SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
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1 MOONEY AIRPLANE COMPANY, INC. SERVICE BULLETIN Louis Schreiner Field Kerrville, Texas THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SERVICE BULLETIN M Date: May 2, 2007 SUBJECT: Aircraft with Garmin GFC Manual Electric Trim and Roll Servo Installation. MODELS/ SN Procedure 1: AFFECTED: M20M: thru M20R: thru 29-TBA M20TN: thru 31-TBA MODELS/ SN Procedure 2: AFFECTED: M20R: , , , , , , , M20TN: , , , , , , , , TIME OF COMPLIANCE: INTRODUCTION: MANDATORY -- Before Next Flight This Bulletin has been written in two procedure steps. Procedure 1: There have been reported occurrences, discovered in the field of the Garmin GFC--700 Manual Electric Trim experiencing intermittent operation in certain flight profiles. Until a permanent solution to this intermittent operation is available, the Manual Electric Trim function shall be temporarily disabled until a next Revision to this Service Bulletin is released. Compliance with this Service Bulletin DOES NOT inhibit normal operation of the aircraft s Manual Trim system, or the operation of the GFC700 Auto Trim system. Procedure 2: There are two control rods connecting the aileron control linkage, which are sensitive to the order in which they are adjusted. We have experienced at least one instance where the mechanic did not realize they were order dependant. Occasionally the aileron control rod is adjusted to center the cushion. When this is done post GFC 700 installation, the servo control rod must be readjusted to center the servo arm. INSTRUCTIONS: Read entire procedures before beginning work. Procedure (1) - Disable Manual Electric Trim: 1-1. Turn master switch -- OFF Locate AMP connector with specified wires at end of the Pilot s Control Wheel tube, verify if factory installed or retrofit installed (see Figure 1) also refer to Chapter of applicable MAC aircraft Service & Maintenance Manual. NOTE: The harness installation may require cable ties to be removed for adequate clearance of connecting wires and cover with PVC Tubing (P/N RM026215) for stowing Remove wire pins with an AMP Extractor Tool (AMP P/N ), cap wires individually with 3 of PVC Tubing (P/N RM026215). Stow and secure wires using (2) cable ties (P/N T50R9M4) on the Pilot s Control Wheel harness (see Figure 1 and 2) also refer to Chapter of applicable MAC aircraft Service & Maintenance Manual Install any cable ties to secure harness if removed for access Install placard (P/N (X)3048(Y)) on instrument panel (see Figure 3), clean surface area with isopropyl alcohol before applying placard to remove any oils or debris.
2 Procedure (2) - Roll Servo Adjustment: 2-1. Remove the forward belly fairing Insertaileronrigpin(seeFigure4) 2-3. Remove the middle panel of the center console to access roll servo Use an alignment tool (or protractor) to check the 58_ (± 2_) required alignment (see Figure 4) If the alignment is unsatisfactory, adjust rod end on the servo control rod as needed (lengthen or shorten) to obtain the proper 58_ (± 2_) alignment (see Figure 4) also refer to Chapter of applicable MAC aircraft Service & Maintenance Manual for Aileron Rigging. NOTE: This alignment should be performed every time the aileron control tube is adjusted Pull aileron pin Check control system for free non--binding movement Install center console panels and belly fairing Complete log book entry for both procedures Return aircraft to service Procedure complete. WARRANTY: Mooney Airplane Company, Inc. will warrant labor (approximately 2 hours), when done in accordance with the procedures of this Service Bulletin for aircraft currently covered under the Mooney Airplane Company, Inc. factory warranty program. REFERENCE DATA: MAC Service & Maintenance Manuals (applicable A/C) PARTS LIST: Mooney Airplane Company, Inc., Parts Kit: M Item P/N Description Qty (X)3048(Y) Placard 1 2. T50R9M4 Cable Tie 5 3. RM PVC Tubing (PVC105/4) 12
3 (Factory Installed GFC700 - Has Lettered Pins) PL20 RC20 K L M N L M N (Retrofit Installed GFC700 - Has Numbered Pins) PL110A RC110A Figure SB M Control Wheel Harness Connector
4 Cut RM PVC Tubing into 3 pieces Cover Pins and Cable Tie (2) Places to Secure CONTROL WHEEL HARNESS CONTROL WHEEL TUBE PILOTS CONTROL WHEEL Figure SB M Control Wheel Harness
5 MANUAL ELECTRIC TRIM DISABLED. MANUAL TRIM FUNCTIONAL. AUTOTRIM FUNCTIONAL (X)3048(Y) Figure SB M Placard
6 ROLL SERVO SERVO CONTROL ROD 58_ (± 2_) REF: FLOOR AILERON CONTROL ROD Aileron Rig Pin Figure SB M GFC700 Roll Servo Adjustment
SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SERVICE BULLETIN M20-318 Date: June 2, 2014 SUBJECT:
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