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747 ELECTRONIC TEST EQUIPMENT
747 PRODUCTS AS LISTED IN BOEING, DOUGLAS
PRODUCTS DIVISION, SUPPORT EQUIPMENT SUMMARY
(ALPHA-NUMERIC BY MAIN P/N)
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Next Page |
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| Main P/N |
G26001 |
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| End Item |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747
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A26001-102 |
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| Main P/N |
G26001 |
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| End Item |
-105 |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
747-SP
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G26001-90,-67
G26001-90,-67
G26001-90,-67
G26001-90,-67
G26001-90,-67
G26001-90,-67
G26001-90,-67
G26001-90,-67 |
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| Main P/N |
G26001 |
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| End Item |
-72 |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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G26001-58 |
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| Main P/N |
G26001 |
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| End Item |
-73 |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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G26001-60 |
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| Main P/N |
G26001 |
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| End Item |
-74 |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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G26001-50 |
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| Main P/N |
G26001 |
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| End Item |
-91 |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
G26001 |
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| End Item |
-92 |
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| Aero Info P/N |
26-B47-1278 |
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| Title |
Test Equip - Fire Extinguisher System. Used to simulate the fire extinguisher bottle squib during engine, APU and cargo compartment fire extinguishing system tests. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
G26003 |
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| End Item |
-1 |
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| Aero Info P/N |
26-B47-1551 |
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| Title |
Breakout Box - DA-15P Connector. Used to test 285U0291 CA11/Smoke Door Indicator Module or any component having a DA-15P type connector. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
G26004 |
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| End Item |
-39 |
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| Aero Info P/N |
31-MUL-1497 |
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| Title |
Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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G26004-1, -10
G26004-1, -10 |
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| Main P/N |
G26004 |
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| End Item |
-40 |
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| Aero Info P/N |
31-MUL-1497 |
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| Title |
Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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G26004-23
G26004-23 |
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| Main P/N |
G26004 |
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| End Item |
-55 |
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| Aero Info P/N |
31-MUL-1497 |
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| Title |
Extender Card - Electronic Card File. Used to monitor and troubleshoot electronic card by providing pin access to connectors. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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G26004-49
G26004-49 |
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| Main P/N |
G27009 |
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| End Item |
-19 |
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| Aero Info P/N |
27-B47-1277 |
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| Title |
Test Box - Alternate Drive Motor L/E Flap. Used to verify three phase electrical power availability to the LE flap alternate drive. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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| Main P/N |
G27021 |
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| End Item |
-1 |
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| Aero Info P/N |
27-B47-1552 |
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| Title |
Breakout Box - ARINC/Filter/Fuse PCA. Used in conjunction with A27039 breakout box to test the ARINC/Filter/Fuse PCA card. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
G27025 |
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| End Item |
-1 |
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| Aero Info P/N |
27-B47-1553 |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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| Main P/N |
G27027 |
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| End Item |
-1 |
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| Aero Info P/N |
27-B47-1554 |
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| Title |
Control Box Equip - Power Pack, TE Flap Drive. Used to test the operation of the Power Pack Drive Unit of the TE Flap. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
G27033 |
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| End Item |
-1 |
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| Aero Info P/N |
27-MUL-1555 |
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| Title |
Adapter Cable - Outboard Aileron Lockout. Used to allow the outboard aileron lockout actuator to be driven to the retracted (locked) position. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
G27033 |
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| End Item |
-2 |
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| Aero Info P/N |
27-MUL-1555 |
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| Title |
Adapter Cable - Outboard Aileron Lockout. Used to allow the outboard aileron lockout actuator to be driven to the retracted (locked) position. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
G28002 |
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| End Item |
-48 |
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| Aero Info P/N |
28-B47-1556 |
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| Title |
Test Equip - Volumetric Top-Off Calibration. Used to test Volumetric Shutoff Control Unit. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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G28002-38
G28002-38
G28002-38
G28002-38
G28002-38
G28002-38
G28002-38
G28002-38 |
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| Main P/N |
G28006 |
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| End Item |
-1 |
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| Aero Info P/N |
28-B47-1557 |
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| Title |
Adapter Equipment - Calibration, Fuel Quantity Totalizer. Used to calibrate fuel quantity totalizer with fuel in tanks. Applicable to airplanes with ten fuel tanks. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
G28007 |
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| End Item |
-15 |
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| Aero Info P/N |
28-B47-1558 |
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| Title |
Test Box - Fuel Quantity Indicating System. Used during test of the Fuel Quantity Indicating System (FQIS) to further isolate faults after BITE analysis. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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G28007-1
G28007-1 |
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| Main P/N |
G28013 |
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| End Item |
-16 |
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| Aero Info P/N |
28-B47-1524 |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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G28013-1
G28013-1
G28013-1
G28013-1
G28013-1
G28013-1
G28013-1
G28013-1
G28013-1
G28013-1 |
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| Main P/N |
G32006 |
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| End Item |
-1 |
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| Aero Info P/N |
32-B47-1559 |
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| Title |
Breakout Box - Control Lever, Landing Gear Actuator Module Assy. Used to test Control Lever Gear Actuator Module Assy. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
G32014 |
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| End Item |
-20 |
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| Aero Info P/N |
32-B47-1560 |
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| Title |
Test Equip - Torque Sensor, Brake Control. Used to test Brake Control Unit response to variations in torque sensor input. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
747-400F
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| Main P/N |
G32016 |
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| End Item |
-1 |
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| Aero Info P/N |
32-B47-1561 |
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| Title |
Breakout Box - Landing Gear Control Lever Module. Used to test the 257U0002 Landing Gear Control Lever Module per CMM 32-31-01. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
G32018 |
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| End Item |
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| Aero Info P/N |
32-B47-1562 |
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| Title |
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. |
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| Notes |
G32018-104, -108 Thru -117 Supercedes -61. G32018-61 Supercedes -1. |
Applicability
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Supersedes
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Replaces
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747-400
747-400F
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See Notes
See Notes |
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| Main P/N |
G36035 |
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| End Item |
-1 |
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| Aero Info P/N |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
G36035 |
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| End Item |
-2 |
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| Aero Info P/N |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
G38001 |
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| End Item |
-21 |
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| Aero Info P/N |
38-B47-1564 |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400F
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G38001-1 |
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| Main P/N |
G77001 |
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| End Item |
-1 |
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| Aero Info P/N |
77-B47-1268 |
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| Title |
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) |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
G77001 |
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| End Item |
-2 |
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| Aero Info P/N |
77-B47-1268 |
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| Title |
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) |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
G77001 |
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| End Item |
-3 |
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| Aero Info P/N |
77-B47-1268 |
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| Title |
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) |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
G77003 |
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| End Item |
-1 |
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| Aero Info P/N |
77-B47-1565 |
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| Title |
Test Box - PIMU. Used to perform manual test of the Propulsion Interface Monitor Unit module per CMM 77-51-01. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-200B
747-200C
747-200F
747-300
747-COMB
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| Main P/N |
J26007 |
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| End Item |
-1 |
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| Aero Info P/N |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-400
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| Main P/N |
J32001 |
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| End Item |
-43 |
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| Aero Info P/N |
32-MUL-1539 |
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| Title |
Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals. |
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| Notes |
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Applicability
|
Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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J32001-39
J32001-39
J32001-39
J32001-39
J32001-39
J32001-39
J32001-39
J32001-39
J32001-39
J32001-39 |
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| Main P/N |
J32001 |
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| End Item |
-46 |
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| Aero Info P/N |
32-MUL-1539 |
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| Title |
Measuring Equipment - Brake Pedal. Used to measure the load applied and the angle of travel of the brake pedals. |
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| Notes |
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Applicability
|
Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
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J32001-43
J32001-43
J32001-43
J32001-43
J32001-43
J32001-43
J32001-43
J32001-43
J32001-43
J32001-43 |
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| Main P/N |
MIT69B62284 |
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| End Item |
-* |
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| Aero Info P/N |
12-B47-1280 |
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| Title |
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. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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|
|
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-COMB
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| Main P/N |
T&E 31-32-04 |
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| End Item |
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| Aero Info P/N |
P/N 31-MUL-1077 |
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| Title |
Simulator, Low Level AC. For checking Flight Data Recorder. Per T&E 31-32-05. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
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|
747-100
747-200B
747-200C
747-200F
747-COMB
747-300
747-100B
747-400SP
747-400
747-400F
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| Main P/N |
TE60B00019 |
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| End Item |
-1 |
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| Aero Info P/N |
77-B47-1317 |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-COMB
747-SP
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| Main P/N |
TE60B00019 |
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| End Item |
-101 |
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| Aero Info P/N |
77-B47-1317 |
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| Title |
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. |
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| Notes |
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Applicability
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Supersedes
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Replaces
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747-100
747-100B
747-200B
747-200C
747-200F
747-COMB
747-SP
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| Main P/N |
TE60B00019 |
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| End Item |
-51 |
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| Aero Info P/N |
77-B47-1317 |
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| Title |
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. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
|
|
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747-100
747-100B
747-200B
747-200C
747-200F
747-COMB
747-SP
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| Main P/N |
TE60B40037-1 |
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| End Item |
-* |
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| Aero Info P/N |
28-B47-1244 |
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| Title |
Test Adapter - Fuel Qty Gage. Used to connect variable capacitance test set to front spar connector for testing individual fuel qty probes. |
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| Notes |
Notes For A/P with Amphenol connectors. |
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
TE60B40147 |
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| End Item |
-* |
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| Aero Info P/N |
28-B47-1566 |
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| Title |
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) |
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| Notes |
A/P line number 540 and on. |
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
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| Main P/N |
TE60B80099 |
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| End Item |
-* |
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| Aero Info P/N |
22-B47-1320 |
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| Title |
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. |
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| Notes |
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Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-COMB
747-SP
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| Main P/N |
TE65B00776 |
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| End Item |
-1 |
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| Aero Info P/N |
28-MUL-1188 |
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| Title |
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). |
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| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
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|
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| Main P/N |
TE65B00776 |
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|
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| End Item |
-101 |
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| Aero Info P/N |
28-MUL-1188 |
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|
|
| Title |
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). |
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| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
TE65B00776 |
|
|
|
| End Item |
-51 |
|
|
|
| Aero Info P/N |
28-MUL-1188 |
|
|
|
| Title |
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). |
|
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|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
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|
| Main P/N |
TE65B40719 |
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| End Item |
-* |
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| Aero Info P/N |
24-MUL-1274 |
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| Title |
Breakout Box - Ground Safety Relay. Used to probe ground safety relays while functioning. |
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| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
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|
| Main P/N |
TE65B40861 |
|
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| End Item |
-* |
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|
|
| Aero Info P/N |
32-B47-1326 |
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|
|
| Title |
Test Equipment, Warning Switches MLG. Used to deactivate electric switches per functional test document D6-13200 Sec. |
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| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
747-SP
|
|
|
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| Main P/N |
TE65B40880 |
|
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| End Item |
-* |
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| Aero Info P/N |
22-B47-1197 |
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|
| Title |
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. |
|
|
|
| Notes |
For 8300 Series North Atlantic Industries Synchro Repeater use 3TE65B40880. |
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
TE65B42891 |
|
|
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| End Item |
-* |
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|
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| Aero Info P/N |
52-B47-1200 |
|
|
|
| Title |
Breakout Box - Side Cargo Door Module. Used to test 747 side cargo door module assembly. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-400
747-400F
747-COMB
|
|
|
|
|
| Main P/N |
TE65B83189 |
|
|
|
| End Item |
-* |
|
|
|
| Aero Info P/N |
27-B47-1639 |
|
|
|
| Title |
Test Unit - Rudder Ratio Control System. Used to detect defective units in the Rudder Ratio Control System. |
|
|
|
| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-100
747-100B
747-200B
747-200C
747-200F
747-300
747-COMB
747-SP
|
|
|
|
|
| Main P/N |
TE65B84683 |
|
|
|
| End Item |
-* |
|
|
|
| Aero Info P/N |
52-B47-1335 |
|
|
|
| Title |
Test Tool - Pressure Vessel Cartridge, Type "A" Door. Used to check the pressure vessel electrical firing system for type "A" door - stretched upper deck. |
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|
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| Notes |
|
Applicability
|
Supersedes
|
Replaces
|
|
|
747-300
747-400
|
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| Previous Page |
Next Page |
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21115 Longeway Road, #A, Sonora, CA 95370
Tel: 209-533-2868 / Fax: 209-536-0497 / E-mail: Sales@AeroInfoInc.com
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