SERVICE BULLETIN REVISION TRANSMITTAL

Transcription

1 REVISION TRANSMITTAL This sheet transmits Revision 1 to, which: A. Updates the part numbers in MATERIAL - Cost and Availability and MATERIAL INFORMATION table. B. Adds new step 5. for the Configuration of the UNS FMS. C. Deletes Configuration Module Programing Instructions attachment. D. Makes minor editorial changes throughout the document. NOTE: This revision replaces the original issue of in its entirety. NOTE: Change bars and pointing hands are not used in this publication to denote revised material. This transmittal sheet provides a complete description of the changes made by this revision, except for editorial changes. REVISION COMPLIANCE NO EFFECT. Airplanes previously modified by this service bulletin are not affected by this revision. LOG OF REVISIONS Original Issue May 03, 2011 Revision 1 February 22, 2012 Original Issue - May 3, 2011 Revision 1 - February 22, 2012 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , customercare@cessna.textron.com COPYRIGHT 2011

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3 TITLE NAVIGATION - INSTALLATION OF SCN FOR UNS-1 FMS EFFECTIVITY MODEL SERIAL NUMBERS 560 (Citation Ultra) thru (Citation Encore) thru This service bulletin only applies to airplanes with 802.X software. REASON To install SCN software due to erroneous UNS-1 FMS information displayed on the PFD. DESCRIPTION This service bulletin provides instructions to return the UNS-1 FMS to Cessna for upgrade to SCN software. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or phase inspection. 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. FLIGHT CREW OPERATIONS Refer to the attached Flight Crew Operations Summary. Original Issue - May 3, 2011 Revision 1 - February 22, 2012 Page 1 of 11 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax , customercare@cessna.textron.com COPYRIGHT 2011

4 WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Cessna Model 560 Maintenance Manual Cessna Model 560 Ultra Approved Flight Manual (56FMA) Cessna Model 560 Encore Approved Flight Manual (56FMB) PUBLICATIONS AFFECTED Cessna Model 560 Maintenance Manual Cessna Model 560 Illustrated Parts Catalog Cessna Model 560 Ultra Approved Flight Manual (56FMA) Cessna Model 560 Encore Approved Flight Manual (56FMB) 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) Disconnect the airplane battery. (2) Disconnect external electrical power. 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 the UNS-1 FMS computer. (Refer to the Model 560 Maintenance Manual, Chapter 34, UNS-1CSP Flight Management System - Maintenance Practices.) NOTE: Airplanes with Dual UNS, two units will need to be removed. A. Send the UNS-1 FMS to Cessna for modification. NOTE: Please make sure that the UNS-1 FMS is protected from electrostatic discharge by placing them in a static shielding bag, and make sure to protect it with bubble wrap or other vibration absorbing packing materials. 3. Install the UNS-1 FMS computer. (Refer to the Model 560 Maintenance Manual, Chapter 34, UNS-1CSP Flight Management System - Maintenance Practices.) NOTE: Airplanes with Dual UNS, two units will need to be installed. 4. Prepare the airplane for power. A. Make sure that all switches are in the OFF/NORM position. B. Remove maintenance warning tags to the battery and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" writtenonthem. C. Connect the airplane battery. D. Connect external electrical power. 5. Configure the UNS FMS as follows: A. Press the ON/OFF DIM key. After five seconds of warming up, the FMS will do a self-test. If there are no faults found, the initiation page will be displayed. B. Press the ACCEPT (L5) key to initialize the UNS FMS. NOTE: Date, time and position do not need to be entered into the system. Page 2 Revision 1 - February 22, 2012

5 C. Push MSG (R1) and review any messages. D. Push RETURN (R5) to go back to the initialization page. E. Push (R1) to highlight the date field and enter 4, 5, 6, 7, 8, and 9. Push enter. F. Push DATA to show the data 1/4 page. G. Push MAINT (R5) to go to the maint 1/1 page. H. Push CONFIG (L1) to go to the first configuration page. I. Push EDIT (R1) to change the configuration. NOTE: DISPLAY (L1) will change to STORE (R1). NOTE: All of the following changes must be entered before pushing STORE because the system will restart immediately after. J. Push DISPLAY (L1) to go show the configuration page. Push COLORS (L3) and set as follows: DISPLAY CONFIG 1/1 DISPLAY TYPE FLAT PANEL COLORS PRIMUS 1000 K. Push RETURN (R5) until you are back on the configuration 1/2 page. L. Push FMS CONFIG (L2) to show the first FMS configuration page. Push FUEL (L2) and set as follows: FUEL OPT 1/1 FUEL MODE EMPTY WEIGHT ** (See the Weight and Balance Sheet) #OFENGINES 2 DISPLAY UNITS FUEL FLOW TYPE LBS DC LINEAR ** If weight and balance information is unavailable, enter a temporary weight of 9250 pounds. This can be corrected at any time. M. Push FF SCALE (R2) and set as follows: FF SCALING 1/1 INPUT RANGE 0-5 VDC FLOW RATE LOWER 0 FLOW RATE UPPER 1990 VOLTAGE (VDC) LOWER 0 VOLTAGE (VDC) UPPER 5.0 MIN FF 75 N. Push RETURN (R5) two times until the FMS CONFIG 1/3 page is displayed. O. Push PERF (L3) and set as follows: Revision 1 - February 22, 2012 Page 3

6 BASIC MANUAL ADVANCED CLIMB GRAD PERF OPT 1/1 500 FT/NM P. Push RETURN (R5) until you are back on the FMS configuration 1/3 page. Q. Push VNAV (L4) key and set as follows: VNAV OPT 1/4 VNAV MODE ENRTE FPA LIMIT -6.0 APPR FPA LIMIT -4.0 VDEV STOW VDEV SCALE NORMAL TGT V/S TGT FPA -3.0 TEMP COMP COLD R. Push NEXT key and set as follows: 429/571/ASCB VDEV (3L) PITCH (4L) VERT SPD (5L) ANALOG VDEV (3R) PITCH (4R) VNAV OPT 2/4 ENRT + APPR ENRT + APPR ENRT + APPR S. Push NEXT key and set as follows: VNAV OPT 3/4 V/S DESCENT ALT HOLD SPD HOLD SPD CLIMB DESCENT V/S APPR STEER PITCH T. Push NEXT key and set as follows: Page 4 Revision 1 - February 22, 2012

7 VNAV OPT 4/4 SPD CLIMB SPD CLIMB 2 SPD CLIMB KTS/ MACH --- KTS/ MACH U. Push RETURN (R5) two times until the CONFIG 1/2 page is displayed. V. Push ARINC (L4) and select RECEIVE (L1) from the ARINC OPT 1/1 and set as follows: NOTE: Select NO SENSOR option for all ports initially. This will allow all possible port input devices to show in the selection list for each port. NOTE: Airplanes with dual FMS installations ARINC RCV 1/1 set as follows: If first FMS, for PORT 0 and PORT 3 select GPS 1 or GNSS 1 If second FMS, for PORT 0 and PORT 3 select GPS 2 or GNSS 2. PORT 0, #1 FMS (Or if dual FMS), #2 FMS PORT 0, #1 FMS (Or if dual FMS), #2 FMS PORT 1 (Or if TAWS) PORT 2 PORT 3 (Or if dual FMS), #1 FMS ARINC RCV 1/1 LS GPS 1 B1 (If UNS-1Csp+ is installed) LS GPS 2 B1 (If UNS-1Csp+ is installed) LS GNSS 1 (If UNS-1ESP or UNS-1L is installed) LS GNSS 2 (If UNS-1ESP or UNS-1L is installed) NO SENSOR TAWS NO SENSOR NO SENSOR (If No #2 FMS Installed) LS GPS 2 B1 (If UNS-1Csp+ is installed) (Or if dual FMS), #1 FMS (Or if dual FMS), #2 FMS (Or if dual FMS), #2 FMS PORT 4 (Or if UNILINK) PORT 5 PORT 6 PORT 7 LS GNSS 2 (If UNS-1ESP or UNS-1L is installed) LS GNSS 1 (If UNS-1ESP or UNS-1L is installed) LS GPS 1 B1 (If UNS-1Csp+ is installed) NO SENSOR UNILINK IC600-R-05 IC600-L-05 (Or if dual FMS) CROSSFILL 1 NO SENSOR (If No #2 FMS Installed) W. Push RETURN (R5) until you are back on the ARINC OPT 1/1 page. X. Select TRANSMIT (L2) and set as follows: NOTE: Select NO SENSOR option for all ports initially. This will allow all possible port input devices to show in the selection list for each port. Revision 1 - February 22, 2012 Page 5

8 PORT 0 PORT 1 (Or if TAWS) (Or if UNILINK) PORT 2 PORT 3 (Or if UNIVISION) (Or if second FMS) ARINC XMIT 1/1 IC HS UNS HS429-1 UNS HS LS NONE 429 HS (Not available if PORT 1is 429HS) 429 XFILL Y. Push RETURN (R5) two times until the CONFIG 1/2 page is displayed. Z. Push CSDB (L5) and set as follows: RCVR 1 RCVR 2 RCVR 3 RCVR 4 XMITTER 1 XMITTER 2 CSDB OPT 1/1 DUAL DME VOR NO SENSOR NO SENSOR TUNE NONE AA. AB. Push RETURN (R5) until the CONFIG 1/2 page is displayed. Push the FMS CONFIG (L2) key and then push the APPR (L5) key and set as follows: APPR MODE REMOTE TUNE REMOTE ARM ROLL GAINS LATERAL STEER APPR OPT 1/1 3X ROLL AC. Push APPR TYPES (L5) and set as follows: Page 6 Revision 1 - February 22, 2012

9 GPS NDB VOR RNV VFR ILS LOC BC APPR TYPES 1/2 ADVISORY AD. TAC GLS GWS AE. AF. Push NEXT key and set as follows: APPR TYPES 2/2 ADVISORY (M) ADVISORY ADVISORY Push RETURN (R5) two times until the FMS CONFIG 1/3 page is displayed. Push NAV (R3) and set as follows: NAV OPT 1/1 A/C TYPE FIXED WING AC ROLL STR HDG SEL (2R) ENRT + APPR AT OR BELOW BANK LIMIT (3R) 27.0 AT OR ABOVE BANK LIMIT (4R) 15.0 AG. Push RETURN (R5) until you are back on the FMS configuration 1/3 page. AH. Push TUNE (R4) and set as follows: TUNE OPT 1/1 COMM RADIO 8.33 KHZ (25 KHZ if installed) #COMMS 2 #NAVS 2 # ADFS 1 (2 IF ADF2 installed) #ATC 1(0IFMST-67installed) AI. Push RETURN (R5) until you are back on the FMS configuration 1/3 page. Revision 1 - February 22, 2012 Page 7

10 AJ. AK. Push NEXT key to go to the FMS configuration 2/3 page. Push XFILL (L1) and set as follows: MASTER INIT FUEL FPL XFILL MODE TUNE PRESENTS XFILL OPT 1/1 (Enabled if second UNS is installed.) (Enabled if second UNS is installed.) (Enabled if second UNS is installed.) (Enabled if second UNS is installed.) PUSH (Enabled if second UNS is installed.) AL. Push RETURN (R5) until the FMS CONFIG 2/3 page is displayed. AM. Push CABIN DISP (L2) and set as follows: CABIN DISPLAY CABIN DISP 1/1 AN. Push RETURN (R5) until you are back on the FMS configuration 2/3 page. AO. Push EFIS (L3) and set as follows: TYPE AP. EFIS OPT 1/1 429 ADV Push the 890R OPTIONS (L3) and set all options to. AQ. Push PL-4 OPTS (L4) and set all options to N/A. AR. Push RETURN (R5) two times until the FMS CONFIG 2/3 page is displayed. AS. Push TAWS (L4) and set as follows: MODE/RANGE SEL PAGE DISPLAY TAWS CONFIG 1/1 A739 (If TAWS is installed) N/A A739 (If TAWS is installed) AT. Push RETURN (R5) until you are back on the FMS configuration 2/3 page. AU. Push the VISION-1 (L3) and set to. AV. Push RETURN (R5) until you are back on the FMS configuration 2/3 page. AW. Push NEXT to go to the FMS configuration 3/3 page and set as follows: Page 8 Revision 1 - February 22, 2012

11 STRUT SWITCH POS EST DISP MAX STBY TIME PLT POWERUP FLIGHT INFO FMS CONFIG 3/3 DIGITAL ANP/RNP 2 HOURS RETAINED NONE AX. Push FAA FIAS (R2) and set as follows: WAAS FEATURES HAL METERS VAL METERS GPA METERS FAAFIAS1/1 xx.xx (non-selectable line items when WAAS disabled) xx.xx (non-selectable line items when WAAS disabled) xx.xx (non-selectable line items when WAAS disabled) AY. AZ. Push RETURN (R5) until you are back on the FMS configuration 3/3 page. (1) Push NASA T38 set to. (2) Push RETURN (R5) until the FMS CONFIG 1/2 page is displayed. Push DISCRETES (L3) and then push DISCRETE INPUT (L2) and set as follows: NOTE: Select NONE option for all discretes initially. This will allow all possible discrete inputs to show in the selection list for each discrete in. DISC IN 1-6 DISC IN 7 DISC IN 8 DISC IN 1/2 NONE FREQ MNGT NONE BA. Push NEXT to go to the DISCRETE in page 2/2. DISC IN 9-11 DISC IN 2/2 NONE BB. BC. Push RETURN (R5) until the DISC OPT 1/1 page is displayed. Push DISCRETE OUT and set as follows: NOTE: Select NONE option for all discretes initially. This will allow all possible discrete inputs to show in the selection list for each discrete in. DISC OUT 1-8 DISC OUT 1/2 NONE BD. Push NEXT to go to page two and set as follows: Revision 1 - February 22, 2012 Page 9

12 DISC OUT 9 DISC OUT 2/2 NONE BE. BF. Push RETURN (R5) until the CONFIG 1/2 page is displayed. Push AIR DATA (R4) and set as follows: ALT DISPLAY A/S DISPLAY MINIMUM TAS SAT FORMAT MACH FORMAT BARO ALT FMT PRESS ALT FMT A/S FORMAT AIR DATA 1/1 BOTH TAS & IAS 50 KTS DIGITAL DIGITAL DIGITAL DIGITAL DIGITAL BG. Push RETURN (R5) until the CONFIG 1/2 page is displayed. BH. Push NEXT to show CONFIG 2/2 page. NOTE: The screen may be flashing. BI. Push L1, type 802.8, and push ENTER. (1) Use the +/- key to enter the decimal point. BJ. Push AIRCRAFT IDENTIFICATION (L2). Fill in aircraft identification up to 24 characters including spaces. Use (+/-) to enter a space. The following format should be followed for the aircraft ID: CITATION ULTRA OR ENCORE S/N XXXX. Where XXXX represents the airplane serial number. BK. To save the new configuration, push STORE (R1) two times. The system will now reset itself and initiate power on self tests. NOTE: If you push return at this point, none of the options will be stored. The configuration module will retain its previous configuration. BL. To display the airshow of additional video input on the UNS-1 FMS, select the ON/OFF DIM function key. Select the display option (R4). The display option window will allow you to select the video option. 6. Do a check of the software version. A. Cycle the airplane power. B. Make sure that software version is now displayed on the bottom RH corner of initialization page of the FMS and that it passes the self test. 7. Power down the airplane and remove the external power. 8. Update the 560 Citation Ultra or Encore FAA Approved Airplane Flight Manual. NOTE: Look at the configuration codes listed in the applicable supplement and/or in Section 1 of the FAA Approved Airplane Flight Manual to make sure all changed crew procedures or limitations are complied with. A. Make sure that Supplement 56FMA-S74-03 or later is inserted in the 560 Citation Ultra FAA Approved Airplane Flight Manual (56FMA). Page 10 Revision 1 - February 22, 2012

13 B. Make sure that Supplement 56FMB-S63-03 or later is inserted in the 560 Citation Encore FAA Approved Airplane Flight Manual (56FMB). 9. Make sure the flight crew receives the Flight Crew Operations Summary, which shows the operational changes that are a result of the accomplishment of this service bulletin. 10. Record that this service bulletin has been completed. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM C/O Camp Systems International, 8200 East 34th Street North, Building 1600 Suite 1607 Wichita, KS MATERIAL INFORMATION Order the part below to install this modification. NEW P/N QUANTITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION (SCN 802.8) 1 UNS-1 FMS Computer SCN 802.X Return to Cessna for Modification (SCN 802.8) 1 UNS-1 FMS Computer (SCN 802.X) Return to Cessna for Modification NOTE: For airplanes with Dual UNS two units will need to be returned to Cessna for modification. NOTE: Contact the Cessna Service Parts & Programs Avionics team to schedule modifications at or telefax or CPDAvionicsTeam@cessna.textron.com available 8:00-4:30 CST weekdays. ADVANCE NOTIFICATION AND COORDINATION IS REQUIRED for Cessna Service Parts & Programs to effectively schedule units, ship to supplier and arrange for return. The Expected turn time for the supplier supporting this service document is 5-7 days. Revision 1 - February 22, 2012 Page 11

14 ATTACHMENT FLIGHT CREW OPERATIONS SUMMARY This summary provides additional information for the flight crew regarding operational changes as a result of accomplishment of this service bulletin. Please remove this summary from the service bulletin and give it to the flight crew. This summary is informational only and does not supersede any information in the FAA-approved airplane flight manual. Refer to Supplement 56FMA-S74-03 or later, Single or Dual Universal UNS-1 CSP+ OR UNS-1 ESP Flight Management System With 802.X Software in the Model 560 Ultra (56FMA) Approved Flight Manual. Refer to Supplement 56FMB-S63-03 or later, Single or Dual Universal UNS-1L, UNS-1 ESP Flight Management System with 802.X software in the Model 560 Encore (56FMB) Approved Flight Manual.

15 OWNER ADVISORY TITLE NAVIGATION - INSTALLATION AND CERTIFICATION OF SCN FOR UNS-1 FMS TO: Cessna Aircraft Owner REASON To install SCN software due to erroneous UNS-1 FMS information displayed on the PFD. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or phase inspection. LABOR HOURS WORK PHASE Modification MAN-HOURS As Required MATERIAL AVAILABILITY PART NUMBER AVAILABILITY COST (SCN 802.8) * * (SCN 802.8) * * *Contact the Cessna Service Parts & Programs Avionics team to schedule modifications at or telefax or CPDAvionicsTeam@cessna.textron.com available 8:00-4:30 CST weekdays. ADVANCE NOTIFICATION AND COORDINATION IS REQUIRED for Cessna Service Parts & Programs to effectively schedule units, ship to supplier and arrange for return. The Expected turn time for the supplier supporting this service document is 5-7 days. Based on availability and lead times, parts may require advanced scheduling. In cases where the required part(s) are available as exchange, order the exchange part and, upon completion, expedite the return of the removed core to avoid return penalties. Contact the Cessna Service Parts & Programs Sales Desk for availability of exchange parts. February 22, 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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