GUARDIAN I STANDBY VACUUM/PRESSURE SYSTEM BEECHCRAFT BONANZA F33 F33A V35A V35B V35A-TC A36 A36-TC 836-TC E33A PARTS LIST

Transcription

1 F33 F33A V35A V35B V35A-TC A36 A36-TC 836-TC E33A PARTS LIST I. II. III. IV. V. VI. VII. VIII PUMP/MOTOR ASSEMBLY 4 VOLT PUMP/MOTOR ASSEMBLY 28 VOLT CHECK VALVES H37-2 BULK HEAD FITTING K " T " FITTING K AIR FILTER J4-6 FEET 5/8 HOSE MIL-H HOSE CLAMPS QS00-MOH FEET 2 GAUGE WIRE M22759 IX. INLINE FUSE HOLDER X. FUSE 20 AMP 4 VOLT SYSTEM FUSE 0 AMP 28 VOLT SYSTEM XI. 2 CRIMP TYPE CONNECTORS 2R84-0 XII. 2 WIRE TERMINALS - SWITCH RB4-0 XIII. 2 WIRE TERMINALS - POWER/GROUND RBRB4-56 XIV. TOGGLE SWITCH MS XV. 8 TI RAPS - CABLE TIE TY524M XVI. MOUNTING HARDWARE: A. 4 BOLTS AN3-6A B. 30 WASHERS AN960-0 C. 4 NUTS MS2042-L3 XVII. PLACARD - AUX INST AIR PL28 PUMP/MOTOR ASSEMBLY 7.3 LBS. INSTALLATION HARDWARE 4. LBS. ALL PARTS SUPPLIED BY AERO SAFE ARE FAA/PMA APPROVED /

2 F33 F33A V35A V35B V35A-TC V35B-TC A36 A36-TC B36-TC E33A I. INSTALLATION OF UNIT ON FIREWALL: A. REMOVE UPPER FIREWALL DOOR (BEECHCRAFT PART # ) B. POSITION AERO SAFE PUMP/MOTOR/PLATE ASSEMBLY ON DOOR AS SHOWN ON DRAWING SHEET 2. C. MATCH DRILL MOUNT HOLES IN UPPER FIREWALL DOOR. D. INSTALL PUMP/MOTOR/PLATE ASSEMBLY ON DOOR AS SHOWN ON THE DRAWING SHEET 3. E. REINSTALL UPPER FIREWALL DOOR ON AIRCRAFT. II. INSTALLATION OF CHECK VALVES, FITTINGS AND PLUMBING: A. REMOVE TUBING - (BEECHCRAFT PART # ). B. INSTALL HOSE AND TEE AS SHOWN ON FIGURE OR DRAWING C. VERIFY DIRECTION OF FLOW OF CHECKVALVES AND INSTALL AS SHOWN IN FIGURE OF DRAWING (INSURE THAT SIDE OF CHECK VALVES MARKED "THIS SIDE UP" ARE TURNED TO THE TOP). D. MOUNT BULKHEAD FITTINGS IN REAR ENGINE BAFFLE AS SHOWN ON SHEET 5 OF DRAWING E. ROUTE HOSE AS REQUIRED TO CLEAR OTHER COMPONENTS AND INSTALL SUPPORT CLAMPS AS REQUIRED TO PREVENT SAGGING, BINDING OR CHAFING. F. INSTALL HOSE CLAMPS ON ALL VALVES AND FITTINGS AND TIGHTEN. PAGE OF 3

3 F33 F33A V35A V35B V35A-TC V35B-TC A36 A36-TC B36-TC E33A III. TO INSTALL ELECTRICAL COMPONENTS: A. CONNECT FUSED ELECTRICAL TERMINAL TO POWER SOURCE NEAREST TO CONTROL SWITCH. (PRIMARY BUS, STARTER SOLENOID, ETC.). SELECTION SHOULD ALLOW FOR CONTINUED ELECTRICAL POWER IN THE EVENT OF LOSS OF GENERATOR. B. CONNECT POSITIVE WIRE TO POSITIVE MOTOR LEAD (MOTOR POSITIVE LEAD IS MARKED RED). C. ROUTE POWER SOURCE AND MOTOR POSITIVE LEAD THRU FIREWALL WITH EXISTING WIRE BUNDLES. D. ROUTE WIRES BEHIND INSTRUMENT PANEL TO SWITCH LOCATION ON SHEET 7 OF DRAWING ROUTE AS TO PREVENT CHAFING OR INTERFERENCE WITH CONTROLS. E. INSTALL TERMINALS ON WIRE AND CONNECT TO SWITCH. F. INSTALL SWITCH AND PLACARD AS SHOWN IN DETAIL A, SHEET 7 OF DRAWING G. CONNECT GROUND WIRE TO MOTOR GROUND LEAD AND GROUND TO FIREWALL. PAGE 2 OF 3

4 F33 F33A V35A V35B V35A-TC V355-TC A36 A36-TC B36-TC E33A IV. TO TEST SYSTEM: A. REVIEW ALL NOTES ON INSTALLATION DRAWINGS TO INSURE PROPER INSTALLATION. B. TURN MASTER SWITCH "ON." C. TURN AUXILIARY INSTRUMENT AIR SWITCH ON MOMENTARILY TO VERIFY PROPER ROTATION OF PUMP. D. WHEN PROPER ROTATION HAS BEEN ESTABLISHED TURN AUXILIARY INSTRUMENT AIR SWITCH "ON" AGAIN AND CHECK INSTRUMENT PRESSURE GUAGE INDICATION. (MINIMUM 3.5 HG.) E. TURN AUXILIARY INSTRUMENT AIR SWITCH "OFF." F. START ENGINE AND CHECK INSTRUMENT PRESSURE GUAGE FOR PROPER INDICATION. ( IN. HG.) G. WITH ENGINE RUNNING, TURN AUXILIARY INSTRUMENT AIR SWITCH "ON" AND AGAIN CHECK INSTRUMENT PRESSURE GUAGE FOR PROPER INDICATION. ( IN. HG.) H. TURN AUXILIARY INSTRUMENT AIR SWITCH "OFF," STOP ENGINE, AND TURN MASTER SWITCH "OFF." TEST COMPLETE. PAGE 3 OF 3

5 LIMITED WARRANTY CERTIFICATE GUARDIAN I AERO SAFE CORPORATION HEREBY LIMITS ITS WARRANTY ON THE GUARDIAN I TO COVER THE REPAIR OR REPLACEMENT OF ANY PART OR COMPONENT WHICH HAS BEEN RETURNED PREPAID AND IN THE OPINION OF AERO SAFE CORPORATION IS DEFECTIVE. THIS LIMITED WARRANTY SHALL BE VALID FOR A PERIOD OF TWO YEARS FROM THE DELIVERY OF THE GUARDIAN I. AERO SAFE CORPORATION ASSUMES NO OBLIGATION FOR WORK ACCOMPLISHED AT A FACILITY OTHER THAN AERO SAFE CORPORATION UNLESS PRIOR WRITTEN AUTHORITY HAS BEEN ISSUED BY COMPANY. AERO SAFE CORPORATION RESERVES THE RIGHT TO FURNISH ANY PARTS REQIRED AND DEFECTIVE PARTS MUST BE RETURNED TO AERO SAFE CORPORATION FOR EXAMINATION IF REQUESTED. ANY ACTION PERFORMED BY AERO SAFE CORPORATION WILL BE PRECEEDED BY A WRITTEN NOTICE OF CLAIM AND DELIVERY OF THE DEFECTIVE PART OR PARTS TO AERO SAFE CORPORATION AT THE ABOVE ADDRESS. ALL WORK REQUIRED OF AERO SAFE CORPORATION WILL BE PERFORMED WITHIN A REASONABLE TIME AFTER RECEIPT OF THE DEFECTIVE COMPONENT. THIS WARRANTY SHALL NOT APPLY IF THE GUARDIAN I HAS BEEN IMPROPERLY INSTALLED, ADJUSTED, STORED, HANDLED, REPAIRED, ALTERED, OR OPERATED CONTRARY TO CURRENT MANUFACTURER'S RECOMMENDATIONS, SERVICE LETTERS AND BULLENTINS, F.A.A. AIRWORTHINESS DIRECTIVES, AND AERO SAFE CORPORATION RECOMMENDATIONS OR SUBJECT TO MISUSE, NEGLECT OR ACCIDENT. EXCEPT AS IS SPECIFICALLY PROVIDED HEREIN, THERE ARE NO OTHER WARRANTIES, EXPRESSED OR IMPLIED, INCLUDING, BUT NOT LIMITED TO, ANY IMPLIED WARRANTIES OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. AERO SAFE CORPORATION SHALL NOT BE LIABLE FPR CONSEQUENTIAL DAMAGES, LOSS OF PROFITS OR SPECIAL DAMAGES DIRECTLY OR INDIRECTLY ARISING FROM THE BREACH OF ANY OF THE TERMS HEREOF OR FROM THE SALE, HANDLING, OR USE OF THE PRODUCTS SOLD. SELLER'S LIABILTY HEREUNDERS, EITHER FOR BREACH OF WARRANTY OR FOR NEGLIGENCE IS EXPRESSLY LIMITED AT THE OPTION OF AERO SAFE CORPORATION TO (I) THE REPAIR OF SUCH PRODUCTS, OR (2) THE REPLACEMENT, OF F.O.B. FACTORY, OF ANY PRODUCT FOUND TO BE DEFECTIVE.