INSTALLATION ASSEMBLY - CIRRUS SR22 GLICZ

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REVISION HISTORY REV DESCRIPTION DATE APPROVED INMAL RELEASE SEE BELOW PROPRIETARY NOTCE INFORMATON DISCLOSED HEREIN IS THE PROPERTY OF CIES INCORPORATED. IT IS FURNISHED FOR EVALUATION PURPOSES ONLY AND SHALL NOT BE DISCLOSED OR USED FOR ANY OTHER PURPOSES EXCEPT AS SPECIFIED BY CONTRACT BETWEEN THE RECIPIENTAND CIES INCORPORATED. DUPUCATION OF ANY PORTON OF THIS DOCUMENT SHALL INCLUDE THIS A ALL SHTS: UPDATED NOTES AND PROCEDURES. L/212020 DRAWN: A FACKRELL CHECKED: S PHILIBEN APPROVED: S PHILIBEN B ALL SHTS: UPDATED BOM TO CURRENT HARDWARE. L/201202r CHECKED: (Uñl* qäilfl S PHILIBEN A FACKRELL CONTRACT NO. 1375 SE WILSON AVE. SUITE 150 BEND, OR977O2 rNc APPROVALS DATE DO NOT SCALE DRAWING ANGLES +.5' DECIMALS .x+.10 .n+.03 .)oo(*.010 UNLE55 OTTIERWISE SPECIFIED DIMENSIONS ARE IN INCHES. TOLERANCES ARE: DRAWN A FACKRFI I Bl28l20L9 THIRD ANGLE PROJECNON ]HECKED I CROGAN r2l5t20t9 ENGINEER C PI.{TI TRFN Lztst20t9 INSTALLATION ASSEMBLY - CIRRUS SR22 GLICZ T]TLE \PPROVED ì PHTITBFN L2l5l20L9 SIZE B 1 APPROVED IAN * O 1 1 3 4 B B A A 1 2 3 4 1 3 4 B B DWG NO. ISH IREV. cc284033001s I 2t B NOTES: REFER TO CIRRUS AIRPLANE MAINTENANCE MANUAL, CHAPTER 51-20 FOR SPECIFICATION ON SURFACE PREPARATON AND BONDING PROCESS. INSTRUCTIONS HERE ARE SUPPLEMENTAL. 1) DRAIN FUEL FROM THETANK(S), 2) REMOVE THE MOST INBD AND THE OUTBD FUEL TANK ACCESS PANELS. 3) LOCATE SENDER HOLE AND NUTRING FASTENER HOLES FOR THE INBD FUEL SENDER. COVER THE INSIDE OF THE FUEL TANK WITH PROTECTIVE PANELS OR CARDBOARD. (sEE SH. B rMAGE 1&2). 5) REMOVE SEAI.ANT FROM THE WING RIB ON THE TANK SIDE AROUND THE NUTRTNG LOCAÏON. 6) ABRADE RIB SURFACE WITH BO TO 120 GRIT SANDPAPER TO REMOVE THE SURFACE SHEEN AND EVEN THE SURFACE. NOTE: DO NOT CUT THROUGH REINFORCEMENT FIBERS, ONLY THE SURFACE RESIN. 7) ABRADE SURFACE OF NUTRING WITH 80 TO 120 GRIT SANDPAPER TO REMOVE THE SURFACE SHEEN. LL ADAPTER PLATE HOLES PER THE TEMPLATE AND CLEAN HOLE EDGES. MOUNT THE ADAPTER PI.ATE. (SEE SH 8 IMAGE 3). 9) APPLY RELEASE AGENT TO ALL BOLTS TO PREVENT THEIR ACCIDENTAL BONDING. ARRANGE BOLTS AND SPRINGS CONTROLLING BOND GAP COMPRESSION TO MAKE AVAILABLE FOR BONDED ASSEMBLY. 10) WEAR PROTECTVE GLOVES. WIPE THE RIB SURFACE ABRADED FOR BONDING IN STEP 6 WITH ISOPROPYL ALCOHOL AND A LINT-FREE CLOTH TO REMOVE COMPLETELY SANDING oR RESrN POWDER. (SEE SH. B IMAGE 4) 12) WIPE NUTRING SURFACE ABRADED FOR BONDING IN STEP 7 WITH ISOPROPYL ALCOHOL TILL CLEAN AND VERIFY SURFACE PREPARATON WITH WATER BREAKTEST. SETASIDE PROTECTED FROM DUST. 13) APPLY CLICKBOND OR EQ ADHESIVE TO WING RIB SURFACE AND NUTRING SURFACE. N NUTRING AND ATTACH WITH BOLTS AND SPRINGS (SUPPLIED). ENSURE BOLTS ARE PROÏECTED WITH RELEASE AGENT. (SEE SH. 5) 15) ALLOW ASSEMBLY TO CURE FOR 8 HOURS IN ROOM TEMPERATURE. 16) LIGHTY ABRADE THE OUTER SURFACE OF THE GASKET TO INSURE TIGHT FIT. 17) CLEAN THE GASKET SURFACE WITH ISOPROPYL ALCOHOL. /Ta\PLAcT THE GASKET UNDER THE SENDER AND BOLT THE FUEL SENDER TO THE NUTRING WITH SUPPLIED FASTENERS. APPLY MIL-S-46163 TYPE II TYPE N MEDIUM THREADLoCKER. - oPERATE THE ARM TO ENSURE rT HAS UNRESTRTCTED MOVEMENT TNSTDE THE TANK. TORQUE BOLTS 20 TO 25 IN-LBS. (SEE SH. 6) 19) RE-SEAL AND INSTALL THE INBD FUEL TANK ACCESS PANELS. IN ACCORDANCE WITH CIRRUS MAINTENANCE MANUAL. THE OUTBD FUEL SENDER AND REMOVE THE SENDER SUPPORT BRACKET FROM THE WTNG. (SEE SH. 8 IMAGE 6). THE GASKET UNDER THE SENDER AND BOLT THE OUTBD FUEL SENDER WITH SUPPLIED FASTENERS. APPLY MIL-S-46163 TYPE II TYPE N MEDIUM THREADLOCKER. OPERATE THE ARM TO ENSURE TT HAS UNRESTRICTED MOVEMENT INSIDE THE TANK. TORQUE TO 20 TO 25 IN-LBS. 22) CONNECT THE SENDER ELECTRICAL CONNECTORS AND VERIFY THAT BOTH SENDERS CONTRIBUTE TO A FREQUENCY OUTPUT (INBD BLUE WIRE) MEASURED WITH A DIGÏTAL MULTIMETER. 23) RESEAL AND INSTALL THE OUTBD FUEL TANK ACCESS PANELS IN ACCORDANCE WITH CIRRUS MAINTENANCE MANUAL. ü ü r{.i"B-l e)}-¡-Ë D ÜÜPY A A 1 2 3 4 1 3 4 B B DWG NO, cc284033001s SH 3 IREV. IB A WING FUEL RIB TANK 35 1 E SEAL 09-05509 34 E49396 EPOXY STRUCTUAL ADHESIVE HYSOL 33 E49395 EPOXY ADHESIVE HYSOL 32 1 c8420 ACRYLIC ADHESIVE CLICKBOND 31 20 AN3-5 BOLT 10-32 X 2 13 30 M551496-P73 WASHER # L2 10 9434K510 COMPRESSION SPRINGS MCMASTER CARR 11 10 92200A244 SOCKET CAP SCREW L0-24X 10 2 cc28404500 1 1-00 1 NUTRTNG 6 2 cc2840450005-001 ADAPTER PLATE 5 2 cc2840450003-001 COVER PI.AÏE 4 6 cc2840440006-001 GASKET 3 2 cc2840220016-101 FUEL SENDER ASSEMBLY OUTBD 2 2 cc2840220015-101 FUEL SENDER ASSEMBLY INBD 1 QTY PART NUMBER DESCRIPTION MATERIAVSPECIFICATON WEIGHT ZONE rÍEM PARTS UST CÜNTROLLED COPY - tNc 1375 SE WILSON AVE SUITE 150 BEND, OR977O2 INSTALLATION ASSEM BLY . CTRRUS SR22 Grlcz 4 JAt{ 2 0 NONE I I A A 1 2 3 4 1 3 4 B B DWG NO. ISH IREV. cc284033001s I 4t B CUT AND DRILL SENDER MOUNTNG HOLES PER SAE 5 BOLT PATTERN SHOWN APPROX. CENTERED (11.s) Øt.so ø2.r2s 5X ø.203 STANDARD SAE 5 BOLT PATTERN SCALE 1 : 1 WING FUEL RIB TANK, INBD DETAIL CTNTRCII-I-ED COPY lNc 1375 SE WILSON AVE SUITE 150 BEND, OR97702 INSTALLATION ASSEM BLY - CTRRUS SR22 Grlcz 4 Ll2 APPROVED JATI 2 O, 01 A A 1 2 3 4 1 3 4 B B DWG NO. cc284033001s SI-I IREV. 5tB 5X CONTROLLED COPY NUTRING EPOXY DETAIL A (INBD RrB ONLY) A A 1 2 3 4 1 3 4 B B DWG NO. cc284033001 s ISH IREV. I 6l B A A 5X es FU EL SEN DER INSTALLATION CO¡.-¡TROLLED COPY (TYPICAL, INBD AND OUTBD RIB) tNc 1375 SE WILSON AVE SUITE 150 BEND, OR977O2 INSTALLATION ASSEM BLY - CTRRUS SR22 Grlcz s/B APPROVED JAN 2O A A 1 2 3 4 1 3 4 B B DWG NO. cc284033001s ISH IREV. l7l B NOTES: 1. OproNAL TO REMOVE COLLECTOR TANK FUEL SENDERS AND REP|-ACE WITH COVER PLATE (ITEM NO.3) AND GASKET (rTEM NO. 2) NOTE: USE EXISTING HARDWARE AND TORQUE tB-22INCH LBS. cc2840450003-00 1 covER PLATE CC284O45OOO5.OO1 ADAPTER PLATE (oPTONAL) CÜhITROLLAD ÜÛPY rNc 1375 SE WILSON AVE SUITE 150 BEND, OR977O2 INSTALLATION ASSEM BLY - CTRRUS SR22 crlcz APPROVEOJAN2OZS2l 1:1 A A 1 2 3 4 1 3 4 B B DWG No' cc284o33oo15 |tn 8 l*tug IMAGE NO. 1 IMAGE NO. 2 A IMAGE NO.4A IMAGE NO. 3 A cur suPPoRT BRA.**A