QR Structural Panel Fasteners

Transcription

1 QR Structural Panel Fasteners The QR Strucutral Panel Fastener qualifies to MIL-F and meets MS17731 and MS The QR fastening system is lightweight, has a small envelope and is fast operating. Most versions lock and unlock in less than two turns. Positive stud retention is featured. Flush or protruding head styles and various recess configurations are available. Optional stud hold-out grommet is available which provides bottom flush condition. Receptacle provides.020 inch minimum radial float. There are other QR Panel Fastener styles and types which are not featured in this catalog; contact for details. Typical QR Fastening System: Stud assembly is retained in retracted position by sprint-loaded grommet and retaining ring. The QR Fastening System has a high-strength-to-weight ratio. Quick operating, it locks and unlocks in less than two turns. Optional stud hold-out grommet is available which provides bottom flush condition. Stud assembly is automatically ejeted free from sub-structure during unlocking cycle. Tridair Products 64

2 QR MS Version Retaining Ring Standard Version FX Material: 18-8 Type 300 Series CRES per AMS 7245 or QQ-W-423. Heat Treat: Stressed relieved. Finish: Passivated per QQ-P-35. Weight:.033 lbs./100, approximate. Installation Tool for FX Retaining Ring: FX T To Install FX Retaining Ring: 1. Slide retaining ring onto mandrel (Figures A and B). 2. Slide handle onto mandrel (Figure C). 3. Place anvil on top side of panel to brace stud assembly. Material: Alloy Steel Finish: Black Oxide per MIL-C Align tool assembly onto stud assembly and push on handle until retaining ring is captivated to the stud assembly (Figures D and E). 5. Remove tool. Retaining Ring Oversize Version. FX Material: 17-7Ph CRES per AMS Heat Treat: Rc Finish: Passivated per QQ-P-35. Weight:.043 lbs./100, approximate. Notes: 1. Ring is designed to be used when hole in substructure is.391 or greater. See hole preparation on Page FX retaining ring is hand installed. Tridair Products 65

3 QR Standard Version Stud Assemblies Flush Head Style. FX ( )( ) Series Protruding Head Style. FX ( )( ) Series Material: Screw: 8740 Alloy Steel per MIL-S Grommet: 4140 Alloy Steel per MIL-S Spring: 17-7PH CRES per AMS Basic A B Grip Range Weight Stud Assembly Ref. Ref. lbs./ea. Part No. M in. Max. FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) Basic A B Grip Range Weight Stud Assembly Ref. Ref. lbs./ea. Part No. M in. Max. FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) FX ( ) Notes: 1. Anti-seize compound per MIL-A-907 applied to thread. 2. For retaining ring information see Page 65. Heat Treat: Screw and Grommet: 160 K.S.I. minimum ultimate tensile strength per MIL-H Spring: Condition CH900 per MIL-H Finish: Screw and Grommet: Cadmium Plated per QQ-P-416, Type II, Class 3. Spring: Passivated per QQ-P-35. Specifications: See Page 2. How to Order: FX P Recess options: p = recess per MS9006, No. 10 size TS = recess per NAS1078, No. 10 size Grip range: (see stud part number selection Page 8 for grip range requirements) FX =.361 to.430 FX =.326 to.395 Head style: FX = Flush head style FX = Protruding head style Tridair Products 66

4 QR Standard Version Stud Assembly Fully Retractable Flush Head Style. FX ( )P Series Receptacle Assemblies FX ( ) Series FX ( ) Series Stud Assembly Part No. A Ref. B Ref. Grip Range M in. Max. Weight lbs./ea. FX P FX P FX P FX P FX P Locking Feature High** Prevailing Torque Eliptical Part No. FX A* Ref. None FX FX FX None FX FX Lubricant Coating Per MIL-L Per MIL-A-907 Material: Screw: 8740 Alloy Steel per MIL-S Grommet: 4140 Alloy Steel per MIL-S Heat Treat: Screw and Grommet: 160 K.S.I. minimum ultimate tensile strength per MIL-H Finish: Screw and Grommet: Cadmium Plated per QQ-P-416, Type II, Class 3. Specifications: See Page 2. Notes: 1. Use with FX hold-out grommet (see Page 6) to provide flush condition on bottom side of panel in retracted position, and with FX ( ) Series or FX ( ) Series receptacle. Retaining ring is not required. 2. Anti-seize compound per MIL-A-907 applied to thread. 3. For stud part number selection see Page For other head styles and recesses, contact Fairchild Fasteners. * A dimension, when.03 or.08, provides extra jackout to allow stud hold-out spring to engage panel. **Locking feature maintains 5 inch pounds minimum running torqueout after 200 complete cycles. Material: Receptacle: 1050 Steel per ASI C1050. Nut: 8740 Alloy Steel per MIL-S Insert: 4140 Alloy Steel per MIL-S Heat Treat: Receptacle: Ftu 150 K.S.I. minimum per MIL-H Nut: Ftu 180 K.S.I. minimum per MIL-H Insert: Ftu 160 K.S.I. minimum MIL-H Finish: Receptacle, Nut, and Insert: Cadmium Plated per QQ-P- 416, Type II, Class 3. Weight:.016 lbs. each, approximate. Tridair Products 67

5 QR Structural Panel Fasteners Hold-Out Grommet FX ( ) Series Material: Grommet: 18-8 Type 300 Series CRES per ASTM-A-582. Spring: 17-7PH CRES per AMS D escription Part No. Heat Treat: Grommet: None. Spring: Condition CH900. Finish: Grommet and Spring: Passivated per QQ-P-35. A Theo. Sharp D Dia. E Ref. G Ref. Notes: 1. Use grommet with FX ( )P Series stud assembly and FX Series or FX Series receptacles. 2. First and second oversize styles are designed to provide greater strength or replacement of basic style due to panel damage. 3. See Page 71 for hole preparation and installation information. Flaring Tool Installation Tools (see below) Back-up Tool Stud Installation Tool Basic FX Max. Ref. FX FX T10 FX T12 1st Oversize FX Max. Ref. FX FX T13 FX T14 FX T11 2nd Oversize Flaring Tool FX T( ) Series FX Max. Ref. FX FX T15 FX T16 Back-Up Tool FX T( ) Series Material: Tool Steel Heat Treat: Rc45 min. per MIL-H-6875 Finish: Black Oxide per MIL-C Stud Assembly Installation Tool FX T11 Used to install FX ( )P Series stud assembly into FX ( ) grommet assembly. Part No. FX T10 FX T13 FX T15 A Dia Material: Tool Steel Heat Treat: Rc45 min. per MIL-H-6875 Finish: Black Oxide per MIL-C Part No. FX T12 FX T14 FX T16 A Dia. Ref Material: Tool Steel Heat Treat: Rc45 min. per MIL-H-6875 Finish: Black Oxide per MIL-C Tridair Products 68

6 QR Structural Panel Fasteners Panel/Substructure Preparation and Installation Data. Flush Head Styles. Protruding Head Styles. A pplication A Dia. B Dia. Basic Installation When curvature of panel is 18 inches or less* *Subject to approval of structures group Retaining Ring Part No. FX Notes: 1. Locate and drill A diameter hole through panel and substructure Countersink panel 99 to.530 diameter FX Counterbore to B diameter backside of panel or frontside of substructure to.035 deep. Location is.030 optional when T 1 =.125 or greater. Otherwise counterbore substructure (panel is preferred location). Notes: 1. Refer to table at left. 2. Locate and drill A diameter hole through panel and substructure. 3. Counterbore to B diameter backside of panel or.035 frontside of substructure to.030 deep. Location is optional when T1 =.065 or greater. Otherwise counterbore substructure (Panel is preferred location). 4. Locate, drill and countersink two holes for rivets (not supplied). 5. Shim is required when total thickness ( T 1 + T 2 plus any compressed gasketing material, paint or other finishes) equals.155 or less. Contact for details. 4. Locate, drill and countersink two holes for rivets (not supplied). 5. Shim is required when total thickness ( T 1 + T 2 plus any compressed gasketing material, paint or other finishes) equals.155 or less. Contact for details. Basic Installation. Notes: 1. Place stud assembly into panel. 2. Install retaining ring (see Page 3). 3. Rivet receptacle in place. Tridair Products 69

7 QR Structural Panel Fasteners Panel/Substrucutre Preparation and Installation Data (cont d.). Grommet FX ( )P Series. Grommet Assembly Part No. Ref. T 1 Panel Thicknes s H J K FX FX FX FX FX FX Notes: 1. Select grommet dash number to panel T1 thickness. 2. Locate and drill H diameter hole through panel Countersink top of panel 99 to J diameter Counersink bottom of panel 99 to K depth Locate and drill diameter hole through substructure Locate and drill two holes for rivets (not supplied). Stud Assembly and Grommet Assembly Installation 6. Rivet receptacle in place. 7. Installation is complete. Notes: 1. Place correct size grommet assembly in panel. 2. Place correct size flaring tool and back-up tool in place and apply sufficient pressure to flare grommet. Stud Part Number Selection 3. Insert pilot of stud installation tool into thread end of stud assembly. 4. Push tool and stud assembly through grommet until stud is captivated by hold-out spring. 5. Remove tool. Notes: 1. Determine grip range thickness. Note: Grip range thickness equals T1 + T2 plus the compressed thickness of any gasket (if used). Also allow for paint or other finish thickness. 2. Refer to appropriate table for stud type and style (see Pages 2, 4 or 5). 3. Locate grip range in table and find the corresponding part no. Tridair Products 70

8 QR Structural Panel Fasteners Panel/Substrucutre Preparation and Installation Data (cont d.). Grommet FX ( )P Series. Grommet Assembly Part No. Ref. T 1 Panel Thicknes s H J K FX FX FX FX FX FX Notes: 1. Select grommet dash number to panel T 1 thickness. 2. Locate and drill H diameter hole through panel Countersink top of panel 99 to J diameter Counersink bottom of panel 99 to K depth Locate and drill diameter hole through substructure Locate and drill two holes for rivets (not supplied). Stud Assembly and Grommet Assembly Installation 6. Rivet receptacle in place. 7. Installation is complete. Notes: 1. Place correct size gromet assembly in panel. 2. Place correct size flaring tool and back-up tool in place and apply sufficient pressure to flare grommet. Stud Part Number Selection 3. Insert pilot of stud installation tool into thread end of stud assembly. 4. Push tool and stud assembly through grommet until stud is captivated by hold-out spring. 5. Remove tool. Notes: 1. Determine grip range thickness. Note: Grip range thickness equals T 1 + T 2 plus the compressed thickness of any gasket (if used). Also allow for paint or other finish thickness. 2. Refer to appropriate table for stud type and style (see Pages 2, 4 or 5). 3. Locate grip range on stud assembly drawing and find the corresponding part dash no. Tridair Products 71

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10 DASH A B GRIP RANGE M IN. MAX. WEIGHT LBS/EA -1[ ] [ ] [ ] [ ] [ ] [ ] [ ] [ ] [ ] /18/80 ECO E JWN REVISION R REDRAW N DRAWING BY LTWH TITLE SCREW ASSY, QR A PPROVED BY: UNLESS OFHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX SHEET 1 OF 2 Tridair Products 73

11 INSTALLATION PANEL PREPARATION HOLD-OUT POSITION NOTES: 1. MATERIAL: 1.1 SCREW: 8740 ALLOY STEEL PER MIL-S GROMMET: 4140 ALLOY STEEL PER MIL-S SPRING: 17-7 PH CRES PER AMS HEAT TREAT: 2.1 SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER MIL-H SPRING: CONDITION CH900 PER MIL-H FINISH: 3.1 SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS SPRING: PASSIVATE PER QQ-P DIAMETER HOLE IN T2 MAY BE ENLARGED TO.390 DIAMETER (MAXIMUM) TO ALLOW FOR HOLE MISALIGNMENT. 5. RECESS OPTIONS AND CALLOUTS: 5.1 MS9006 RECESS: ADD P AFTER DASH. EXAMBLE: FX P 5.2 NAS1078 RECESS: ADD TS AFTER DASH. EXAMPLE: FX TS. 6. ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD. DRAWING BY JWH TITLE SCREW ASSY, QR AND FUNTION DATA. DO NOT A PPROVED BY: UNLESS OFTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX /18/86 ECO E JWH REVISION D REDRAW N SHEET 2 OF 2 Tridair Products 74

12 DASH A B GRIP RANGE M IN. MAX. WEIGHT LBS/EA -1[ ] [ ] [ ] [ ] [ ] [ ] [ ] /18/86 ECO E JWH AND FUNTION DATA. DO NOT DRAWING BY JWH TITLE SCREW ASSY, -8[ ] [ ] [ ] [ ] QR A PPROVED BY: UNLESS OTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX SHEET REVISION G REDRAW N 1 OF 2 Tridair Products 75

13 INSTALLATION PANEL PREPARATION HOLD-OUT POSITION NOTES: 1. MATERIAL: 1.1 SCREW: 8740 ALLOY STEEL PER MIL-S GROMMET: 4140 ALLOY STEEL PER MIL-S SPRING: 17-7 PH CRES PER AMS HEAT TREAT: 2.1 SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER MIL-H SPRING: CONDITION CH900 PER MIL-H FINISH: 3.1 SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS SPRING: PASSIVATE PER QQ-P USE WITH FX OR FX RECEPTACLE AND FX RETAINING RING DIAMETER HOLE IN T2 MAY BE ENLARGED TO.390 DIAMETER (MAXIMUM) TO ALLOW FOR HOLE MISALIGNMENT. 6. RECESS OPTIONS AND CALLOUTS: 6.1 MS9006 RECESS: ADD P AFTER DASH. EXAMBLE: FX P. 6.2 NAS1078 RECESS: ADD TS AFTER DASH. EXAMPLE: FX TS. 7. ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD ECO H JWH REVISION G REDRAW N DRAWING BY JWH TITLE SCREW ASSY, QR A PPROVED BY: UNLESS OTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX SHEET 2 OF 2 Tridair Products 76

14 DASH A B GRIP RANGE M IN. MAX. WEIGHT LBS/EA -1P OMJ 11/18/86 ECO AND FUNTION DATA. DO NOT DRAWING BY JWH TITLE SCREW ASSY, QR -2P P P P A PPROVED BY: UNLESS OTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX []P SHEET E JWH REVISION D REDRAW N 1 OF 2 Tridair Products 77

15 NOTES: 1. MATERIAL: 1.1 SCREW: 8740 ALLOY STEEL PER MIL-S GROMMET: 4140 ALLOY STEEL PER MIL-S HEAT TREAT: 2.1 SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER MIL-H FINISH: 3.1 SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS USE WITH FX OR CA17064 HOLD-OUT GROMMET TO PROVIDE FLUSH CONDITION ON BOTTOM SIDE OF PANEL IN RETRACTED POSITION, AND FX RECEPTACLE. SEE GROMMET DRAWING FOR PANEL PREPARATION AND INSTALLATION. 5. AN FX T11 INSTALLATION TOOL MUST BE USED TO INSTALL SCREW ASSEMBLY INTO FX GROMMET. 6. ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD. JWH E DRAWING BY JWH TITLE SCREW ASSY, QR AND FUNTION DATA. DO NOT A PPROVED BY: UNLESS OTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX []P REVISION D REDRAW N 2937 SHEET 2 OF 2 Tridair Products 78

16 NOTES: 1. MATERIAL: 1.1 RECEPTACLE: 1050 STEEL PER AISI C1050 OR AMS NUT: 4140 OR 8740 ALLOY STEEL PER MIL-S-5626 OR MIL-S INSERT: 4140 ALLOY STEEL PER MIL-S HEAT TREAT: 2.1 RECEPTACLE: FTU 150ksi MINIMUM PER MIL-H NUT: FTU 180 KSI MINIMUM PER MIL-H INSERT: FTU 160 KSI MINIMUM PER MIL-H FINISH: 3.1 RECEPTACLE, NUT AND INSERT: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS TO BE USED WITH FX AND FX SERIES, 4 LEAD SCREW ASSEMBLIES. 5. SHIMS FOR THIS RECEPTACLE: SEE FX DRAWING. 6. RECEPTACLE MAINTAINS 5 IN-LBS (MINIMUM) RUNNING TORQUE-OUT AFTER 200 COMPLETE CYCLES. S43022 UNLESS OTHERWISE SPECIFIED TOLERANCE:.XX =.±.02. XXX =.010 ANGLE = ±2 SURFACE FINISH: 125 MICROINCHES APPROVED DATE 31 MAR 80 REV LETTER AND DATE J 16 OCT 92 ECN AEROSPACE FASTENER DIVISION ENGINEERING R&D CENTER I CIVIC PLAZA, SUITE 500 CARSON, CA Q.R. RECEPTACLE ASSEMBLY UNF-3B, 4 LEAD CAGE CODE FX E CN SHEET 1 OF 1 Tridair Products 79

17 NOTES: 1. MATERIAL: 1.1 RECEPTACLE: 1050 STEEL PER AISI C1050 OR AMS NUT: 4140 OR 8740 ALLOY STEEL PER MIL-S-5626 OR MIL-S INSERT: 4140 ALLOY STEEL PER MIL-S HEAT TREAT: 2.1 RECEPTACLE: FTU 150 KSI MINIMUM PER MIL-H NUT: FTU 180 KSI MINIMUM PER MIL-H INSERT: FTU 160 KSI MINIMUM PER MIL-H FINISH: 3.1 RECEPTACLE, NUT AND INSERT: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS TO BE USED WITH FX AND FX SERIES, 4 LEAD SCREW ASSEMBLIES. 5. SHIMS FOR THIS RECEPTACLE: SEE FX DRAWING. S43023 UNLESS OTHERWISE SPECIFIED TOLERANCE:.XX =.±.02. XXX =. ±..010 ANGLE = ±2 SURFACE FINISH: 125 MICROINCHES APPROVED DATE 19 MAR 80 REV LETTER AND DATE T 16 OCT 92 ECN AEROSPACE FASTENER DIVISION ENGINEERING R&D CENTER I CIVIC PLAZA, SUITE 500 CARSON, CA Q.R. RECEPTACLE ASSEMBLY UNF-3B, 4 LEAD CAGE CODE FX E CN SHEET 1 OF 1 Tridair Products 80

18 NOTES: 1. THIS RING DESIGNED FOR USE ON FX SERIES SCREW ASSEMBLIES AND CA1797 TYPE STUD NUTS. 2. INSTALLATION TOOL: A.) USE FX T TO INSTALL RINGS ON FX SERIES SCREW ASSEMBLYS. B.) USE CA1797-T10 TO INSTALL RINGS ON CA1795-( ) AND CA17036-( ) STUD NUTS. 3. PANEL PREPARATION DATA: A.) RETAINING RING RECESS: C BORE.531 DIA X DEEP. B.) MAX SUBSTRUCTURE HOLE:.390 DIA. 4. MATERIAL: 18-8 TYPE 300 SERIES CRES, PER MIL-S-5059 AND/OR QQ-S-766 (CHEMISTRY ONLY). 5. HEAT TREAT: STRESS RELIEVE. 6. FINISH: PASSIVATED PER QQ-P WEIGHT:.312 LBS/1000 PIECES (APPROXIMATE). UNLESS OTHERWISE SPECIFIED TOLERANCE: DECIMALS. XX =.±.02 XXX =.010 ANGLE = ±2 SURFACE FINISH: 125 MICROINCHES APPROVED DATE 29 MAY 73 REV LETTER AND DATE AEROSPACE FASTENER DIVISION ENGINEERING R&D CENTER I CIVIC PLAZA, SUITE 500 CARSON, CA TRIDAIR PRODUCT S42840 T 27 JUL 93 RETAINING RING FX ECN OR FASTENER E CN SHEET 1 OF 1 Tridair Products 81

19 FEDERAL SUPPLY C ODE W EIGHT : 23 LB/E A. E S CAL 3000 W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90505, PHONES: SHEET 1 OF 1 MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS. XXX ±.01 0 ANGLES ± FX T PER MIL-C-13924, CL I. TOLERANCES: DECIMALS:. XX ±.01 5 BLACK OXIDE APP'D FJ C FINISH: H EAT TREAT: ENG N 10/25/6 8 U NLESS OTHERWISE SPECIFIED E NG N E.E. 10/9/6 8 INSTALLATION TOOL - RETAINING RING - AND FUNCTION DATA. DO NOT M ATERIAL OR NAME SPECIFICATIO N ALLOY STEEL F F E REDRAWN. DATE HE V CHANG E FX T Tridair Products 82

20 DATE REV CHANGE F REVISED & REDRAWN G CORRECTED TOLERANCE S AND FUNCTION DATA. DO NOT FX G Tridair Products 83 NOTES: 1. TO BE USED WITH FX , FX , FX FX SCREW ASSEMBLIES. 2. C BORE DIA. x.031 DEEP IN OUTER PANEL, OR INNER STRUCTURE FOR RETAINING RING RECESS. TOLERANCES: DECIMALS:. XX ±.010. XXX ±.005 ANGLES ± 1 UNLESS OTHERWISE SPECIFIED FINISH: PASSIVATED PER QQ-P-35 HEAT TREAT: Rc PH CRES AMS 5528 MATERIAL OR NAME ENGN ENGN APP'D SPECIFICATIO N RETAINING RING FX FEDERAL SUPPLY MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS C ODE WEIGHT :. 043 LBS/100 SCALE: 4: W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90908, PHONES: SHEET 1 OF 1

21 DATE REV A B C CHANGE D ECO E ECO F ECO AND FUNCTION DATA. DO NOT FX NOTES: 1. SELECT DASH NO. ACCORDING TO PANEL THICKNESS T 2. USE FX T11 TOOL TO INSTALL STUD IN GROMMET AS SHOWN ON SHT 2 3. SEE SHT 2 FOR GROMMET & PANEL PREPARATION DIMENSIONS. Tridair Products 84 UNLESS OTHERWISE SPECIFIED TOLERANCES: DECIMALS:. XX ±.015. XXX ±.010 ANGLES ± 1 FINISH: PASSIVATED PER QQ-P HEAT TREAT: SPRING: COND CN900 GROMMET TYPE 300 SERIES CRES ASTM-A-582 ENGN ENGN APP'D FJC SPRING PN CRES AMS56T5 MATERIAL OR NAME GROMMET ASSY STUD HOLD-OUT SPECIFICATIO N FX FEDERAL SUPPLY MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS C ODE W EIGHT : SCALE: 4: W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90908, PHONES: SHEET 1 OF 2

22 DATE REV CHANGE SEE SHEET 1 FX F Tridair Products 85 S IZE PART NO. A THEO SHARP B MIN DIA GROMMET DIMENSIONS C C' SMALL DIA D GROM DIA E HOLLST. (REF) F GROMMET LENGTH G GROMMET LENGTH T PANEL THIC PANEL AREA H HOLE SIZE J C' SINC DIA K C'SMIL DEPTH L FLARING TOOL INSTALLATION TOOLS M STUD INST. TOOL N BACK-UP TOOL BASIC 1ST OVERSIZE 2ND OVERSIZE FX FX FX FX FX FX FX T10 FX T11 FX T12 FX T19 FX T11 FX T14 FX T15 FX T11 FX T16 UNLESS OTHERWISE SPECIFIED TOLERANCES: DECIMALS:. XX ±.015. XXX ±.010 ANGLES ± F INISH: HEAT TREAT: AND FUNCTION DATA. DO NOT ENGN ENGN APP'D FJC MATERIAL OR NAME GROMMET ASSY STUD HOLD-OUT SPECIFICATIO N FX FEDERAL SUPPLY MFR'S OF NEWTON INSERTS AND CALFAX FASTENERS C ODE W EIGHT : SCALE: 4: W. LOMITA BLVD., TORRANCE, CALIFORNIA, 90908, PHONES: SHEET 2 OF 2

23 NOTES: 1. MATERIAL: TOOL STEEL, AISI TYPE HEAT TREAT: Rc 45 MINIMUM PER MIL-H FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I. 4. THIS TOOL IS TO BE USED WITH A FX T12 BACK-UP TOOL TO INSTALL FX AND FX GROMMET. 5. TOOL SHALL HAVE PART ETCHED OR STAMPED IN AREA SHOWN. AND FUNTION DATA. DO NOT REVISION D RAWING BY TITLE FLARING TOOL A PPROVED BY: UNLESS OFTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS.XX = MICROINCHES PROJECT. XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX T10 SHEET 1 OF 1 Tridair Products 86

24 FX [ ] SCREW ASSEMBLY (REF.) FX [ ] GROMMET ASSEMBLY (REF.) FX T11 TOOL (REF.) NOTE: INSERT TOOL AND SCREW ASSEMBLY AS SHOWN THROUGH TOP SIDE OF GROMMET. NOTES: 1. MATERIAL: TOOL STEEL. 2. HEAT TREAT: Rc 45 MINIMUM PER MIL-H LTWH FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS TOOL SHALL HAVE DASH, (-T11) ETCHED OR STAMPED ON DIA. AND FUNTION DATA. DO NOT DRAWING BY RSR APPROVED BY RLW TITLE INSTALLATION TOOL SCREW ASSY. A PPROVED BY: UNLESS OFTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX T11 SHEET ELO# 6156 REVISION A 1 OF 1 Tridair Products 87

25 NOTES: 1. MATERIAL: TOOL STEEL. 2. HEAT TREAT: Rc PER MIL-H JWT FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I. 4. THIS TOOL IS TO BE USED WITH A FX T10 FLARE TOOL TO INSTALL FX AND FX GROMMETS. 5. TOOL SHALL HAVE PART ETCHED OR STAMPED IN AREA SHOWN. DRAWING BY RSR APPROVED BY RLW TITLE TOOL, BACKUP AND FUNTION DATA. DO NOT A PPROVED BY: UNLESS OTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX T12 SHEET ECO# 7924 REVISION A JW H B 1 OF 1 Tridair Products 88

26 NOTES: 1. MATERIAL: TOOL STEEL. 2. HEAT TREAT: Rc 45 MINIMUM PER MIL-H FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I. 4. THIS TOOL IS TO BE USED WITH A FX T14 BACK-UP TOOL TO INSTALL FX AND FX GROMMETS 5. TOOL SHALL HAVE PART ETCHED OR STAMPED IN AREA SHOWN. AND FUNTION DATA. DO NOT REVISION A JW H D RAWING BY APPROVED BY RLW TITLE FLARING TOOL A PPROVED BY: UNLESS OFTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX T13 SHEET 1 OF 1 Tridair Products 89

27 NOTES: 1. MATERIAL: TOOL STEEL. 2. HEAT TREAT: Rc 45 PER MIL-H FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I. 4. THIS TOOL IS TO BE USED WITH A FX T16 BACKUP TOOL TO INSTALL FX AND FX GROMMET. 5. TOOL SHALL HAVE PART ETCHED OR STAMPED IN AREA SHOWN. AND FUNTION DATA. DO NOT REVISION A JW H D RAWING BY APPROVED BY RLW TITLE FLARING TOOL A PPROVED BY: UNLESS OFTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 ANGLES = 2 FSC: West Lomit Boulevard Torrance, CA USA FX T15 SHEET 1 OF 1 Tridair Products 90

28 NOTES: 1. MATERIAL: TOOL STEEL. 2. HEAT TREAT: Rc 45 MINIMUM PER MIL-H FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I. 4. THIS TOOL IS TO BE USED WITH A FX T16 BACK-UP TO INSTALL FX AND FX GROMMETS. 5. TOOL SHALL HAVE PART ETCHED OR STAMPED IN AREA SHOWN. AND FUNTION DATA. DO NOT REVISION A JW H D RAWING BY APPROVED BY MSC TITLE TOOL, BACK-UP APPROVED BY: UNLESS OFTHER RANGE SPECIFIE D RLW TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX =.020 FSC: ANGLES = West Lomit Boulevard Torrance, CA USA FX T15 SHEET 1 OF 1 Tridair Products 91

29 NOTES: 1. MATERIAL: TOOL STEEL. 2. HEAT TREAT: Rc PER MIL-H FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I. 4. THIS TOOL IS TO BE USED WITH A FX T15 FLARE TOOL TO INSTALL FX AND FX GROMMETS. 5. TOOL SHALL HAVE PART ETCHED OR STAMPED IN AREA SHOWN. AND FUNTION DATA. DO NOT REVISION A JW H DRAWING BY RSR APPROVED BY RLW TITLE TOOL, BACK-UP A PPROVED BY: UNLESS OFTHER RANGE SPECIFIE D TOLERANCES MILLIMETERS SURFACE FINISH DECIMALS XX = MICROINCHES PROJECT XXX = ANGLES + = 2 FSC: West Lomit Boulevard Torrance, CA USA FX T16 SHEET 1 OF 1 Tridair Products 92