SERVICE BULLETIN M20--289A
Mooney M20D Master · Service Bulletins
Overview
This Service Bulletin M20-289A, dated August 01, 2005, addresses a critical issue regarding the aileron center link clearance in various Mooney aircraft models, including the Mooney M20D. The bulletin is intended for aircraft maintenance personnel and outlines the necessary steps to prevent the left and right aileron links from rubbing against the gear retraction bellcrank when the gear is extended. Compliance with this bulletin is required at the next scheduled annual inspection or within the next 100 flight hours. The document provides detailed instructions for the procedure, including parts required and safety precautions to ensure proper aileron operation after maintenance.
- Compliance is required at the next scheduled annual inspection or within the next 100 flight hours.
- The procedure involves removing the belly skin and disconnecting aileron links.
- Specific hardware must be replaced with parts from kit M20-289-000.
- Verify smooth operation of aileron controls after maintenance.
- For warranty-covered aircraft, labor and parts for the installation are covered.
Document
Source
Originally published by mooney.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Service Bulletins
- Year
- 2005
- Pages
- 2
- File size
- 420 KB
- Publisher
- mooney.com
Common. Rarer than 24% of the aircraft models we track.
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Introduction
The introduction outlines the purpose of the bulletin, which is to prevent the left and right aileron links from rubbing on the gear retraction bellcrank when the gear is extended. This is crucial for maintaining safe and effective aileron control.
Instructions
The instructions section provides a step-by-step guide for performing the necessary maintenance. It includes turning off the master switch, removing the belly skin for access, disconnecting the aileron links, replacing specific hardware, and verifying the smooth operation of the aileron controls before reassembling.
Parts List
A detailed parts list is provided, including the part numbers and quantities needed for the maintenance procedure. This includes bolts, spacers, nuts, and cotter pins necessary for the installation of the new hardware.
Warranty Information
The bulletin includes warranty information stating that for Mooney aircraft under warranty, the company will cover labor (1 hour) and parts required for the installation of the subject spacer when performed according to the bulletin's procedures.
Safety notes
- Ailerons will be unsupported when links are disconnected; support ailerons to prevent uncontrolled falling.
Full document text
MOONEY AIRPLANE COMPANY, INC. SERVICE BULLETIN Louis Schreiner Field Kerrville, Texas 78028 MOONEY AIRPLANE COMPANY, INC. Louis Schreiner Field, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SERVICE BULLETIN M20--289A Date: August 01, 2005 SUBJECT: AILERON CENTER LINK CLEARANCE MODELS/ SN AFFECTED: MOONEY M20B S/N 1701 and ON MOONEY M20C S/N 1852 and ON MOONEY M20D S/N 1 and ON (with Retractable Gear) MOONEY M20E S/N 101 and ON MOONEY M20F S/N 660003 and ON (with Electric Retractable Gear) MOONEY M20G S/N 680001 and ON (with Electric Retractable Gear) MOONEY M20J S/N 24--0001 and ON MOONEY M20K S/N 25--0001 and ON MOONEY M20L S/N 26--0001 and ON MOONEY M20M S/N 27--0002 through 27--0341 MOONEY M20R S/N 29--0001 through 29--0376 MOONEY M20S S/N 30--0001 and ON TIME OF COMPLIANCE: AT NEXT SCHEDULED ANNUAL INSPECTION, BUT WITHIN NEXT 100 FLIGHT HOURS INTRODUCTION: To prevent Left and Right Aileron Links from rubbing on Gear Retraction Bellcrank with gear extended. INSTRUCTIONS: Read entire procedure before beginning work. 1. Turn master switch - OFF 2. Per instructions provided in Section 53 of applicable aircraft Service and Maintenance Manual, remove Belly Skin for access to Center Bellcrank Assembly. 3. Locate Center Bellcrank Assembly and remove attaching hardware securing Left and Right Aileron Links (ref. Figure M20--289--1). NOTE: Ailerons will be unsupported when links are disconnected. Support ailerons to prevent their un- controlled falling prior to removing attaching hardware at Center Bellcrank Assembly. 4. Discard existing AN3--13 Bolt, 913029 Spacer, MS17825-003 Nut and MS24665-151 Cotter Pin. 5. Reassemble Left and Right Aileron Links to Center Bellcrank Assembly with hardware from kit M20-289-000. Follow order of hardware assembly as follows (ref. Figure M20--289--1): AN3-13 Bolt (Install from back to front) 913029-003 Spacer (Install between aft lug on Center Bellcrank and Right Aileron Link) 913029 Spacer (Install between Right Aileron and Left Aileron Links) 913029-003 Spacer (Install between Left Aileron Link and forward lug on Center Bellcrank) MS17825-003 Nut MS24665-151 Cotter Pin 6. Verify smooth operation of aileron controls. 7. Re-install Belly Skin removed in step 2 above. 8. Remove supports from ailerons. 9. Complete logbook entry. 10. Return aircraft to service. MOONEY AIRPLANE COMPANY, INC. Louis Schreiner Field, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com WARRANTY: For Mooney Aircraft under warranty, Mooney Airplane Company, Inc. will warrant labor (1 hour) and parts (ref. Kit below) required for the installation of subject spacer when done in accordance with procedures of this Service Bulletin. REFERENCE DATA: MAC Service and Maintenance Manuals (applicable A/C) Chapters 27 and 53. PARTS LIST: Mooney Airplane Company, Inc., Parts Kit: M20-289-000 Item P/N Description Qty 1. AN3--13 BOLT 1 2. 913029 SPACER (.090 LONG) 1 3 913029--003 SPACER (.050 LONG) 2 4 MS17825--003 NUT 1 5. MS24665--151 COTTER PIN 1 CENTER BELLCRANK AN3-13 BOLT 913029 SPACER 913029-003 SPACER MS17825---003 NUT MS24665---151 COTTER PIN LEFT AILERON LINK RIGHT AILERON LINK (REF.) (REF.) ASSEMBLY (REF.) CENTER BELLCRANK ASSEMBLY (REF.) (M20R INSTALLATION SHOWN IN PHOTOGRAPH) (.050) (.090) 913029-003 SPACER (.050) Figure SB M20-289-1





