Mooney SBM20-294 Owner's manual

  • Hello! I've reviewed the Mooney Service Bulletin regarding the inspection and replacement of the retaining nut fastener on the engine throttle arm for TCM engines in M20R, M20S, and M20TN aircraft. This document covers the necessary steps, torque specifications, and associated procedures. I'm ready to answer any questions you might have about this bulletin.
  • What is the purpose of this service bulletin?
    Which aircraft models are affected by this bulletin?
    What is the required torque for the new retaining nut?
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--294
Date: January 18, 2007
SUBJECT: Inspection and replacement of retaining nut fastener on the engine throttle arm for TCM
engines.
MODELS/ SN
AFFECTED: M20R -- All aircraft
M20S -- All aircraft
M20TN -- All Aircraft
TIME OF
COMPLIANCE: Next 10 hour of Flight Time
INTRODUCTION: There has been one reported instance, discovered in the field, of the throttle body control arm
being loose. This will require a (1) time inspection and replacement of the throttle body retaining
nut fastener.
INSTRUCTIONS: Read entire procedure before beginning work.
1. Turn master switch -- OFF.
2. Remove top cowling per instructions provided in Chapter 71-10-00 of applicable MAC aircraft Ser
vice & Maintenance Manual.
3. Remove and clean any torque seal from threads and retaining nut fastener on the engine throttle
arm.
NOTE:
If the throttle body arm is removed, adjustments will be required per instructions provided in Chap-
ters 71-00-52 and 76--00--01 of applicable MAC aircraft Service & Maintenance Manual.
4. Remove retaining nut from throttle body arm and Inspect mating surface for any unusual wear.
Install new retaining nut p/n MS21042-5 included in your SB Kit [P/N SB M20-294-001] and
torque to 100-120 IN-LB (see Figure M20-294-1).
5. Verify throttle linkage adjustment per instructions provided in Chapters 71--00--52 and 76-10-00
of applicable MAC aircraft Service & Maintenance Manual.
6. Apply a bead of torque seal to threads and fastener.
7. Re-install top cowling (and bottom cowling if removed) per instructions provided in Chapter
71-10-00 of applicable MAC aircraft Service & Maintenance Manual.
8. Complete the Inspection Card (positive or negative) p/n Form 07-0001 included in your SB Kit
[P/N SB M20-294-001] and return it to Mooney Airplane Company.
9. Complete log book entry.
10. Return aircraft to service.
11. Procedure complete.
WARRANTY: Mooney Airplane Company, Inc. will warrant labor (approximately 1 hour), when done in accor-
dance 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: M20--294--001
Item P/N Description Qty
1. MS21042-5 Locknut 1
2. Form 07-0001 Inspection Card 1
MOONEY AIRPLANE COMPANY, INC. Louis Schreiner Field, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com
OVATION (M20R) & EAGLE (M20S) -- THROTTLE ASSEMBLY
ACCLAIM (M20TN) -- THROTTLE ASSEMBLY
Remove and Install
Torque to 100-120 IN-LB
New Nut P/N MS21042--5
Remove and Install
Torque to 100-120 IN-LB
New Nut P/N MS21042--5
Figure SB M20-294-1
/