Weight & Balance for the Piper PA-34 Seneca II

NOTE: Use parts list/bill of materials on kit drawing 102600 in lieu of parts list on Goodrich drawing 7E1431. Reference Goodrich Drawing 7E1431 and Hartzell kit drawing 102600. Install Slip Ring Assembly P/N 4E2422 and Mounting Plate P/N 4E3153 on the engine flange in accordance with Drawing 7E1431 with kit hardware specified on Hartzell drawing 102600. Install 1 each item 17 washer (not shown on Goodrich Drawing 7E1431) between item 15 plate and item 18 nut. It is recommended to loosely fasten the mounting plate and slip ring together with item 14 to facilitate alignment of the mounting plate holes with the propeller mounting studs. If converting from a two blade propeller installation, remove and replace ammeter, shunt, timer, circuit breaker and associated hardware. Install new components in same location as previously installed. Modify aircraft wiring as required per Goodrich Drawing 7E1431 note 3. Remove the top spark plug from #6 cylinder. Rotate the engine crankshaft until #6 cylinder is on approximate top dead center. This will position the dowel pin holes on the crankshaft flange at 12 o'clock and 6 o'clock. Ensure the propeller shaft O-ring is properly seated before mounting the propeller. Page 6 of 10 Rev. D 1/22/08 8. 9. 10. 11. 12. 13. 14. 15. DRAWING B-4060 INSTRUCTIONS FOR INSTALLATION OF HARTZELL PHC-C3YF-2(L)UF/F(J)C7663(B)-2R PROPELLERS AND C-4558-( ) SPINNERS ON PIPER PA-34-200T – SENECA II STC SA1118SO Rotate the Slip Ring Assembly as necessary to align the lead wires with the de-ice wire screw holes in the spinner bulkhead before installing the propeller and torquing the propeller mounting nuts. Align and install the appropriate propeller with one blade oriented straight-up, in-line with the top engine case split line. Complete installation of propeller mounting hardware per “Installation of “F” Flange Propellers" in Hartzell Manual 115N. NOTE: Torque the mounting plate-to-slip ring nuts after the propeller is installed on the engine crankshaft but before torquing the propeller mounting nuts. Reference Goodrich Drawing 7E1431. Install all Goodrich de-icing components on the spinner bulkhead including the slip ring wire leads and de-ice boot wire leads to the screw-post. Fasten de-icer boot wire leads with clamps and tie-straps as shown on drawing 7E1431. Install spinner dome and complete spinner installation per Hartzell Manual 115N Spinner Installation Section 3.6. Based on the dome configuration, use the appropriate installation procedure for single-piece spinner dome for spinners with no dome cap, or two-piece spinner dome (Procedure 2) for spinners with a dome cap. Remark tachometers by extending green arc from 500 to 2575 RPM (Red Radial at 2575 RPM). Optional: install new tachometers, Piper Code 548- 303. Remove RPM restriction placards from instrument panel (Cross wind restriction and/or MP-RPM restriction). Attach Hartzell P.O.H. Supplement No. B-4060 to the existing FAA Approved Airplane Flight Manual. 16. Page 7 of 10 Rev. D 1/22/08 DRAWING B-4060 INSTRUCTIONS FOR INSTALLATION OF HARTZELL PHC-C3YF-2(L)UF/F(J)C7663(B)-2R PROPELLERS AND C-4558-( ) SPINNERS ON PIPER PA-34-200T - SENECA II STC SA1118SO Apply the following weight and moment corrections to the weight and balance records based on the propeller configuration replaced: For Replacing Hartzell Two-Blade Propellers Items Installed on the Aircraft Weight and Balance Change Wt. Arm Moment (lb) (in) (lb-in) PHC-C3YF-2UF/FC7663-2R and PHC-C3YF-2LFU/FJC7663-2R +32 20.3 +650 PHC-C3YF-2UF/FC7663B-2R and PHC-C3YF-2LUF/FJC7663B-2R +34 20.3 +690 C-4558-( ) Spinners No significant change For Replacing McCauley Three-Blade Propellers Items Installed on the Aircraft Weight and Balance Change Wt. Arm Moment (lb) (in) (lb-in) PHC-C3YF-2UF/FC7663-2R and PHC-C3YF-2LFU/FJC7663-2R -5.2 20.3 -106 PHC-C3YF-2UF/FC7663B-2R and PHC-C3YF-2LUF/FJC7663B-2R C-4558-() Spinners -3.2 20.3 -65 No significant change If Woodward Governors Are Replaced Items Installed on the Aircraft Weight and Balance Change Wt. (lb) Arm Moment (in) (lb-in) E-3 and E-3L or E-3 and E-8L +2.4 28.1 +67 Page 8 of 10 Rev. D 1/22/08 DRAWING B-4060 INSTRUCTIONS FOR INSTALLATION OF HARTZELL PHC-C3YF-2(L)UF/F(J)C7663(B)-2R PROPELLERS AND C-4558-( ) SPINNERS ON PIPER PA-34-200T - SENECA || STC SA1118SO 17. Perform ground engine run for a functional and leak check per Hartzell Manual 115N. 18. 19. 20. Make the appropriate logbook entries and return aircraft to service with FAA Form 337 referencing STC. Fly a functional check-flight using normal procedures, note maximum RPM setting and readjust governor high-RPM stop if necessary. Post-installation dynamic balance of the propeller/engine combination is recommended, but not required, per Section 61-00-15 of Hartzell Owner's Manual 115N. Page 9 of 10 Rev. D 1/22/08 DRAWING B-4060 INSTRUCTIONS FOR INSTALLATION OF HARTZELL PHC-C3YF-2(L)UF/F(J)C7663(B)-2R PROPELLERS AND C-4558-( ) SPINNERS ON PIPER PA-34-200T - SENECA II STC SA1118SO REPLACEMENT OF WOODWARD GOVERNORS WITH HARTZELL GOVERNORS 1. Refer to the appropriate airplane maintenance manual for propeller governor removal and installation instructions. Install appropriate governors using existing engine attachment hardware. Torque the four attachment nuts to 18-20 ft-lbs. 2. Remove the propeller control cable anchor hardware form the engine bracket. 3. Install Piper Plate P/N 37833-2 to the engine bracket (see Sketch #1) with existing hardware. 4. Drill a 0.166" diameter hole through the engine bracket using the aft hole of part 37833-2 as a guide. 5. Anchor the engine control cable as shown on Sketch #1. 6. Attach the propeller control cable rod end as shown in Sketch #1. Page 10 of 10 Rev. D DRAWING B-4060 INSTRUCTIONS FOR INSTALLATION OF HARTZELL PHC-C3YF-2(L)UF/F(J)C7663(B)-2R PROPELLERS AND C-4558-( ) SPINNERS ON PIPER PA-34-200T - SENECA II STC SA1118SO -MS 35338-43 (ZREQ) AN 3-7 BOLT -№960-10 WASHER DRILL 0.166 DIA. HOLE THRU ENGINE BRACKET THIS LOCATION ENGINE BRACKET Top View ·SAFETY WASHER PIPER AV 62833-101 Leer SIDE VIEW PROP GoverNOR, M524665-132 CATER PIN AN 310-3 CASTLE NUT SKETCH #1 PROP CONTROL BRACKET MODIFICATION FOR REPLACEMENT OF WOODWARD WITH HARTZELL PROP. GOVERNORS 1/22/08 Z PLACES MS 35206-246 AN 960-8L M520365-832 (AN365-832) BRACKET ASSY PIPER PAN 37833–2 MAKE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATIONS MODEL NO. Piper IDENTIFICATION PA-34-200T TYPE (Airplane, Radio, Helicopter, etc.) Airplane LIST OF DATA TITLE DATE: Jan 22, 2008 Page 1 of 1 NAME OF APPLICANT Hartzell Propeller Inc. Document: B-4060, Revision D Dated 1/22/08 INSTRUCTIONS FOR INSTALLATION OF HARTZELL PHC-C3YF-2(L)UF/F(J)C7663(B)- 2R PROPELLERS AND C-4558-( ) SPINNERS ON PIPER PA-34-200T SENECA II. END PURPOSE OF DATA Revise Installation Instructions for Piper Seneca II, STC SA1118SO to update kit effectivity table and revise installation steps to include reference to new de-ice kit drawing 102600. APPLICABLE REQUIREMENTS (List specific sections) 14 CFR 23.901 have been examined in CERTIFICATION - Under authority vested by direction of the Administrator and in accordance with conditions and limitations of appointment under Part 183 of the Federal Aviation Regulations, data listed above and on attached sheets numbered XXX accordance with established procedures and found to comply with applicable requirements of the Federal Aviation Regulations. Recommend approval of these data I (XX) therefore, ☑ Approve these data SIGNATURE(S) OF DESIGNATED ENGINEERING REPRESENTATIVE(S) Leslie A. Doud DESIGNATION NUMBER(S) DERY-410155-CE CLASSIFICATION(S) Chart B A7, B7, A16, B16 Chart G A5, A7, A8, A10 FAA FORM 8110-3 (11-70) SUPERCEDES PREVIOUS EDITION