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 077-68485, 077-78209, 077-78209-1, 077-78222, 1002110-001. 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 Moog Aircraft Group, Drs C3 And Aviation Company, Columbus Jack Corporation, Fleet Readiness Center Southwest, Directie Materieel Koninklijke. Our team provides superior quality assurance testing for and more. So if you are in need of Fixture Set Aircraft Maintenance 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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077-68485 | 4920-00-219-1592 | Special Features: Aluminum Functional Description: Used To Establish The Following Tolerances In The Pitch And Roll Channel Of The Csbpc: Pitch Input To Unit, Roll Input To Unit, Auxiliary Input To Unit, Pitch Input To Pitch Output, Roll Input To Roll Output End Item Identification: F-15 Acft | Avl | RFQ |
077-78209 | 4920-01-003-9873 | Special Features: C/O Three Different Items And Carrying Case Functional Description: Used During Maintenance Operations And Testing Of The Pitch Trim Controller Of The 68-690085-101 Pitch And Roll Channel Assembly End Item Identification: F-15 Acft | Avl | RFQ |
077-78209-1 | 4920-01-301-0216 | Special Features: C/O E04811, Tester, Solenoid Selector, Multi-Coil; 077-68298, Manifold, Test, Flow, Pitch Trim Controller; 077-69323, Fixture, Alignment, Lofes Housing; 077-69326, Adapter, Maintenance Holder, Pitch Trim Controller; 077-98648, Tool, Orientation; Manifold, Test-Casi Solenoid Valve; A06196-024, Cable Assembly Lofes Valve To 077-68264 Per P2; A06196-026 Cable Assemblt Casa Valve To 077-68259 Temp P2; A06196-027 Cable Assemblt Casb Valve To 077-68259 Temp P2; A06196-164 Cable Assemblt Cas Sol To 077-68264 Perm; A06196-165 Cable Assembly Cas Sol To 077-68264 Temp Cable Assembly Fly-Up Tq. Mtr. To 077-68259; Storage Case, Wood, Two; Dim. 22.000 In. W; 15.000 In. D; 8.000 In. H; Marking: Mil-Std-130C Functional Description: Used During Maintenance Operations And Functional Testing Of The Pitch Trim Controller (Ptc) Of The 68-690085-107 Or -109 Pitch And Roll Channel Assembly End Item Identification: F-15 Acft | Avl | RFQ |
077-78222 | 4920-01-006-1788 | Special Features: C/O Three Separate Fixtures, An An Adapter, And A Gage Functional Description: Used During Overhaul Of The Yaw Ratio Controller Of The Ari End Item Identification: F/Tf-15 A Acft | Avl | RFQ |
1002110-001 | 4920-01-589-3598 | Part Name Assigned By Controlling Agency: Boresight Adapter Kit F-15 Rev:X1 Supply Items And Quantities: 1 Bracket Assy Aft Boresight Reference Line, Bracket Assy Forward Boresight Reference Line, Bracket Assy 20 Mm Gun Alignment, Bracket Assy Radar, Bracket Assy Hud, Adapter Assy Heads Up Display, Bracket Imu, Adapter Inertial Measurement Unit, Bracket Assy Navigation Pod, Bracket Assy Targeting Pod, Adapter Assy Targeting Pod, Bracket Assy Radar Mount, 2 Transit Cases, Adapter Assy Jhmcs Bracket | Avl | RFQ |
120D149 | 4920-01-367-0753 | Unpackaged Unit Weight: 10.000 Ounces Cubic Measure: 0.75 Cubic Feet | Avl | RFQ |
120D160 | 4920-01-344-6051 | End Item Identification: Special Acft & Eng Tools, Support Equip & Parts Cubic Measure: 0.50 Cubic Feet | Avl | RFQ |
160198-1 | 4920-01-360-1535 | Special Features: Strain Sensor Bonding Fixtures Assembly Is Designed For Use At The Intermediate And Depot Maintenance Levels, Provides 75 Gram Weight And Metal Plate For Testing The Strain Gauges Prior To Installation, Assembly Also Provides Strain Gauge Locating Tools And Bonding Fixtures Required For Installing All Strain Gauges On The Airframe End Item Identification: Aircraft Model F/A-18 | Avl | RFQ |
16A74029-3 | 4920-01-158-5867 | Special Features: W/Ring Gyro; Litton Mount This Configuration Only; -1 And -5 Use Singer-Kearfott Mount Functional Description: Vorescope Kit End Item Identification: F-16C Aircraft | Avl | RFQ |
16A74029-3NL | 4920-01-158-5867 | Special Features: W/Ring Gyro; Litton Mount This Configuration Only; -1 And -5 Use Singer-Kearfott Mount Functional Description: Vorescope Kit End Item Identification: F-16C Aircraft | Avl | RFQ |
1C5659G01 | 4920-00-068-8566 | Functional Description: Used During Air Extraction Port Repair/Maintenance End Item Identification: Tf-39 Aircraft Engine Reference Data And Literature: T.O. 2J-Tf39-4 | Avl | RFQ |
1C5993G01 | 4920-00-179-5422 | Special Features: Takes Configuration Of Two Arches; Company Item Name-Retainer Set Functional Description: Used During Tip Grinding Of The Compressor Rotor Blades End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
1C6024G01 | 4920-00-407-4016 | Special Features: To Name: Closure Set, Ebu Spline Drive; Consists Of Expansion Plugs 9408M15p16 And 9408M15p17 End Item Identification: Tf39 Engine Age Reference Data And Literature: To 2J-Tf39-4 | Avl | RFQ |
1C6133G01 | 4920-00-407-3993 | Functional Description: Used During Shot Peening End Item Identification: Tf-39 Aircraft Engine Reference Data And Literature: T.O. 2J-Tf39-4 | Avl | RFQ |
1C6135G01 | 4920-00-407-3995 | Special Features: Company Item Name-Fixture Set Functional Description: Used During Shot Peening Of Rotor Dove Tails End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
1C6144G01 | 4920-00-179-5422 | Special Features: Takes Configuration Of Two Arches; Company Item Name-Retainer Set Functional Description: Used During Tip Grinding Of The Compressor Rotor Blades End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
1C6197G01 | 4920-00-159-8739 | Special Features: C/O Mtg Ring, 2 Clamp Bar, 13 Rings, 1 Mtg Ring, 1 End Cover, 3 Studs, 1 End Cover, 1 Speed Handle, 1 Hand Knob; Compressor Rotor End Item Identification: Tf39 Acft Engine Reference Data And Literature: T.O. 2J-Tf39-4 | Avl | RFQ |
1C6244G01 | 4920-00-169-2821 | Functional Description: Used During No. 4 Ball Bearing Rotating Vent Repair End Item Identification: Tf-39 Aircraft Engine Reference Data And Literature: T.O. 2J-Tf39-4 | Avl | RFQ |
1C6245G01 | 4920-00-169-2822 | Special Features: Company Item Name-Fixture Set, Repair-Seal Functional Description: Used During Rotating Air. No. 4 Bearing Repair End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
1C6246G01 | 4920-00-169-2823 | Special Features: Company Item Name-Fixture Set, Repair Functional Description: Used During Vent Repair Of No. 4 Roller Bearing End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
1C6273G01 | 4920-00-139-7884 | NA | Avl | RFQ |
1C6286G01 | 4920-00-078-2245 | Special Features: Company Item Name-Fixture Set Functional Description: Used During Fan Stator Vane Spacing; Stage 1 And 2 End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
1C6326G01 | 4920-00-255-1200 | Special Features: C/O Fixture Assy 2, Plug 2, Pin Dowel 3, And Misc Hardware Fsc Application Data: Tf-39 Turbofan Engine Usage Design: Sump Tube, Turbine Rear Frame | Avl | RFQ |
1C7193G01 | 4920-01-502-2911 | Special Features: C/O 18 Alignment Subassemblies; Housed In Container (12 X 9 X 5); 20 Lbs Functional Description: Used Used To Allow Fit Up Of Stage 1 Disks (Hpt) And Spacers End Item Identification: Tf-39 Acft Engine | Avl | RFQ |
212-240-002-101 | 4920-01-413-0198 | End Item Identification: H-1 Helicopter | Avl | RFQ |
21C3765G01 | 4920-01-004-6567 | Special Features: To Name: Kit, Adapter Test; Consists Of Two Adapters And Gasket Functional Description: Used During Aircraft Maintenance End Item Identification: Afterburner Fuel Pump And Shutoff Valve | Avl | RFQ |
21C5367G01 | 4920-01-444-0663 | NA | Avl | RFQ |
21C5670G01 | 4920-01-442-0305 | End Item Identification: Tf34 Engine Unpackaged Unit Weight: 14.000 Pounds | Avl | RFQ |
21C5788G01 | 4920-01-092-4447 | Special Features: Set Consists Of Brazing/Holding Fixture, Drawing Fixture, Expanding Fixture, Adapters, Fittings And Tubing To Permit Cleaning And Pressure Testing The Joint After Brazing, Hand Held Hydraulic Swaging Fixture Used To Size Used Tube End To Maintain .001-.004 Gap When Mated With Cleaned Or New Fittings; Weight 20 Lbs, Cubage 10 In. By 10 In. By 5 In. Boxed End Item Identification: Tf-34-Ge-100 Age. Part Name Assigned By Controlling Agency: C-Sump Scavenge Tube Braze Set | Avl | RFQ |
21C895G001 | 4920-00-779-5224 | Functional Description: Used For Bearing And Plug Removal From Shaft Gears Of Accessory Drive Gearbox End Item Identification: J-85 Engine Age. Reference Data And Literature: T.O. 2J-J85-4 | Avl | RFQ |
21C895G001 | 4920-00-779-5224 | Functional Description: Used For Bearing And Plug Removal From Shaft Gears Of Accessory Drive Gearbox End Item Identification: J-85 Engine Age. Reference Data And Literature: T.O. 2J-J85-4 | Avl | RFQ |
21C895G003 | 4920-00-148-6671 | Functional Description: Used To Disassemble Bearings And Plugs From Shaft Gears Of Accessory Drive Gear Box End Item Identification: J-85-Ge Series Turbojet Engines Reference Data And Literature: To 2J-J85-94 | Avl | RFQ |
21C895G1 | 4920-00-779-5224 | Functional Description: Used For Bearing And Plug Removal From Shaft Gears Of Accessory Drive Gearbox End Item Identification: J-85 Engine Age. Reference Data And Literature: T.O. 2J-J85-4 | Avl | RFQ |
21C895G1 | 4920-00-779-5224 | Functional Description: Used For Bearing And Plug Removal From Shaft Gears Of Accessory Drive Gearbox End Item Identification: J-85 Engine Age. Reference Data And Literature: T.O. 2J-J85-4 | Avl | RFQ |
2506000-3 | 4920-01-587-5066 | Special Features: Support Equipment, Foresight Kit End Item Identification: Helicopter Part Name Assigned By Controlling Agency: Fixture Set Up | Avl | RFQ |
2929-91500 | 4920-01-424-9371 | NA | Avl | RFQ |
2929-91600 | 4920-01-420-5876 | NA | Avl | RFQ |
2929-91600 | 4920-01-420-5876 | NA | Avl | RFQ |
2929-91700 | 4920-01-424-9369 | NA | Avl | RFQ |
332159-1 | 4920-01-406-3971 | Special Features: Test Fixture Assy Tf Second If; Consists Of Terminal 1; Contact 12; Connector 4 | Avl | RFQ |
363614G01 | 4920-01-254-6793 | Functional Description: Used To Test Vsv Actuator End Item Identification: F108-Cf-100 Engine Usage Design: Tool Set | Avl | RFQ |
3C3220G01 | 4920-01-148-7894 | Special Features: Weight 3.000 Lbs; 13.000 In. L, 9.000 W, 6.500 In. H, C/O 1 Steel Plate2.380 In. L, 4.180 In. W, 0.380 In. H; 1 Steel Plate 2.380 In. L, 3.380 In. W, 0.500 In. H; A Special Mounting Pin 5/8 In. Dia, 2.500 In. Lg Functional Description: Used As Special Device To Extend Surfaces To Be Measured (Axial Position Between The Aft Flange Of The Exhaust Nozzle Duct And The Actuation Ring End Item Identification: F101-Ge-102 | Avl | RFQ |
3C3380G01 | 4920-01-204-7391 | Special Features: C/O 2 Parts: Forward End Made Of Sae 4130 Stl W/Special Tempering For Dimensional Stability; Its Final Hardness Is 36-40 Rockwell C Scale. Black Xide Finish; Aft End Is An Assy Of A Modified Lock Nut, A Cradle Made Of Anodized 6061 Aluminum And Misc Components Of Hardened Steel; Forward End Is A Large Cylindrical Piece That Simulatesthe Mass Properties And Approx Geometry 0F The Compressor Rotor. It Has A Prrcision Rabbet And Bolt Circle For Interface W/Frnt Shaft Of Hpt Rotor And Has Captive Hook Bolts For Secruing Thethe Tooling To The Rotor End Item Identification: F101-Ge-102 Acft Eng Age | Avl | RFQ |
3C3392G01 | 4920-01-202-9688 | Special Features: Consists Of 740433 Assembly Fixture, 740434 Matrix Puller, 742885 Oil Bypass Test Block End Item Identification: F-110-Ge-100 & F118-Ge-100 Engine Fuel/Oil Cooler Series 736597 Reference Data And Literature: To 7J1-91-3 | Avl | RFQ |
3C3392G01 | 4920-01-202-9688 | Special Features: Consists Of 740433 Assembly Fixture, 740434 Matrix Puller, 742885 Oil Bypass Test Block End Item Identification: F-110-Ge-100 & F118-Ge-100 Engine Fuel/Oil Cooler Series 736597 Reference Data And Literature: To 7J1-91-3 | Avl | RFQ |
3C3408G04 | 4920-01-246-1545 | Functional Description: Performs 3 Different Tests On The Sump Area End Item Identification: F110-Ge-100 Engine Fsc Application Data: Vacuum Test Cart, 3C3154 | Avl | RFQ |
3C3531G01 | 4920-01-208-3155 | NA | Avl | RFQ |
3C3609G01 | 4920-01-254-6786 | Functional Description: Tests Lubrication Unit End Item Identification: F108-Cf-100 Engine Fsc Application Data: Electrical Accessory Test Stand P/N 3C3963g03 | Avl | RFQ |
3C3611G01 | 4920-01-254-6787 | Functional Description: Tests N1 Speed Sensor End Item Identification: F108-Cf-100 Engine Fsc Application Data: Electrical Accessory Test Stand | Avl | RFQ |
3C3612G01 | 4920-01-255-1283 | Special Features: To Name: Tool Set, Test Functional Description: Tests Main Engine Control End Item Identification: F108-Cf-100 Main Engine Control | Avl | RFQ |
3C3613G01 | 4920-01-256-1927 | Functional Description: Required To Test Main Fuel Pump End Item Identification: F108-Cf-100 Engine Support Equipment | Avl | RFQ |
3C3615G01 | 4920-01-254-6788 | NA | Avl | RFQ |
3C3621G01 | 4920-01-254-6789 | Special Features: Used To Test Oil Tank Assy Fsc Application Data: Lube Accessory Test Stand 3C3966g03 | Avl | RFQ |
3C3622G01 | 4920-01-254-6790 | Special Features: Used To Test Oil Indicator Fsc Application Data: Lube Accessory Test Stand 3C3966g03 | Avl | RFQ |
3C3623G01 | 4920-01-254-6791 | Special Features: Used To Test Turbine Clearance Valve Fsc Application Data: Fuel Accessory Test Stand 3C3970g03 | Avl | RFQ |
3C3624G01 | 4920-01-254-6792 | Special Features: Used To Test Fuel Nozzle Fsc Application Data: Fuel Accessory Test Stand 3C3970g03 | Avl | RFQ |
3C3644G02 | 4920-01-447-2870 | Special Features: Prov Tech Doc Pccn S4aayj, Serd 2225, Used With Serd 0812 P/N 3C3652g01nsn 492001-325-0174 Functional Description: Used For Seal Teeth Restoration Only, Using Thermal Spray. May Be Used To Mask Seal Teeth During Grit Blasting End Item Identification: Supports 2840-01-322-4759 Spool, Compressor Rotor Stage 1 & 2; Usable Onengines F101-Ge-102, F110-Ge-400, F118-Ge-100, F110-Ge-100 | Avl | RFQ |
3C3671G01 | 4920-01-432-2386 | NA | Avl | RFQ |
3C3687P11 | 4920-01-355-4468 | Special Features: Steel, Sae 4130-4142, Rc Hardener 38-40 | Avl | RFQ |
3C3818G01 | 4920-01-462-7882 | Special Features: 21.000 By 3.20 By 6.50 Functional Description: Used As Support Arm Which Is Attached To The Head Of The Edm Machine And Postions The Electrode Relative To The Work Piece To Edm Excessive Braze Material From Filled Honeycomb Cells End Item Identification: F118-Ge-100 Engine | Avl | RFQ |
3C3886G02 | 4920-01-564-3023 | Special Features: Next Higher Assembly Ge129c, Support Equipment, Fixture Pilot And Guidefront Frame End Item Identification: F110 Aircraft | Avl | RFQ |
3C4274G01 | 4920-01-499-5817 | Special Features: C/O Two Steel Hardened Rings Functional Description: Used To Restrain The Aft And Fwd Blade Retainers On The High Pressure Turbine Rotor End Item Identification: F110-Ge-129 Engine | Avl | RFQ |
570-4203-01 | 4920-01-345-8712 | Model Number: Jf-269A | Avl | RFQ |
570-4205-01 | 4920-01-345-8713 | Model Number: Jf-278A | Avl | RFQ |
6798767 | 4920-00-866-0411 | Special Features: C/O Pin P/N6798767-5, 6Ea;Indicator 6798767-8, 1Ea;Adapter 6798767-9, 1Ea;Ring 6798767-11, 1Ea Functional Description: Used During Low Pressure Compressor Housing Inspection End Item Identification: Tf41 Acft Engine | Avl | RFQ |
6798931 | 4920-00-111-1032 | Special Features: Company Item Name-Nozzle, Exhaust Functional Description: Directs Exhaust Gasses During Engine Test End Item Identification: Tf41 Acft Engine | Avl | RFQ |
6798958 | 4920-00-136-0020 | Special Features: Company Item Name:Kit, Pressure Test, Oil Filter Functional Description: Used During Oil Filter Pressure Test End Item Identification: Tf41 Acft Engine | Avl | RFQ |
739093 | 4920-01-202-9688 | Special Features: Consists Of 740433 Assembly Fixture, 740434 Matrix Puller, 742885 Oil Bypass Test Block End Item Identification: F-110-Ge-100 & F118-Ge-100 Engine Fuel/Oil Cooler Series 736597 Reference Data And Literature: To 7J1-91-3 | Avl | RFQ |
739093 | 4920-01-202-9688 | Special Features: Consists Of 740433 Assembly Fixture, 740434 Matrix Puller, 742885 Oil Bypass Test Block End Item Identification: F-110-Ge-100 & F118-Ge-100 Engine Fuel/Oil Cooler Series 736597 Reference Data And Literature: To 7J1-91-3 | Avl | RFQ |
8-19575-501 | 4920-01-607-0985 | Functional Description: Used While Repotting The F-16 To Align Potting Cups Only Part Name Assigned By Controlling Agency: Kit, F-16 Hold Fixtr F-16 Laser Boresight Criticality Code Justification: Ftld | Avl | RFQ |
8-19576-501 | 4920-01-589-5220 | Part Name Assigned By Controlling Agency: Boresight Adapter Kit F-16 W/O Hf, Rev:Pd00 Supply Items And Quantities: Bracket Assy Datum Line, Bracket Assy Reference Line, Bracket Assy Bulkhead, Bracket Assy Radar, Bracket Assy Inertial Nav Unit, Bracket Assy 20Mm Gun, Bracket Assy/Adapter Assy Head-Up Display, Adapter Hard Point Xmtr, Bracket Assy Right And Left Hard Point, Bracket Assy Right And Left Angle Of Attack, Adapter Assy Right And Left Attack Recieiver And Transmitter, Hardware Kit, Two Transit Cases | Avl | RFQ |
8005-897 | 4920-01-518-4449 | NA | Avl | RFQ |
8485-3-LH | 4920-01-356-9126 | Functional Description: Mounts And Secures Left Forward Side Fuselage Radome Of B1-B Aircraft During Electrical Acceptance Test Reference Data And Literature: Serd 11F79c | Avl | RFQ |
8485-3-RH | 4920-01-356-9128 | Special Features: Designed For Forward, Right Side Radome, B1-B Aircraft Functional Description: Mounts And Secures The Radome Forelectrical And Acceptance Testing Reference Data And Literature: Serd11g75c | Avl | RFQ |
8485-4 | 4920-01-356-9127 | Functional Description: Supports Left Aft Side Fuselage Radome On The B1-B For Electrical Acceptance Testing Reference Data And Literature: Serd 11F80c | Avl | RFQ |
8485-5 | 4920-01-357-7908 | Functional Description: Mounts And Secures Aft Side Fuse-Lage Radome For Performance Of Electrical Acceptance Test End Item Identification: B1-B Aircraft Reference Data And Literature: Serd No. 11Fb1c | Avl | RFQ |
856A1283G02 | 4920-01-202-3140 | Special Features: E31.000 In. Lg;25.000 In. W;25.000 In. H;C/O Forward End Group, Aft End Group, Storage Container;Sae 4130 Steel;Forward End Group Hardened To Rc 30-35;Aft End Group Hardened To 36-40;Blackoxide Coated Functional Description: Needed To Simulate Mass Properties And Approximate Geometry Of High Pressure Turbine Rotor And Also Provide Means Of Locating Compressor Rotor On Its True Rotational Axis As Described By Reference Diameter Per Rotor Print End Item Identification: B-1B Acft Age. | Avl | RFQ |
856A1283G02 | 4920-01-202-3140 | Special Features: E31.000 In. Lg;25.000 In. W;25.000 In. H;C/O Forward End Group, Aft End Group, Storage Container;Sae 4130 Steel;Forward End Group Hardened To Rc 30-35;Aft End Group Hardened To 36-40;Blackoxide Coated Functional Description: Needed To Simulate Mass Properties And Approximate Geometry Of High Pressure Turbine Rotor And Also Provide Means Of Locating Compressor Rotor On Its True Rotational Axis As Described By Reference Diameter Per Rotor Print End Item Identification: B-1B Acft Age. | Avl | RFQ |
856A1283G03 | 4920-01-219-4986 | NA | Avl | RFQ |
856A1354G01 | 4920-01-341-0123 | Special Features: The Bracket Set C/O Two Flat Plates, Mounting Hardward And A Ball-Lock Pin; Material: Tool Steel With Black Oxide Finish Functional Description: Used In Support On The Core Engine During Maintenance; Used With 856A1122g10 Reference Data And Literature: Serd No. Cfc3709 | Avl | RFQ |
856A2522G01 | 4920-01-146-4941 | Special Features: C/O Two Identical Steel Fixtures; Each C/O A Mounting Plate On Which Is Welded A V Shaped Tube With A Trunnion; Company Item Name-Adapter Assembly Trunnion; 21 In. L, 14 In. W, 8 In. H End Item Identification: Kc-135R Aircraft | Avl | RFQ |
87000594-ASTO | 4920-01-342-1747 | Specification/Standard Data: 81873-87000594-Asto Manufacturers Standard | Avl | RFQ |
901-215-039-101 | 4920-01-465-7655 | NA | Avl | RFQ |
AGE10589 | 4920-01-333-9018 | Special Features: Material: Delrin; Finish: Natural Functional Description: Used To Hold The Ram Air Turbine (Rat) Assembly P/N 752149 During Disassembly/Assembly. Used In Support Of The C-17 Acft Reference Data And Literature: Douglas Aircraft Serd No. 450171 | Avl | RFQ |
AGSE-T056-G01 | 4920-01-574-7460 | Functional Description: Used To Hold Open Left And Right Hand Thrust Reverser Cowl Halves During Removal And Installation Of Cf6-80C2l1f Aircraft Engines End Item Identification: C-5M Aircraft Part Name Assigned By Controlling Agency: Fixture Set, Thrust Reverser Hold Open | Avl | RFQ |
AGSE-T064-G01 | 4920-01-568-3761 | Special Features: Consists Of Two Thrust Reverser Adapter Tubes And Two Nacelle Hold-Open Rods Functional Description: Used To Hold Open Inboard/Outboard And Left/Right Thrust Reverser Halves And Nacelles During Cf6 Engine Change End Item Identification: C-5M Reliability Enhancements And Re-Engineering Program | Avl | RFQ |
CD45A709 | 4920-00-179-5422 | Special Features: Takes Configuration Of Two Arches; Company Item Name-Retainer Set Functional Description: Used During Tip Grinding Of The Compressor Rotor Blades End Item Identification: Tf-39 Aircraft Engine | Avl | RFQ |
G1791 | 4920-00-219-1592 | Special Features: Aluminum Functional Description: Used To Establish The Following Tolerances In The Pitch And Roll Channel Of The Csbpc: Pitch Input To Unit, Roll Input To Unit, Auxiliary Input To Unit, Pitch Input To Pitch Output, Roll Input To Roll Output End Item Identification: F-15 Acft | Avl | RFQ |
GS18264 | 4920-01-419-1236 | NA | Avl | RFQ |
GS21319-1 | 4920-01-310-2871 | Functional Description: Used As Arbors To Support The Rotors During Balance Procedures; Precision Balanced Shafts Coincide With Diameters To Match Rotors; For Maintenance Of The Crew Pack, Turbocompressor End Item Identification: Air Conditioning And Pressurization Subsystem, B-1B Acft | Avl | RFQ |
GS21795-1 | 4920-01-378-0034 | Special Features: Kit C/O Three Cement Fixtures, C/O A Locating Hub With Two Teflon Hole Plugs And Threaded Stud In Center, With Locking Ring Over It, All Stored In Wooden Box 4.750 L, 4.750 W, 3.500 In. H, Materail: Aluminum, Steel & Teflon, ; Size Of Each Fixture 1.750 Dia, By 1.620 In. L, Wght 3.500 Lbs Functional Description: Set Is Used To Position And Clamp Three Washers On 786205-3 Transducer Frame While Cement Is Curing, Also Keeps Holes In Frame Free Of Cement End Item Identification: F100-Pw-220/229 Engine Age. | Avl | RFQ |
HS9695 | 4920-01-569-9690 | Special Features: Spinner Balancing Adapter Kit End Item Identification: Used On Anti Icing Aircraft Propeller Spinner Afterbody P/N 549427 | Avl | RFQ |
IG68A810755-1005TD | 4920-01-144-4667 | Special Features: C/O Holding Fixture, Machine Tooled Beamsplitter, Illuminated Vsd Target, And Dial Gage Indicator; Company Name-Tool, Beamsplitter Optical/Mechanical Alignment; Aluminum And Steel Functional Description: Holding Fixture Supports Beamsplitter Wich Can Be With Or Without Sensor & Either The Vsd Target Or Dial Indicator; Beamsplitter Duplicates The Interface Between The Acft Panel And The Sensor. Dial Gage Is Used To Correctly Position The Combining Glass Within The The Tooled Beamsplitter. Illuminated Target Is Used To Project A Simulated Vsd Display Test Pattern To Properly Position Optical Alignment Of The Vsd Sensor. Carrying Case Provided End Item Identification: F-15 Acft | Avl | RFQ |
PWA50576 | 4920-00-883-3005 | Special Features: Slotted Receiver Block Secured With Bal-Loks End Item Identification: F100-Pw-100/200/220 Engine Reference Data And Literature: Serd No. 0294; T.O. 2J-F100-94 | Avl | RFQ |
PWA50576D | 4920-00-883-3005 | Special Features: Slotted Receiver Block Secured With Bal-Loks End Item Identification: F100-Pw-100/200/220 Engine Reference Data And Literature: Serd No. 0294; T.O. 2J-F100-94 | Avl | RFQ |
PWA50587 | 4920-00-439-6045 | Special Features: Company Item Name-Bracket End Item Identification: F100-Pw-100/200/220 Engine Reference Data And Literature: Serd No. 0167 | Avl | RFQ |
ST-7401-1 | 4920-01-319-1469 | Special Features: C/O Four Bases; Four Rams; The First Fixture Is 4.060 In. Lg; 4.060 In.W; 4.000 In. H; The Second On Is 4.240 In. Lg; 4.240 In. W; 3.000 In. H; The Third One Is 3.000 In. Lg; 3.000 In. W; 3.50 In. H; The Fourth One Is 3.000 In. Lg; 3.000 In. W; 2.75 In. H Functional Description: Used To Overhaul And Repair The Leading Edge Flap Rotary Actuators; Used In Support Of The F-16 Acft | Avl | RFQ |
ST7401 | 4920-01-319-1469 | Special Features: C/O Four Bases; Four Rams; The First Fixture Is 4.060 In. Lg; 4.060 In.W; 4.000 In. H; The Second On Is 4.240 In. Lg; 4.240 In. W; 3.000 In. H; The Third One Is 3.000 In. Lg; 3.000 In. W; 3.50 In. H; The Fourth One Is 3.000 In. Lg; 3.000 In. W; 2.75 In. H Functional Description: Used To Overhaul And Repair The Leading Edge Flap Rotary Actuators; Used In Support Of The F-16 Acft | Avl | RFQ |
ST7401-2 | 4920-01-338-4459 | Special Features: C/O 2 Bases & 2 Rams;The 2 Bases Are Machined To Support The Different Fixed Ring Gears During Stiffener & Retaining Ring Installation & Removal;The Rams Are Machined To Fit Inside The Different Fixed Ring Gears & Ensure That The Stiffeners & Retaining Rings Are Installed Flat In The Fixed Ring Gears Functional Description: Used To Overhaul & Repair The Leading Edge Flap Rotary Actuators End Item Identification: F-16 Acft | Avl | RFQ |
TN9534 | 4920-01-092-8254 | Special Features: C/O Base Plate Support Frame Assembly And Pointer Assembly; The Base Plate Provides Locating Holes To Mount A Photometer; Pointer Assembly-Rectangular Shaped Bar With Pointer Atch To One End To Point 90 Deg. Down With Respect To Bar Long Axis; Bar Is Slotted On Opposite End To Permit Length Adjustment Mating W/Base Plate Assembly End Item Identification: F-16A/B Acft Age | Avl | RFQ |
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