Supplemental Type Certificate for Piper PA-46 Malibu Mirage

The list of valid MT-Propeller manuals, service bulletins, AD's and their latest revisions can be downloaded from the homepage of MT-Propeller (www.mt-propeller.com). Hardcopies can also be obtained from MT-Propeller Germany and MT-Propeller USA. MT-Propeller Entwicklung GmbH Flugplatzstr.1 94348 Atting, Germany Phone: ++49-(0)-9429-9409-0 Fax: +49-(0)-9429-8432 MT-Propeller USA, Inc. 1180 Airport Terminal Drive DeLand, FL 32724 Phone: 386-736-7762 Fax: 386-736-7696 Issued 04 August 2009 Page 4 of 13 mt-propeller ENTWICKLUNG GMBH mt-propeller straubing Doc. No. E-1803 Installation Instructions DOA No. EASA.21J.020 2. REMOVAL AND INSTALLATION INSTRUCTIONS BEFORE MODIFYING THE AIRCRAFT, IT MUST BE ASSURED BY THE EXECUTING COMPANY, THAT THE AIRWORTHINESS OF THE AIRCRAFT IS NOT AFFECTED BY ANY PREVIOUS MODIFICATION IN CONNECTION WITH THIS MODIFICATION. A. APPLICABLE MANUALS - JetProp Maintenance Manual, latest revision. - MT-Propeller's Operation and Installation Manual Doc. No. ATA 61-06-10 (E-610), latest revision. -MT-Propeller's EASA approved Airplane Flight Manual Supplement Doc. No. E-1802, latest revision Qty 8 8 1 1 Spare Parts List / Tool and Equipment for the MT-Propeller Item CHART 01 9/16 inches stop nuts Washers O-ring Spinner assembly Part Number C-066 A-1181-1 C-048-E-1 P-659-( ) 40 40 1 Spinner screws Washers Carbon Block assembly C-306-9 C-344 C-131 Torque Data for MT-Propeller Model MTV-16-1-E-C-F-R(P)/CFR206-58a 9/16 inches propeller mounting stop nuts Component Beta Rod Cover Caps Spinner screws CHART 02 Torque 92-98 NM (68 - 72 foot-pounds) 8-11 NM (6-8 foot-pounds) 4-5 NM (3-4 foot-pounds) Mounting Torques of 9/16 inches stop nuts with lubricated threads: Liberally apply anti-seize thread compound, per MIL-T-83483 (e.g. Loctite® Moly 50 ™) only, to threads of studs & nuts; also to faces of nuts & washers. Torque nuts 68 to 72 foot-pounds equals 92 to 98 Nm. LUBRICATED TORQUE ONLY Lubrication / Materials for MT-Propeller Model MTV-16-1-E-C-F-R(P)/CFR206-58a CHART 03 Approved Lubrication/Material Location Engine lubrication oil refer to Pratt & Whitney Service Bulletin No. 1001, and all revisions or O-ring (C-048-E-1) 9/16 inches stop nuts and washers supplement thereto Anti-seize thread compound (MIL-T-83483) Blade angles at 77 cm (30.3 in) station for MT-Propeller Model MTV-16-1-E-C-F-R(P)/CFR206-58a Recommended Low Pitch (beta pick up) CHART 04 Feathered Full Reverse Issued - 04 August 2009 17.0°+/-0.2° 79.0°+/-1.0° -15.0+/-1.0° Page 5 of 13 mt-propeller ENTWICKLUNG GMBH mt-propeller Podo Doc. No. E-1803 Installation Instructions DOA No. EASA.21J.020 straubing NOTE Engine power lever and control rigging of the airplane must be in accordance with the rigging instructions of Jetprop Maintenance Manual before starting the propeller removal and installation work! B. REMOVAL OF HARTZELL PROPELLER 1. Remove Hartzell propeller per Jetprop Maintenance Manual. C. INSTALLATION OF MT-PROPELLER 1. Make sure that Battery Master, Ignition and Start Switch is OFF. Open the appropriate circuit breakers. 2. Remove the upper engine cowling. 3. Remove reversing lever with carbon block. Discard the cotter pins. See Figure 01, 02, 04, 05. 4. Remove spinner dome and spinner filler plates. 5. Remove Beta Rod Cover Caps on the propeller front plate. See Figure 02. WARNING BETA ROD COVER CAPS ARE PRELOADED BY REVERSE RETURN SPRINGS 6. After removal of the Beta Rod Cover Caps, the springs and white plastic spring guide, push the beta-ring forward by hand to get better access to the stops nuts (C-066). 7. Install a slip on the propeller. Use a hoisting crane to take the weight of the propeller. 8. Clean propeller and engine flange. Do not lubricate propeller and/or engine flange. 9. Check for O-ring (C-048-E-1) in the propeller hub (Propeller is delivered with pre-installed O-ring). 10. Slightly lubricate O-ring (C-048-E-1) with new engine oil. See CHART 03. 11. Do not put another O-ring to the engine flange. 12. Align dowels on engine flange with holes on propeller flange. 13. Install propeller with mounted spinner front plate and spinner back plate, but without dome on engine shaft, engaging dowel pins. 14. Apply anti-seize thread compound (see CHART 03) to the eight washers (A-1181-1) and stop nuts (C-066) and install them hand tight. CAUTION PUT WASHERS P/N: A-1181-1 UNDER HEAD OF STOP NUTS P/N: C-066. DO NOT PUT THEM BETWEEN PROPELLER FLANGE AND ENGINE SHAFT FLANGE. IT IS IMPORTANT THAT PROPELLER BE SEATED AGAINST ENGINE FLANGE WITH A STRAIGHT PUSH: ROTATION, COCKING OR WIGGLING IT ON WILL VERY PROBABLY DAMAGE THE O-RING GROOVE AND OIL LEAKAGE MAY RESULT. Issued - 04 August 2009 Page 6 of 13 mt-propeller ENTWICKLUNG GMBH Doc. No. E-1803 mt-propeller Poda straubing Installation Instructions DOA No. EASA.21J.020 C. INSTALLATION OF MT-PROPELLER 15. Pre-torque the eight stop nuts to approx. 45 Nm (35 foot-pounds). 16. Torque the eight stop nuts to 92-98 NM (68-72 foot-pounds. 17. Move beta-ring back by hand and reinstall Beta Rod Cover Caps. Make sure that all removed parts (spring, spring guide, caps) are reinstalled in the correct sequence. Torque caps as listed in CHART 02 and safety wire. CAUTION Overtorquing of the caps can damage the thread in the front plate 18. Install the carbon block assembly (C-131) and reversing lever. Use new cotter pins. 19. Make sure the side clearance between the beta-ring and carbon block is between 0.001 and 0.01 inches (0.03 and 0.25 mm). If necessary, remove material from, or replace, the carbon block to get the correct clearance. 20. Make sure that the work area is clean and clear of tools and other items. 21. Install engine cowling. 22. After installation, check track. Up to 3 mm (0.12 inches) are max. allowed, measured 10 cm (3.9 inches) from blade-tip at the trailing edge. 23. Install spinner filler plates and fit spinner dome onto the propeller. Observe markings for alignment of the spinner (#1 blade to #1 in spinner). Torque spinner screws with washers. See CHART 02. 24. Placards and markings None. NOTE Markings and signs concerning other propellers are obsolete and must be removed or permanently covered. 25. Check engine oil level. Issued 1-04 August 2009 Page 7 of 13 mt-propeller ENTWICKLUNG GMBH Doc. No. E-1803 Installation Instructions D. POWERPLANT ADJUSTMENT/TEST D-1: Beta valve setting check. mt-propeller straubing DOA No. EASA.21J.020 1. Move the power control lever to the MAX forward position. 2. Make sure that the propeller is feathered and FACE "1" of the beta valve lines up with FACE "2" within +/- 0.010 inches (0.25 mm). See Figure 03. 3. If necessary, adjust the beta control cable according to the Jetprop Maintenance Manual. D-2: Propeller Low Pitch Stop. 1. Low pitch stop adjustments of the propeller should be performed according to the MT-Propeller's Operation and Installation Manual Doc. No. ATA 61-06-10 (E-610). CAUTION For propeller torque corrections, adjust the propeller beta rods as explained in the MT-Propeller's Operation and Installation Manual Doc. No. ATA 61-06-10 (E-610). Do not disturb beta valve rigging position as described in D-1. Since the MT-Propellers may also pick up loose pieces of rock and debris from the ramp and runway, it is recommended to clean run-up area as far as possible before conducting rigging runs. D-3: Maximum Propeller Speed Check. 1. With condition lever set at flight idle and propeller lever set full forward (high rpm), advance power lever until maximum Np is reached, verify 2190 to 2200 RPM. If necessary, adjust governor maximum speed to 2190 to 2200 RPM. Issued - 04 August 2009 Page 8 of 13 mt-propeller ENTWICKLUNG GMBH Doc. No. E-1803 Installation Instructions mt-propeller straubing DOA No. EASA.21J.020 E. CHANGE WEIGHT AND BALANCE RECORD AND EQUIPMENT LIST MT-Propeller Model MTV-16-1-E-C-F-R(P)/CFR206-58a with spinner and de-ice: Total Weight 48.3 kg (106.5 lbs) Total Moment Arm 0.2718 m (10.70 in) 13.13 kgm (1139.55 in-lbs) Hartzell Propeller with spinner and de-ice: Total Weight 58.2 kg (128.3 lbs) Arm Total Moment 0.3368 m (13.26 in) 19.60 kgm (1701.3 in-lbs) When installing the MTV-16-1-E-C-F-R(P)/CFR206-58a propeller, the equipment list must be amended to reflect addition of this propeller. F. OPERATIONAL/FUNCTIONAL CHECKS/DYNAMIC BALANCING NOTE: The aircraft may be operated on ground without the spinner but the spinner filler plates must be removed prior to engine start. Perform engine ground run and verify engine linkage requirements per JetProp Maintenance Manual. Check for function and oil leakage make adjustments as required. After adjustments are completed, final safety checks are made, safety wire installation as required. Perform propeller dynamic balancing. MT-Propeller recommends Dynamic Solutions Systems Inc., MicroVib IITM Vibration Analyzer/Dynamic Balancer. NOTE The MT-Propeller has twelve anchor nuts on the spinner back plate which must be used to install dynamic balance weights. The maximum allowable total balance weight per anchor nut is 50 grams. Perform flight test and make all required log book entries. - Issued 04 August 2009 Revision 204 November 2010 Page 9 of 13 mt-propeller ENTWICKLUNG GMBH Doc. No. E-1803 Installation Instructions mt-propeller DOA No. EASA.21J.020 straubing G. REMOVAL OF MT-PROPELLER 1. Make sure that Battery Master, Ignition and Start Switch is OFF. Open the appropriate circuit breakers. 2. Remove the upper engine cowling. 3. Remove reversing lever with carbon block. Discard the cotter pins. See Figure 01, 02, 04, 05. 4. Remove spinner dome and spinner filler plates. 5. Remove Beta Rod Cover Caps on the propeller front plate. See Figure 02. WARNING BETA ROD COVER CAPS ARE PRELOADED BY REVERSE RETURN SPRINGS 6. After removal of the Beta Rod Cover Caps, the springs and white plastic spring guides, the beta-ring forward by hand to get better access to the stops nuts (C-066). 8. Install a slip on the propeller. Use a hoisting crane to take the weight of the propeller. 9. Put a container or plastic bag below the propeller flange for the engine oil. 10. Remove the eight stop nuts (C-066) and washers (A-1181-1). 11. Carefully remove the propeller from the engine. Discard the propeller O-ring (C-048-E-1). 12. Do not store propeller on the beta-ring. Beta-ring can be damaged. 14. Reinstall Beta Rod Cover Caps with springs and white plastic spring guides. Issued- 04 August 2009 Page 10 of 13 mt-propeller ENTWICKLUNG GMBH Doc. No. E-1803 Installation Instructions H. FIGURES 0.001 TO 0.01 in (0,03 TO 0.25 mm) FWD B Figure 01 Carbon block assy C-131 mt-propeller Hodd DOA No. EASA.21J.020 Figure 02 Beta Rod Cover Caps Issued 04 August 2009 Page 11 of 13 straubing mt-propeller ENTWICKLUNG GMBH Doc. No. E-1803 Installation Instructions H. FIGURES Forward Clevis Face "2" is Cap top of Nut Beta Feed Back Arm B mt-propeller straubing DOA No. EASA.21J.020 Beta Valve Cap Nut Beta Valve - Face "1" is the bottom of beta valve clevis see aux. view I a... These surfaces must be rigged flush within +.010 inches. Bottom of beta: valve clevis (Face "1") Auxilliary View Figure 03 I a Figure 04 Reverse Lever Issued 04 August 2009 Page 12 of 13 mt-propeller ENTWICKLUNG GMBH mt-propeller Doc. No. E-1803 Installation Instructions DOA No. EASA.21J.020 H. FIGURES Figure 05 Stop Nuts C-066 and Washers A-1181-1 Issued 04 August 2009 straubing Page 13 of 13