background image

Citation

SERVICE BULLETIN

SB750-55-10

TITLE

STABILIZERS - HORIZONTAL STABILIZER TRIM ACTUATOR ELECTRONIC CONTROL MODULE
IMPROVEMENT

EFFECTIVITY

MODEL

SERIAL NUMBERS

750 (Citation X)

-0001 thru -0313

REASON

The current horizontal stab trim actuator electronic control module (HTSA ECM) contains some
components that are becoming obsolete. An improved modular design HSTA ECM will be available as
a spares replacement, but will require wire termination and connector conversions during the initial
installation.

DESCRIPTION

This service bulletin contains the parts and instructions necessary to perform HSTA ECM wire termination
and connector conversions from the current HSTA ECM connector design to the spares replacement
HSTA ECM that includes product improvements.

COMPLIANCE

OPTIONAL. This service bulletin can be accomplished at the discretion of the owner.

A service bulletin published by Cessna Aircraft Company may be recorded as “completed” in an aircraft
log only when the following requirements are satisfied:

1)

The mechanic must complete all of the instructions in the service bulletin, including the intent
therein.

2)

The mechanic must correctly use and install all applicable parts supplied with the service bulletin
kit. Only with written authorization from Cessna Aircraft Company can substitute parts or rebuilt
parts be used to replace new parts.

3)

The mechanic or airplane owner must use the technical data in the service bulletin only as
approved and published.

4)

The mechanic or airplane owner must apply the information in the service bulletin only to aircraft
serial numbers identified in the “Effectivity” section of the bulletin.

5)

The mechanic or airplane owner must use maintenance practices that are identified as acceptable
standard practices in the aviation industry and governmental regulations.

No individual or corporate organization other than Cessna Aircraft Company is authorized to make or
apply any changes to a Cessna-issued service bulletin, service letter, or flight manual supplement without
prior written consent from Cessna Aircraft Company.

Cessna Aircraft Company is not responsible for the quality of maintenance performed to comply with this
document, unless the maintenance is accomplished at a Cessna-owned Citation Service Center.

APPROVAL

Cessna received FAA approval for the technical data in this publication that changes the airplane type
design.

Original Issue - June 27, 2012

SB750-55-10

Revision 4 - April 7, 2016

Page 1 of 18

Textron Aviation Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800

This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States

in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991

COPYRIGHT © 2012

Содержание SB750-55-10

Страница 1: ...issue and previous revisions to SB750 55 10 in their entirety REVISION COMPLIANCE NO EFFECT Airplanes previously modified by this service bulletin are not affected by this revision LOG OF REVISIONS Or...

Страница 2: ......

Страница 3: ...s or rebuilt parts be used to replace new parts 3 The mechanic or airplane owner must use the technical data in the service bulletin only as approved and published 4 The mechanic or airplane owner mus...

Страница 4: ...acturing Corp 526 Thorp Road Orlando FL 32824 To crimp contacts Daniels Crimper AMT4001 or equivalent Daniels Manufacturing Corp 526 Thorp Road Orlando FL 32824 To crimp terminals Daniels Crimper GMT2...

Страница 5: ...screws for installation later C Remove the quick release pins that attach the ECM to the base plate D Remove the ECM from the airplane and return to Cessna E Remove the six screws washers and nuts th...

Страница 6: ...1 16 Screws into the top and bottom holes of the 6738022 7 HSTA Controller Assemblies as shown I Refer to Figure 1 Detail B Install the four MS27039 1 20 Screws thru the aft side of the two 6738022 7...

Страница 7: ...as possible NOTE To make sure that the wire length will be sufficient all wires should be cut as close to the solder joints as possible D Do a check to make sure the wire bundles will reach the intend...

Страница 8: ...and EICAS switch in the ON position 5 Do a check of the pilot s split trim switch a Move the left half of the pilot s split trim switch for NOSE UP and then NOSE DOWN momentarily at least three second...

Страница 9: ...2 Run the trim system to full leading edge down position a Make sure the EICAS indicated position is 12 degrees 0 6 or 0 6 degrees b Make sure the EICAS position indication is not amber 3 Run the tri...

Страница 10: ...Identification Description and Operation 12 Put the AVIONICS and EICAS switch in the OFF position 13 Turn the power off A Disconnect external electrical power 14 Make sure that ICA 750 55 00001 HSTA E...

Страница 11: ...Citation SERVICE BULLETIN SB750 55 10 Figure 1 Horizontal Stabilizer Trim Actuator Electronic Control Module Improvement Sheet 1 SB750 55 10 Revision 4 April 7 2016 Page 9...

Страница 12: ...SB750 55 10 Page 10 Revision 4 April 7 2016 Citation SERVICE BULLETIN SB750 55 10 Figure 1 Horizontal Stabilizer Trim Actuator Electronic Control Module Improvement Sheet 2...

Страница 13: ...Citation SERVICE BULLETIN SB750 55 10 Figure 2 Horizontal Stabilizer Trim Actuator Electronic Control Module Wiring Modification Sheet 1 SB750 55 10 Revision 4 April 7 2016 Page 11...

Страница 14: ...SB750 55 10 Page 12 Revision 4 April 7 2016 Citation SERVICE BULLETIN SB750 55 10 Figure 2 Horizontal Stabilizer Trim Actuator Electronic Control Module Wiring Modification Sheet 2...

Страница 15: ...Citation SERVICE BULLETIN SB750 55 10 Figure 2 Horizontal Stabilizer Trim Actuator Electronic Control Module Wiring Modification Sheet 3 SB750 55 10 Revision 4 April 7 2016 Page 13...

Страница 16: ...SB750 55 10 Page 14 Revision 4 April 7 2016 Citation SERVICE BULLETIN SB750 55 10 Figure 2 Horizontal Stabilizer Trim Actuator Electronic Control Module Wiring Modification Sheet 4...

Страница 17: ...18 PV017 D38999 26FC4SN 2 Plug PV008 PV009 D38999 26FE8SN 2 Plug PV015 PV016 M81824 1 1 8 Splice MS15795 846 6 Washer MS21295 22 2 Screw MS27039 1 16 8 Screw MS27039 1 20 4 Screw MS24694 S50 6 Screw M...

Страница 18: ...es Electrical Wire Marked 2SC015 1N0SC023 M81044 12 22 9 48 Inches Electrical Wire Marked GV001 5PV007 M81044 12 22 9 48 Inches Electrical Wire Marked GV002 5PV010 M81044 12 22 9 12 Inches Electrical...

Страница 19: ...1 Nameplate Marked PV018 TMS3 16 1 50 2 Sleeve Marked 4SC0015 19PC013 TMS3 16 1 50 2 Sleeve Marked 3SC015 20PC013 TMS3 16 1 50 2 Sleeve Marked AJT023 1PV007 TMS3 16 1 50 2 Sleeve Marked BJT023 6PV007...

Страница 20: ...7 2016 Citation SERVICE BULLETIN SB750 55 10 NEW P N QUAN TITY KEY WORD REFERENCE INSTRUCTIONS DISPOSITION TMS3 16 1 50 2 Sleeve Marked SJT024 3PV010 TMS3 16 1 50 2 Sleeve Marked TJT024 1PV010 TMS3 1...

Страница 21: ...equired MATERIAL AVAILABILITY PART NUMBER AVAILABILITY COST SB750 55 10 0 SB750 55 10 1 Please contact Cessna Service Parts Programs for current cost and availability of parts listed in this service b...

Страница 22: ......

Отзывы: