SERVICE BULLETIN TFE731-76-3065

overshoot, driving transients and the need for constant power lever adjustment during take-off and climb. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 2 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 1. B. (1) (b) The current engine controls are aging, they are expensive to repair and parts are difficult to locate. (c) The current engine controls do not have the capability of automatic monitoring and recording of data necessary for engine condition trending. (2) Background: The N1 DEEC has been developed as a replacement for the original analog and digital controllers for the TFE731 engine. Using the latest circuit design and components and digital technology, this light-weight, reliable, directly interchange- able unit reduces the pilot’s workload and maintenance effort by controlling engine fan speed directly and automatically recording engine and flight parameters. Direct control on N1 allows automatic, stable thrust setting throughout takeoff, climb and cruise and eliminates “trimming” required with the previous N2 controls. Engine start logic has been improved to provide automatic enrichment, eliminating the need to utilize the cockpit SPR/Fuel Enrich switch during engine start. Increased fault detection has been added to aid in trouble shooting. The Engine Condi- tion Trend Monitoring (ECTM) software integrated into the controller automatically records all data needed to track component life, fault detection and reporting, trouble- shooting and parameter exceedance events. (3) Action: Refer to Figure 1, Service Bulletin Incorporation Flow Chart, for a process overview, and comply with the following. NOTE: The fault monitoring capability of the N1 DEEC is more capable than the older controllers. Therefore in some cases when the N1 DEEC is installed, LRU and wiring faults that were not detected by by older controllers will be de- tected by the N1 DEEC requiring the repair or replacement of LRUs or wiring. (a) Install N1 DEEC(s) as applicable in the aircraft. Engine Model Old Part No. New Part No. TFE731-4R-2S 2118002-41/-42 2119010-7000 TFE731-5BR-1C/-2C 2118002-51/-52/-60 2119010-9000 TFE731-5R/-5BR-1H 2118002-6/-62 2119010-8000 TFE731-5-1J 2118002-6/-8/-9/ 2119010-2 2119010-2001 (b) Complete N1 DEEC Installation Data Work Sheet. (c) Install ECTM Software on personal computer (PC) and configure ECTM soft- ware. (d) Perform N1 DEEC download operations and enter engine statistics. (e) Perform N1 DEEC static adjustments. (f) Perform N1 DEEC Built-In-Test (BIT) fault verification. (g) Perform engine test run to verify proper overspeed solenoid operation. (h) Conduct operational check and update installation documentation. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 3 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. READ ENTIRE SERVICE BULLETIN FOR FAMILIARITY START END INSTALL N1 DEEC (PARAGRAPH 2.A.) PERFORM ENGINE ACCELERATION TEST AND TAKE-OFF N1 CHECK (PARAGRAPH 2.H.) PERFORM STATIC N1 DEEC ADJUSTMENT (PARAGRAPH 2.E.) CONFIGURE ECTM, PERFORM ECTM DOWN- LOAD AND ENTER ENGINE STATISTICS (PARAGRAPH 2.D.) PERFORM ENGINE RUN TO VERIFY OVERSPEED SOLENOID OPERATION (PARAGRAPH 2.G.) CHECK FOR N1 DEEC BIT FAULTS (PARAGRAPH 2.F.) COMPLETE N1 DEEC DATA WORKSHEET (PARAGRAPH 2.B.) INSTALL ECTM SOFTWARE (PARAGRAPH 2.C.) COMPLETE THE ATTACHED COMPLIANCE CERTIFI- CATE AND RETURN TO ENGINES, SYSTEMS & SERVICES (PARAGRAPH 2.H.) Service Bulletin Incorporation Flow Chart Figure 1 SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 4 TFE731-76-3065July 28/97 Revision 9, Feb 20/03 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 1. C. Description This service bulletin provides instructions to install N1 DEEC, Part No. 2119010-2001/ 2119010-7000/2119010-8000/2119010-9000 (as applicable). Also provided are instructions for the use of TFE731 ECTM plus Kit. Part number information for the TFE731 ECTM plus Kit and other tooling necessary to support the installation of the N1 DEEC are provided in Para- graph 1.H. D. Compliance Compliance addresses durability, maintainability, or product improvement. NOTE: The procedures outlined in this service bulletin may be accomplished at Line Maintenance level or greater. +MSP Yes [X] or No [ ] +Special Program No. 27 Yes [X] or No [ ] #MSP Yes [ ] or No [X] #Warranty Coverage Yes [X] or No [ ] +TFE731-5B/-5BR-1H, TFE731-5BR-1C/-2C. #TFE731-5-1J. +TFE731-4R-2S. This service bulletin may be accomplished at operator’s option. However, when complying with this service bulletin, the aircraft Supplemental Type Certificate (STC) must be complied with concurrently when installing the N1 DEEC. Applicable STC is as follows. Aircraft Model No. Engine Model No. STC Cessna Citation VII TFE731-4R-2S ST01756CH-D Falcon 900B TFE731-5BR-1C ST01444CH-D Falcon 20-5 TFE731-5BR-2C ST01445CH-D Hawker 800 TFE731-5R-1H ST01424CH-D Hawker 800XP TFE731-5BR-1H ST01424CH-D CASA 101 TFE731-5-1J *NA *Must be in compliance with Construcciones Aeronauticas S.A. (CASA) Service Bulletin SB-101-76-02. E. Approval The change to the engine type design authorized by this service bulletin complies with applicable Federal Aviation Regulations and is FAA approved. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 5 TFE731-76-3065July 28/97 Revision 9, Feb 20/03 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 1. F. Manhour Requirements An estimated two manhours are required for completion of this service bulletin. G. Material - Price and Availability (TFE731-4R-2S, TFE731-5BR-1C/-2C, TFE731-5BR/-5R-1H) A special program may be available for this modification, under certain conditions, providing compliance recommenda- tions of Paragraph D are met. Information on special program and availability of parts may be obtained from a Honeywell authorized service facility. (Refer to Service Information Letter (SIL) F731-3.) A listing of authorized service facilities is also available on e-engines (www.e- engines.honeywell.com). (TFE731-5-1J) Warranty coverage may be available for this modification, under certain conditions, providing compliance recommendations of Paragraph D are met. Information on special program and availability of parts may be obtained from a Honeywell authorized ser- vice facility. (Refer to Service Information Letter (SIL) F731-3.) A listing of authorized service facilities is also available on e-engines (www.e-engines.honeywell.com). H. Tooling - Price and Availability Review the following ground support equipment for use in accomplishing the instructions outlined in this service bulletin in addition to tooling listed in publications referenced in Paragraph J. Part No. Nomenclature *Unit List Price +831702-19 Kit, ECTM plus #831702-20 Kit, ECTM plus %4243811-All J2 Extension Cable Customer Furnished Personal Computer *Information regarding price and availability of ground support equipment may be obtained from Honeywell Engines, Systems & Services, Customer Support Center, M/S 26-06/2102-323, P.O. Box 29003, Phoenix, AZ 85038-9003, Telephone: (Domestic) 1-800-421-2133 (International) 1-602-365-2180, FAX: 1-602-365-3343. NOTE: Kit, ECTM plus, Part No. 831702-5/-6/-12/-13, may be reworked per Service Bulletin 831702-SB NO. 2, refer to Paragraph 1.K. +Kit, ECTM plus, Part No. 831702-5/-12/-19 (-5/-12 are obsolete and no longer available for ordering), enables the ECTM data to be downloaded from the N1 DEEC. This kit is avail- able to the operator at no charge, one kit per aircraft, following the purchase of the N1 DEEC. This kit consists of ECTM software (Users Manual 21-9505 information is now part of the software), and required cables for use with a PC (customer supplied) to comply with this service bulletin. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 6 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. #Kit, ECTMplus, Part No. 831702-6/-13/-20 (-6/-13 are obsolete and no longer available for ordering), provides the Service Center with the software and cables required to interface with all N1 DEEC TFE731 engine applications. This complete ECTM plus kit allows the Service Centers to support the operator’s installation, downloading, maintenance, and trou- bleshooting needs. Only one Kit, Part No. 831702-6/-13/-20, per service center is required. %J2 Extension Cable, Part No. 4243811-All. Refer to aircraft certification documents for spe- cific cable part number used and installation instructions. Its purpose is to extend the J2 connector on the N1 DEEC to a point which is more convenient for communications with the PC and may be permanently installed per aircraft certification documents for ease of con- nection during future maintenance actions that involve the PC. 1. I. Weight and Balance (TFE731-4R-2S) Replacing DEEC, Part No. 2118002-41/-42, weight difference from this change is minus (-) 8.95 pounds per unit. (TFE731-5-1J) Replacing DEEC, Part No. 2118002-6/-8/-9, weight difference from this change is minus (-) 8.95 pounds. (TFE731-5-1J) Replacing N1 DEEC, Part No. 2119010-2, no weight (change) difference. (TFE731-5BR/-5R-1H) Replacing DEEC, Part No. 2118002-6/-62, weight difference from this change is minus (-) 8.95 pounds per unit. (TFE731-5BR-1C/-2C) Replacing DEEC, Part No. 2118002-51/-52/-60, weight difference from this change is minus (-) 8.95 pounds per unit. J. Publications References The sources of information used in the preparation of this service bulletin include Honeywell engineering documentation and the following. Part/ Model No. Heavy Maintenance Manual Light Maintenance Manual Illustrated Parts Catalog TFE731-4R-2S NA *72-02-33 *72-02-32 TFE731-5-1J NA *72-02-75 *72-02-29 TFE731-5R-1H NA *72-02-75 *72-02-51 TFE731-5BR-1C NA *72-02-96 *72-02-95 TFE731-5BR-1H NA *72-02-96 *72-02-95 TFE731-5BR-2C NA *72-02-96 *72-02-95 *Affected Chapter/Section/Subject 76-10-02, 76-10-03 (as applicable). SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 7 TFE731-76-3065July 28/97 Revision 9, Feb 20/03 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 1. K. Service Bulletin References The following shall be accomplished prior to or concurrent with this service bulletin. The accomplishment instructions outlined in each service bulletin stand alone; therefore com- pliance with this service bulletin does not indicate compliance with any other service bulletin. Service Bulletin No. Service Bulletin Title 831702-SB NO. 2 TFE – ECTM GROUND SUPPORT EQUIPMENT KIT - Install Version 5.1 Software Incorporation of the following is recommended at the time this service bulletin is accomplished. Service Bulletin No. Service Bulletin Title TFE731-72-3397 (Rev 2 or subsequent revisions) ENGINE – Initiate Component Maintenance/Modification Record Card (Card-Log Book) Accomplishment of the following will no longer be applicable when the equipment has been modified in accordance with the accomplishment instructions outlined in this service bulletin. Service Bulletin No. Service Bulletin Title #TFE731-76-3041 ENGINE – CONTROLS – Install Electronic Engine Control (EEC), Part No. 2118002-6 +TFE731-76-3043 ENGINE – CONTROLS – Install Electronic Engine Control (EEC), Part No. 2118002-6 +TFE731-76-3047 ENGINE – CONTROLS – Install Digital Electronic Engine Control (DEEC), Part No. 2118002-9 +TFE731-76-3052 ENGINE – CONTROLS – Digital Electronic Engine Control (DEEC), Part No. 2118002-6 or 2118002-8 Installation %TFE731-76-3053 ENGINE – CONTROLS – Install Digital Electronic Engine Control (DEEC), Part No. 2118002-52 **TFE731-76-3055 ENGINE – CONTROLS – Install Digital Electronic Engine Control (DEEC), Part No. 2118002-42 %TFE731-76-3057 ENGINE – CONTROLS – Install N1 Control Digital Elec- tronic Engine Control (DEEC), Part No. 2118002-60 **TFE731-4R-2S. #TFE731-5R-1H. +TFE731-5-1J. %TFE731-5BR-1C/-2C. L. Other Publications Affected Same as those listed under Paragraph J, Publications References. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 8 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. Accomplishment Instructions NOTE: Publications listed in Section 1 provide applicable disassembly, cleaning, inspection, reassembly, and testing instructions and shall be referred to during the accomplishment of the following instructions. Accomplishment instructions are divided into Paragraphs 2.A through 2.H. Paragraph 2.A provides instructions for installing the N1 DEEC, Paragraph 2.B fills out the N1 DEEC Installation Data Worksheet. Paragraph 2.C pro- vides instructions to install and configure the ECTM software, and Para- graphs 2.D through 2.H provide instructions on fault code downloading, programing, fault code corrective action and operation of the installed N1 DEEC. Refer to Paragraph 1.D for applicable aircraft certification docu- ments. Paragraphs 2.C through 2.H require a PC to be connected. All programs requiring port communication such as networking or fax modem programs must not share the same COM port as the ECTM program. Shar- ing the COM port will result in communication errors with the N1 DEEC. A. Install Digital Electronic Engine Control (N1 DEEC) (1) Gain access to and remove DEEC in accordance with the Aircraft Maintenance Manual and the Engine Light Maintenance Manual. (2) Install N1 DEEC, Part No. 2119010-2001, 2119010-7000, 2119010-8000, or 2119010-9000 (as applicable) in accordance with the Aircraft Maintenance Manual, and the following instructions. (See Figure 2.) (a) Install N1 DEEC to the mount in accordance with the Aircraft Maintenance Manual. Refer to aircraft certification documents. (b) Connect the Pt2 pneumatic tube to the N1 DEEC Pt2 port. (c) Unplug the Ps0 port and leave open to ambient air as applicable per aircraft certification documents. (d) Connect DEEC wiring harness connector to the N1 DEEC J1 connector. (e) (As applicable) If installed, connect J2 extension cable to J2 connector. (3) Proceed to Paragraph 2.B. J1 J2 Pt2 Ps0 Part No. 2119010-X N1 DEEC Front Panel Figure 2 SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 9 TFE731-76-3065July 28/97 Revision 6, Aug 27/01 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. B. N1 DEEC Installation Data Worksheet (1) Reproduce a copy of the following worksheet for use as an N1 DEEC Installation Data Worksheet. (2) Fill out accordingly using previous control settings, N1 DEEC and engine nameplates and logbook. N1 DEEC Installation Data Worksheet Date:______________ Facility:_____________________ Technician/Operator:_____________________ Aircraft Tail #:___________________________ Aircraft Flight Hours:_______________ Comments/Reason for Down-load:_________________________________________________________ Engine Statistics: DATA EXAMPLES Engine Serial No. (Enter C designation if converted engine) 99999C = Conversion Engine Engine Part No. 3074970-3 Engine Model No. TFE731-5-1J N1 DEEC Part No.* 2119010-2001-01-00 (2119010=base number, -2001=dash number, -01=series number and -00=mod record) N1 DEEC Serial No.* 090-AG0001 *These numbers are provided for display example only. Data Tag Info Engine #1 Engine #2 Engine #3 Engine Model Engine P/N Engine S/N N1 DEEC P/N N1 DEEC S/N SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 10 TFE731-76-3065July 28/97 Revision 3, Apr 10/01 Copying, use or disclosure of information on this page is subject to proprietary restrictions. NOTE: For instructions on using the ECTM software, please refer to the ECTM (Version 5.0 or subsequent revisions) manual included within the software. This electronic manual can be accessed by clicking on “Help” on the menu bar. 2. C. Installing ECTM Software (1) Close all other programs. (2) Install the “ECTM” Installation Disk 1 in your A: or auxiliary drive. (3) Click on the MS Windows start button, located in the lower left hand corner of the MS Windows desktop and select “Run” from the start menu. (4) Type in the file location “A:\setup.exe” in the Run Dialog Box and click on “OK”. (5) Click on “Continue” from the welcome screen. (6) The next screen will set up the directory name (ECTM = Default) for the ECTM data download files and application software. Once you have determined the appropriate drive destination of the application software (typically “C:” drive), click “Next”. (7) When prompted, remove the ECTM Installation Disk 1 and insert Installation Disk 2, then click “OK” to continue the installation. (8) Installation is automatic. When completed, a program listing will appear on the MS Windows programs menu under “ECTM”. (9) Installation of the application software is now complete and you are ready to begin viewing TFE731 engine data. (10) Click on finish. (11) Go to the MS Windows desktop “Start” button, select “Programs”, the “ECTM” program group, then the “ECTM Version 5.X” program. (12) This will open the ECTM application. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 11 TFE731-76-3065July 28/97 Revision 3, Apr 10/01 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. D. DownLoading ECTM Data and Entering N1 DEEC/Engine Statistics NOTE: Downloading the N1 DEEC using ECTM software will erase all the N1 DEEC STORED faults. Engine condition trend monitoring is accomplished using the N1 DEEC, GSE cabling, a customer furnished personal computer, ECTM software, and for additional features, contact the JET CARE DATA MANAGEMENT FACILITY. The N1 DEEC automatically collects engine operational data and stores the information in the N1 DEEC memory. Downloading of the N1 DEEC allows customer access to raw data for typical maintenance action. Further data analysis may be provided by JET CARE. Basic features include: Recording control system faults. N1, N2 rolldown times. Exceedance peaks and duration. Engine operating and flight hours. Starts, landings, touch and go’s and landings without shutdowns for life cycle calculations. Event recording for significant events. Transfers to Manual Mode. Uncommanded engine shutdowns. Type 2 exceedances. Pilot events recorded when the pilot presses the SPR/ Fuel Enrich switch. For more events, refer to the Help File within the ECTM (Version 5.0 or subsequent revisions) software. Advanced features include: JET-CARE performance trending. Engine operational profile. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 12 TFE731-76-3065July 28/97 Revision 3, Apr 10/01 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. D. (1) Downloading the N1 DEEC data with ECTM software. (a) At first N1 DEEC installation and PRIOR to removal, swapping or reworking of the N1 DEEC, the N1 DEEC must be downloaded to assure data integrity. NOTE: ECTM software in the PC automatically correlates data files back to the engine serial number and historically sequences them. ECTM software will store the data files in an engine directory that is named per the serial number of the engine from which it was just removed from (in the case of an initial installation) or the engine on which it is currently located. The data file itself is named per the N1 DEEC serial number. For example: Engine SN: 91999 N1 DEEC SN: 090-AG0001 Download Count = 3 Upon ECTM data download, the following will be stored: Within the C:drive: Directory created: 91999.edr Data file created: 090-AG0001.003 NOTE: This following procedure is required only when the data downloader is first installed on the computer or the communication port settings have been changed. (b) Verify the PC communication port is set up properly using the following proce- dure. 1 Start the ECTM software by clicking the MS Windows “Start” button, then select “Programs”, the “ECTM” program group, then the “ECTM Version 5.X” program. 2 Select “CONFIGURE” on the menu bar. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 13 TFE731-76-3065July 28/97 Revision 3, Apr 10/01 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. D. (1) (b) 3 Select “HARDWARE” from the pulldown menu and validate the following typi- cal settings. NOTE: The following settings are typical. These settings may vary based on the PC being used. Adjust as appropriate. All programs requiring port communication such as net- working or fax modem programs must not share the same COM port as the ECTM program. Sharing the COM port will result in communication errors with the N1 DEEC. COM PORT COM1 Backup Media Drive Letter A: 4 Select the “OK” when entry is complete. (c) Perform the ECTM data download with the following procedure. 1 Connect the applicable COM port of the PC to the J2 connector on the N1 DEEC using the download/converter cable provided in the ECTM plus kit. 2 With the PC and appropriate cables installed and the ECTM data downloader software installed, turn the N1 DEEC power ON then OFF then ON. 3 Record the following information from the engine and N1 DEEC nameplates prior to download, as per Paragraph 2.B, N1 DEEC Installation Data Work- sheet. DATA EXAMPLES Engine Serial No. (Enter C designation if converted engine) 99999C = Conversion Engine Engine Part No. 3074970-3 Engine Model No. TFE731-5-1J N1 DEEC Part No.* 2119010-2001-01-00 (2119010=base number, -2001=dash number, -01=series number and -00=mod record) N1 DEEC Serial No.* 090-AG0001 *These numbers are provided for display (example) only. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 14 TFE731-76-3065July 28/97 Revision 3, Apr 10/01 Copying, use or disclosure of information on this page is subject to proprietary restrictions. NOTE: The default password when ECTM is first installed is “DOWNLOAD”. To change the password, go to the main menu, select “CONFIGURE” then “PASSWORD” and follow the screen prompts. 2. D. (1) (c) 4 When the main menu is displayed select the “DOWNLOAD AND CLEAR N1 DEEC DATA” button. 5 Enter the current password and click on the “OK” button. 6 Enter the aircraft tail number, press “Tab”, then enter engine flight hours to date. NOTE: The time and date can be changed by double clicking the time in the lower right hand corner of the MS Windows desktop or via the “Date/Time” functions within the MS Windows control panel. 7 If the date and time are correct, select the “Yes” button from the “Is This The Correct Date And Time” section. If the date and time are NOT CORRECT, exit the program and update the PC date and time via the control panel. Re-enter the program at Step 2.D.(1)(c)1. NOTE: In the ECTM software version 5.0 or subsequent revi- sions, there is an option called “Enter Engine Build Data”. This button is for life cycle data growth opportuni- ties and should be ignored and not checked. 8 If previous step is complete, and the date and time is correct, install a diskette in the A:drive (or drive appropriate based on hardware configuration set-up) and select the “START” button to begin the download. This step will save data currently stored in the N1 DEEC and clear the N1 DEEC for the installa- tion of new engine statistics. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 15 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. D. (1) (c) 9 When the “Download Comments” screen appears, type in comments. Exam- ples of typical comment information is as follows. a Mechanic/Operator name. b Aircraft tail number. c Aircraft flight hours. d Comments on observations/maintenance actions. e Reason for download. f (TFE731-5-1J) Click on the correct position (Engine/Other/Test Cell) for the DEEC being downloaded. g (TFE731-4R-2S, TFE731-5BR-1C/-2C, TFE731-5BR/-5R-1H) Click on the correct engine position (Left, Right, Center/Other/Test Cell) for the DEEC being downloaded. 10 Click on “CONTINUE” when comments are completed. NOTE: When first downloading a newly installed N1 DEEC, ECTM will save the data in c:\731ECTM\.EDR folder. All subsequent downloads will be saved in a folder accord- ing to the engine serial number. 11 ECTM will display an acknowledgement indicating the data has been suc- cessfully saved. Click “OK” and continue with Step 2.D.(2). (2) Enter engine statistics into N1 DEEC. (a) An “ENGINE STATISTICS” screen will be displayed. Enter/Verify the data into the following fields. NOTE: Ignore the fields marked N/A. No information is required in these areas. DATA EXAMPLES Engine Serial No. (Enter C designation if converted engine) 99999C Engine Part No. 3074970-3 Engine Model No. TFE731-5-1J N1 DEEC Part No.* 2119010-2001-01-00 (2119010=base number, -2001=dash number, -01=series number and -00=mod record) N1 DEEC Serial No.* 090-AG0001 *These numbers are provided for display (example) only. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 16 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. D. (2) (b) Select “STORE” and the new statistics data will be stored. If no data is changed a message that “no data has changed” will be displayed. (c) Select the “CONTINUE” button at this time and the downloader will return to the main menu display. (d) Proceed to Paragraph 2.E. E. N1 DEEC Static Adjustment NOTE: When the N1 DEEC is first installed, the engine configuration ID, SG setting, and N1 compensator value must be entered for proper operation. A value of “1” must be entered to indicate no compensation on engines that do not have an N1 compensator. (1) Set up. (a) Apply power to the N1 DEEC. (b) Start the ECTM software by clicking the MS Windows “Start” button, then select “Programs”, the “ECTM” program group, then the “ECTM Version 5.X” program. (c) When the main menu is displayed, select the “DEEC HHT COMMUNICATION” button. (d) At the prompt (>), type “ENG” and press “Enter”. (e) The N1 DEEC will return with SETUP DEEC (Y/N)?. 1 Typing “Y” will allow N1 DEEC adjustment and press “Enter”. 2 Typing “N” will return user to the prompt. (f) After a “Y” is entered, the N1 DEEC will respond with: ENG_ID: X (where “X” is the current setting) (g) Enter the appropriate engine ID value using Table 1, 2, 3, or 4 (as applicable). SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 17 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 1. N1 DEEC, Part No. 2119010-8000 Engine Model to Engine ID Value Engine Model Nozzle Engine ID Value Resulting PC Display TFE731-5R-1H Grumman 1 TFE731-5R-1H H800G TFE731-5R-1H *TR5000BA 2 TFE731-5R-1H H800 TR5000BA TFE731-5BR-1H *TR5000BR 5 TFE731-5BR-1H H800XP TR5000BR *TR50000XX is a Dee Howard thrust reverser. Table 2. N1 DEEC, Part No. 2119010-2001 Engine Model to Engine ID Value Engine Model Nozzle Engine ID Value Resulting PC Display TFE731-5-1J Standard 6 TFE731-5 C101CC Table 3. N1 DEEC, Part No. 2119010-9000 Engine Model to Engine ID Value Engine Model Nozzle Engine ID Value Resulting PC Display TFE731-5BR-1C Standard 1 TFE731-5BR-1C F900 STD Side Engine TFE731-5BR-1C TR 2 TFE731-5BR-1C F900 TR Center Engine TFE731-5BR-2C TR 3 TFE731-5BR-2C F20 TR TFE731-5BR-2C Standard 4 TFE731-5BR-2C F20 STD Table 4. N1 DEEC, Part No. 2119010-7000 Engine Model to Engine ID Value Engine Model Nozzle Engine ID Value Resulting PC Display TFE731-4R-2S Thrust Reverser 12 TFE731-4R-2S 2. E. (1) (h) Press “Enter” and the N1 DEEC will display the string corresponding to the En- gine ID Value selected. Confirm that the string displayed corresponds to the “Resulting PC Display” column in Table 1, Table 2, Table 3, or table 4 (as appli- cable), for the Engine ID Value selected. (i) Press “Enter” and the N1 DEEC will respond as follows. N1_COMP_ADJ: X (where “X” is the current setting) SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 18 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. E. (1) (j) Enter the N1 compensator value and press “Enter”. (k) Press “Enter” again and the N1 DEEC will respond as follows. SG: X (where “X” is the current setting) (l) Enter “5.0” for the SG setting and press “Enter”. (m) Press “Enter” again and the N1 DEEC will respond with: MMSW:(AM=0, MM=1) 0 (n) Pressing “Enter” will end the adjustment process and return user to the prompt. (o) Cycle power to the N1 DEEC. (p) Verify the adjustments entered are correct (see example below) by re-typing “ENG” and pressing “Enter”. The following displays/action required will be dis- played. Displayed Action Required Setup DEEC (Y/N)? Type “Y” and press “Enter” Eng_ID: X Confirm proper ID and press “Enter” N1_Comp_Adj: X Confirm proper N1 compensation number and press “Enter” SG: X Confirm and press “Enter” MMSW: (AM=0, MM=1) Confirm 0 and press “Enter” (q) If proper values are not observed, return to Step 2.E.(1)(d). NOTE: If this was the first ECTM download of a new N1 DEEC, there will be a configuration error, Fault 219. In order to clear this stored fault, the DEEC will have to be downloaded one more time. (r) Exit the DEEC HHT Communication Screen by selecting the “Return to Main Menu” button. (s) If this was the first ECTM download of an N1 DEEC just installed, perform a second download by accomplishing Steps 2.D (1)(c) 1 through 11. Proceed to Paragraph 2.F. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 19 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. F. Check for N1 DEEC Bit Faults NOTE: The N1 DEEC records faults in “CURRENT” and “STORED” memory locations. “CURRENT” faults indicate engine/control system anomalies which have occurred since last DEEC power cycle. Cycling DEEC power after a fault has occurred may remove a current fault from the “CURRENT” fault memory location. “STORED” faults are a history of “CURRENT” faults which have occurred. Cycling DEEC power will not erase stored faults. The most recent 50 faults are retained for display and ECTM download. Downloading ECTM will erase “STORED” faults. (1) Displaying “CURRENT” faults. (a) Apply power to the N1 DEEC. (b) Start the ECTM program and select “DEEC HHT Communication”. (c) Type “ERR” and press enter to display CURRENT faults. Press “Enter” to dis- play each fault until prompted. NOTE: If no codes are displayed, a “No Record” is displayed. Exit at any time using (esc) key. (d) The faults are listed in the following format. ERRXXX where: XXX is the fault code, refer to Table 5. (e) Correct any engine control system fault using the appropriate troubleshooting procedures listed in the Engine Light Maintenance Manual. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 20 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. F. (2) Displaying “STORED” Faults. (a) Type “FLT” and press “Enter” to display the STORED faults. (b) The faults are listed in the following format. FLTXXX,Y,HHH:MM:SS.T where: XXX=fault code, refer to Table 5. Y= fault severity. · 1 = Auto Mode normal operation (log only, no action required). · 2 = Auto Mode Dispatch capable, only fault code 237 (ECTM Memory Full or Event) will cause a slow (every 2 seconds) flash of the manual mode light after engine shutdown. All other level 2 severi- ty faults will be recorded in ECTM, but will not result in any flash- ing of the manual mode light (take correction action at earliest convenience). · 3 = Auto Mode Not Dispatch capable, fast (once per second) flash of the manual mode light after engine shutdown (download ECTM to determine cause of fault. Take corrective action prior to next flight). · 4 = Manual Mode transfer, manual mode light on (download ECTM to determine cause of fault. Take corrective action prior to next flight). · 5 = Pilot selected manual mode, Manual Mode light on (via cockpit switch). · HHH:MM:SS.T = Time stamp that shows the hours that the N1 DEEC has been powered since new (hours:minutes: seconds:tenths). (c) The N1 DEEC categorizes the severity of N1, N2 and ITT limitations per the Engine Light Maintenance Manual limits and assigns the following types: Type 1 exceedance requires download of ECTM data and logging of exceedance type, peak and duration in the Engine Log Book. Type 2 exceedance requires appropriate Engine Light Maintenance Manual or Heavy Maintenance Manual maintenance actions, a download of ECTM data and logging of exceedance type, peak and duration in the Engine Log Book. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 21 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. NOTE: Fault codes displayed in the previous step have occurred since last erasure of DEEC faults but do not necessarily exist at this time. These faults may have been the result of intermittent problems that are not duplicated during ground runs and are a useful aid in trouble shooting to prevent re-occur- rence. Some codes are not used for all applications. For fault severity explanation, refer to Step 2.F.(2)(b). When a “Section” is referenced in the following table, it pertains to a Section and the maintenance instructions in the Engine Light Maintenance Manual. The following fault code corrective action table is applicable only to N1 DEECs, Part No. 2119010-2001/2119010-7000, 2119010-8000/2119010-9000. Refer to applicable Engine Light Maintenance Manual for N1 DEEC fault code corrective actions for other N1 DEEC(s). Table 5. N1 DEEC Fault Code Corrective Action Fault Code Fault Description Fault Severity Problem LRU and/or Associated Harness Corrective Action 2 N1 OPEN OR SHORT TO GROUND 4 N1 Monopole and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 4 N1 SIGNAL CONDITIONER 4 DEEC Refer to Fault Code 2 for Corrective Action. Inspect DEEC harness for damage. If no damage is evident, replace DEEC using instructions in this service bulletin. 5 N1 NOT REASONABLE 4 N1 Monopole and Associated Harnesses Refer to Fault Code 4 for Corrective Action. 6 N1 MAX LIMIT 4 N1 Monopole and Associated Harnesses Refer to Fault Code 4 for Corrective Action. 8 N1 OUTPUT LOW 4 N1 Monopole and Associated Harnesses Refer to Fault Code 2 for Corrective Action. 9 UNCOMMANDED ACCELERATION 4 Various ECTM Download Required. Contact Honeywell Representative for Trouble- shooting. 12 N2 OPEN OR SHORT TO GROUND 4 N2 Monopole and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 22 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 5. N1 DEEC Fault Code Corrective Action (Cont) Fault Code Corrective Action Problem LRU and/or Associated Harness Fault Severity Fault Description 14 N2 SIGNAL CONDITIONER 4 DEEC Refer to Fault Code 12 for Corrective Ac- tion. Inspect DEEC harness for damage. If no damage is evident, replace DEEC using instructions in this service bulletin. 15 N2 NOT REASONABLE 4 N2 Monopole and Associated Harnesses Refer to Fault Code 14 for Corrective Ac- tion. 16 N2 MAX LIMIT 4 N2 Monopole and Associated Harnesses Refer to Fault Code 14 for Corrective Ac- tion. 23 ITT MAX LIMIT 2 ITT Harness and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 24 ITT MIN LIMIT 2 ITT Harness and Associated Harnesses Refer to Fault Code 23 for Corrective Ac- tion. 25 ITT RATE LIMIT 2 ITT Harness and Associated Harnesses Refer to Fault Code 23 for Corrective Ac- tion. 26 ITT SENSOR OPEN 2 ITT Harness and Associated Harnesses Refer to Fault Code 23 for Corrective Ac- tion. 30 DEEC PS0 MAX LIMIT 2 DEEC Disconnect pneumatic line from DEEC in accordance with Section 76-10-03. Clear DEEC faults by typing FER, then type ERR to verify that fault does not exist. If fault still exists, replace DEEC using instructions in this service bulletin. 31 DEEC PS0 MIN LIM- IT 2 DEEC Refer to Fault Code 30 for Corrective Ac- tion. 32 DEEC PS0 RATE LIMIT 2 DEEC Refer to Fault Code 30 for Corrective Ac- tion. 34 TT2 MAX LIMIT 4 DEEC Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 35 TT2 MIN LIMIT 4 PT2 Sensor and Associated Harnesses Refer to Fault Code 34 for Corrective Ac- tion. 36 TT2 RATE LIMIT 4 PT2 Sensor and Associated Harnesses Refer to Fault Code 34 for Corrective Ac- tion. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 23 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 5. N1 DEEC Fault Code Corrective Action (Cont) Fault Code Corrective Action Problem LRU and/or Associated Harness Fault Severity Fault Description 37 TT2 SENSOR OPEN 4 PT2 Sensor and Associated Harnesses Refer to Fault Code 34 for Corrective Ac- tion. 38 TT2 SENSOR SHORT 4 PT2 Sensor and Associated Harnesses Refer to Fault Code 34 for Corrective Ac- tion. 41 DEEC PT2 MAX LIMIT 4 DEEC Disconnect pneumatic line from DEEC in accordance with Section 76-10-02. Clear DEEC faults by typing FER, then type ERR to verify that fault does not exist. If fault still exists, replace DEEC using instructions in this service bulletin. 42 DEEC PT2 MIN LIMIT 4 DEEC Refer to Fault Code 41 for Corrective Ac- tion. 43 DEEC PT2 RATE LIMIT 4 DEEC Refer to Fault Code 41 for Corrective Ac- tion. 61 FCU TM OPEN 4 FCU and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 62 FCU TM SHORT TO GROUND 4 FCU and Associated Harnesses Refer to Fault Code 61 for Corrective Ac- tion. 64 FCU TM COIL 1 SHORT 4 FCU and Associated Harnesses Refer to Fault Code 61 for Corrective Ac- tion. 65 FCU TM COIL 1 OPEN 2 FCU and Associated Harnesses Refer to Fault Code 61 for Corrective Ac- tion. 66 FCU TM COIL 2 SHORT 4 FCU and Associated Harnesses Refer to Fault Code 61 for Corrective Ac- tion. 67 FCU TM COIL 2 OPEN 2 FCU and Associated Harnesses Refer to Fault Code 61 for Corrective Ac- tion. 70 FCU OVERSPEED SOLENOID OPEN 3 FCU and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 71 FCU OVERSPEED SOLENOID SHORT 3 FCU and Associated Harnesses Refer to Fault Code 70 for Corrective Ac- tion. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 24 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 5. N1 DEEC Fault Code Corrective Action (Cont) Fault Code Corrective Action Problem LRU and/or Associated Harness Fault Severity Fault Description 75 FCU TM SHORT 4 FCU and Associated Harnesses Refer to Fault Code 61 for Corrective Ac- tion. 78 DEEC OVERSPEED SOLENOID DRIVER FAILED 3 DEEC Refer to Fault Code 70 for Corrective Ac- tion. 80 SBV A SOLENOID OPEN 4 SBV A Solenoid and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 81 SBV A SOLENOID SHORT 4 SBV A Solenoid and Associated Harnesses Refer to Fault Code 80 for Corrective Ac- tion. 85 SBV B SOLENOID OPEN 4 SBV B Solenoid and Associated Harnesses Refer to Fault Code 80 for Corrective Ac- tion. 86 SBV B SOLENOID SHORT 4 SBV B Solenoid and Associated Harnesses Refer to Fault Code 80 for Corrective Ac- tion. 89 BVA SOLENOID DRIVER FAILED 4 DEEC Refer to Fault Code 80 for Corrective Ac- tIon. 90 FCU MM SOLENOID OPEN 4 FCU and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 91 FCU MM SOLENOID SHORT 4 FCU and Associated Harnesses Refer to Fault Code 90 for Corrective Ac- tion. 92 DEEC MM SOLENOID DRIVER OPEN 4 DEEC Refer to Fault Code 90 for Corrective Ac- tion. 93 DEEC MM SOLENOID DRIVER SHORT 3 DEEC Refer to Fault Code 90 for Corrective Ac- tion. 94 FCU BVB SOLENOID DRIVER FAILED 4 DEEC Refer to Fault Code 80 for Corrective Ac- tion. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 25 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 5. N1 DEEC Fault Code Corrective Action (Cont) Fault Code Corrective Action Problem LRU and/or Associated Harness Fault Severity Fault Description 102 CLIMB INDICATOR DRIVER OPEN OR SHORTED 2 DEEC Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 105 DEEC COLD JUNCTION COMPENSATOR EXCEEDS MAX 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 106 DEEC COLD JUNCTION COMPENSATOR BELOW MIN LIMIT 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 153 DEEC POSITIVE 10 VOLTS FAIL 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 155 DEEC EEPROM WRITE FAIL 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 156 DEEC TRIM VARIABLES DEFAULTED 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 157 DEEC GROUND ERROR 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 158 DEEC +/- 15 VOLT- AGE FAIL 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 183 DEEC WATCH DOG FREQUENCY ERROR 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 184 DEEC (COP) TIMEOUT 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 185 COP TEST FAILED 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 188 DEEC ROM CHECKSUM 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 189 SERIAL EEPROM CHECKSUM 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 26 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 5. N1 DEEC Fault Code Corrective Action (Cont) Fault Code Corrective Action Problem LRU and/or Associated Harness Fault Severity Fault Description 190 DEEC BUFFER1 BIT FAILED 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 210 thru 214 FCU PLA FAULT 4 PLA POT and Associated Harnesses Perform appropriate procedures specified in Section 72-00-00, Troubleshooting- Check Instructions, Paragraph 5 or 6. 218 DEEC OVERSPEED LOGIC FAILED 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 219 ENGINE HARNESS ID MISMATCH 4 DEEC, Setup or Harness Aircraft jumper pin(s) P1-u, v, w, x or CC faulted. Repair faulted jumper pin(s) in accordance with applicable aircraft manufacturers’ instructions. Verify DEEC setup per Paragraph 2.E. 221 DEEC PT2 TRANSDUCER FAULT 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 222 DEEC PT2 TRANSDUCER FAULT 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 233 **ENGINE TYPE 2 N1 EXCEEDANCE 3 ENG Type 2 N1 Exceedance has occurred. Re- fer to Section 72-00-00, Table 501 for cor- rective action. 234 **ENGINE TYPE 2 N2 EXCEEDANCE 3 ENG Type 2 N2 Exceedance has occurred. Re- fer to Section 72-00-00, Table 501 for cor- rective action. 235 **ENGINE TYPE 2 ITT EXCEEDANCE 3 ENG Type 2 ITT Exceedance has occurred. Re- fer to Section 72-00-00, Table 501 for cor- rective action. 237 ECTM DATA DOWN-LOAD REQUIRED 2 ENG Down-load of ECTM data from DEEC is required. Download ECTM data from DEEC in accordance with Step 2.D.(1). 240 OVERSPEED SOLENOID ACTUATION 1 ENG An overspeed event has occurred in which the overspeed solenoid was energized. Refer to Section 72-00-00, Table 501 for corrective action. 242 ECTM DATA CHECKSUM FAIL 1 DEEC Indicates ECTM data may be suspect. Per- form ECTM download per Step 2.D.(1). If problem persists, replace DEEC using instructions in this service bulletin. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 27 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. Table 5. N1 DEEC Fault Code Corrective Action (Cont) Fault Code Corrective Action Problem LRU and/or Associated Harness Fault Severity Fault Description 244 PS0 TRANSDUCER FAULT 2 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 245 PS0 TRANSDUCER FAULT 2 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 246 *ENGINE TYPE 1 N1 EXCEEDANCE 2 ENG Type 1 N1 Exceedance has occurred. Re- fer to Section 72-00-00, Table 501 for cor- rective action. 247 *ENGINE TYPE 1 N2 EXCEEDANCE 2 ENG Type 1 N2 Exceedance has occurred. Re- fer to Section 72-00-00, Table 501 for cor- rective action. 248 *ENGINE TYPE 1 ITT EXCEEDANCE 2 ENG Type 1 ITT Exceedance has occurred. Re- fer to Section 72-00-00, Table 501 for cor- rective action. 249 DEEC REAL TIME FAILURE 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 250 DEEC REAL TIME MONITOR 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 251 DEEC STACK OVERFLOW 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. 255 OVERFLOW 4 DEEC Perform ECTM data download per Step 2.D.(1) then replace DEEC using instruc- tions in this service bulletin. *Type 1 exceedance requires download of ECTM data and logging of exceedance type, peak and duration in the Engine Log Book. **Type 2 exceedance requires appropriate Engine Light Maintenance Manual or Heavy Maintenance Manual maintenance actions, a download of ECTM data and logging of exceedance type, peak and duration in the Engine Log Book. 2. F. (2) (d) Record any N1 DEEC faults for future maintenance actions. (e) Correct any engine control system faults using the appropriate troubleshooting procedures listed in the applicable Engine Light Maintenance Manual. (f) N1 DEEC bit fault check is now complete. (g) Proceed to Paragraph 2.G. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 28 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. G. Verify Overspeed Solenoid Operation (1) To transfer the N1 DEEC to Powered Manual Mode: (a) Apply power to the N1 DEEC. (b) Start the ECTM software by clicking the MS Windows “Start” button, then select “Programs”, then “ECTM” program group, then the “ECTM Version 5.X” program. (c) When the main menu is displayed, select the “DEEC HHT COMMUNICATION” button. (d) At the prompt (>), type ”ENG” and press “Enter”. (e) Perform required action per the following example. Displayed Action Required Setup DEEC (Y/N)? Type “Y” and press “Enter” Eng_ID: X Confirm proper ID and press “Enter” N1_Comp_Adj: X Confirm proper N1 compensation number and press “Enter” SG: X Confirm setting and press “Enter” MMSW: (AM=0, MM=1) Type a “1” and press “Enter” (2) Overspeed test. CAUTION: MANUAL MODE BATTERY STARTS ARE NOT RECOM- MENDED, BATTERY STARTS COULD RESULT IN AN OVER- TEMPERATURE AND DAMAGE THE TURBINE SECTION. NOTE: When the engine is started with powered manual mode selected, the N1 DEEC will actuate the overspeed solenoid at approximately 40-45% N2 speed momentarily. The engine will noticeably “Droop” to about 30-40% speed and recover to a normal start. (a) Perform an engine start in accordance with Aircraft Flight Manual and/or ap- propriate aircraft documents to idle with the N1 DEEC in powered manual mode. 1 If the engine exhibits the “Droop” at about 40-45% N2 speed and recovers to a normal start, the overspeed test is successful. 2 If the engine does not respond properly, first verify that powered manual mode was selected and repeat the test. 3 If manual mode was selected, perform the appropriate troubleshooting per Table 5 and the Engine Light Maintenance Manual to identify the problem component. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 29 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. G. (3) To transfer the N1 DEEC to Normal Mode: (a) At the prompt (>), type ”ENG” and press “Enter”. (b) Perform required action per the following example. Displayed Action Required Setup DEEC (Y/N)? Type “Y” and press “Enter” Eng_ID: X Confirm proper ID and press “Enter” N1_Comp_Adj: 1 Confirm proper N1 compensation number and press “Enter” SG: X Confirm setting and press “Enter” MMSW: (AM=0, MM=1) Type a “0” and press “Enter” (c) Proceed to Paragraph 2.H. H. Operational Check (1) Check engine(s) acceleration. If acceleration rate/time differs, and requires adjustment, the SG setting may be moved up or down as follows. NOTE: Raising SG will decrease (shorten) engine acceleration time. Lowering SG will increase (lengthen) engine acceleration time. Excessive upward adjustment is undesirable since it may result in engine compressor instability (surge) during rapid power lever advance. Excessive adjustment in the downward direction is also undesirable in that it may reduce engine acceleration capability to an undesirable extent and may result in lean blowout. To compensate for individual engine characteristics or installation effects, a typical variation in acceleration adjustment setting (SG) may be to decrease by one value (setting number), or increase by two values (setting number), however, adjustments are not limited to these values and may be increased or decreased as necessary. (a) Apply power to the N1 DEEC. (b) Start the ECTM software by clicking the MS Windows “Start” button, then select “Programs”, then “ECTM” program group, then the “ECTM Version 5.X” program. (c) When the main menu is displayed, select the “DEEC HHT COMMUNICATION” button. (d) At the prompt (>), type ”ENG” and press “Enter”. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 30 TFE731-76-3065July 28/97 Revision 9, Feb 20/03 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 2. H. (1) (e) Perform required action per the following example. Displayed Action Required Setup DEEC (Y/N)? Type “Y” and press “Enter” Eng_ID: X Confirm proper ID and press “Enter” N1_Comp_Adj: X Confirm proper N1 compensation number and press “Enter” SG: X Enter revised value of SG per Step 2.H.(1) and “NOTE” preceding Step (a), press “Enter” MMSW: (AM=0, MM=1) Confirm “0” and press “Enter” (f) Cycle power to the N1 DEEC. (g) Repeat the engine acceleration test. (h) Repeat SG adjustment as necessary. (2) Verify that N1 speed meets the required N1 of the day in the Aircraft Flight Manual takeoff charts. (a) Stabilize at idle for two minutes. (b) Advance power lever to N1 of the day. (c) Perform engine shutdown in accordance with the Aircraft Flight Manual and/or appropriate aircraft documents. (3) Check for faults in accordance with Table 5 or the Engine Light Maintenance Manual. (4) Update the Component Maintenance/Modification Record Card in accordance with Service Bulletin TFE731-72-3397 (Rev 2 or subsequent revisions) on the removed DEEC and installed N1 DEEC. NOTE: When complying with this service bulletin, revision (Rev 9), ensure that the revision number is entered in the engine log book when completing the following step. (5) Make entry in engine log book noting date of compliance, engine operating time, part number(s) and serial number(s) of installed component(s) (as applicable), and compliance with this service bulletin (and service bulletin revision number, if applicable). (6) Complete the attached Compliance Certificate form and send to Engines, Systems & Services. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 31 TFE731-76-3065July 28/97 Revision 8, Oct 11/02 Copying, use or disclosure of information on this page is subject to proprietary restrictions. 3. Material Information NOTE: Applicable illustrated parts catalogs and spare parts bulletins, dated later than the original issue date of this service bulletin, may introduce different parts for installation. Refer to these documents before ordering parts. Expendable parts, discarded in gaining access to the affected area of the equipment, are not included. The following parts are required to accomplish the instructions outlined in this service bulletin. New PN Quantity Unit Exchange List Price* Key Word Old PN Instructions- Disposition +2119010-2001 1 DEEC 2118002-6/-8/-9 or 2119010-2 D, O K @2119010-7000 1 DEEC 2118002-41/-42 D, O #2119010-8000 1 DEEC 2118002-6/-62 D, O %2119010-9000 1 DEEC 2118002-51/-52/ -60 D, O Disposition Code D. Return old part to Honeywell Engines, Systems & Services, Material Receiving, 1944 East Sky Harbor Circle, Phoenix, AZ 85034, “Attn: Core Dept”. State on packing list the shipper/invoice number. Identify (tag) part as removed in accor- dance with Service Bulletin TFE731-76-3065. Disposition Code K. Old and new parts are interchangeable. Disposition Code O. Replacement part is available on exchange basis or a special program may be available for this modification under certain conditions. Refer to Section 1, Paragraph G for program information. *Refer to Section 1, Paragraph G for program information. @TFE731-4R-2S. +TFE731-5-1J. #Used on both TFE731-5BR/-5R-1H engine models. %Used on both TFE731-5BR-1C/-2C engine models. SERVICE BULLETIN Engines, Systems & Services – Phoenix, Arizona Page 32 TFE731-76-3065July 28/97 Revision 9, Feb 20/03 Copying, use or disclosure of information on this page is subject to proprietary restrictions. ATTN: Technical Data Distribution FAX (602) 365-5577 (Phone (602) 365-2493) (No Header Sheet Required) SERVICE BULLETIN TFE731-76-3065 SUPPLEMENTAL TYPE CERTIFICATE (STC) ORDER FORM (NO CHARGE) NOTE: This STC is also available at www.e-engine.honeywell.com. Customer Name: Address: Shipping Address: (if different from above or provide email address if you prefer delivery via the internet) Aircraft Model and Serial No.: (Example Hawker 800-XXXX)
STC ST01424CH-D, Engine Model TFE731-5R/-5BR-1H (Hawker 800/ 800XP)
STC ST01444CH-D, Engine Model TFE731-5BR-1C (Falcon 900B)
STC ST01445CH-D, Engine Model TFE731-5BR-2C (Falcon 20-5)
STC ST01756CH-D Engine Model TFE731-4R-2S (Cessna Citation VII) Comments: , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , , Engines, Systems & Services – Phoenix, Arizona CERTIFICATE OF COMPLIANCE To: Operator or Service Center Performing Modification Upon modification of equipment, please fill in the information requested below, then mail or fax the completed certificate to: Honeywell Engines, Systems & Services P.O. Box 29003, Mail Stop 2102-127 Phoenix, AZ 85038-9003 FAX: 602-365-5638 Owner/Operator ____________________________________________________________ _________________________________________________________________________ Aircraft Model ____________________________Aircraft Serial No. ___________________ I certify that the following engine/equipment has been modified in accordance with the listed Service Bulletins. ENGINE/EQUIPMENT NO. 1 NO. 2 NO. 3 NO. 4 PART NO. PART NO. PART NO. PART NO. MODEL NO. MODEL NO. MODEL NO. MODEL NO. SERIAL NO. SERIAL NO. SERIAL NO. SERIAL NO. TSN/TSO TSN/TSO TSN/TSO TSN/TSO CYCLES CYCLES CYCLES CYCLES SERVICE BULLETIN NO. REVISION NO. SERVICE BULLETIN NO. REVISION NO. SERVICE BULLETIN NO. REVISION NO. SERVICE BULLETIN NO. REVISION NO. Signature _______________________Date_________________ Repair Facility ________________________________________