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 10047-10, 101-01401, 11941D100, 11941D100, 164101-100. 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 Aps Systems Inc, Barfield Instrument Corp, Custom Manufacturing Inc, Freund Precision Inc, Hamilton Sundstrand Corporation. Our team provides superior quality assurance testing for and more. So if you are in need of Test Station Fuel Control System 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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10047-10 | 4920-01-201-1593 | Special Features: Jconsists Of Hoses; Cable Assemblies; Weight Tank; Internal Heat Exchanger; Requires Electrical/Pneumatic Input; Operating Tempture 70 To 90 Deg.F, 22 To 33 Deg. C; Voltage 220 To 440 Vac; 3 Phase; 60 Hertz Functional Description: Used To Calibrate Flowmeters At A Calbration Viscosity Equivalent To That Of The Fluid In Which The Flowmeter Will Be Used End Item Identification: F-16A/B Aircraft | Avl | RFQ |
101-01401 | 4920-01-392-1833 | Special Features: The Tester Can Measure Tank Capacitance From 0.1 To 1999.9 Pf And Can Sulate From 10 To 1999.9 Pf, It Can Measure Insulation Breakdown To 2000 Mw And Can Also Measure And Simulate Current To Drive Ma Style Indicators Part Name Assigned By Controlling Agency: Digital Fuel Quanity Tester | Avl | RFQ |
11941D100 | 4920-01-051-9235 | Functional Description: Used To Test Fuel Vent And Presurriaztion Control Valves End Item Identification: F-16 Acft Reference Data And Literature: T.O. 33D2-3-96-1 | Avl | RFQ |
11941D100 | 4920-01-051-9235 | Functional Description: Used To Test Fuel Vent And Presurriaztion Control Valves End Item Identification: F-16 Acft Reference Data And Literature: T.O. 33D2-3-96-1 | Avl | RFQ |
164101-100 | 4920-01-194-3773 | Functional Description: Provides Means Of Adapting And Supplying Test Fluid To Manifold Assy; Collects And Measures Flow From Each Of Six Ejectors And Compares The Flow; Adapts And Supplies Test Fluid To Start Nozzle End Item Identification: F16a/B/C/D Acft Age. | Avl | RFQ |
1C2950G1 | 4920-00-652-8883 | Special Features: 1C/O Control And Instrument Console; Fuel Storage And Pumping Unit; Electrical Control And Power Cabinet; Electronic Recording And Television Assy; 110.0/440.0 Vac, 60.0 Hz, Single/Three Phase; 94.000 In H, 168.000 In W, 96.000 In D; 24, 340.0 Lbs Functional Description: Designed To Test Fuel Accessories Which Have Modifications For Bendix And Hamilton Standard Afterburner Fuel Controls Reference Data And Literature: T.O. 33D4-6-87-11 And -21 | Avl | RFQ |
1C2950G2 | 4920-00-652-8884 | Special Features: To Name: Fuel Accessory Test Stand With Nozzle Area Control Kit Functional Description: Y4-Units Consisting Of Control And Instrument Console, Feuel Storage And Pumping Unit, Electrical Control And Power Cabinet, And Electronic Flowmeter Assy. For Testing General Electric Fuel Accessories And Bendix Nozzle Area Controls Reference Data And Literature: T.O. 33D4-6-87-21 | Avl | RFQ |
1C2950G3 | 4920-00-652-8885 | Special Features: To Name: Fuel Accessory Test Stand With Flow Divider And Selector Valve Kit Functional Description: 4-Units Consisting Of Control And Instrument Console, Fuel Storage And Pumping Unit, Electrical Control And Power Cabinet, And Electronic Recording And Television Assy; Tests Flow Divider And Selector Valves Reference Data And Literature: T.O. 33D4-6-87-31 | Avl | RFQ |
1C3594G01 | 4920-00-016-9558 | NA | Avl | RFQ |
1C3596G01 | 4920-00-016-9545 | Special Features: C/O Pressure Gage 3, Duplex Gage 3, Various Valve, Temp Control, Drip Indicator 2, Hand Pump, Stand Pipe Fixture, 8-Day Clock, Manometer, Hose Reel Air Filter, Purifier, Regulator, Temp Transmitter, Cylinder, Automatic Filler, Fill Unit, Fuel Tank, Pump 2, Heat Exchanger, Muffler, Exhaust Blower, Sink Drain, Motor 3, Transducer 2, Flowmeter 2, Starter 3 End Item Identification: J79 Jet Eng. | Avl | RFQ |
1C5083G01 | 4920-00-043-0663 | Special Features: C/O Main Test Section, And Remote Electrical Cabinet (24 X 20 X 61) Functional Description: Used To Test The Performance And Operating Characteristics Of Turbojet Engine Nozzle Area Controls Reference Data And Literature: T.O. 33D4-6-351-1 | Avl | RFQ |
1C5087G01 | 4920-00-109-8359 | Special Features: Main Test Stand 84 In. D, 100 In. W. 90 In. H, Section Ii 108 In. D, 100 In. W, 90 In. H, Electrical Control Cabinet 36 In. D, 22 In. W, 63 In. H; 440 Volts, 3 Phase, 60 Hz, 130 Kva Functional Description: Used To Provide A Means Of Testing The Performance And Operating Charactertics Of The Presurrizing Valve For The Ge J79 Turbo Jet Engine Reference Data And Literature: T.O.33D4-6-381-1 | Avl | RFQ |
1C5158G01 | 4920-00-483-2693 | End Item Identification: C-5 Aircraft Part Name Assigned By Controlling Agency: Stand, Test, Fuel Accessories | Avl | RFQ |
1C5852G01 | 4920-00-420-2508 | Special Features: Reservoir Capacity: 25 Gals. Instrumentation: Pressure Gage: Range: 0-100Psig 0-400Psig, 0-1500Psig; Differential Pressure Gage: Range: 0-60Psid; Specific Gravity Ind Range: 0.8/0.9; Temperature Ind Range: 30-180 Deg F; Requires Electrical 220/440 Volt, 3 Phase, 60 Hz, 24/12 Amp; Water: 6 Gpm, 70 Deg F, 40 Psig Functional Description: Supplies Preserving Fluid To Various Fuel Accessories, Such As Main Fuel Pump, Fuel Control, Pressuring/Drain Valve, Nozzle Cluster C.I.T. Sensor, Various Variable Vane Actuator/Fuel Heater. It Incorporates A Recirculating Hydraulic System To Supply Preserving Fluid To A Unit, Connected To The Stand, At Specified Pressure/Temperatures Reference Data And Literature: T.O.33D4-6-365-1 | Avl | RFQ |
1C847 | 4920-00-334-4698 | Special Features: To Name: Fuel Pump Stand;Floor Mounted With Work Surface Reference Data And Literature: To 33D4-6-65-4 | Avl | RFQ |
1C848 | 4920-00-337-9843 | End Item Identification: B-1B Aircraft Reference Data And Literature: To 33D4-6-65-14 Part Name Assigned By Controlling Agency: Test Stand, Fuel Acc | Avl | RFQ |
1C848G2 | 4920-00-337-9843 | End Item Identification: B-1B Aircraft Reference Data And Literature: To 33D4-6-65-14 Part Name Assigned By Controlling Agency: Test Stand, Fuel Acc | Avl | RFQ |
1F60957 | 4920-01-097-2349 | Special Features: C/O Reservoir, Pump, Calibrated Flow Tanks, Flow Meters, Gauges, Fuel Port Caps And Adapters, Test Article Support Fixture Functional Description: Used On The F-16A/B Fuel System End Item Identification: F-16A/B Acft Age | Avl | RFQ |
1G852-101 | 4920-01-542-8823 | NA | Avl | RFQ |
21C3805G01 | 4920-01-061-8507 | Special Features: 7Fuel Delivery Section; Component Including Drive; Fuel Receiving; Remotely Located On Explosion Proof Electrical Cabinet; 220.0/400.0 Vac, 50.0 Hz, 3-Phase; Contains Built-In Fire Suppression System; 120.000 In L, 96.000 In W, 84.000 In H; 10000.0 Lbs Functional Description: Designed To Functionally Test Ab Control And Pump To Assure Their Proper Operation After Overhaul End Item Identification: J85-Ge-13, -21, 21A Acft Engine | Avl | RFQ |
21C3805G02 | 4920-01-064-1783 | Special Features: 220.0 Vac, 60.0 Hz, 3-Phase; 10000.0 Lbs; Contains A Built In Fire Suppression System For Sink And Closed Area; 10.0 Ft W, 7.0 Ft H, 8.0 Ft D Functional Description: Designed To Functionally Test Thej85-13 And J85-21 Ab Fuel Control And Pump Simulating Actual Operating Conditions After Overhaul End Item Identification: J85-13 And J85-21 Acft Ab Control System | Avl | RFQ |
21C3838G06 | 4920-00-026-4338 | Functional Description: Plotting System Reference Data And Literature: T.O. 33D4-6-448-14 Supplementary Features: Company Item Name-Jet Engine And Fuel Control Analyzer | Avl | RFQ |
21C3838G06 | 4920-00-026-4338 | Functional Description: Plotting System Reference Data And Literature: T.O. 33D4-6-448-14 Supplementary Features: Company Item Name-Jet Engine And Fuel Control Analyzer | Avl | RFQ |
21C3838G07 | 4920-01-078-3258 | Special Features: 24 X 24 X 18 Functional Description: Used In Conjunction With J85-Ge-13/-21/-21A Engine Supplementary Features: Performance Plotting System | Avl | RFQ |
21C3900G01 | 4920-01-024-5670 | Special Features: 220Vac, 50Hz End Item Identification: J-85-Ge Series Turbojet Engines Reference Data And Literature: To 2J-J85-54 | Avl | RFQ |
21C3900G02 | 4920-01-024-6749 | Special Features: 10 Ft Lg. 6 Ft W. 7 Ft H. Elec 440 Vac, 60 Hz, 3 Phase, 12 Kva, Water 8Gpm, 40 To 70 Psig, 70 Deg. F, Max Compressor Air 10 Scfm, 90 To 140 Psig End Item Identification: J85 Acft Engine Fuel Systems | Avl | RFQ |
21C3954G02 | 4920-01-308-0442 | Special Features: C/O Test Set; Interface Test Adapter; Cables; Both Items In Their Own Containers Functional Description: Used To Test The J-85 Fuel System | Avl | RFQ |
21C3954G05 | 4920-01-333-9172 | Functional Description: Used To Test The The Fuel System On The J85-8 Stage And J85-21 Engine Reference Data And Literature: Serd No. 3954.4 | Avl | RFQ |
21C3954P01 | 4920-01-209-5044 | Special Features: C/O 2 Weatherproof Carrying Cases; Instrumentation Case Contains Press System For Estab False P3 Press; Press Transducer; Instruments; Signal Cond Circuitry; Press System; 2Nd Case C/O Turbine Flow Sensor; Eng Main Fuel Pump Adapters; Hoses/Fittings; Eng Tach Alternator Adapter Functional Description: Used To Perf Eng Faults At Cell Tst End Item Identification: J85-Ge-5/13/17/17A/-21 Turbojet Engine | Avl | RFQ |
21C6522G02 | 4920-01-080-5283 | Functional Description: Used To Support Main Fuel Controlw/Cavity In Down Position To Provide Fuel At Inlet, And To Direct A Jet Of Fuel Into Cavity W/Oscillating Motion End Item Identification: J85-Ge-21 Engine Age. Supplementary Features: Company Item Name-Test Stand, Power Fuel Control | Avl | RFQ |
21C9503G01 | 4920-01-020-4857 | Special Features: Electrical Power: 380Vac, 50Hz, 3Ph End Item Identification: J85-Ge-21 Turbojet Engine Main Fuel Control And Pump Reference Data And Literature: To 6J3-4-96-4 | Avl | RFQ |
21C9505G02 | 4920-01-068-0298 | Special Features: C/O 2 Sections;Removable Panels And Folding Door For Repair Access; Angle Iron And Sheet Metal Construction, One Air Purge Box House Non Explosive Type Electrical Equip. And Maintains An Internal Pressure Of 0.1 In Of Water Above Atmospheric; Remote Electrical Cabinet Houses Control Equip And Must Be Located In A Non-Hazardous Area, Cbinet Size Is 42.0 In Lg, 8.0 In W, 59.0 In H Functional Description: Used To Provide The Capability Of Testing/Monitoring The Operational Parameters As Established For Over Speed Control Assembly And The Isochronous Governor Assembly End Item Identification: J85-Ge-13/17/21/21A Turbojet Engine | Avl | RFQ |
2755000 | 4920-01-218-4171 | Special Features: 480.0 Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output/Operating Characteristics: Fuel: 0-1400 Psig, 0-36 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air: 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm, High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut Gn2: 50 Psia; Water: Hot Water, 40 Psig, 2 Gpm, 140 Deg F; Cold Water: 40 Psig, 10 Gpm, 55 Deg F; Computer Controlled; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H; Fixed Mount Functional Description: Used For Fault Isolation, And Final Service Acceptance On Assemblies/Sub-Assemblies Of The Augmentor Pump Controller End Item Identification: F100-Pw-220 Acft Engine | Avl | RFQ |
2755010 | 4920-01-217-0109 | Special Features: Input Power: 480.0Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output Characteristics: Fuel: 0-1400 Psig, 0-218 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm; High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut: Gn2 50 Psia; Facility Provides Hot Water 40 Psig 2 Gpm; 140 Deg F; Cold Water 40 Psig, 10 Gpm, 55 Deg F; Fixed Mount; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H Functional Description: Used To Supply Fuel And Facility Supplied Air And Appropriate Instrumentation For Performing Depot Level Tests On Assemblies/Sub-Assemblies End Item Identification: F100-Pw-220 Engine Augmentor Fuelcontrol | Avl | RFQ |
2756000 | 4920-01-218-4171 | Special Features: 480.0 Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output/Operating Characteristics: Fuel: 0-1400 Psig, 0-36 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air: 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm, High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut Gn2: 50 Psia; Water: Hot Water, 40 Psig, 2 Gpm, 140 Deg F; Cold Water: 40 Psig, 10 Gpm, 55 Deg F; Computer Controlled; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H; Fixed Mount Functional Description: Used For Fault Isolation, And Final Service Acceptance On Assemblies/Sub-Assemblies Of The Augmentor Pump Controller End Item Identification: F100-Pw-220 Acft Engine | Avl | RFQ |
2756010 | 4920-01-217-0109 | Special Features: Input Power: 480.0Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output Characteristics: Fuel: 0-1400 Psig, 0-218 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm; High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut: Gn2 50 Psia; Facility Provides Hot Water 40 Psig 2 Gpm; 140 Deg F; Cold Water 40 Psig, 10 Gpm, 55 Deg F; Fixed Mount; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H Functional Description: Used To Supply Fuel And Facility Supplied Air And Appropriate Instrumentation For Performing Depot Level Tests On Assemblies/Sub-Assemblies End Item Identification: F100-Pw-220 Engine Augmentor Fuelcontrol | Avl | RFQ |
2756020 | 4920-01-216-0455 | NA | Avl | RFQ |
311A | 4920-00-535-1065 | Functional Description: Self-Contained Precision Instrument Used For Calibrating Direct Reading And Turbine Type Flowmeters By The Direct Weight Method, Has High And Low Flow System, Which Are Independent Of Each Other;126.000 In. Lg, 104.000 In. W, 60.000 In. H Reference Data And Literature: T.O. 33A6-3-30-1, T.0. 33A6-3-30-4 Supplementary Features: Company Item Name-Tester, Calibration, Flowmeter | Avl | RFQ |
311AHT | 4920-00-535-1065 | Functional Description: Self-Contained Precision Instrument Used For Calibrating Direct Reading And Turbine Type Flowmeters By The Direct Weight Method, Has High And Low Flow System, Which Are Independent Of Each Other;126.000 In. Lg, 104.000 In. W, 60.000 In. H Reference Data And Literature: T.O. 33A6-3-30-1, T.0. 33A6-3-30-4 Supplementary Features: Company Item Name-Tester, Calibration, Flowmeter | Avl | RFQ |
3C3973G01 | 4920-01-144-8407 | Functional Description: Used For Calibration/Testing Of Augmenter Fuel Controls, Including Fixturing, Electric Cables, Hoses/Fittings Required To Connect The Test Part To The Test Stand Reference Data And Literature: Serd Nos. 0517, 0517A, 5063 And 1738 Fsc Application Data: F101-Ge-102, F110-Ge-100 And F110-Ge-129 Engine, B-1B Acft Age. | Avl | RFQ |
3C3973G02 | 4920-01-144-8407 | Functional Description: Used For Calibration/Testing Of Augmenter Fuel Controls, Including Fixturing, Electric Cables, Hoses/Fittings Required To Connect The Test Part To The Test Stand Reference Data And Literature: Serd Nos. 0517, 0517A, 5063 And 1738 Fsc Application Data: F101-Ge-102, F110-Ge-100 And F110-Ge-129 Engine, B-1B Acft Age. | Avl | RFQ |
3C3973G03 | 4920-01-144-8407 | Functional Description: Used For Calibration/Testing Of Augmenter Fuel Controls, Including Fixturing, Electric Cables, Hoses/Fittings Required To Connect The Test Part To The Test Stand Reference Data And Literature: Serd Nos. 0517, 0517A, 5063 And 1738 Fsc Application Data: F101-Ge-102, F110-Ge-100 And F110-Ge-129 Engine, B-1B Acft Age. | Avl | RFQ |
6798297 | 4920-00-081-6725 | NA | Avl | RFQ |
6798299 | 4920-00-876-2437 | NA | Avl | RFQ |
6872122 | 4920-00-443-2204 | NA | Avl | RFQ |
6872182 | 4920-00-480-6393 | Supplementary Features: Company Item Name-Fuel Nozzle Test Stand | Avl | RFQ |
6872259 | 4920-00-498-1027 | Special Features: 108.000 In W, 118.000 In D, 78.000 In H; 230.0/460.0 Vac, 60.0 Hz, 3 Phase Functional Description: Designed To Test And Calibrate Various Fuel Accessories For The Allison Tf41 Series Engines End Item Identification: Tf41 Acft Engines | Avl | RFQ |
6872993 | 4920-00-084-3094 | Special Features: Test Stand Assy Consists Of (All Measurements Are In Inches) Console-78X146x143;Variable Speed Drive Control-96X94.75X24;Electrical Enclosure 72X34x9.5; Vacuum Package-54X68x34;Isolation Transformer-40.5X36x21.25; Isolation Transformer 26.5X23.5X15.5;Contactor-32X17.25X10; Contactor-9X6.75X4.25; Power Requirements-230/460 Volts, 3 Phase, 60 Hz; Water-53.5 Gpm At 30-40 Psig And 70Degrees F Max; Shop Air(Instrument Quality) 20 Scfm Free Air At 90-110 Psig;Compressed Air 80 Sfcm Air At 500 Psig Functional Description: The Test Stand Assy Is A Self-Contained Unit Which Incorporates Its Own Hydraulic System To Supply Test Fluid To The Unit Under Test At Specified Pressures And Flows End Item Identification: Allison Tf41 Series Engines | Avl | RFQ |
8230800-0501 | 4920-01-390-1852 | Special Features: The Fuel Wetted Section Has To Belocated In A Room For Class 1, Division 1, Group D, Hazardous Environment Functional Description: Low Pressure Module Pump Consistsof Fuel Wetted Section, Utilities Drive, Process Controller; 480 Vac +/- 10%60 Hz +/-2%, 3 Phase Reference Data And Literature: Serd 1002 | Avl | RFQ |
8543-01 | 4920-01-460-0332 | Functional Description: Test Stand Can Operate Switch Assys Up To 12, 000 Rpm And Indicate Switch Actuation Within Specified Ranges. If Switch Actuates Outside Specified Range, A Fault Will Be Indicated End Item Identification: F-15 Aircraft; Tests 2 Speed Switch Assy P/N 367119-2; Governor Assy P/N 367036-3 & P/N 367036-5 Part Name Assigned By Controlling Agency: F-15 Speed Calibration Test Standrdalgcontract F41608-98-C-0419 | Avl | RFQ |
AC2K | 4920-01-392-1833 | Special Features: The Tester Can Measure Tank Capacitance From 0.1 To 1999.9 Pf And Can Sulate From 10 To 1999.9 Pf, It Can Measure Insulation Breakdown To 2000 Mw And Can Also Measure And Simulate Current To Drive Ma Style Indicators Part Name Assigned By Controlling Agency: Digital Fuel Quanity Tester | Avl | RFQ |
AD 50199M1 | 4920-01-040-2903 | Special Features: F-16 Acft Peculiar Functional Description: 60Hz, Provide Controlled System For Post-Overhaul Testing Of The Back Up Fuel Control And Vgtv Valve; Designed For Use In Hazardous Test Areas End Item Identification: F100-Pw-100 Turbo Engines | Avl | RFQ |
AT1405 | 4920-00-511-3777 | NA | Avl | RFQ |
AT1405 | 4920-00-511-3777 | NA | Avl | RFQ |
BEI3668 | 4920-01-024-5670 | Special Features: 220Vac, 50Hz End Item Identification: J-85-Ge Series Turbojet Engines Reference Data And Literature: To 2J-J85-54 | Avl | RFQ |
BEI3668B | 4920-01-024-6749 | Special Features: 10 Ft Lg. 6 Ft W. 7 Ft H. Elec 440 Vac, 60 Hz, 3 Phase, 12 Kva, Water 8Gpm, 40 To 70 Psig, 70 Deg. F, Max Compressor Air 10 Scfm, 90 To 140 Psig End Item Identification: J85 Acft Engine Fuel Systems | Avl | RFQ |
CHA415-73 | 4920-00-337-9843 | End Item Identification: B-1B Aircraft Reference Data And Literature: To 33D4-6-65-14 Part Name Assigned By Controlling Agency: Test Stand, Fuel Acc | Avl | RFQ |
D20297 | 4920-00-337-9843 | End Item Identification: B-1B Aircraft Reference Data And Literature: To 33D4-6-65-14 Part Name Assigned By Controlling Agency: Test Stand, Fuel Acc | Avl | RFQ |
D21413 | 4920-00-337-9843 | End Item Identification: B-1B Aircraft Reference Data And Literature: To 33D4-6-65-14 Part Name Assigned By Controlling Agency: Test Stand, Fuel Acc | Avl | RFQ |
D22051 | 4920-00-652-8883 | Special Features: 1C/O Control And Instrument Console; Fuel Storage And Pumping Unit; Electrical Control And Power Cabinet; Electronic Recording And Television Assy; 110.0/440.0 Vac, 60.0 Hz, Single/Three Phase; 94.000 In H, 168.000 In W, 96.000 In D; 24, 340.0 Lbs Functional Description: Designed To Test Fuel Accessories Which Have Modifications For Bendix And Hamilton Standard Afterburner Fuel Controls Reference Data And Literature: T.O. 33D4-6-87-11 And -21 | Avl | RFQ |
D22056 | 4920-00-652-8884 | Special Features: To Name: Fuel Accessory Test Stand With Nozzle Area Control Kit Functional Description: Y4-Units Consisting Of Control And Instrument Console, Feuel Storage And Pumping Unit, Electrical Control And Power Cabinet, And Electronic Flowmeter Assy. For Testing General Electric Fuel Accessories And Bendix Nozzle Area Controls Reference Data And Literature: T.O. 33D4-6-87-21 | Avl | RFQ |
D22061 | 4920-00-652-8885 | Special Features: To Name: Fuel Accessory Test Stand With Flow Divider And Selector Valve Kit Functional Description: 4-Units Consisting Of Control And Instrument Console, Fuel Storage And Pumping Unit, Electrical Control And Power Cabinet, And Electronic Recording And Television Assy; Tests Flow Divider And Selector Valves Reference Data And Literature: T.O. 33D4-6-87-31 | Avl | RFQ |
E13714 | 4920-00-997-1955 | End Item Identification: Used For Check Out And Adjustmentin Support Of The Ov-10A Acft | Avl | RFQ |
F10018 | 4920-00-605-9446 | Functional Description: Provides Oil At The Temperatures, Pressure And Flow Required To Test Both Adg/Idg And Fuel Thermostatic Valves; Accomplish Pressure Drop Tests End Item Identification: Fuel/Oil Heat Exchanger Reference Data And Literature: To 7J1-79-3 | Avl | RFQ |
FR216D0000-3 | 4920-01-176-2120 | Special Features: C/O A Tow Bar, Battery Box Stowage, Fuel And Air Hose And Storage, Certfier Assembly, Four Wheeled Cart; 115 Vac, 60 Hz, 10 Functional Description: Used In Operational Testing Of External Fuel Tank (Off Of The Acft) End Item Identification: F-16 And F-15 Acft Age. | Avl | RFQ |
FR216D0000-5 | 4920-01-378-0137 | Special Features: C/O A Mobile Service/Storage Cart Adapter Kits For Various Acft; Certifier Assembly; Battery Box; Gravity Fill Port Defueler Assy; 9 Grounding Cable Assy's; 2 Fuel Hose Assys; 2 Air Hose Assys; Browser Hose; Single Point Adapter And 3 Universal Adapter Plates Functional Description: Used To Connect Incoming Fuel From An External Source And Route Fuel To An External Tank End Item Identification: Multi Acft Useage | Avl | RFQ |
GH15090 | 4920-00-545-1779 | End Item Identification: J-57 Engine Fuel Pressurizing And Dump Valve Reference Data And Literature: To 6J15-14-1-103 Part Name Assigned By Controlling Agency: Test Stand | Avl | RFQ |
GH7811 | 4920-00-340-2633 | Reference Data And Literature: To 33D4-6-196-1 | Avl | RFQ |
GR-11941D100 | 4920-01-051-9235 | Functional Description: Used To Test Fuel Vent And Presurriaztion Control Valves End Item Identification: F-16 Acft Reference Data And Literature: T.O. 33D2-3-96-1 | Avl | RFQ |
GR-11941D100 | 4920-01-051-9235 | Functional Description: Used To Test Fuel Vent And Presurriaztion Control Valves End Item Identification: F-16 Acft Reference Data And Literature: T.O. 33D2-3-96-1 | Avl | RFQ |
GS7800-150 | 4920-00-026-4338 | Functional Description: Plotting System Reference Data And Literature: T.O. 33D4-6-448-14 Supplementary Features: Company Item Name-Jet Engine And Fuel Control Analyzer | Avl | RFQ |
GS7800-150 | 4920-00-026-4338 | Functional Description: Plotting System Reference Data And Literature: T.O. 33D4-6-448-14 Supplementary Features: Company Item Name-Jet Engine And Fuel Control Analyzer | Avl | RFQ |
GS7800-162 | 4920-01-101-4950 | End Item Identification: J-85 Engine | Avl | RFQ |
HA5000 | 4920-00-041-1142 | Special Features: C/O Cabinet; Instrument Panel; V-S Drive Control Cabinet; Pressure Port; Drain Sump; Pump Mounting Pad; Speed Control; Suction Port; Sight Gauge; Steel Panel Functional Description: Used To Test The Performance And Operating Characteristics Of New And/Or Newly Overhauled Or Faulty Aircraft Fuel Pumps Reference Data And Literature: T.O. 33A6-7-10-1 | Avl | RFQ |
KT-3447 | 4920-01-149-0297 | Functional Description: Used To Accomplish Leakage And Proof Pressure Tests On F-16 Fuel/Oil Heat Exchanger End Item Identification: F-16A/B Acft Fuel/Oil Heat Exchanger Reference Data And Literature: To 7J1-79-3 | Avl | RFQ |
L9604-101-001-1 | 4920-01-390-7247 | Special Features: Consists Of A Test Console Approx108.000 In. W X 72.000 In. D X 78.000 In. H; Operator Console Approx 24.000 In. W X 24.000 D X 65.000 H; Remote Pwr Supply Skid, Approx 120.000 W X 72.000 In. D X 84.000 In. H; Requires 460 Vac, 200 Amps, 3 Phase 60 Hz (Non-Hazard Area); 120 Vac, 15 Amps, 1 Phase, 60 Hz; Pneumatic Requirements, Purge Air, 3000 Scfm Maximum At Atmospheric Pressure; Exhaust Air, 800 Scmf Maximum , Less Than 0.001 In. Water Restriction; Shop Air, 60 To 120 Psig, 20 Scfm Maximumm Consumption, Dew Point Less Than 40 Deg. F; Cooling Water, 85 Gpm Maximum At 45 Deg. F Functional Description: The Aircraft Fuel Componets Test System (Afcts)(High Flow) Will Performance Test And Evaluate Acft. Fuel Componets Characterized By High Flows (Up To 750 Gpm) The Afcts Is Primarily To Suport Test And Evaluation Of In-Tank Refueling And Fuel Transfer Componets Which Require Open Loop Operation End Item Identification: B1b | Avl | RFQ |
PD-T-84-005A | 4920-01-201-1593 | Special Features: Jconsists Of Hoses; Cable Assemblies; Weight Tank; Internal Heat Exchanger; Requires Electrical/Pneumatic Input; Operating Tempture 70 To 90 Deg.F, 22 To 33 Deg. C; Voltage 220 To 440 Vac; 3 Phase; 60 Hertz Functional Description: Used To Calibrate Flowmeters At A Calbration Viscosity Equivalent To That Of The Fluid In Which The Flowmeter Will Be Used End Item Identification: F-16A/B Aircraft | Avl | RFQ |
PD94-TILDD-3 | 4920-01-390-7247 | Special Features: Consists Of A Test Console Approx108.000 In. W X 72.000 In. D X 78.000 In. H; Operator Console Approx 24.000 In. W X 24.000 D X 65.000 H; Remote Pwr Supply Skid, Approx 120.000 W X 72.000 In. D X 84.000 In. H; Requires 460 Vac, 200 Amps, 3 Phase 60 Hz (Non-Hazard Area); 120 Vac, 15 Amps, 1 Phase, 60 Hz; Pneumatic Requirements, Purge Air, 3000 Scfm Maximum At Atmospheric Pressure; Exhaust Air, 800 Scmf Maximum , Less Than 0.001 In. Water Restriction; Shop Air, 60 To 120 Psig, 20 Scfm Maximumm Consumption, Dew Point Less Than 40 Deg. F; Cooling Water, 85 Gpm Maximum At 45 Deg. F Functional Description: The Aircraft Fuel Componets Test System (Afcts)(High Flow) Will Performance Test And Evaluate Acft. Fuel Componets Characterized By High Flows (Up To 750 Gpm) The Afcts Is Primarily To Suport Test And Evaluation Of In-Tank Refueling And Fuel Transfer Componets Which Require Open Loop Operation End Item Identification: B1b | Avl | RFQ |
PMU-64 E | 4920-01-390-1852 | Special Features: The Fuel Wetted Section Has To Belocated In A Room For Class 1, Division 1, Group D, Hazardous Environment Functional Description: Low Pressure Module Pump Consistsof Fuel Wetted Section, Utilities Drive, Process Controller; 480 Vac +/- 10%60 Hz +/-2%, 3 Phase Reference Data And Literature: Serd 1002 | Avl | RFQ |
PSD90S-F16 | 4920-01-590-6791 | Special Features: Used To Calibrate And Trouble Shoot The Fuel Quantity Measuring System And The Level Sensing System. Length: 21.5 In; Width: 14.7 In; Height: 9.0 In; Weight: 26.5 Lbs. Special Features:Interface Unit Has Low Level Sensor Menaurement Board That Allows Testing Ofthe Low-Level Sensors To Verify If Thesensors Are Either Wet, Dry, Open Or Shorted End Item Identification: F16a/B/C/D | Avl | RFQ |
PTS9100 | 4920-00-334-4698 | Special Features: To Name: Fuel Pump Stand;Floor Mounted With Work Surface Reference Data And Literature: To 33D4-6-65-4 | Avl | RFQ |
PWA10602 | 4920-00-625-6851 | Functional Description: Used For Static Testing Fuel System Components End Item Identification: Pratt Whitney Engine Reference Data And Literature: T.O. 33D4-6-156-1/11 | Avl | RFQ |
PWA15090 | 4920-00-545-1779 | End Item Identification: J-57 Engine Fuel Pressurizing And Dump Valve Reference Data And Literature: To 6J15-14-1-103 Part Name Assigned By Controlling Agency: Test Stand | Avl | RFQ |
PWA50199 | 4920-01-040-2903 | Special Features: F-16 Acft Peculiar Functional Description: 60Hz, Provide Controlled System For Post-Overhaul Testing Of The Back Up Fuel Control And Vgtv Valve; Designed For Use In Hazardous Test Areas End Item Identification: F100-Pw-100 Turbo Engines | Avl | RFQ |
PWA50199-1 | 4920-01-040-2903 | Special Features: F-16 Acft Peculiar Functional Description: 60Hz, Provide Controlled System For Post-Overhaul Testing Of The Back Up Fuel Control And Vgtv Valve; Designed For Use In Hazardous Test Areas End Item Identification: F100-Pw-100 Turbo Engines | Avl | RFQ |
PWA53111-1 | 4920-01-218-4171 | Special Features: 480.0 Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output/Operating Characteristics: Fuel: 0-1400 Psig, 0-36 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air: 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm, High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut Gn2: 50 Psia; Water: Hot Water, 40 Psig, 2 Gpm, 140 Deg F; Cold Water: 40 Psig, 10 Gpm, 55 Deg F; Computer Controlled; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H; Fixed Mount Functional Description: Used For Fault Isolation, And Final Service Acceptance On Assemblies/Sub-Assemblies Of The Augmentor Pump Controller End Item Identification: F100-Pw-220 Acft Engine | Avl | RFQ |
PWA53111-3 | 4920-01-218-4171 | Special Features: 480.0 Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output/Operating Characteristics: Fuel: 0-1400 Psig, 0-36 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air: 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm, High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut Gn2: 50 Psia; Water: Hot Water, 40 Psig, 2 Gpm, 140 Deg F; Cold Water: 40 Psig, 10 Gpm, 55 Deg F; Computer Controlled; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H; Fixed Mount Functional Description: Used For Fault Isolation, And Final Service Acceptance On Assemblies/Sub-Assemblies Of The Augmentor Pump Controller End Item Identification: F100-Pw-220 Acft Engine | Avl | RFQ |
PWA53112-3 | 4920-01-217-0109 | Special Features: Input Power: 480.0Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output Characteristics: Fuel: 0-1400 Psig, 0-218 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm; High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut: Gn2 50 Psia; Facility Provides Hot Water 40 Psig 2 Gpm; 140 Deg F; Cold Water 40 Psig, 10 Gpm, 55 Deg F; Fixed Mount; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H Functional Description: Used To Supply Fuel And Facility Supplied Air And Appropriate Instrumentation For Performing Depot Level Tests On Assemblies/Sub-Assemblies End Item Identification: F100-Pw-220 Engine Augmentor Fuelcontrol | Avl | RFQ |
PWA53114-1 | 4920-01-216-0455 | NA | Avl | RFQ |
PWA56214-3 | 4920-01-301-8266 | Special Features: C/O Fuel Flow-Pump; Fuel Flow-Bearing; Air Flow; Fuel Outlet Pressure Air Inlet Pressure; Air Inlet Temperature T/C; Fuel Inlet Temperature T/C; Thermocouple Indicator; Fuel Leakage; Fuel Inlet Pressure; Shaft Speed; Air Outlet Pressure; Fuel Wetted Turbine Air Module; Power Cabinet; Console; Sink; Cables; Dedicated Remote Pump Module;Power: 277/480 Volt, 3 Phase, 60 Hz Or 380 Volt, 3 Phase, 50 Hz; Control Circuit; 120 Volts, Single Phase, 60 Hz; Or 220 Volts, Single Phase, 50 Hz; Compressed Air; Low Presseur; 100 Scfm, 90 Psig; 30 Degree F Dew Point; Facility Turbine Air: 120 Ppm, 400 Psig, 600 F; Chilled Water: 150 Gpm, 75 Psig, 45Degree F Functional Description: Used For Testing Of Model Tpc-23/24 Pumps Used On The F100-Pw-220/229 Engine End Item Identification: F100-Pw-100/200/220/220E/229 Aircraft Engine | Avl | RFQ |
PWA7811 | 4920-00-340-2633 | Reference Data And Literature: To 33D4-6-196-1 | Avl | RFQ |
PWA7811C | 4920-00-340-2633 | Reference Data And Literature: To 33D4-6-196-1 | Avl | RFQ |
RA1FT | 4920-00-944-0123 | Special Features: 4Manual Method Of Testing; Hoses Method Of Connect; Two Main Units; 1 Main Structure Which Houses Gauges, Instruments, Controls, Valves, Motors, Andpumps; 2 Open Structure Which C/O Reservoir, Filter, And 20 Hp Variable Speed Motor And Main Pump Functional Description: The Fuel Pump Test Stand Is To Provide For Accurate And Rapid Testing Of Fuel Pumps & Components Used On Modern Aircraft In Accordance With The Manufacturer's Test Specifications Reference Data And Literature: T.O. 33D2-3-48-1 | Avl | RFQ |
SOW-T-84-005 | 4920-01-201-1593 | Special Features: Jconsists Of Hoses; Cable Assemblies; Weight Tank; Internal Heat Exchanger; Requires Electrical/Pneumatic Input; Operating Tempture 70 To 90 Deg.F, 22 To 33 Deg. C; Voltage 220 To 440 Vac; 3 Phase; 60 Hertz Functional Description: Used To Calibrate Flowmeters At A Calbration Viscosity Equivalent To That Of The Fluid In Which The Flowmeter Will Be Used End Item Identification: F-16A/B Aircraft | Avl | RFQ |
T1070-200 | 4920-00-944-0123 | Special Features: 4Manual Method Of Testing; Hoses Method Of Connect; Two Main Units; 1 Main Structure Which Houses Gauges, Instruments, Controls, Valves, Motors, Andpumps; 2 Open Structure Which C/O Reservoir, Filter, And 20 Hp Variable Speed Motor And Main Pump Functional Description: The Fuel Pump Test Stand Is To Provide For Accurate And Rapid Testing Of Fuel Pumps & Components Used On Modern Aircraft In Accordance With The Manufacturer's Test Specifications Reference Data And Literature: T.O. 33D2-3-48-1 | Avl | RFQ |
TE10602 | 4920-00-625-6851 | Functional Description: Used For Static Testing Fuel System Components End Item Identification: Pratt Whitney Engine Reference Data And Literature: T.O. 33D4-6-156-1/11 | Avl | RFQ |
TE15569 | 4920-00-605-9446 | Functional Description: Provides Oil At The Temperatures, Pressure And Flow Required To Test Both Adg/Idg And Fuel Thermostatic Valves; Accomplish Pressure Drop Tests End Item Identification: Fuel/Oil Heat Exchanger Reference Data And Literature: To 7J1-79-3 | Avl | RFQ |
TTU-499 F | 4920-01-217-0109 | Special Features: Input Power: 480.0Vac, 60.0 Hz, 3-Phase, 9.5 Kva; Output Characteristics: Fuel: 0-1400 Psig, 0-218 Gpm, 85 Deg F Porm 2 Deg; Pneumatic: Shop Air 100 Psig, 20 Scfm; Purge Air: 300 Scfm; High Pressure Air: 750 Psig, 10 Scfm; High Pressure Gn2: 200 Psig, 5 Scfm; Test Station Provides To Uut: Gn2 50 Psia; Facility Provides Hot Water 40 Psig 2 Gpm; 140 Deg F; Cold Water 40 Psig, 10 Gpm, 55 Deg F; Fixed Mount; 11.000 Ft W, 8.000 Ft D, 8.000 Ft H Functional Description: Used To Supply Fuel And Facility Supplied Air And Appropriate Instrumentation For Performing Depot Level Tests On Assemblies/Sub-Assemblies End Item Identification: F100-Pw-220 Engine Augmentor Fuelcontrol | Avl | RFQ |
WIE52 | 4920-01-051-9235 | Functional Description: Used To Test Fuel Vent And Presurriaztion Control Valves End Item Identification: F-16 Acft Reference Data And Literature: T.O. 33D2-3-96-1 | Avl | RFQ |
WIE52 | 4920-01-051-9235 | Functional Description: Used To Test Fuel Vent And Presurriaztion Control Valves End Item Identification: F-16 Acft Reference Data And Literature: T.O. 33D2-3-96-1 | Avl | RFQ |
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