SERVICE BULLETIN REVISION TRANSMITTAL

Transcription

1 REVISION TRANSMITTAL TO: Cessna Distributors, Single Authorized Service Facilities, and CPC's SUBJECT: Single Service Bulletin Revision 2: Control Column Internal Glide Attach Screw Installation REASON To divide the airplane serials in the Effectivity section into two groups. Group A lists the airplane serials that require modification of the glide screw on the pilot's and the copilot's control column and Group B lists the airplane serials that require modification of the glide screw on the copilot's control column only. Added to art to clarify that not all configurations have a plug installed. Added instruction for tightening of screws in configurations where there is no plug installed. Miscellaneous changes as required. Please replace any copy of and Revision 1 with the attached copy of Revision 2, which is printed in its entirety. NOTE: Compliance with Revision 2 is not required if in compliance with the Original Issue or Revision 1. LOG OF REVISIONS Page No. Date 1 April 20, April 20, April 20, April 20, April 20, April 20, April 20, April 20, April 20, April 20, 2012 Original Issue - February 28, 2012 Revision 2 - April 20, 2012 Page1of1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , customercare@cessna.textron.com COPYRIGHT 2012

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3 TITLE FLIGHT CONTROLS - CONTROL-COLUMN INTERNAL GLIDE ATTACH-SCREW INSTALLATION EFFECTIVITY Group A airplanes The airplanes that follow must do the modification of the internal glide attach screw on the pilot's and the copilot's control column (if the airplane is equipped with a control column on the right side): NOTE: On some airplanes the control column on the copilot's side was optional equipment. MODEL SERIAL NUMBERS thru , thru , thru , 634 T thru R182 & TR182 R thru R S thru T thru T182T T thru T thru , thru P206 & TP206 P thru P U206 & TU206 U thru U , U thru U , H thru T206H T thru T & T thru thru , thru T210 T thru T , , thru P210 P thru P Original Issue - February 28, 2012 Revision 2 - April 20, 2012 Page1of10 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , customercare@cessna.textron.com COPYRIGHT 2012

4 Group B airplanes The airplanes that follow must do the modification of the internal glide attach screw on the copilot's control column only (if the airplane is equipped with a control column on the right side): NOTE: On some airplanes the control column on the copilot's side was optional equipment. NOTE: Group B airplanes are not required to do a modification of the internal glide attach screw on the pilot's control column. MODEL SERIAL NUMBERS thru RG 177RG0001 thru 177RG1366 F177RG F177RG0001 thru F177RG thru , 675 T thru F182 F thru F R182 R thru R TR182 R thru R FR182 FR thru FR P206 & TP206 P thru P , P thru P U206 & TU206 U thru U , U thru U & T thru thru T210 T thru T , thru P210 P thru P REASON If the control-column internal glide attach-screw is not correctly attached, it can loosen and fall off inside the control column tube. This condition can cause looseness of the control column and the fallen screw may limit full range of elevator control. DESCRIPTION The control-column internal glide attach-screw is removed and a new one is installed and steel wire is used to safety the screw to the installation as specified in this service bulletin. COMPLIANCE Mandatory: Shall be accomplished at the next 100-hour inspection or 12-month (annual-type) inspection, whichever occurs first. NOTE: Compliance with Revision 2 is not required if in compliance with the Original Issue or Revision 1. This service bulletin supersedes Cessna Service Bulletin SB , Control-Column Internal Slide Attach-Screw Inspection. Airplanes in compliance with Cessna Service Bulletin SB , Control-Column Internal Slide Attach-Screw Inspection must also comply with this service bulletin. Page 2 Revision 2 - April 20, 2012

5 APPROVAL FAA approval has been obtained on technical data in this publication that affects airplane type design. Cessna received EASA approval for the technical data in this publication that changes the airplane type design. CONSUMABLE MATERIAL You must use the consumable material that follows, or equivalent, to complete this service bulletin. NAME NUMBER MANUFACTURER USE steel safety Commercially available To secure the screw wire WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Applicable Cessna Airplane Maintenance Manuals and Illustrated Parts Catalogs. NOTE: Make sure all publications used are complete and current. Refer to NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for Continued Airworthiness and must be accomplished for ongoing airworthiness compliance as necessary in accordance with 14 CFR Part PUBLICATIONS AFFECTED Applicable Cessna Airplane Maintenance Manuals and Illustrated Parts Catalogs. ACCOMPLISHMENT INSTRUCTIONS 1. Prepare the airplane for maintenance. A. Make sure that all switches are in the OFF/NORM position. B. Disconnect electrical power from the airplane. (1) Electrically ground the airplane. (2) Disconnect external electrical power. (3) Disconnect the airplane battery. C. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" writtenonthem. 2. Remove and replace the control-column internal glide attach-screw on the pilot's control column as follows: A. (Refer to Figure 1, Detail A.) To get access to the control-column internal glide attach-screw, remove the control wheel from the control column. (Refer to the applicable maintenance manual.) B. If installed, remove the control wheel gust lock from the pilot's control column. C. Make sure that the elevators are at the fully down position and that the ailerons are at the neutral position. D. Remove and discard the old screw. E. Cut a section of steel safety wire to approximately 24 inches in length. Revision 2 - April 20, 2012 Page 3

6 F. Install the new MS Screw and the 0.20 steel safety wire as follows: (1) {Refer to Figure 1, Detail B (Step 1).} Put one end of the safety wire through the large diameter hole and through the gap between the square tube and the stake nut support, and pull the two ends of the safety wire aft until they come together aft of the square tube. Make sure that you install the safety wire through the large diameter hole and not through one of the 0.25-inch diameter holes for the gust lock. If the square tube is installed with the large diameter hole on the top surface of the square tube, make sure that the safety wire goes through the gap between the right side of the square tube and the stake nut support. If the square tube is installed with the large diameter hole on the bottom surface of the square tube, make sure that the safety wire goes through the gap between the left side of the square tube and the stake nut support. NOTE: The square tube may be installed with the large diameter hole on the top surface or on the bottom surface of the square tube. (2) {Refer to Figure 1, Detail B (Step 2) and View A-A.} At the corner (on the outer diameter) of the aft end of the square tube, begin to twist the two parts of the safety wire together until the twisted section is approximately one inch in length. Make sure that you do not twist the safety wire on the end surface of the square tube. (3) {Refer to Figure 1, Detail B (Step 3).} Install the glide, plug (if installed), and the MS Screw. NOTE: On some installations, the square tube is not centered in the control tube. As you install the screw, to make it easier to align the hole in the plug with the screw hole in the square tube, you can use one hand to move the control tube left, right, up, or down as applicable. Make sure that you install the glide with one of the troughs between the lobes turned straight up. As you do the installation, make sure that you keep the safety wire in the trough between two of the lobes of the glide. (4) {Refer to Figure 1, Detail B (Step 4).} Tighten the MS Screw until there is no lateral free play in the control column between the glide and the outer control tube and there is no friction through the full range of travel of the control column. To make sure that there is no friction, move the control column forward and aft through the full range of travel while you adjust the MS Screw. As you move the control column, make sure that the orientation of the glide stays the same. If the glide configuration on the airplane does not include a plug, tighten the MS Screw until the glide fits snugly against the square tube. (5) {Refer to Figure 1, Detail B (Step 5), View B-B, and View C-C.} Finish the installation of the safety wire through the head of the MS Screw. (Refer to the applicable maintenance manual.) (6) Move the control column forward and aft through the full range of travel while you make sure that the safety wire does not rub against the control tube. 3. Remove and replace the control-column internal glide attach-screw on the copilot's control column as follows: A. (Refer to Figure 1, Detail A.) To get access to the control-column internal slide attach-screw, remove the control wheel from the control column. (Refer to the applicable maintenance manual.) B. If installed, remove the control wheel gust lock from the pilot's control column. C. Make sure that the elevators are at the fully down position and that the ailerons are at the neutral position. D. Remove and discard the old screw. Page 4 Revision 2 - April 20, 2012

7 E. Cut a section of steel safety wire to approximately 24 inches in length. F. Install the new MS Screw and the 0.20 steel safety wire as follows: (1) {Refer to Figure 1, Detail B (Step 1).} Put one end of the safety wire through the large diameter hole and through the gap between the square tube and the stake nut support, and pull the two ends of the safety wire aft until they come together aft of the square tube. Make sure that you install the safety wire through the large diameter hole and not through one of the 0.25-inch diameter holes for the gust lock. If the square tube is installed with the large diameter hole on the top surface of the square tube, make sure that the safety wire goes through the gap between the right side of the square tube and the stake nut support. If the square tube is installed with the large diameter hole on the bottom surface of the square tube, make sure that the safety wire goes through the gap between the left side of the square tube and the stake nut support. NOTE: The square tube may be installed with the large diameter hole on the top surface or on the bottom surface of the square tube. (2) {Refer to Figure 1, Detail B (Step 2) and View A-A.} At the corner (on the outer diameter) of the aft end of the square tube, begin to twist the two parts of the safety wire together until the twisted section is approximately one inch in length. Make sure that you do not twist the safety wire on the end surface of the square tube. (3) {Refer to Figure 1, Detail B (Step 3).} Install the glide, plug (if installed), and the MS Screw. NOTE: On some installations, the square tube is not centered in the control tube. As you install the screw, to make it easier to align the hole in the plug with the screw hole in the square tube, you can use one hand to move the control tube left, right, up, or down as applicable. Make sure that you install the glide with one of the troughs between the lobes turned straight up. As you do the installation, make sure that you keep the safety wire in the trough between two of the lobes of the glide. (4) {Refer to Figure 1, Detail B (Step 4).} Tighten the MS Screw until there is no lateral free play in the control column between the glide and the outer control tube and there is no friction through the full range of travel of the control column. To make sure that there is no friction, move the control column forward and aft through the full range of travel while you adjust the MS Screw. As you move the control column, make sure that the orientation of the glide stays the same. If the glide configuration on the airplane does not include a plug, tighten the MS Screw until the glide fits snugly against the square tube. (5) {Refer to Figure 1, Detail B (Step 5), View B-B, and View C-C.} Finish the installation of the safety wire through the head of the MS Screw. (Refer to the applicable maintenance manual.) (6) Move the control column forward and aft through the full range of travel while you make sure that the safety wire does not rub against the control tube. 4. Install the control wheel(s) on the control column(s). (Refer to the applicable maintenance manual.) 5. Remove maintenance warning tags from battery and external power receptacle and connect the battery. Revision 2 - April 20, 2012 Page 5

8 6. Make an entry in the airplane logbook that states compliance and method of compliance with this service bulletin. NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for Continued Airworthiness and must be accomplished for ongoing Airworthiness Compliance as necessary in accordance with 14 CFR Part Page 6 Revision 2 - April 20, 2012

9 Figure 1. Control-Column Internal Glide Attach-Screw Installation - Typical Glide Shown (Sheet 1) Revision 2 - April 20, 2012 Page 7

10 Figure 1. Control-Column Internal Glide Attach-Screw Installation - Typical Glide Shown (Sheet 2) Page 8 Revision 2 - April 20, 2012

11 Figure 1. Control-Column Internal Glide Attach-Screw Installation - Typical Glide Shown (Sheet 3) Revision 2 - April 20, 2012 Page 9

12 MATERIAL INFORMATION Order the part below to install this modification. NEW P/N QUANTITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION MS As required Screw Page 10 Revision 2 - April 20, 2012

13 OWNER ADVISORY TITLE FLIGHT CONTROLS - CONTROL-COLUMN INTERNAL SLIDE ATTACH-SCREW INSTALLATION TO: Cessna 177, 182, 205, 206, 207, or 210 Owner: REASON This owner advisory is to inform you that Revision 2 has been issued. If the control-column internal glide attach-screw is not correctly attached, it can loosen and fall off inside the control column tube. This condition can cause looseness of the control column and the fallen screw may limit full range of elevator control. Control-Column Internal Slide Attach-Screw Installation was issued to provide parts and instructions to remove the control-column internal slide attach-screw and install a new one steel wire is used to safety the screw to the installation as specified in this service bulletin. Revision 2 has been issued to divide the airplane serials in the Effectivity section into two groups. Group A lists the airplane serials that require modification of the glide screw on the pilot's and the copilot's control column and Group B lists the airplane serials that require modification of the glide screw on the copilot's control column only. Revision 2 also adds instruction for tightening of screws in configurations where there is no plug installed. COMPLIANCE Mandatory: Shall be accomplished at the next 100-hour inspection or 12-month (annual-type) inspection, whichever occurs first. NOTE: Compliance with Revision 2 is not required if in compliance with the Original Issue or Revision 1. This service bulletin supersedes Cessna Service Bulletin SB , Control-Column Internal Slide Attach-Screw Inspection. Airplanes in compliance with Cessna Service Bulletin SB , Control-Column Internal Slide Attach-Screw Inspection must also comply with this service bulletin. LABOR HOURS 1.5 man-hours to accomplish this service bulletin on the pilot's side. 1.5 man-hours to accomplish this service bulletin on the copilot's side. WARRANTY For airplanes identified within the serial effectivity in warranty on the original issue date of this service bulletin: Applicable parts credit and a labor allowance credit of 1.5 man-hours per airplane will be provided to accomplish this service bulletin on the pilot's side. Applicable parts credit and a labor allowance credit of 1.5 man-hours per airplane will be provided to accomplish this service bulletin on the copilot's side. Freight will be credited at the most economical method unless pre-approved by Cessna. For pre-approval contact Cessna Service Parts and Programs Warranty Administration at Telephone: , Fax: or cpd2claims@cessna.textron.com. Original Issue - February 28, 2012 Revision 2 - April 20, 2012 Page1of2 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , customercare@cessna.textron.com COPYRIGHT 2012

14 OWNER ADVISORY To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Authorized Service Facility within 30 calendar days of service bulletin compliance before the credit expiration dates shown below. Domestic... April 20, 2013 International... April 20, 2013 Please contact a Cessna Single Authorized Service Facility for detailed information and arrange to have Cessna Service Bulletin Revision 2 accomplished on your airplane. Special Note to Authorized Service Facilities: When you complete the Warranty Claim, the labor allowance claimed shall be itemized for each above action completed. NOTE: As a convenience, service documents are now available online to all our customers through a simple, free-of-charge registration process. If you would like to sign up, please visit the "Customer Access" link at to register. Page 2 Revision 2 - April 20, 2012