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 10-166525-1, 128SEAV17550-21, 13793-2A, 13A1280, 13A1282. 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 Joint Electronics Type Designation, Goodrich Corporation, Honeywell Inc, Aeronautical And Support Equipment, General Electric Company. Our team provides superior quality assurance testing for and more. So if you are in need of Test Set Flight 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
|
NSN NSN Parts
|
Details Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
10-166525-1 | 4920-01-236-9041 | Inclosure Feature: Multiple Item W/Carrying Case Major Components: Age Van; 3 Bay Rack; Single Bay Rack; Double Bay Rack; Uhf Antenna; Vhf Antenna; Rotary Chair ; Microphone Assembly; Computer System; Graphic Printer; Detector | Avl | RFQ |
128SEAV17550-21 | 4920-01-367-0853 | Test Type For Which Designed: Tc Flight System Width: 42.000 Inches Nominal Height: 76.000 Inches Nominal | Avl | RFQ |
13793-2A | 4920-00-601-4037 | Functional Description: Used To Test The 15816 And 15831 Three Axis Rate Controls M545b1/M546b1 Mechanism Assy, Part Of 15831 And To Test The 15839 Pitch And Yaw Rate Control Which Is Part Of The Pb20d Automatic Flight Control System End Item Identification: E-3A Acft Age Reference Data And Literature: T.O. 33D7-47-60-1 | Avl | RFQ |
13A1280 | 4920-00-732-5919 | NA | Avl | RFQ |
13A1282 | 4920-00-825-3775 | NA | Avl | RFQ |
13A3490 | 4920-00-940-9275 | NA | Avl | RFQ |
18903260000 | 4920-00-118-9378 | Functional Description: Used To Test, Calibrate And Certify The Test Set, Automatic Altitude Reporting Encoder And Altimiter End Item Identification: Ttu-229/E Test Type For Which Designed: Certification, Procurement Data | Avl | RFQ |
18903260000 | 4920-00-118-9378 | Functional Description: Used To Test, Calibrate And Certify The Test Set, Automatic Altitude Reporting Encoder And Altimiter End Item Identification: Ttu-229/E Test Type For Which Designed: Certification, Procurement Data | Avl | RFQ |
1C5239G1 | 4920-00-956-5183 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Dynamic Leak Tests Test Type For Which Designed: Pneumatic System Leak Test | Avl | RFQ |
1C5239G2 | 4920-00-990-5087 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Leak Tests End Item Identification: Multi Acft Application Age | Avl | RFQ |
215-00133-1 | 4920-00-824-1422 | Test Type For Which Designed: Gyro Inclosure Feature: Multiple Item W/Carrying Case Electrical Power Source Relationship: Self-Contained | Avl | RFQ |
215-00133-2 | 4920-00-435-0789 | Special Features: To Name: Flight Control Bench Test Set Reference Data And Literature: To 33D3-9-150-2 Width: 19.650 Inches Nominal | Avl | RFQ |
215-00133-3 | 4920-00-106-9696 | Test Type For Which Designed: Test And Facilitate Trouble Analysis Inclosure Feature: Multiple Item W/Carrying Case Width: 20.000 Inches Nominal | Avl | RFQ |
215-00134-2 | 4920-00-050-8687 | Test Type For Which Designed: Accelerometer Signals; Approach Power Control Inclosure Feature: Single Item W/Carrying Case Width: 20.000 Inches Nominal | Avl | RFQ |
215-00137-2 | 4920-00-069-5126 | Ac Voltage Rating: 115.0 Volts Nominal Frequency Rating: 400.0 Hertz Nominal | Avl | RFQ |
216-00901-2 | 4920-00-118-6879 | Special Features: To Name: Angle Of Attack Transducer Test Set; Used With Adapter Cable 216-09927-101; Aluminum Case; 20.5Lbs Reference Data And Literature: To 33D3-23-5-2 Width: 10.000 Inches Nominal | Avl | RFQ |
2418S585ASI-2000 | 4920-01-526-5071 | Special Features: Aviation Electronics Test Equipment; For Testing Digital Avionics, Asi | Avl | RFQ |
2487H4 | 4920-01-016-2865 | NA | Avl | RFQ |
2587558 | 4920-00-872-7046 | Functional Description: Used To Detect And Isolate Malfunctions In C-12 Gyroscopic Compass System Reference Data And Literature: T.O.33D3-6-38-1 Test Type For Which Designed: Continuity; Resistance; Voltage | Avl | RFQ |
292E800G3 | 4920-01-034-7670 | Special Features: Company Item Name-Test Set, Automatic Flight Control System Functional Description: Used To Functionally Test And Fault Isolate The Afcs And Mechanical Fight Control Components Controlled By The Afcs End Item Identification: F-1F, F-15 Acft | Avl | RFQ |
3145100-3 | 4920-00-876-0555 | Test Type For Which Designed: Aircraft Voltage, Continuity, Operational Check, Resistance Check Inclosure Feature: Single Item W/Carrying Case Width: 13.800 Inches Nominal | Avl | RFQ |
32E150010-301 | 4920-00-871-7597 | NA | Avl | RFQ |
35847R | 4920-01-147-4526 | Special Features: C/O Control Panel, Test Points, Switches, Indicator Lights, Power Supplies And Interface Cables; Energizes Aircraft Flight Control Subsystem Electro Mechanical Actuators And Linear Servomechanisms; 230.0 Vac, 400.0 Hz, 3 Phase Input Power End Item Identification: B-Ab Acft Test Type For Which Designed: Energy And Drive Control | Avl | RFQ |
3S60022-101 | 4920-00-867-5975 | Special Features: Cable Assembly Storage In Bottom Of Test Set Case Functional Description: Used To Test Flight Control De-Iceing Systems Reference Data And Literature: T.O. 33D2-16-10-1 | Avl | RFQ |
40262-40000-10 | 4920-01-441-1376 | Special Features: 5The Aircraft Boresight Unit C/O Reference Unit, Measurement Unit, Handheld Display Unit, System Controller, Interface Cable Assys In Two Cases 28L X 32W X 24H Ea, Total Weight 214 Lbs, Finish-Olive Drab, Design: Mil-T-28800D, Class 2 Modified End Item Identification: Specialized Ground Servicing Equipment; Multi-Aircraft Applicability Reference Data And Literature: Air Force Serd 570769/A | Avl | RFQ |
40292-40000-10 | 4920-01-441-1376 | Special Features: 5The Aircraft Boresight Unit C/O Reference Unit, Measurement Unit, Handheld Display Unit, System Controller, Interface Cable Assys In Two Cases 28L X 32W X 24H Ea, Total Weight 214 Lbs, Finish-Olive Drab, Design: Mil-T-28800D, Class 2 Modified End Item Identification: Specialized Ground Servicing Equipment; Multi-Aircraft Applicability Reference Data And Literature: Air Force Serd 570769/A | Avl | RFQ |
426400-01-01 | 4920-00-109-6343 | Test Type For Which Designed: Functional Testing Of Automatic Flight Control System; Servo Actuator Inclosure Feature: Single Item W/Carrying Case Width: 11.780 Inches Nominal | Avl | RFQ |
426400-01-02 | 4920-00-109-6343 | Test Type For Which Designed: Functional Testing Of Automatic Flight Control System; Servo Actuator Inclosure Feature: Single Item W/Carrying Case Width: 11.780 Inches Nominal | Avl | RFQ |
427150-01-01 | 4920-00-435-0789 | Special Features: To Name: Flight Control Bench Test Set Reference Data And Literature: To 33D3-9-150-2 Width: 19.650 Inches Nominal | Avl | RFQ |
53E210002-1 | 4920-00-066-3136 | Functional Description: Used For Functional Tests, Calibration And Trouble Shooting Of End Item And Individual Modules End Item Identification: Age For F4c Acft Reference Data And Literature: T.O. 33D7-3-41-4 | Avl | RFQ |
53E210002-317 | 4920-00-951-0929 | Functional Description: Used For Functional Tests, Calibration And Trouble Shooting Of End Item And Individual Modules End Item Identification: Age For F4c Acft Reference Data And Literature: T.O. 33D7-3-41-4 | Avl | RFQ |
53E350024-303 | 4920-00-798-3574 | End Item Identification: Non-Auto Avionics Test Equip | Avl | RFQ |
53E350062-1 | 4920-00-872-8596 | Functional Description: Used To Determine And Adjust Gyro Bias Currents Necessary To Compensate For Inherent Drift Of Gyros In The Gyro Stabelized Platform End Item Identification: F-4 Acft Age Reference Data And Literature: T.O. 33D2-8-221-1 | Avl | RFQ |
607330-3-1 | 4920-00-065-6114 | Special Features: Test Set Pressure And Temperatureflight Control Functional Description: Provides The Pressures Necessary For Maintenance & Verification Of The Flight Control System End Item Identification: Multi Acft Application | Avl | RFQ |
607330-4-1 | 4920-00-967-0122 | Functional Description: Provides The Necessary Pressure &Temperature For The Maintenance & Verification Of The Flight Control System End Item Identification: Multi Acft Application Test Type For Which Designed: Pneumatic System Leak Test Of Theflight Control System | Avl | RFQ |
607330-5-1 | 4920-00-757-6786 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Dynamic Leak Tests End Item Identification: Multi Acft Application Age | Avl | RFQ |
607330-5-1 | 4920-00-757-6786 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Dynamic Leak Tests End Item Identification: Multi Acft Application Age | Avl | RFQ |
607330-8-1 | 4920-00-757-6786 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Dynamic Leak Tests End Item Identification: Multi Acft Application Age | Avl | RFQ |
607330-9-1 | 4920-00-245-4033 | Special Features: Test Set, Pressure-Temperature.Ttu-205 C/E Functional Description: Provides The Pressure & Temperature Necessary For The Maintenance & Verification Of The Flight Control Sys End Item Identification: Multi Acft Application Age | Avl | RFQ |
6137145 | 4920-00-628-4832 | Test Type For Which Designed: Range Coordinate; Temperature; Velocity Integrator Inclosure Feature: Single Item W/Housing Width: 45.000 Inches Nominal | Avl | RFQ |
622-0846-001 | 4920-00-175-7844 | Special Features: Company Name-Flight Director System | Avl | RFQ |
6400-2300 | 4920-01-527-6841 | End Item Identification: Light Combat Fixed Wing Aircraft, L159 Part Name Assigned By Controlling Agency: Computer, Eye Level, Test Bench Test Type For Which Designed: Part Number 5159-101Pilot Displayunit Maintenance | Avl | RFQ |
817306 | 4920-00-888-9961 | Test Type For Which Designed: Output Of True Airspeed Synchro; Measure Output Of Aircraft Temperature Probe Inclosure Feature: Single Item W/Carrying Case Width: 17.750 Inches Nominal | Avl | RFQ |
8505540-901 | 4920-01-276-5294 | Special Features: Capabilities: 0 To +10 Vdc, Accurate To 0.5 Vdc; 0 To 11.8 Vac, 400 Hz.2 Wire Source Accurate To 0.5 Vac; Voltage Measuring Capability Of +19 Vdc; Air Data Sensor Unit; Status Test Panel; B-52 Mode Select Unit; Flight Controller; Pitch And Roll Servo; Horizontal Stabilizer Trim Actuator; Pitch Force Link Assy; Roll Axis Force Transducer End Item Identification: An/Asw-49 | Avl | RFQ |
912476-4-1 | 4920-01-142-6581 | NA | Avl | RFQ |
912476-5-1 | 4920-01-126-1759 | Functional Description: Used To Test The Emergency Power Unit On The F-16A/B Acft Reference Data And Literature: T.O. 33D7-38-102-1 Test Type For Which Designed: Emergency Power Unit | Avl | RFQ |
91A1550-10 | 4920-01-441-1376 | Special Features: 5The Aircraft Boresight Unit C/O Reference Unit, Measurement Unit, Handheld Display Unit, System Controller, Interface Cable Assys In Two Cases 28L X 32W X 24H Ea, Total Weight 214 Lbs, Finish-Olive Drab, Design: Mil-T-28800D, Class 2 Modified End Item Identification: Specialized Ground Servicing Equipment; Multi-Aircraft Applicability Reference Data And Literature: Air Force Serd 570769/A | Avl | RFQ |
9G002-101 | 4920-01-612-2224 | NA | Avl | RFQ |
9M002-10 | 4920-01-612-2224 | NA | Avl | RFQ |
A03G0042 | 4920-00-906-9030 | Test Type For Which Designed: Circuitry Inclosure Feature: Single Item W/Carrying Case Major Components: Cable Adapter | Avl | RFQ |
A03G0042-1 | 4920-00-906-9030 | Test Type For Which Designed: Circuitry Inclosure Feature: Single Item W/Carrying Case Major Components: Cable Adapter | Avl | RFQ |
AD32807-8 | 4920-01-234-4033 | Special Features: Orig Dwg Name-Simulator Back Pressure.C/O Valve Assy 1; Plug, Pipe 1;0.250 In. O/D - 0.035 In. Wall Tubing Ar;0.250 Tee 2; Relief Valve 1;Valve, Ball, Normally Closed 1; Nipple 6 End Item Identification: 4920-00-090-6521 Test Type For Which Designed: Back Pressure | Avl | RFQ |
AD50002-540 | 4920-01-234-4033 | Special Features: Orig Dwg Name-Simulator Back Pressure.C/O Valve Assy 1; Plug, Pipe 1;0.250 In. O/D - 0.035 In. Wall Tubing Ar;0.250 Tee 2; Relief Valve 1;Valve, Ball, Normally Closed 1; Nipple 6 End Item Identification: 4920-00-090-6521 Test Type For Which Designed: Back Pressure | Avl | RFQ |
ADTS405-8325 | 4920-01-449-8072 | End Item Identification: Avionics Support Equipment | Avl | RFQ |
AN AJM-28 | 4920-00-912-0095 | Reference Data And Literature: To33d2-40-2-4 Test Type For Which Designed: Stall Prevent Inclosure Feature: Single Item W/Housing | Avl | RFQ |
AN ARM-163(V)4 | 4920-01-325-1929 | Functional Description: Provides Complete, Flightline Testfacilities For The An/Arw-83(V)5 Radio Receiving Set End Item Identification: Detecting System, Special Purpose An/Usd-9A Internal Battery Accommodation: Not Included | Avl | RFQ |
AN ARM-163(V)5 | 4920-01-236-9041 | Inclosure Feature: Multiple Item W/Carrying Case Major Components: Age Van; 3 Bay Rack; Single Bay Rack; Double Bay Rack; Uhf Antenna; Vhf Antenna; Rotary Chair ; Microphone Assembly; Computer System; Graphic Printer; Detector | Avl | RFQ |
AN ASM-247 | 4920-00-872-8596 | Functional Description: Used To Determine And Adjust Gyro Bias Currents Necessary To Compensate For Inherent Drift Of Gyros In The Gyro Stabelized Platform End Item Identification: F-4 Acft Age Reference Data And Literature: T.O. 33D2-8-221-1 | Avl | RFQ |
AN ASM-387 | 4920-00-118-6879 | Special Features: To Name: Angle Of Attack Transducer Test Set; Used With Adapter Cable 216-09927-101; Aluminum Case; 20.5Lbs Reference Data And Literature: To 33D3-23-5-2 Width: 10.000 Inches Nominal | Avl | RFQ |
AN ASM-497 | 4920-01-034-7670 | Special Features: Company Item Name-Test Set, Automatic Flight Control System Functional Description: Used To Functionally Test And Fault Isolate The Afcs And Mechanical Fight Control Components Controlled By The Afcs End Item Identification: F-1F, F-15 Acft | Avl | RFQ |
ANASM117 | 4920-00-867-0029 | NA | Avl | RFQ |
ANASM117 | 4920-00-867-0029 | NA | Avl | RFQ |
ANASM133 | 4920-00-888-9961 | Test Type For Which Designed: Output Of True Airspeed Synchro; Measure Output Of Aircraft Temperature Probe Inclosure Feature: Single Item W/Carrying Case Width: 17.750 Inches Nominal | Avl | RFQ |
ANASM148 | 4920-00-877-3906 | Test Type For Which Designed: Align Isolate And Test Malfunctions Of Ins Inclosure Feature: Single Item W/Carrying Case Width: 20.000 Inches Nominal | Avl | RFQ |
ANASM160 | 4920-00-066-3136 | Functional Description: Used For Functional Tests, Calibration And Trouble Shooting Of End Item And Individual Modules End Item Identification: Age For F4c Acft Reference Data And Literature: T.O. 33D7-3-41-4 | Avl | RFQ |
ANASM167 | 4920-00-876-0555 | Test Type For Which Designed: Aircraft Voltage, Continuity, Operational Check, Resistance Check Inclosure Feature: Single Item W/Carrying Case Width: 13.800 Inches Nominal | Avl | RFQ |
ANASM201 | 4920-00-951-0929 | Functional Description: Used For Functional Tests, Calibration And Trouble Shooting Of End Item And Individual Modules End Item Identification: Age For F4c Acft Reference Data And Literature: T.O. 33D7-3-41-4 | Avl | RFQ |
ANASM201B | 4920-00-951-0929 | Functional Description: Used For Functional Tests, Calibration And Trouble Shooting Of End Item And Individual Modules End Item Identification: Age For F4c Acft Reference Data And Literature: T.O. 33D7-3-41-4 | Avl | RFQ |
ANASM210 | 4920-00-798-3574 | End Item Identification: Non-Auto Avionics Test Equip | Avl | RFQ |
ANASM225 | 4920-00-872-7046 | Functional Description: Used To Detect And Isolate Malfunctions In C-12 Gyroscopic Compass System Reference Data And Literature: T.O.33D3-6-38-1 Test Type For Which Designed: Continuity; Resistance; Voltage | Avl | RFQ |
ANASM244 | 4920-00-824-1422 | Test Type For Which Designed: Gyro Inclosure Feature: Multiple Item W/Carrying Case Electrical Power Source Relationship: Self-Contained | Avl | RFQ |
ANASM244A | 4920-00-435-0789 | Special Features: To Name: Flight Control Bench Test Set Reference Data And Literature: To 33D3-9-150-2 Width: 19.650 Inches Nominal | Avl | RFQ |
ANASM244B | 4920-00-106-9696 | Test Type For Which Designed: Test And Facilitate Trouble Analysis Inclosure Feature: Multiple Item W/Carrying Case Width: 20.000 Inches Nominal | Avl | RFQ |
ANASM245A | 4920-00-109-6343 | Ac Voltage Rating: 115.0 Volts Nominal Frequency Rating: 400.0 Hertz Nominal | Avl | RFQ |
ANASM334 | 4920-00-050-8687 | Test Type For Which Designed: Accelerometer Signals; Approach Power Control Inclosure Feature: Single Item W/Carrying Case Width: 20.000 Inches Nominal | Avl | RFQ |
ANFSM26 | 4920-00-868-8174 | End Item Identification: Fixed Wing Unique Avionics | Avl | RFQ |
ANPSM17C | 4920-00-691-5913 | Test Type For Which Designed: Adjustments; Calibration; Checking Indexer; Stall Warning Vibrator Inclosure Feature: Single Item W/Carrying Case Width: 15.000 Inches Nominal | Avl | RFQ |
AS111694 | 4920-01-126-1759 | Functional Description: Used To Test The Emergency Power Unit On The F-16A/B Acft Reference Data And Literature: T.O. 33D7-38-102-1 Test Type For Which Designed: Emergency Power Unit | Avl | RFQ |
ASI-2000 | 4920-01-526-5071 | Special Features: Aviation Electronics Test Equipment; For Testing Digital Avionics, Asi | Avl | RFQ |
ASI-210 | 4920-01-529-0145 | Part Name Assigned By Controlling Agency: Al-101 Radio Altimeter System Ramp Test Fixture | Avl | RFQ |
ASI-282 | 4920-00-175-7844 | Special Features: Company Name-Flight Director System | Avl | RFQ |
E00064 | 4920-00-959-0675 | Test Type For Which Designed: Synchro Transmitter Performance Inclosure Feature: Multiple Item W/Console Housing Width: 66.000 Inches Nominal | Avl | RFQ |
E00064 | 4920-00-959-0675 | Test Type For Which Designed: Synchro Transmitter Performance Inclosure Feature: Multiple Item W/Console Housing Width: 66.000 Inches Nominal | Avl | RFQ |
F71375 | 4920-01-349-7931 | Functional Description: C/O Panel Assembly, Input Power Cable, Cabinet Assembly; The Analyzer Is Installed In Place Of The Machine Trim Coupler During Test Procedures; Item Is Used To Perform Unscheduled Maintenance On The Joint Stars Aircraft; Itis Required To Analyze The Rest Of Thesystem End Item Identification: Joint Stars Aircraft; E-8A Reference Data And Literature: Serd 1321(Org); Tech Order=Flight Control Test Set-Mach Trim Analyzer | Avl | RFQ |
GR-912476-5-1 | 4920-01-126-1759 | Functional Description: Used To Test The Emergency Power Unit On The F-16A/B Acft Reference Data And Literature: T.O. 33D7-38-102-1 Test Type For Which Designed: Emergency Power Unit | Avl | RFQ |
LS67A | 4920-00-906-9030 | Test Type For Which Designed: Circuitry Inclosure Feature: Single Item W/Carrying Case Major Components: Cable Adapter | Avl | RFQ |
LT4662-02-01 | 4920-00-798-3574 | End Item Identification: Non-Auto Avionics Test Equip | Avl | RFQ |
MILT38191 | 4920-00-065-6114 | Special Features: Test Set Pressure And Temperatureflight Control Functional Description: Provides The Pressures Necessary For Maintenance & Verification Of The Flight Control System End Item Identification: Multi Acft Application | Avl | RFQ |
R-TBD-148 | 4920-01-147-4526 | Special Features: C/O Control Panel, Test Points, Switches, Indicator Lights, Power Supplies And Interface Cables; Energizes Aircraft Flight Control Subsystem Electro Mechanical Actuators And Linear Servomechanisms; 230.0 Vac, 400.0 Hz, 3 Phase Input Power End Item Identification: B-Ab Acft Test Type For Which Designed: Energy And Drive Control | Avl | RFQ |
TE127950 | 4920-01-068-7583 | Special Features: Has Provisions For Simulation And Varying All Acft Inputs To The Head Up Display Control Panel Outputs End Item Identification: A-10A Acft Age. Reference Data And Literature: T.O. 33K1-4-45-1 | Avl | RFQ |
TE60592 | 4920-00-166-9049 | Special Features: To Name: Field Test Set End Item Identification: Cpu-80/A; Encased With Removable Hinged Cover Reference Data And Literature: To 33D3-24-25-4 | Avl | RFQ |
TS2473AJM25 | 4920-00-942-8285 | Test Type For Which Designed: Rate Gyroscope Transmitter; Switching Rate Gyroscope Inclosure Feature: Single Item W/Carrying Case Width: 7.500 Inches Nominal | Avl | RFQ |
TT4205BE | 4920-00-757-6786 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Dynamic Leak Tests End Item Identification: Multi Acft Application Age | Avl | RFQ |
TT4205BE | 4920-00-757-6786 | Special Features: Pneumatic System Leak Test Simulates Temperature Functional Description: Used To Do Dynamic Leak Tests End Item Identification: Multi Acft Application Age | Avl | RFQ |
TTU292E | 4920-00-118-9378 | Functional Description: Used To Test, Calibrate And Certify The Test Set, Automatic Altitude Reporting Encoder And Altimiter End Item Identification: Ttu-229/E Test Type For Which Designed: Certification, Procurement Data | Avl | RFQ |
TTU292E | 4920-00-118-9378 | Functional Description: Used To Test, Calibrate And Certify The Test Set, Automatic Altitude Reporting Encoder And Altimiter End Item Identification: Ttu-229/E Test Type For Which Designed: Certification, Procurement Data | Avl | RFQ |
W101470-1 | 4920-01-146-5166 | End Item Identification: F-4 Acft | Avl | RFQ |
W104300-3 | 4920-01-531-3877 | End Item Identification: Se For 8-Blade Np2000 Prop Sys Part Name Assigned By Controlling Agency: Inavy) Test Set, Deicer, Aircraft Test Type For Which Designed: Deicer For Np2000 Prop Sys-Blades | Avl | RFQ |
Y63-315880-941 | 4920-00-867-0029 | NA | Avl | RFQ |
Y63-315880-941 | 4920-00-867-0029 | NA | Avl | RFQ |
All Orders are Fulfilled in the U.S.A.
All shipments must comply with U.S.A export laws.
No exceptions.
The only independent distributor
with a NO CHINA SOURCING Pledge
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”.
Remember Us the Next Time You’re Looking for NSN Parts. We Can Get You Some of the Quickest and Most Competitive Quotes In the Industry.
Request for Quote