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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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| Previous Page |
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| Main P/N |
TE65B88745 |
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| End Item |
-* |
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| Aero Info P/N |
26-B47-1636 |
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| Title |
Test Set - Flowmeter Hyd Sys Leakage. Provides means of monitoring internal leakage rate in each hydraulic system with Arkwin Flowmeter installed on airplane. |
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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
747-300
747-SP
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| Main P/N |
TE65B90115 |
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| End Item |
-* |
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| Aero Info P/N |
71-B47-1269 |
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| Title |
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. |
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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 |
TE65B91156 |
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| End Item |
-* |
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| Aero Info P/N |
71-B47-1270 |
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| Title |
Cable - Oil Tank Probe, Engine. Used to check the engine oil tank probe for capacitance. Applicable to JT9D-3 and -7 engines only. |
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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 |
TE69B48251 |
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| End Item |
-* |
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| Aero Info P/N |
30-MUL-1638 |
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| Title |
Used to verify that lightning protectors will dissipate lightning surge. |
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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 |
TSJ60B00002-2 |
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| End Item |
-* |
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| Aero Info P/N |
34-B47-1273 |
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| Title |
Autothrottle Adapter Attitude Sim. Table. To mount the autothrottle computer for simultaneous tilting operations during functional test. |
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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 |
TSJ60B80099 |
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| End Item |
-* |
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| Aero Info P/N |
77-B47-1323 |
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| Title |
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. |
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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 |
TSJSPZ1-1 |
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| End Item |
-* |
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| Aero Info P/N |
22-B47-1183 |
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| Title |
Test Jig - Pitch and Roll Computer Test. Test box to gain access to test connector terminals of autopilot pitch & roll computers. |
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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 |
TSJSPZ1-2 |
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| End Item |
-* |
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| Aero Info P/N |
22-B47-1184 |
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| Title |
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. |
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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 |
TSJSPZ1-3 |
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| End Item |
-* |
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| Aero Info P/N |
22-B47-1185 |
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| Title |
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. |
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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 |
TSJSPZ1-4 |
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| End Item |
-* |
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| Aero Info P/N |
22-B47-1186 |
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| Title |
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. |
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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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21115 Longeway Road, #A, Sonora, CA 95370
Tel: 209-533-2868 / Fax: 209-536-0497 / E-mail: Sales@AeroInfoInc.com
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