DSWC's.
|
27-B37-1579 |
737-300
737-400 |
|
|
| C27014 |
-1 |
Test Box - Discrete Input/Output PCA, DSWC. Used to test Digital Stall Warning Computer discrete input/output printed circuit assy.
Notes: Used on airplanes equipped with 65-52819-3 & -10 Digital Stall Warning Computers. C27014-21 used on all others.
|
27-B37-1305 |
737-300 |
|
|
| C27014 |
-21 |
Test Box - Discrete Input/Output PCA, DSWC. Used to test Digital Stall Warning Computer discrete input/output printed circuit assy.
Notes: Used on airplanes equipped with 65-52819-3 & -10 Digital Stall Warning Computers. C27014-21 used on all others.
|
|
737-300
737-400
|
C27014-11
C27014-11
|
|
| C27016 |
-1 |
Test Box - Central Processing Unit PCA Card. Used to test Central Processing Unit printed circuit assembly card.
Notes: C27016-1 used on airplanes equipped with 65-52819-3 and -10 Digital Stall Warning Computer. C27016-11 used on all others.
|
27-B37-1306 |
737-300 |
|
|
| C27016 |
-11 |
Test Box - Central Processing Unit PCA Card. Used to test Central Processing Unit printed circuit assembly card.
Notes: C27016-1 used on airplanes equipped with 65-52819-3 and -10 Digital Stall Warning Computer. C27016-11 used on all others.
|
27-B37-1306 |
737-300
737-400 |
|
|
| C29002 |
-17 |
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. |
|
737-600
737-700
737-800
737-900
|
C29002-1
C29002-1
C29002-1
C29002-1
|
|
| C30001 |
-1 |
Test Box - P5-9, Window and Pitot Heat Module. Used to bench test the P5-9 Window and Pitot Heat Module. |
|
737-600
737-700
737-800
737-900 |
|
|
| C30001 |
-21 |
Test Box - P5-9, Window and Pitot Heat Module. Used to bench test the P5-9 Window and Pitot Heat Module. |
|
737-600
737-700
737-800
737-900
|
|
|
| C31001 |
-13 |
Test Box - Printed Circuit Card Window & Pitot Heat. Used to test window and pitot heat printed circuit assembly. |
31-B37-1307 |
737-300
737-400
737-500 |
C31001-1
C31001-1
C31001-1
|
|
| C31003 |
-1 |
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. |
31-B37-1571 |
737-300
737-400
737-500 |
|
|
| C32001 |
-1 |
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. |
32-B37-1308 |
737-300
737-400
737-500
737-600
737-700
737-800 |
|
|
| C32004 |
-58 |
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. |
27-B37-1518 |
737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
|
C32004-47,-52
C32004-47,-52
C32004-47,-52
C32004-47,-52
C32004-47,-52
C32004-47,-52
C32004-47,-52
|
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