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SBM20-322 2015 June 23 Temporary

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SBM20-322 2015 June 23 Temporary MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 SERVICE BULLETIN M20-322 Date: June 23, 2015 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SUBJECT: Temporary Replacement of Icing System Stall Strip MODELS/ SN Mooney Aircraft with Known Icing System Installed AFFECTED: TIME OF AS SOON AS PRACTICABLE COMPLIANCE: INTRODUCTION: For instances involving missing icing system stall strips, airplanes are grounded. To remedy this situation, a temporary non-icing system stall strip can be installed in place of the icing stall strip to allow the aircraft to operate as a “Not Certified for Flight in Known Icing Conditions” aircraft until the icing strip can be installed. This Service Bulletin is to provide instructions for installing the temporary stall strip. The attached compliance card needs to be filled out and returned to Mooney International Corporation upon completion of this Service Bulletin M20-322. WARNING: Flight into known icing conditions and the use of the aircraft’s icing system is prohibited until the permanent icing system stall strip can be installed. This Service Bulletin only allows for a temporary non-icing stall strip to be installed for temporary flight until the permanent icing stall strip can be obtained. INSTRUCTIONS: Read entire procedures before beginning work. INSTALLING TEMPORARY STALL STRIP: 1.1. Disable and secure circuit breaker to prevent accidental operation of icing system. 1.2. Remove all old sealant and thoroughly clean the porous surface of the wing where the temporary stall strip is to be installed. Acceptable cleaning solvents are listed below. NOTE: The primary factor affecting the adhesion of the stall strip is absolute cleanliness of the porous panel. It is necessary that this panel be completely clean before installing a new stall strip. WARNING: Do not use MEK (Methyl Ethyl Ketone) to clean titanium panels. Discoloration will result. Porous panels contain plastic parts which will be damaged by some solvents including MEK and some paint thinners. ONLY the following solvents are permitted for cleaning porous panels: - Water (with soap or detergent) - De-icing Fluids (TKS 80, TKS R238, DTD 406B) - Isopropyl or Ethyl Alcohol - Aircraft Fuels (Gasoline or Kerosene) 1.3. Prepare temporary stall strip. (See Figure M20-322-1) a.) Determine the location on the stall strip where the TKS feeder tube will enter the stall strip. b.) Create a notch in this location using a die grinder to allow feeder tube provision. c.) Deburr and smooth the notch to ensure no rough edges scrape or cut into the TKS feeder tube. Page1of4 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road North, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 SERVICE BULLETIN M20-322 Date: June 23, 2015 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN 1.4. Place PN 210241-007 temporary stall strip on leading edge at stations shown in Figure M20-322-1. Attach securely with two (2) strips of ½” aluminum tape for test flights. 1.5. Adjust stall strip so that, during stall recovery, normal use of flight controls should prevent the following: a.) More than 15 roll b.) More than 15 yaw c.) More than 30 pitch below flight level NOTE: Make sure porous panel surface is completely clean before using sealer. 1.6. Once the temporary stall strip has been adjusted to the above conditions: a.) Mark the desired location of the stall strip. b.) Remove the stall strip. c.) Apply masking tape onto the porous panel around the stall strip marks to avoid getting excess sealer on the porous panel. (See Figure M20-322-1) 1.7. Secure temporary stall strip using CS3204B2 sealer as required. 1.8. Place PN M20-322-002 decal adjacent to TKS control panel under the Windshield Anti-Ice decal. (See Figure M20-322-2) NOTE: Fill out compliance card and send by MAIL or FAX to Mooney International Corporation as indicated on the attached Compliance Card. (See Figure M20-322-3) 1.9. Return aircraft to service. 1.10. Procedure complete. WARRANTY: N/A REFERENCE 1. Mooney Service and Maintenance Manual (applicable A/C) DATA: 2. TKS Installation Manual 08153-01 PARTS LIST: Refer to Mooney Service Parts Department for part procurement. Parts Kit P/N: Service Bulletin Kit M20-322-001 (Temporary Stall Strip) Item P/N Description Qty 1. 210241- 007 TRIGGER, STALL STRIP (WITHOUT HOLES) 1 2. M20-322-002 DECAL 1 Note: The following items are to be supplied as required by the shop performing the work. Item P/N Description Qty 1. ALUMINUM TAPE ½” ALUMINUM TAPE AR 2. MASKING TAPE MASKING TAPE AR 3. CS3204B2 SEALER AR Page2of4 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road North, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 SERVICE BULLETIN M20-322 Date: June 23, 2015 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN LEFT WING - SHOWN RIGHT WING - OPP. FWD STA. 43.5 - RIB RIVET LINE 1.2 STA. 60.12 CLEAN SURFACE WITH APPROPRIATE SOLVENT 2.0 TEMPORARY STALL STRIP POROUS PANEL STALL STRIP FWD 1.3 CREATE NOTCH USING DIE GRINDER AND SMOOTH AND DEBURR 1.7 APPLY SEALANT CS3204B2 1.4 ATTACH WITH 1/2” ALUMNIUM TAPE (AR) FOR TEST FLIGHTS 1.6 MARK POSITION OF STALL STIP, REMOVE, AND APPLY MASKING TAPE TO PROTECT POROUS PANEL FROM SEALANT Figure SB M20-322-1 - TEMPORARY STALL STRIP INSTALLATION Page3of4 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road North, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 SERVICE BULLETIN M20-322 Date: June 23, 2015 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN 20 200 40 180 AIRSPEED 60 160 MSTR WARN KNOTS 80 140 120 100 MASTER RT/LT POWER ALT ICE LIGHT SWITCH EMER BATT (REF) BUS 1/2 TKS CONTROL 100 FEET 0 PANEL 9 1 8 2 300 GEAR NOT 302301 EXTENDED S-TEC FIFTYFIVEX (REF) 7 3 HIGH BOOST A/P ELEV ICE PITOT ELT LITE HEAT L GEAR UP BOOST PUMP POWER TRIM 6 4 A 106 KIAS 5 N D HDG NAV APR REV ALT VS I N PUSH G GEAR SAFETY BYPASS G LIGHTS 1OS4 V LT E GLARE PANEL A GEAR DOWN SHIELD R 140 KIAS GEAR EXTD RUDDER 165 KIAS TRIM 3 AMPSXMA 5EA INT RTMITTEN WINDSHIELD ANTI- ICE DECAL AIRCRAFT CURRENT (REF) CONFIGURATION PROHIBITS FLIGHT INTO KNOWN ICING CONDITIONS Figure SB M20-322-2 - PLACEMENT OF M20-322-002 DECAL ON INSTRUMENT AND CONTROL PANEL Page4of4 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road North, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 SERVICE BULLETIN M20-322 Date: June 23, 2015 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN MOONEY INTERNATIONAL CORPORATION KERRVILLE, TEXAS 78028 - FAX 830- 257- 4635 SERVICE (BULLETIN) (INSTRUCTION) NO.________________HAS BEEN COMPLIED WITH ON AIRCRAFT MODEL _______________ SERIAL NUMBER ________________ Tach. Time: N-Number (Reg. No.) Date of Owner: Compliance: Complied By: Inspection Report: Form 07-0001 PLACE STAMP HERE MOONEY INTERNATIONAL CORPORATION ATT’N: TECHNICAL SUPPORT 165 Al Mooney Road, North Kerrville, Texas 78028 SEND TO: Mooney International Corporation 165 Al Mooney Road North Kerrville, TX 78028 FAX: (830) 257-4635 or EMAIL [email protected] Figure SB M20-322-3 - Compliance Card Page5of4 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road North, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com.
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