INSTALLATION INSTRUCTIONS P/N BI 6005 AIR/OIL SEPARATOR KING AIR 300, B300 SERIES KIT P/N BI-6001-3

THAT COLLECTS ALONG THE FLAP TRAILING EDGE AS WELL AS THE BOTTOM OF THE NACELLE. MODIFICATION REQUIRES INSTALLATION OF THE SEPARATOR TO THE FIREWALL. IT ALSO REQUIRES THE INSTALLATION OF AN OIL RESIDUE TANK TO HOLD THE OIL COLLECTED. IT REQUIRES THE INSTALLATION OF HOSES FROM THE ENGINE TO THE SEPARATOR AND FROM THE SEPARATOR TO THE NORMAL EXIT ON THE FIREWALL. IT ALSO REQUIRES INSTALLATION OF A DRAIN HOSE TO THE RESIDUE TANK. NOTE: INSTALLATION OF THE SYSTEM REQUIRES INSTALLATION OF THE RAISBECK ‘OIL RESDUE COLLECTION SYSTEM’ STC SA00975CH. THIS PROVIDES A CONTAINER FOR THE OIL TO BE COLLECTED IN. DRAWING NUMBER BI 6005 REV. G PAGE 9 3.2 KIT CONTENTS THE CONTENTS OF THE BI-6001-3 KIT ARE AS SPECIFIED IN THE LIST OF MATERIALS ON SHEET 1 OF THE DRAWING LISTED IN PARAGRAPH 2.1. ADDITIONALLY, THE KIT CONTAINS A DATA PACKAGE CONTAINING: 1) BI 6005 - INSTALLATION INSTRUCTIONS 2) DRAWINGS LISTED IN PARAGRAPH 2.1 3) ONE COPY OF THE STC 4) BI 6025 (ICA) INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RAISBECK ENGINEERING SHOULD BE NOTIFIED IMMEDIATELY OF ANY SHORTAGES OR OTHER DISCREPANCIES. 3.3 SPECIALIZED TOOLING REQUIRED IN ADDITION TO STANDARD AIRCRAFT TECHNICIAN’S TOOLS, THE FOLLOWING TOOLING WILL BE REQUIRED: 3.3.1 CUSTOMER SUPPLIED TOOLS NONE 3.3.2 RAISBECK ENGINEERING SUPPLIED TOOLS NONE DRAWING NUMBER BI 6005 REV. G PAGE 10 4.0 AIRPLANE PREPARATION NO SPECIAL AIRPLANE PREPARATION IS REQUIRED PRIOR TO INITIATING INSTALLATION OF THE AIR/OIL SEPARATOR KIT. 5.0 REMOVALS THE OPERATION DEFINED HERE ARE THOSE NECESSARY TO REMOVE AND ALTER COMPONENTS FROM THE LEFT AND RIGHT HAND NACELLE. THE EVENTS ARE PRESENTED IN A RECOMMENDED SEQUENCE. HOWEVER, THAT SEQUENCE MAY BE ALTERED TO SUIT THE CUSTOMER OR THE INSTALLATION FACILITY. REF. DRAWING BI-6001 SHEET 1 REF. BEECHCRAFT SUPER KING AIR 300 MAINTENANCE SUBJECT 71-00-00 1) OPEN BOTH SIDE COWLINGS 2) IF THE OIL RESIDUE COLLECTION SYSTEM HAS NOT BEEN INSTALLED, YOU MAY WISH TO REMOVE THE AFT LOWER COWLING TO GAIN ACCESS TO THE LOWER FIREWALL. 3) REMOVE STARTER GENERATOR COOLING DUCT FOR ACCESS. 4) REMOVE CLAMPS ON BREATHER LINES AT THE ENGINE AND AT THE FIREWALL EXIT FIXTURE. 5) REMOVE BREATHER LINES AND DISCARD: L/H P/N SCDEETS4-168-5 R/H P/N SCDEETS4-116-5 ON SOME INSTALLATIONS, THERE IS AN ADEL CLAMP INSTALLED TO SECURE THE ABOVE LISTED BREATHER LINE TO THE FIREWALL. DRAWING NUMBER BI 6005 REV. G PAGE 11 NOTE: FOR THOSE MODELS WITH AN INSULATION BLANKET INSTALLED ON THE FIREWALL, IT WILL BE NECESSARY TO REMOVE OR AT LEAST PARTLY REMOVE THIS COVER TO EXPOSE THE FIRESWALL. RECOMMEND REMOVAL OF THE TOP COWLING. REMOVE SCREWS HOLDING INSULATION BLANKET FROM THE TOP DOWN. IT WILL ONLY NEED TO BE REMOVED ENOUGH TO ALLOW FOR INSTALLATION OF STUDS. 6.0 KIT INSTALLATION 6.1 SEPARATOR INSTALLATION REF: DRAWING BI-6001 SHEET 2 & 3 -5 INSTALLATION IS FOR LEFT HAND NACELLE -7 INSTALLATION IS FOR RIGHT HAND NACELLE THE INSTALLATION OF THE SEPARATOR UNIT ITSELF IS COMMON TO BOTH SIDES AND WILL BE DESCRIBED IN SECTION 6.1 HOSE INSTALLATION WILL BE OUTLINED IN SECTION 6.2. 1) LOCATE THE REFERENCE POINT ON DRAWING BI-6001 SHEET 2 OR SHEET 3. IT SHOULD BE ON THE FOURTH ROW OF RIVETS DOWN. THEN COUNT FOUR RIVETS TO THE RIGHT FROM THE VERTICAL LINE ON THE LEFT SIDE OF THE FIREWALL. (ABOUT 7 INCHES) (FACING THE FIREWALL). THE POINT YOU ARE LOOKING FOR IS HALFWAY BETWEEN THAT RIVET AND THE RIVET TO THE RIGHT. MARK THAT POINT. HOLD THE SEPARATOR TO THE FIREWALL USING THE LOWER LEFT MOUNT HOLE TO THIS SPOT. INSURE IT MATCHES APPROPRIATE DRAWINGS. DRAWING NUMBER BI 6005 REV. G PAGE 12 NOTE: THE ACTUAL LOCATION OF THE SEPARATOR CAN VARY IN THIS AREA DUE TO LOCATION OF OTHER COMPONENTS MOUNTED ON THE FIREWALL. 2) HOLD BOTTOM EDGE OF MOUNT PLATE HORIZONTAL, USING EXISTING HOLE AT BOTTOM RIGHT CORNER OF MOUNT, FIND SECOND SPOT TO MARK. NOTE: DUE TO CHANGE IN MOUNTING HARDWARE, THE TWO TOP HOLES IN THE SEPARATOR MOUNT HAVE NOT BEEN DRILLED. 3) WHILE HOLDING THE SEPARATOR ON THE FIRST TWO MARKS, DETERMINE WHERE TO INSTALL THE TWO STUDS ON THE NEXT LINE OF RIVETS UP. THEY SHOULD ALIGN ON EITHER SIDE OF A RIVET. TRANSFER HOLE PATTERN TO THE MOUNT AND DRILL A .250 HOLE TO CORRESPOND WITH STUD LOCATION. USING DIRECTION WITH THE STUDS (CS125-1032-8CR) MOUNT THE FOUR STUDS AT THE DESIRED LOCATIONS. ALTHOUGH IT TAKES 24 HOURS FOR THE STUD EPOXY TO CURE, IN A COUPLE OF HOURS IT WILL BE HARD ENOUGH TO MOUNT THE SEPARATOR SO THAT HOSE LENGTH CAN BE DETERMINED. BE CAREFUL NOT TO PULL TOO HARD ON THE STUDS DURING THIS TIME. NOTE: FOR THOSE AIRCRAFT WITH INSULATION BLANKET THAT HAD TO BE LOOSENED OR REMOVED, REINSTALL MAKING HOLES AT LOCATION OF STUDS. INSTALL NUTS AND WASHERS. DRAWING NUMBER BI 6005 REV. G PAGE 13 6.2 HOSE INSTALLATION REF: DRAWING BI-6001 SHEET 2 & 3 -5 (L/H ) INSTALLATION USING THE 10’ HOSE P/N HTFL15-120, CUT A LENGTH SUITABLE TO CONNECT THE ENGINE TO THE INLET (LH) END OF THE SEPARATOR. SECURE ENDS WITH MS35842-11 CLAMPS. REINSTALL ANY OTHER DEVICES USED TO SECURE ORIGINAL HOSE. CUT A SUITABLE LENGTH OF BREATHER HOSE TO CONNECT THE EXIT ON THE SEPARATOR (TOP) AND THE BREATHER EXIT FIXTURE ON THE FIREWALL. SECURE WITH MS35842-11 HOSE CLAMPS. IF THE OIL RESIDUE COLLECTION SYSTEM TANK HAS NOT BEEN INSTALLED BEFORE NOW, YOU MUST DO SO TO CONTINUE. ON THE TANK THERE WILL BE ONE 3/8” HOSE NIPPLE EMPTY. YOU WILL CUT A SUITABLE LENGTH PIECE OF 3/8” F4040A TUBING AND CONNECT THIS EMPTY NIPPLE WITH THE OIL RESIDUE EXIT ON THE SEPARATOR. SECURE BOTH ENDS OF THIS LINE WITH A BREEZE 6604 CLAMP. -7 (R/H) INSTALLATION CUT A LENGTH OF BREATHER LINE TO BE CONNECTED TO THE ENGINE AND THE SEPARATOR. THIS LENGTH OF HOSE WILL BE THE SAME LENGTH AS THE FIRST PIECE YOU CUT. INSTALL USING MS35842-11 CLAMPS. DRAWING NUMBER BI 6005 REV. G PAGE 14 THE EXIT LINE WILL BE CONSIDERABLY LONGER AND WILL BE IN TWO PIECES. THIS IS DUE TO THE FACT THE FIREWALL EXIT IS HIGHER THAN THE EXIT FROM THE SEPARATOR. SEE ON DRAWING BI-6001 SHEET 3, YOU WILL HAVE TO INSTALL A BI-6102-1 TEE IN THE LINE TO DRAIN ANY MOISTURE THAT MAY ACCUMLATE IN THE LINE. CUT ENOUGH BREATHER LINE TO MAKE THE ENTIRE LOOP FROM THE SEPARATOR TO THE EXIT ON THE FIREWALL. DETERMINE THE LOW POINT OF YOUR LOOP AND CUT THE HOSE. INSTALL BI-6102-1 TEE IN LINE WITH 3/8” NIPPLE POINTING DOWN. SECURE ALL FOUR ENDS OF BREATHER LINE WITH MS35842-11 CLAMPS. CUT A SUITABLE LENGTH OF F4040A TUBING AND SECURE TO NIPPLE OF LARGE BI-6102-1 TEE WITH BREEZE 6604 CLAMP. THE SUITABLE LENGTH OF THE PREVIOUS TUBE WILL BE DETERMINED BY WHERE YOU WANT TO INSTALL THE 3/8” ‘Y’ FIXTURE. ONCE YOU HAVE DETERMINED THIS, INSTALL THE BI-6102-3 ‘Y’ FIXTURE ON THE END OF THE PREVIOUS TUBE AND SECURE WITH A BREEZE 6604 CLAMP. CUT A LENGTH OF F4040A TUBING TO CONNECT THE OPEN UPPER END OF THE BI-6102-3 ‘Y’ FIXTURE WITH THE DRAIN FITTING ON THE SEPARATOR. NOW CUT A SUITABLE LENGTH OF F4040A TUBING TO CONNECT THE BI-6102-3 ‘Y’ FIXTURE WITH THE OPEN 3/8” NIPPLE ON THE RESIDUE OIL TANK. SECURE BOTH ENDS WITH BREEZE 6604 CLAMPS. 6.3 FINAL INSTALLATION CHECK TO SEE IF NEW BREATHER LINE OR F4040A TUBING NEEDS SECURING TO PREVENT CHAFFING ON OTHER LINES. WHATEVER DEVICE IS USED, INSURE THE TUBE IS NOT DEFORMED AS TO RESTRICT THE FLOW OF AIR OR FOR FLUID DRAINAGE. DRAWING NUMBER BI 6005 REV. G PAGE 15 REINSTALL STARTER-GENERATOR COOLING DUCT ALONG WITH ANY OTHER ITEMS REMOVED TO FACILITATE INSTALLATION OF THIS KIT. REINSTALL COWLINGS, IF REMOVED TO INSTALL THE RESIDUE TANK. 6.4 INSPECTION THERE IS NO INSPECTION CRITERIA FOR THE SEPARATOR. IT IS NOT A COLLECTION POINT NOR IS IT SUBJECT TO ACCUMULATION OF ANY FOREIGN MATERIAL. CHECK BI 6025 (ICA) INSTRUCTIONS CONTINUED AIRWORTHINESS FOR REQUIRED PERIODIC MAINTENANCE. 7.0 RETURN AIRPLANE TO SERVICE 1) COMPLETE AN APPROPRIATE ENTRY IN THE AIRPLANE LOGBOOK EXAMPLE: INSTALLED RAISBECK ENGINEERING AIR/OIL SEPARATOR SYSTEM PART NUMBER BI-6001-1 AS PER STC SA00829CH. 2) COMPLETE THREE COPIES OF FAA FORM 337. INSERT ORIGINAL IN AIRPLANE FLIGHT MANUAL. MAIL ONE COPY TO LOCAL FAA-FSDO AND RETAIN ONE COPY FOR THE INSTALLER 3) NO WEIGHT AND BALANCE CHANGE