CHERRYMAX PROCESS MANUAL - Cherry Aerospace
CHERRY AEROSPACE SANTA ANA, CALIF. THE ACTUAL GRIP IN 1/16THS IS STAMPED ON THE HEADS OF ALL CHERRY SERRATED RIVETS GAGE NO. 269C3 OVERSIZE DIAMETER 269C3 Gage The gradations on the measuring end represent the grip of the fastener to be selected; the in-between gradations represent even grips (2, 4, 6 etc.). GRIP GAGE USE 1.
Download CHERRYMAX PROCESS MANUAL - Cherry Aerospace
Information
Domain:
Source:
Link to this page:
Please notify us if you found a problem with this document:
Advertisement
Documents from same domain
Cherry AerospACe produCts
www.cherryaerospace.comlockbolt PIns anD collaRs The Cherry Lockbolt Pins and Collars are two piece structural fasteners available in a variety of materials and configurations.
blind bolT - cherryaerospace.com
www.cherryaerospace.comperformance capabilities for metallic and composite blind fastening applications. They provide a flush, burr-free installation with no shaving required.
CHERRYMAX 'AB' RIVET - cherryaerospace.com
www.cherryaerospace.com2 CHERRYMAX 'AB' FEATURES AND INSTALLATION SEQUENCE As part of the CherryMAX® family of proven fastener systems, CherryMAX ‘AB’ Rivets are lock-spindle, flush fracturing,
FASTENING SYSTEMS FOR AEROSPACE
www.cherryaerospace.comtool configuration, go to www.cherryaerospace.com by selecting “Tooling Manuals” from the “Technical” drop down menu. Cherry Technical Services may be reached via our main number 714-545-5511; we would be happy to assist you with tool selection,
CHERRYBUCK TITANIUM SHEAR PIN - cherryaerospace.com
www.cherryaerospace.com2 CHERRYBUCK® TITANIUM SHEAR PIN STRENGTH ALLOWABLE JOINT STRENGTH — Joint allowable loads (lbs.) per MMPDS-02 criteria STRENGTH IN LBS. Fastener Type CSR924 CSR925 CSR922 Sheet Material CLAD 7075—T6 CLAD 2024—T3 CLAD …
MBC BLIND FASTENING SYSTEM - Cherry Aerospace LLC
www.cherryaerospace.comMBC® BLIND FASTENING SYSTEM INSTALLATION SEQUENCE & PERFORMANCE DATA Typical installation sequence of MBC® rivets is shown here with the Lock Creator, a three-component design providing a unique lock feature. sleeve Lock Creator anvil
CHERRY MAXIBOLT PROCESS MANUAL
www.cherryaerospace.com4 FASTENER IDENTIFICATION CHERRY PART NUMBER IDENTIFICATION CR7310 S 06 -064 D = 3/16" Nominal diameter Cherry MAXIBOLT blind bolt, .219 min.
CHERRYLOCK BLIND RIVET - Cherry Aerospace
www.cherryaerospace.comto Procurement Specification NAS1740 and Standards Pages NAS1738 and NAS1739. The bulbed CherryLOCK® rivet is a complete shear fastening system. Its features can be utilized for optimum strength and performance in both thick and thin sheets. It provides the highest possible design integrity, particularly in double dimple or high vibration areas.
CHERRY 1900 BULBING BLIND RIVET - Cherry Aerospace
www.cherryaerospace.comSleeve Material Code "C" = A-286 CRES "M" = Monel Basic Part Number CR1919 = Protruding head ... ©2009 CHERRY AEROSPACE ... 4 Lubricants may be applied to any or all components if required for performance unless prohibited by the governing specification. 5 Rivets for use with single-action (non-shifting) tooling shall be identified with a ...
CHERRYMAX
www.cherryaerospace.comMeets requirements of PS-CMR-3000. ... 1⁄8 (-4) 2X.156 664 814 995 1220 1220 285 250 345 400 360 490 570 5⁄32 (-5) 2X.187 1030 1245 1545 1865 1865 445 390 530 635 555 740 860 3⁄16 (-6) 2X.219 1480 1685 2215 2525 2525 635 560 710 890 800 1000 1160 1⁄4 (-8) 2X.281 2615 2925 3920 4390 4390 1125 1000 1260 1570 1410 1755 2030 ...
Related documents
Hi-Lok - Collar Quick Reference Guide - Monroe Aerospace
catalog.monroeaerospace.comhi-lok & collar quick reference guide hl10 hl11 hl18 hl19 hl20 hl21 hl22 hl23 hl30 hl40 hl41 hl48 hl50 hl51 hl62 hl63 hl64 hl65 hl110 hl111 hl218 hl219 hl220 hl221 hl325 hl326 hl327 hl328 hlt900 hlt912 hl70 hl75 hl77 hl79 hl82 hl84 hl86 hl87 hl90 hl93 hl94 hlt77 hl18 hl19 hl20 hl21 hl22 hl23 hl30 hl40 hl41 hl48 hl50 hl51 hl62 hl63 stud ...
AEROSPACE AMS-QQ-P-416™ REV. E MATERIAL SPECIFICATION
chemresearchco.comAvailable from Aerospace Industries Association, 1000 Wilson Boulevard, Suite 1700, Arlington, VA 22209-3928, Tel: 703-358-1000, www.aia-aerospace.org. NASM1312-1 Fastener Test Methods - Method 1, Salt Spray . NASM1312-5 Fastener Test Methods - Method 5, Stress Durability
Supplier Evaluation Checklist - Sargent Aerospace
www.sargentaerospace.comservices to Sargent Controls and Aerospace, an evaluation either by on-site audit or by the information supplied on the enclosed “Evaluation Checklist” portion must be performed. As this is a general checklist based on AS9100 (a erospace requirements), some sections ... or reference to them
Composites in Aerospace Applications - Markit
ihsmarkit.comComposites in Aerospace Applications By Adam Quilter, Head of Strength Analysis Group, IHS ESDU Introduction ... The image below, from Reference 1, shows the distribution of materials in the F18E/F aircraft. The AV-8B Harrier GR7 has composite wing sections and 2. the GR7A features a composite rear fuselage.
Aerospace Supply Chain and Manufacturing
nari.arc.nasa.govReference: Oliver Wyman Global Fleet & MRO Forecast Commentary 2019 - 2029 •In 2017, the U.S. accounted for 49% of the global aerospace industry •The future growth in aviation will be concentrated in Asia and the developing world, particularly China and India •By 2035, the Civil Aviation Administration of China projects the
Manufacturing, Reference, Supply, Chain, Aerospace, Aerospace supply chain and manufacturing
Aerospace Threaded Fastener Strength in Combined Shear …
ntrs.nasa.govreference value. NASA’s counterpart of peer-reviewed formal professional papers but has less stringent limitations on manuscript length and extent of graphic presentations. ... The strength capability of aerospace threaded fasteners is typically specified as a minimum
1.0 BASIS OF ESTIMATE (BOE) “HOW TO”
www.aia-aerospace.orgJun 02, 2016 · UNCLASSIFIED JSCC BOE Guidebook Section XXXXX A-1 UNCLASSIFIED 1.0 BASIS OF ESTIMATE (BOE) “HOW TO” 1.1 Definition A Basis of Estimate (BOE) is a document that identifies the logic, data, methodology and calculations used to estimate the resources required to perform a specific task or group of related
Airfoils - Michigan State University
www.egr.msu.eduME 440 Aerospace Engineering Fundamentals Fall 2006 3 Pitching Moment Coefficient: V Sc 2 1 m c 2 m ρ = where m: pitching moment (will depend on the moment reference center) c: chord length Center of Pressure: The moment reference center for which the moment is zero. Depends on the angle of attack.
AEROSPACE PART AND MATERIAL CROSS-REFERENCE
www.fst.comAEROSPACE PART NUMBER CROSS-REFERENCE Industry Standard Part Number Freudenberg Sealing Technologies Part Number Material Specification MS9387-YY Inquire, some parts are tight tolerance V75 AMS-R-83248, MIL-R-83248, or M83248/1 (superseded by AS83248/1) AS9966-YY* Inquire, parts over 0.500" ID are tight tolerance F273 AMS7273