Diamond ALERT SERVICE BULLETIN AIRCRAFT

Similar documents
Service Bulletin No.: DA Rev 0 Date Issued: 8 January, 1999 Title: Nose Gear Fork, Fatigue Page: 1 of 6

Service Bulletin No.: DAC Rev. 3 Date Issued: August 28, 2002 Title: Sensenich Propeller Installation Page: 1 of 8

Service Bulletin No.: DA Rev. 1 Date Issued: July 13, 2010 Title: Replacement of Steel MLG Struts with Aluminum MLG Struts

Service Bulletin No.: DAC Rev 0 Date Issued: 29 June 2017 Title: Removal of OAT/Clock AA Battery Page: 1 of 5

Service Bulletin No.: DAC Rev 0 Date Issued: 27 July 2018 Title: Installation of Diamond Flap Module and Microswitch Tray

Service Bulletin No.: DAC Date Issued: February 18, 2000 Title: Starting Vibrator Battery Installation Page: 1 of 6

Service Bulletin No.: DAC Rev 5 Date Issued: 26 November 2010 Title: Engine Fuel System Conversion from IO-240-B17B to IO-240-B3B

Part A Describes the procedure for the replacement of the Mitchell type tachometer. These parts are supplied in Kit A as described below.

Service Bulletin No.: DAC Rev 2 Date Issued: Oct 04, 2016 Title: Installation of LED Anti-Collision and Position light Assembly

Service Bulletin No.: DAC Rev 3 Date Issued: October 27, 1999 Title: 2-Speed Electric Prime Fuel Pump Page: 1 of 8

Service Bulletin No.: DA C , Rev.0 Date Issued: October 8, 1998 Title: Type II Fuel System/Pump Retrofit Page: 1 of 13

Service Bulletin No.: D42L Rev 2 Date Issued: 05 October 2012 Title: ADF System Improvements Page: 1 of 16

Service Bulletin No.: DAC Rev. 0 Date Issued: 25 August 2014 Title: Installation of a Heated Pitot Static Probe Page: 1 of 34 PRINT IN COLOUR

Single Engine MODIFICATION KIT

MAIN ROTOR RIGGING, VALIDATION OF. HELICOPTERS AFFECTED: Serial numbers through 65013, through 65023, 65025, and 65031

Service Bulletin No.: DAC Rev 3 Date Issued: 12 May 2017 Title: Installation of Improved Indicating Systems

MODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru

Service Bulletin No.: DAC Rev. 2 Date Issued: 28 January 2013 Title: Installation of backup Artificial Horizon Indicator

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32

Service Bulletin No.: D42L Rev 0 Date Issued: 06 June 2016 Title: GTX 33ES Installation Page: 1 of 6

Single Engine. Service Bulletin TITLE ELEVATOR TRIM TAB ACTUATOR ASSEMBLY INSPECTION EFFECTIVITY. Group A airplanes: Serial Numbers

Service Bulletin. ATA 52-10: Passenger and Crew Doors Door Latching Assembly Upgrade

ATTACHMENT. Orders for the required parts listed below must be placed by using this form only. Service Station/Company Code: Company Name:

CIRRUS AIRPLANE MAINTENANCE MANUAL

CHAPTER 4 GOVERNORS AND LINKAGE

Section 4 GOV. CONTROLS & GOVERNOR

FAA approval has been obtained on technical data in this publication that affects airplane type design.

SERVICE BULLETIN. AS350 Cargo Hook replacement kits manual release cable & bumper

Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification


1. SUBJECT: Cyclic Trim System Cyclic Trim Assembly Kit for the Lateral and Longitudinal Trim Actuator Assemblies

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

CIRRUS AIRPLANE MAINTENANCE MANUAL

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

"Figure 2: Trim Washer" was "Figure 1: Trim Washers". Page: 40A-06 REV 1: In Step 6, added "Fully torque the nut."

This Service Bulletin is applicable only to airplanes equipped with placards that are written in English.

Chapter 52 DOORS -Title

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

June 16, 1947 OPTIONAL CHANGE SERVICE BULLETIN NO. 17 INSTALLATION STEERABLE TAIL WHEEL. (Includes Supplement 1 and Supplement 2)

Revision Transmittal Sheet

12NPR Reason For Revision

SERVICE BULLETIN SB0017 Rev A Page 1 of 5

1139A. The New Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A Date: April 9, 2004 (S)(M)

Nomad FLIGHT CONTROLS -FITMENT OF MASS BALANCE TO RUDDER TAB

SERVICE BULLETIN SB

Maximum Motorsports Caster/Camber Plates (03-04 Cobra) - Installation Instructions

Nomad RUDDER CONTROL SYSTEM STRENGTHENING OF CABLE PULLEY MOUNTING AT STA (MOD N630)

PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR

CIRRUS AIRPLANE MAINTENANCE MANUAL

RIGGING THE FLIGHT CONTROLS

STEERING SYSTEM - MANUAL RACK & PINION

OPTIONAL SERVICE BULLETIN OSB OSB 42NG-062

CHAPTER 65 TAIL ROTOR DRIVE SYSTEM. Section Title Page

A Product Line of Sonex Aircraft LLC 511 Aviation Road Oshkosh, WI Tel. (920) Fax. (920)

S E R V I C E B U L L E T I N

MANDATORY SERVICE BULLETIN NO. MSB /1

Chapter 27. Flight Controls

OPTIONAL SERVICE BULLETIN OSB 40NG-007/1

COMPONENTS REAR DIFFERENTIAL COMPONENTS

SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair

CIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012

PROSPECTOR TRACK MOUNT KIT

SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN

Service Bulletin. SB-GA Issue 1. Subject: Horizontal Stabiliser Attachment Area Inspection and Reinforcement. Applicability: Amendments:

2. Remove front wheels.

SERVICE INFORMATION LETTER

PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524

SERVICE BULLETIN REVISION TRANSMITTAL

Service Bulletin No: Ref No: 165 Modification No: EC ATA Chapter: 21

Page: REV 3: Add drill and tap information to Figure 4 DRILL #3, TAP 1/4-28 BOTH ENDS.

SERVICE INSTRUCTION SI Revision 1

EFFECTIVITY Serial Numbers thru , 698

FOR REVIEW SERVICE BULLETIN SB-AG-65. Installation of Click Bond Electrical Grounding Spacer Stud on the Header Tank. Revision IR 11/20/2017

SERVICE KIT. TITLE McCAULEY 2A34C203/90DCA-2 TWO BLADED THREADLESS PROPELLER INSTALLATION

PARAVION TECHNOLOGY, INC AIRWAY AVENUE FORT COLLINS, COLORADO 80524

Fisher 2052 Diaphragm Rotary Actuator

Service Bulletin SB 07-03

Owner s Manual. PH-T-60-AOS-L-8 Swivel Mount Pintle Hook. XL-PH20032UM-en-US Rev A

SAFARI Helicopter Flight Control Rigging Manual Revision 9 4/3/2010 CHR International Inc.

Service Bulletin No: Ref No: 49 Modification No: EC ATA Chapter: 32

ALERT SERVICE LETTER

MANPOWER REQUIREMENTS

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

HSR Carburetor Sportster & Buell. Installation Manual. Revised 7/5/00

STEERING SYSTEM 6 A POWER STEERING

CALIPER BRAKE INSTALLATION AND MAINTENANCE MANUAL

Page REV 1: Added 'Step 2: See the "REMOVE THIS TAB, BOTH SIDES" callout near Detail A. Modify four SB375-4 Snap Bushings as shown.

FOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN.

Service Information Letter

FAA approval has been obtained on technical data in this publication that affects airplane type design.

w w w. h d o n l i n e s h o p. d e CRUISE CONTROL KIT GENERAL INSTALLATION -J04064 REV Kit Number Models Additional Parts Required

1154B. Piper Aircraft, Inc Piper Drive Vero Beach, Florida, U.S.A Date: March 28, 2007 (S)

SERVICE KIT thru , 631, 634, 675 R thru R F thru F FR thru FR

FRONT & 4 REAR GM WD LOWERING KIT

1. SUBJECT: : New Improved Tail Rotor Teeter Bearing Assembly. 2. MODELS: F28C, 280C, F28F, 280F, 280FX, TH-28 and 480 Helicopters

INSTALLATION MANUAL Models &

It has been determined that some airplanes may have a hose plug installed in the inflatable belt assembly hose end.

CHAPTER 15 WINCH MAINTENANCE. This chapter contains maintenance instructions for disassembly and repair of winch components at the Direct

Cable Shift Linkage Kit

Transcription:

Title: Throttle Cables, Replacement Page: 1 of 7 1. ATA Code: 7610 2. Effectivity: DA 20 Katana Aircraft S/N 10002 through 10300. 3. General: This service bulletin supersedes S.B. #DA20-76-01A Rev 4. A long life throttle control cable is installed to replace the existing cable type which currently requires replacement every two hundred hours. An improved throttle friction adjustment is incorporated. The friction force is preset by maintenance personnel to a minimum level. Fine adjustment is then made by the pilot using the existing friction control knob. 4. Compliance: At the next 100 hour inspection. 5. Approval: Engineering data referenced or contained in this bulletin is approved as part of the type design. 6. Labor: 2.5 hours. 7. Material: Item Qty Part Number Description 1 1 MS24665-172 Cotter Pin 2 1 MS14144 L3 Castellated Nut 3 2 20-7600-01-96 Inner Wire 4 2 AN960C10 Washer 5 1 AN3C10 Bolt 6 1 20-7600-01-97 Return Spring, Left 7 1 20-7600-01-98 Return Spring, Right 9 1 AN960C10L Washer 10 1 DS-50 Spring Washer 11 1 20-7610-01-08 Spacer 12 1 165-061 Nut, Self Locking 13 4 654-014 Washer, Nylon 14 2 W-513 Washer, Brass 15 1 HC 143 Bolt, 2 1/4" 16 2 W-5006 Washer 17 1 HC 144 Bolt, 2 1/2" The above items may be ordered as kit DA20-76-01MK5. Parts required for S/N 150 and below see Accomplishment Instructions 10.1 Item Qty Part Number Description 8 2 20-7600-01-13 Conduit, Control Throttle Aeroshell Grease 5, Loctite 495 (or equivalent instant adhesive) procure locally. 8. Special Tools: Not Applicable. 9. References: Doc #DA201 Maintenance Manual.

ALERT Title: Throttle Cables, Replacement Page: 2 of 7 10. Accomplishment Instructions: 10.1 Inspect the throttle-control conduit for damage and replace if required before performing this service bulletin. Aircraft S/N 150 and below have longer 41 inch 'Throttle Cable Conduits' installed which need to be replaced with 39 inch conduits to accommodate the new inner wires. 10.2 Remove the throttle-quadrant friction-knob and temporarily install a 5/16-24 nut to prevent loss of any parts. 10.3 Remove the screws holding the throttle quadrant. Pull the throttle quadrant up enough to gain access to the throttle cables and remove the inner-wire retaining-hardware. Discard the bolt, washers and nut. Keep the bushings. 10.4 Cut the 90 degree bend off the end of the inner-wire throttle-cable at the throttle quadrant. 10.5 Loosen the nut on the swivel on the throttle lever arms and pull the cables forward out of the throttle-control conduit. 10.6 Remove the throttle lever arm, spring and stop lever from the left carburetor and install the left return spring as shown in figure 1. The spring is installed so that it aids the existing spring in opening the throttle. 10.7 Repeat the procedure of 10.6 for the right carburetor. 10.8 Reinstall the stop lever, throttle lever and spring on the left and right carburetor. 10.9 Refer to Figure 3. Disassemble the throttle quadrant as shown discarding the parts as indicated. Reassemble the throttle quadrant adding the new parts and orienting the DS-50 washers as shown. Torque the 5/16-24 nut to 5-5.4 ft.lbs ( 6.8-7.3 Nm). Note: For A/C serial numbers 10002 to 10200 use the 2 1/2" bolt. For A/C serial numbers 10201 to 10300 use the 2 1/4" bolt. 10.10 Refer to figure 4. Use Loctite 595 (or equivalent instant adhesive) to bond the existing bushings into the throttle lever. 10.11 Insert the new inner cables from the throttle quadrant end. 10.12 Install the throttle cable retaining hardware (see 10.12 and 10.13) in the order shown in figure 4, detail 'A'. Lubricate the bolt with Aeroshell Grease 5. 10.13 Tighten the throttle cable retaining hardware until the cable eyelets do not rotate independently of each other. Back off the nut by 3/4 of a turn. The Cable eyelets should rotate freely and independently of each other. Check that there is no possibility of interference between the bolt head and the throttle-quadrant center-frame due to excessive side play. If the bolt head interferes with the center frame install the washers as shown in figure 4 'Detail B'.

Title: Throttle Cables, Replacement Page: 3 of 7 Figure 1 Figure 2

Title: Throttle Cables, Replacement Page: 4 of 7 Figure 3

Title: Throttle Cables, Replacement Page: 5 of 7 Figure 4

Title: Throttle Cables, Replacement Page: 6 of 7 Figure 5

Title: Throttle Cables, Replacement Page: 7 of 7 10.14 Insert the cotter pin and bend it to obtain the lowest possible profile. Check for interference between the cotter pin and the structure through the full travel of the throttle lever. Check for interference between the cotter pin and the throttle-quadrant top-plate through the full travel of the throttle lever. 10.15 If necessary remove a small amount of FRP to maintain adequate bolt clearance from the structure. 10.16 Reinstall the throttle quadrant leaving the friction knob, spacer and DS-50 washer off. 10.17 Pull throttle lever to idle stop. 10.18 Thread the inner wire through the hole in the swivel. Check that the position of the washers is correct (Figure 2). 10.19 Move the throttle arm on the carburetor to the idle stop (it may be easier to remove the spring on the throttle arm). While gently pulling the inner throttle cable forward and holding the throttle lever to idle stop, tighten the throttle arm swivel. Lubricate the swivel with Aeroshell Grease 5. Ensure that the swivel can rotate freely. 10.20 Refer to figure 5. With throttles rigged (ie. all springs installed) adjust the self locking nut so that a preload force of 4.5 lbs min (2 Kg) is required to pull the throttle lever aft when it is a point 0.25" (6mm) before the end of travel. 10.21 Install the spacer, DS-50 washer and friction knob. 10.22 Conduct a test run. If idle to 1500 rpm is rough, carburetor synchronization must be carried out as per Maintenance Manual Chapter 71-00 Page 16. 11. Weight and Balance: Negligible 12. Electrical Load Data: Not Applicable 13. Credit: A full parts credit and labor credit of will be issued upon receipt of a completed warranty claim form when received within 90 days from the issue date of this service bulletin. To obtain satisfactory results, procedures specified in this service bulletin must be accomplished in accordance with accepted methods and current government regulations. Aircraft Industries Inc. cannot be responsible for the quality of work performed in accomplishing the requirements of this service bulletin. Aircraft Industries Inc. 1560 Crumlin Sideroad, London, Ontario, Canada N5V 1S2 Phone: (519) 457-4041 Fax: (519) 457-4045 COPYRIGHT 1997