ASAP Part Services, owned and operated by ASAP Semiconductor, has over 6 billion parts inventoried. This includes new, old, used, and obsolete parts, such as 05340001, 101-00900, 101-00901, 101-00930, 1543. As an ISO 9001:2015 certified and FAA AC 00-56B accredited company, we go to great lengths to ensure we are delivering quality parts. We partner exclusively with reliable manufacturers such as Eads North America Inc, Barfield Instrument Corp, Habco Incorporated, Hamilton Sundstrand Corporation, General Dynamics Ots Aerospace Inc. Our team provides superior quality assurance testing for and more. So if you are in need of Test Set Aircraft Engine or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.
Part No Part No
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NSN NSN Parts
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Details Item Name
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QTY QTY
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RFQ RFQ
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05340001 | 4920-01-445-4420 | Special Features: Mfg Noun:Test System Automatic Functional Description: An Automated System Which Monitors/Measures Engine Test Parameters Such As Temperature, Pressure, Engine Speed, Fuel Flow, Angular Positions And Engine Vibration When Installed Into The A/F32t-4 And -9, A/M37t-20, -20A, -21, -21A, Aw35-14, And 100-480 Test Cells/Stand Configurations End Item Identification: All Aircraft Engines | Avl | RFQ |
101-00900 | 4920-01-436-9924 | Functional Description: Used To Measure System Lead Resistance, Insulation And Performing Indicator Run Outs With A Range Up To 1000 Celsius Test Type For Which Designed: Aircraft Turbine Temperature System Inclosure Feature: Single Item W/Housing | Avl | RFQ |
101-00901 | 4920-01-514-9947 | Special Features: (Inavy)Test Set, Aircraft Material End Item Identification: Pt6a25/34B;T-44A Engine Support | Avl | RFQ |
101-00930 | 4920-01-527-1690 | Special Features: Microprocessor Based; Backlit 16 Character Alphanumeric Display With User Prompts; True 4-Wire Resistance Measurements; Powered From C Batteries With Auto-Off Feature; Operating Temperature -10/+50 Degrees C Part Name Assigned By Controlling Agency: Turbine Temperature Test Set Test Type For Which Designed: Temperature Test Set | Avl | RFQ |
1543 | 4920-01-366-1822 | NA | Avl | RFQ |
1543003 | 4920-01-372-9239 | Special Features: Provides A Regulated Vacuum Source To The Bearing Compartment Under Test/Measures The Exact Pressure In Psia & Indicates Rate Of Air Flow Digitally In Pounds Per Hour End Item Identification: F100-Pw-100/200/220/229 Engine (F-15, F-16 Acft) Reference Data And Literature: Serd No. 6793 | Avl | RFQ |
1544001 | 4920-01-536-6079 | Functional Description: Tests Seals In Aircraft Engines End Item Identification: F119-Pw-F100 Engine Reference Data And Literature: Http:/Www.Habco.Biz/Habco Products | Avl | RFQ |
1607 | 4920-01-504-7839 | Special Features: Lightweight Portable System; Rollaway Case W/Wheel And Handle; Sunlight Readable Lcd Display; Built-In Pentium Pc Board W/Hard Drive For Data Storage; Rugged Touchscreen For Operator Input Test Type For Which Designed: Auxiliary Power Unit; Engine Sequencing Unit Inclosure Feature: Single Item W/Carrying Case | Avl | RFQ |
16U23510-5 | 4920-01-607-8242 | End Item Identification: F16a/B/C/D Acft Age Special Features: Case, Hardness And Adapter Reference Data And Literature: T.O. 33D2-19-12-1 | Avl | RFQ |
1C2854 | 4920-00-607-9330 | End Item Identification: Tf39 Acft Eng Age Reference Data And Literature: T.O. 33D4-6-204-1 | Avl | RFQ |
1C2854G6 | 4920-00-861-3204 | End Item Identification: Tf39 Acft Eng Age Reference Data And Literature: T.O. 33D4-6-204-1 | Avl | RFQ |
1C2947 | 4920-00-768-9952 | Special Features: Test Set, Oil Cooler | Avl | RFQ |
1C2947G2 | 4920-00-960-4684 | Special Features: Used With 1C2946g1 Stand End Item Identification: J79-Ge-15/17 Engine Oil Cooler Reference Data And Literature: To 7J1-48-3 | Avl | RFQ |
1C2994G2 | 4920-00-981-7597 | Special Features: To Name: Flightline Troubleshooting Tester; 20In L, 12In W, 16In H, 37Lbs; 24Vdc And 115Vac 400Hz Functional Description: Used To Measure Engine Speed, Variable Nozzle Position, Variable Inlet Guide, Stator Vane Position, And Throttle Position End Item Identification: Acft Maint | Avl | RFQ |
1C2994G2A | 4920-00-981-7597 | Special Features: To Name: Flightline Troubleshooting Tester; 20In L, 12In W, 16In H, 37Lbs; 24Vdc And 115Vac 400Hz Functional Description: Used To Measure Engine Speed, Variable Nozzle Position, Variable Inlet Guide, Stator Vane Position, And Throttle Position End Item Identification: Acft Maint | Avl | RFQ |
1C3576G1 | 4920-00-981-7599 | Special Features: Tank Capacity 3 Gal; Oil Type Mil-L-7808 Functional Description: For Pumping And Measuring Oil Flow To An Isolated Engine Lubrication Area, Has Facilities For Preheating The Oil Supply To Simulate Engine Operating Temperature And A Means To Control The Pressure At Which The System Is Operated End Item Identification: Ge-J-79-15 Engine | Avl | RFQ |
1C3576G4 | 4920-00-928-2861 | Special Features: 21 In's X 28 In's X 30 In's; 125 Lbs Dry, 155 Lbs Wet; 220 Vac, 60 Cps Functional Description: Used To Provide A Means For Pumping Measuring Oil Flow To An Isolated Engine Lubrication Area End Item Identification: Tf-39 Acft Age. | Avl | RFQ |
1C3959G3 | 4920-00-109-8366 | Special Features: Requested Name-Set, Pressure Test-Transfer Gearbox Assembly Functional Description: To Seal Gearbox Ports And Openings Not Sealed By Gearbox Assembly Seals End Item Identification: J79 Turbine Engines | Avl | RFQ |
1C5841G01 | 4920-00-489-6489 | Special Features: To Name: Test Set, Lube Accessory End Item Identification: Tf39 Engine Age Reference Data And Literature: To 2J-Tf39-4 & 33D4-6-364-1 | Avl | RFQ |
1C7050G01 | 4920-01-051-7489 | Special Features: C/O Flow Meter; Gages (3); Control Valves; Blade Fixture; Regulators; Dryer; Filters; Fittings; Pressure Probe; Interconnecting Lines To Form A Functional Test Manifold; Approx. Wt. 70.0 Lbs; 60.000 In. Lg; 40.000 In. Ht Functional Description: Used To Flow Check Tf-39 Engine Stage 1 High Pressure Turbine Blades End Item Identification: Tf-39 Jet Engine | Avl | RFQ |
1C7125G01 | 4920-01-212-0998 | Functional Description: Used To Test Accelerometer Cables, Test The Accelerometers And Provide A Signal To Test The Aircraft Charge Amplifier End Item Identification: C-5B Acft Age. | Avl | RFQ |
21C2757G001 | 4920-00-038-1047 | Special Features: 115V Ac/60Hz/Single Phase/22.5V Battery/Max Energy Measurement Level 30.0 Joules/C/O Tester, Ignition Exciter 1;Cable Assy 3 End Item Identification: J85-5, 5A, 13 Turbojet Engines Reference Data And Literature: T.O.33D4-6-248-1 | Avl | RFQ |
21C3944G01 | 4920-01-176-9099 | Special Features: To Name: Test Set, Pto; C/O Change Type Plug 1, Blank-Off Gasket 1, Adapter 1, Plastic Container 1;Required To Plug Oil Passages And Adapt To The Oil Inlet Tube During Bench Tests On Power Takeoff Subassembly After Buildup End Item Identification: J-85-Ge Series Turbojet Engines Reference Data And Literature: To 2J-J85-54 | Avl | RFQ |
21C3947P01 | 4920-01-207-5256 | Test Type For Which Designed: Functional Inclosure Feature: Single Item W/Carrying Case Phase: Single | Avl | RFQ |
21C4399G01 | 4920-01-424-2843 | Width: 6.000 Inches Nominal Height: 6.000 Inches Nominal Length: 36.000 Inches Nominal | Avl | RFQ |
21C7085G02 | 4920-01-319-3960 | End Item Identification: T701c Engine Test Type For Which Designed: Circuit Continuity Inclosure Feature: Multiple Item W/Carrying Case | Avl | RFQ |
21C912G001 | 4920-00-895-5414 | Special Features: Mfg Name:Tester, Control, Nozzle End Item Identification: Used On J85&5 Turbo Jet Engine Reference Data And Literature: To 33D4-6-170-4 | Avl | RFQ |
21C912G002 | 4920-00-895-5414 | Special Features: Mfg Name:Tester, Control, Nozzle End Item Identification: Used On J85&5 Turbo Jet Engine Reference Data And Literature: To 33D4-6-170-4 | Avl | RFQ |
21C912G003 | 4920-00-895-5414 | Special Features: Mfg Name:Tester, Control, Nozzle End Item Identification: Used On J85&5 Turbo Jet Engine Reference Data And Literature: To 33D4-6-170-4 | Avl | RFQ |
21C912G004 | 4920-00-068-1231 | Special Features: Mfg Name:Tester, Control, Nozzle End Item Identification: J85 Engine | Avl | RFQ |
21C912G004 | 4920-00-068-1231 | Special Features: Mfg Name:Tester, Control, Nozzle End Item Identification: J85 Engine | Avl | RFQ |
21C912G005 | 4920-00-357-5011 | Special Features: Mfg Name:Tester, Nozzle Control;Provides Instrumentation And Simulated Components To Electrically Troubleshoot The Electrical Parts Of The Exhaust Nozzle Control System End Item Identification: J-85-Ge Series Turbojet Engines Reference Data And Literature: 33D4-6-529-4; T.O 2J-J85-94 | Avl | RFQ |
23002970 | 4920-01-097-6079 | Functional Description: Provides A Method Of Functionallytesting The Turbine Clearance Control Valve At Overhaul End Item Identification: Kc-135R Acft Age | Avl | RFQ |
23003276 | 4920-01-124-0709 | Special Features: To Name: Thermocouple Resistance Tester; 18.000 In. Lg, 9.500 In. H;C/O Capacitor 1, Terminal Strip 1, Spacer 8, Separator 1, Transformer 2, Rectifier 4, Relay 1, Resistor 1, Chassis 1, Neon Lamp 1, Lampholder 1, Meter 2, Contact 6, Switch 1, Housing Cover 1, Cabinet 1, Fuse 4, Fuseholder 4 End Item Identification: Allison Engine T56a15, T56a7a, And T56a9a Age. Reference Data And Literature: To 2J-T56-24; Navair 02B-5Da-504 | Avl | RFQ |
281069-1 | 4920-00-778-6091 | Functional Description: Used In Conjunction With The P/N 289526-1 Adapter Kit For Testing Of The Jet Fuel Starter, Also Used As Age In Support Of The A/M-32A-60A Power Cart End Item Identification: F-15 & C-130 Aircraft Reference Data And Literature: T.O.33D2-3-21-1 & 1C-130A-4 | Avl | RFQ |
290122-500 | 4920-00-101-8893 | End Item Identification: C-9A Acft Age | Avl | RFQ |
293030-3 | 4920-01-096-2556 | Special Features: C/Ocontrol Panel; Branched Cable And A Metal Carrying Case Functional Description: Simulates Speed And Temperature Of Engine End Item Identification: A-10A Acft Age | Avl | RFQ |
3654AS100 | 1680-01-477-9550 | NA | Avl | RFQ |
3654AS100 | 4920-01-519-0312 | NA | Avl | RFQ |
3654AS100-3 | 4920-01-525-1002 | End Item Identification: F414 Turbofan Engine Reference Data And Literature: 0050 Test Type For Which Designed: Engine Testing | Avl | RFQ |
3654AS100-4 | 4920-01-519-0312 | NA | Avl | RFQ |
3654AS300-2 | 4920-01-568-2044 | End Item Identification: T56 Turbo Prop Engine Part Name Assigned By Controlling Agency: Turbo Prop Engine Test Set | Avl | RFQ |
3C3991G01 | 4920-01-146-4916 | Special Features: Serd Name: Stator/Compressor Inspection Machine; C/O (1) Console W/Computer And Description Three Display Units, (2) Two Sony Scales (3) Probe 1, (4) Teleprinter1, (5) Applicable Fixtures And Restraining Rings For F101-Ge-102 Engine; Used W/Vertical Turret Lathe To Measure The Radii At 24 Points Of Each Interstage Seal And Liner Stage End Item Identification: F101-Ge-102 Enging Age. | Avl | RFQ |
3C3991G07 | 4920-01-505-0353 | Special Features: C/O Console And 3 Display Units (22.4 In. H, 25.5 In. Deep); Two Sony Scales 60 In. Long; 2 Probes; Teletype Printer (4.875 X 14.500 X 18 In. Deep)And Grinding Assembly Functional Description: Used To Measure The Radii Of The Blade Lands At 24 Points And To Measure And Grind The Interstate Seals Of The Stator Assembly End Item Identification: F110, F118, F101, F110-109, F110-129 Engines | Avl | RFQ |
51-62615 | 4920-00-778-6091 | Functional Description: Used In Conjunction With The P/N 289526-1 Adapter Kit For Testing Of The Jet Fuel Starter, Also Used As Age In Support Of The A/M-32A-60A Power Cart End Item Identification: F-15 & C-130 Aircraft Reference Data And Literature: T.O.33D2-3-21-1 & 1C-130A-4 | Avl | RFQ |
53E36-9B | 4920-00-547-8952 | Special Features: Test Set, Combustion | Avl | RFQ |
6-76204-1 | 4920-00-585-8813 | Functional Description: Used To Trim And Check Installed Engines And Engine Instruments In T-38 And F-5A Acft End Item Identification: J85-Ge-5 Engines Reference Data And Literature: T.O.33D4-6-386-1 | Avl | RFQ |
6799053 | 4920-00-650-4312 | Special Features: Portable Case With Cables Functional Description: Used To Check Out Electrical Components Reference Data And Literature: To 33D4-6-189-4 | Avl | RFQ |
6799327 | 6625-00-015-7462 | Functional Description: Used To Measure The Resistance Of A Thermocouple End Item Identification: T-56-A-7 And T-56-A-9 Engines Reference Data And Literature: To 33D4-6-187-1 | Avl | RFQ |
6799327 | 4920-00-974-8221 | Functional Description: Used To Measure The Resistance Of A Thermocouple End Item Identification: T-56-A-7 And T-56-A-9 Engines Reference Data And Literature: To 33D4-6-187-1 | Avl | RFQ |
6799876 | 4920-00-868-7143 | Special Features: 16.750 W, 18.375 In. Deep, 7.500 In. H; 32 Lbs Functional Description: Used To Check Out Runout Of Any Shaft If Gear Is Attached End Item Identification: C-130H Acft Eng Age | Avl | RFQ |
6889887 | 4920-00-563-9247 | Special Features: Company Item Name-Test Set, Wall Thickness, Ultrasonic, Blade Hollow End Item Identification: Tf-41 Aircraft Engine Reference Data And Literature: T.O. Tf41-4 | Avl | RFQ |
68D170009-1001 | 4920-01-084-1541 | Special Features: Aluminum Alloy Structure, 115 Vac, 400 Hz, Single Phase Functional Description: Checks For Voltage/Continuity, Measures The R/L Amad Speed, And The Gasgenerator Speed End Item Identification: F15 Aircraft Age. | Avl | RFQ |
720663A | 4920-01-083-2639 | End Item Identification: F-16 Acft Age. Reference Data And Literature: T.O. 33D2-3-93-1 Test Type For Which Designed: Functional | Avl | RFQ |
729900 | 4920-01-097-2350 | Special Features: Powered From Acft Or Alternate 28.0 Vdc Power Supply Functional Description: Used To Test The Aircraft Starting/Ignition System End Item Identification: F-16 Acft Age | Avl | RFQ |
767D001-2 | 4920-01-504-7839 | Special Features: Lightweight Portable System; Rollaway Case W/Wheel And Handle; Sunlight Readable Lcd Display; Built-In Pentium Pc Board W/Hard Drive For Data Storage; Rugged Touchscreen For Operator Input Test Type For Which Designed: Auxiliary Power Unit; Engine Sequencing Unit Inclosure Feature: Single Item W/Carrying Case | Avl | RFQ |
768771-1 | 4920-01-087-3464 | Special Features: Consists Of 6 Connectors And Control Box With 4 Switching Controls And Built-In Indication;Control Box Is 13.0 In. Lg, 7.0 In., 2.0 In. H;Cable Length 36.0 In. Approx;115 Vrms, 60 Hz, 10 Amp Power Required; Manufacture Name:Shield Continuity Test Set End Item Identification: F-100Pw-100 Engine Electronic Control Model Jfc90 Reference Data And Literature: To 6J3-4-102-4 | Avl | RFQ |
856A1214P01 | 4920-01-155-4687 | Special Features: Requested Name - Set, Transmitter Indicator, Variable Stator Position/N2 Core Speed Functional Description: This Indicator And Cable Set Is Used With 856A1194 And 856A2001 To Display The Stage 1 Compressor Vane's Aerodynamic Position (Beta Angle) And The Core Engine Speed (N2) Independent Of The Aircraft Wiring End Item Identification: F108-Cf-100 | Avl | RFQ |
856A1214P02 | 4920-01-155-4687 | Special Features: Requested Name - Set, Transmitter Indicator, Variable Stator Position/N2 Core Speed Functional Description: This Indicator And Cable Set Is Used With 856A1194 And 856A2001 To Display The Stage 1 Compressor Vane's Aerodynamic Position (Beta Angle) And The Core Engine Speed (N2) Independent Of The Aircraft Wiring End Item Identification: F108-Cf-100 | Avl | RFQ |
856A1214P03 | 4920-01-155-4687 | Special Features: Requested Name - Set, Transmitter Indicator, Variable Stator Position/N2 Core Speed Functional Description: This Indicator And Cable Set Is Used With 856A1194 And 856A2001 To Display The Stage 1 Compressor Vane's Aerodynamic Position (Beta Angle) And The Core Engine Speed (N2) Independent Of The Aircraft Wiring End Item Identification: F108-Cf-100 | Avl | RFQ |
9184 | 4920-01-355-0052 | End Item Identification: F110-Ge-100 Acft Engine | Avl | RFQ |
93066 | 4920-00-038-1047 | Special Features: 115V Ac/60Hz/Single Phase/22.5V Battery/Max Energy Measurement Level 30.0 Joules/C/O Tester, Ignition Exciter 1;Cable Assy 3 End Item Identification: J85-5, 5A, 13 Turbojet Engines Reference Data And Literature: T.O.33D4-6-248-1 | Avl | RFQ |
93584 | 4920-00-439-5525 | Special Features: Used On F-16 Acft Age. Reference Data And Literature: T.O. 2J-F100-94; 33D4-6-515-1 Test Type For Which Designed: Ignition System | Avl | RFQ |
9458M23 | 4920-01-318-0632 | End Item Identification: F-16 Support Equipment, Aircraft Test Type For Which Designed: Aircraft, Engine | Avl | RFQ |
9458M23G02 | 4920-01-318-0632 | End Item Identification: F-16 Support Equipment, Aircraft Test Type For Which Designed: Aircraft, Engine | Avl | RFQ |
9461M37G03 | 4920-01-579-2979 | Special Features: Requires Pressurized Clean Air Supply Functional Description: Uses Air Pressure To Test Oil Flow Rates Thru Engine End Item Identification: Tf-39 Engine | Avl | RFQ |
A02G1012-8 | 4920-01-367-0857 | NA | Avl | RFQ |
AD44001-1 | 4920-01-449-7334 | NA | Avl | RFQ |
AHT56038 | 4920-01-197-5666 | Special Features: Requested Name-Test Set, Pressure Functional Description: Iused To Measure Various Engine Operating Pressures As A Supplement To Maintenance Analyzer Unit Capability And To Complete Engine Troubleshooting Routines To Identify Specific Malfunctioning Components End Item Identification: F100-Pw-220/229 Aircraft Engine | Avl | RFQ |
AN ASM-651 | 4920-01-084-1541 | Special Features: Aluminum Alloy Structure, 115 Vac, 400 Hz, Single Phase Functional Description: Checks For Voltage/Continuity, Measures The R/L Amad Speed, And The Gasgenerator Speed End Item Identification: F15 Aircraft Age. | Avl | RFQ |
AS-161144 | 4920-01-097-2350 | Special Features: Powered From Acft Or Alternate 28.0 Vdc Power Supply Functional Description: Used To Test The Aircraft Starting/Ignition System End Item Identification: F-16 Acft Age | Avl | RFQ |
BH112JA | 4920-00-776-8756 | Special Features: To Name: Jet Engine Analyzer Functional Description: Used To Test/Analyze Gas Turbine Acft Engines End Item Identification: C123, C5a, B-52, F-16 Acft Age | Avl | RFQ |
BH112JA51T2 | 4920-01-268-2007 | Special Features: Drawing Name=Analyzer, Jetcal Functional Description: Used To Test Gas Turbine Aircraft Engines; Tests: Thermocouple Harness For Error, Thermocouple Continuity, Precision Of The Temperature Indicator, Temperature Circuit Resistance, Temperature Circuit Insulation Resistance, Rpm System Precision, Temperature Indicating System Precision During Trim Procedures Monitors: Temperature And Rpm, Exhaust Gas Pressure, Fuel Flow, Epr, Acceleration & Deceleration, Vane Angle, Engine Torque; Bench Tests: Thermocouples, Thermal Switches; Auto & Manual Record Up To 90 Input Data Records; Portable Trim Module May Be Used To Test Cockpit Indicators Within Cockpit End Item Identification: Jet Engine Maintenance | Avl | RFQ |
BH112JB-77 | 4920-01-230-5964 | Special Features: To Name: Jetcal Analyzer; Integral Dolly With 2 Wheels Functional Description: Used To Control Heater Probe Temperature & Measure Engine Thermocouple Output End Item Identification: F-5 Acft. Engine | Avl | RFQ |
BH112JB-77-4 | 4920-01-250-8034 | End Item Identification: Aircraft Maintenance Equipment Test Type For Which Designed: Analyzer, Trimmer Components Inclosure Feature: Multiple Item W/Carrying Case | Avl | RFQ |
CTE6075 | 4920-01-366-1822 | NA | Avl | RFQ |
EAU-15 E | 4920-01-150-2037 | Special Features: Analyzer Unit, Jet Engine;Communicates With Deec And Edu Via Rs422 Type Interface;Provides Deec And Edu Pwr;Simulates Control System Inputs And Analyzes Deec/Edu Response;Monitors Deec And Edu Input/Output Signals;Reads And Displays Engine Maintenance Information And Operating Constants;Accepts Local Or Remote Operating Commands;Performs Self-Tests And Provides Operational Status On Panel Indicators Functional Description: Test Equipment To Diagnose Problems In F-100 Engines End Item Identification: F100-Pw-100/200 Aircraft Engine | Avl | RFQ |
F311186-3-8-2-1 | 4920-01-237-7725 | Functional Description: Used In Conjunction W/Control Cab And Fuel Trailer, Air Supply, Power Supply, Electric Load Bank And Hydraulic Load Bank, Engine Control And Adaption Kit End Item Identification: Kc-135E Acft Eng. | Avl | RFQ |
GSU-312 E | 4920-01-149-9950 | Special Features: Retrieves Stored Data From In-Flight Control System And Downloads It To Intermediate Level Test Stand For Diagnotic Examination; 17 By 16.5 Inches End Item Identification: F100-Pw Engine Age. Test Type For Which Designed: Diagnostic | Avl | RFQ |
H605 | 4920-01-197-5666 | Special Features: Requested Name-Test Set, Pressure Functional Description: Iused To Measure Various Engine Operating Pressures As A Supplement To Maintenance Analyzer Unit Capability And To Complete Engine Troubleshooting Routines To Identify Specific Malfunctioning Components End Item Identification: F100-Pw-220/229 Aircraft Engine | Avl | RFQ |
PWA50025 | 4920-00-439-5525 | Special Features: Used On F-16 Acft Age. Reference Data And Literature: T.O. 2J-F100-94; 33D4-6-515-1 Test Type For Which Designed: Ignition System | Avl | RFQ |
PWA50081 | 4920-01-020-8041 | Special Features: C/O Of Three Components: An Instrument Case, A Transducer Case, And An Accessory Case Stacked To Form A Single Compacted Wheeled Unit End Item Identification: F100-Pw-100/200 Acft Eng Age Reference Data And Literature: T.O. 2J-F100-94; T.O. 33D4-6-556-4 | Avl | RFQ |
PWA50096 | 4920-01-035-6342 | Functional Description: The Test Equipment Serves As A Pressure Source To Manually Position The Compressor Variable Vanes During Maintenance At Depot, Intermediate, And Organizational Maintenance Levels End Item Identification: F100-Pw-100/-200/-229 Series Aircraft Engines Reference Data And Literature: 33D4-6-617-1 | Avl | RFQ |
PWA50096D | 4920-01-035-6342 | Functional Description: The Test Equipment Serves As A Pressure Source To Manually Position The Compressor Variable Vanes During Maintenance At Depot, Intermediate, And Organizational Maintenance Levels End Item Identification: F100-Pw-100/-200/-229 Series Aircraft Engines Reference Data And Literature: 33D4-6-617-1 | Avl | RFQ |
PWA56015 | 4920-01-149-9950 | Special Features: Retrieves Stored Data From In-Flight Control System And Downloads It To Intermediate Level Test Stand For Diagnotic Examination; 17 By 16.5 Inches End Item Identification: F100-Pw Engine Age. Test Type For Which Designed: Diagnostic | Avl | RFQ |
PWA56016 | 4920-01-150-2037 | Special Features: Analyzer Unit, Jet Engine;Communicates With Deec And Edu Via Rs422 Type Interface;Provides Deec And Edu Pwr;Simulates Control System Inputs And Analyzes Deec/Edu Response;Monitors Deec And Edu Input/Output Signals;Reads And Displays Engine Maintenance Information And Operating Constants;Accepts Local Or Remote Operating Commands;Performs Self-Tests And Provides Operational Status On Panel Indicators Functional Description: Test Equipment To Diagnose Problems In F-100 Engines End Item Identification: F100-Pw-100/200 Aircraft Engine | Avl | RFQ |
PWA56020 | 4920-01-262-5613 | Special Features: C/O Ability To Display Fault Indications; Self Contained Power, For Readout And On-Board Memory Interrogation; Increase Engine Availability; All Weather Use; Provide Trend Data; Self Status; Interrogate Stored Engine Status Data; Store Engine Data Records; Display Recorded Or Realtime Data; Perform Diagnostic Logic; Condition Data For Transfer To External Media; Dim. 17.000 In. Lg; 15.500 In. W; 14.500 In. H End Item Identification: F100-Pw-220/229 Turbofan Engine Reference Data And Literature: Serd No. 5476 | Avl | RFQ |
PWA56038 | 4920-01-197-5666 | Special Features: Requested Name-Test Set, Pressure Functional Description: Iused To Measure Various Engine Operating Pressures As A Supplement To Maintenance Analyzer Unit Capability And To Complete Engine Troubleshooting Routines To Identify Specific Malfunctioning Components End Item Identification: F100-Pw-220/229 Aircraft Engine | Avl | RFQ |
PWA56083 | 4920-01-262-5613 | Special Features: C/O Ability To Display Fault Indications; Self Contained Power, For Readout And On-Board Memory Interrogation; Increase Engine Availability; All Weather Use; Provide Trend Data; Self Status; Interrogate Stored Engine Status Data; Store Engine Data Records; Display Recorded Or Realtime Data; Perform Diagnostic Logic; Condition Data For Transfer To External Media; Dim. 17.000 In. Lg; 15.500 In. W; 14.500 In. H End Item Identification: F100-Pw-220/229 Turbofan Engine Reference Data And Literature: Serd No. 5476 | Avl | RFQ |
PWA56084 | 4920-01-264-2332 | Functional Description: Portable Unit; Provides Capability To Compare Response Of Feedback Circuits To The Stored Expected Values Of The Unit End Item Identification: F100-Pw-220/229 Turbofan Engine Reference Data And Literature: Serd No. 5477 | Avl | RFQ |
PWA56154 | 4920-01-372-9239 | Special Features: Provides A Regulated Vacuum Source To The Bearing Compartment Under Test/Measures The Exact Pressure In Psia & Indicates Rate Of Air Flow Digitally In Pounds Per Hour End Item Identification: F100-Pw-100/200/220/229 Engine (F-15, F-16 Acft) Reference Data And Literature: Serd No. 6793 | Avl | RFQ |
PWA56282 | 4920-01-449-7334 | NA | Avl | RFQ |
TE124738 | 4920-01-552-3263 | Special Features: Test Set End Item Identification: F111 Aircraft Part Name Assigned By Controlling Agency: Adi Field Test Set | Avl | RFQ |
TT1000A | 4920-01-279-0652 | Test Type For Which Designed: Temperature Inclosure Feature: Single Item W/Carrying Case Width: 8.000 Inches Nominal | Avl | RFQ |
TT1000A | 4920-01-546-8771 | Part Name Assigned By Controlling Agency: Tester Temp Turbine | Avl | RFQ |
TT1200 | 4920-01-456-4876 | Special Features: Simulates Thermocouple Outputs And System Lead Resistance From 2 - 25 Ohms Test Type For Which Designed: Temp. And Resistance Measuring And Simulating Inclosure Feature: Single Item W/Carrying Case | Avl | RFQ |
TTU-372 E | 4920-01-035-6342 | Functional Description: The Test Equipment Serves As A Pressure Source To Manually Position The Compressor Variable Vanes During Maintenance At Depot, Intermediate, And Organizational Maintenance Levels End Item Identification: F100-Pw-100/-200/-229 Series Aircraft Engines Reference Data And Literature: 33D4-6-617-1 | Avl | RFQ |
TTU-471 E | 4920-01-197-5666 | Special Features: Requested Name-Test Set, Pressure Functional Description: Iused To Measure Various Engine Operating Pressures As A Supplement To Maintenance Analyzer Unit Capability And To Complete Engine Troubleshooting Routines To Identify Specific Malfunctioning Components End Item Identification: F100-Pw-220/229 Aircraft Engine | Avl | RFQ |
UPUA4-2 | 4920-00-778-6091 | Functional Description: Used In Conjunction With The P/N 289526-1 Adapter Kit For Testing Of The Jet Fuel Starter, Also Used As Age In Support Of The A/M-32A-60A Power Cart End Item Identification: F-15 & C-130 Aircraft Reference Data And Literature: T.O.33D2-3-21-1 & 1C-130A-4 | Avl | RFQ |
WT62889 | 4920-01-010-1977 | Functional Description: Used To Simulate Known Values Of Compressor Inlet Temperature To The Main Fuel Control When Troubleshooting Suspected Engine Malfunctions End Item Identification: J79-11A Engine Reference Data And Literature: T.O. 33D4-6-535-1 | Avl | RFQ |
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