SIL Technical Portions FAA Approved

Transcription

1 SIL--0 REASON FOR ACTION PURPOSE COMPLIANCE MODELS AFFECTED PURPOSE: Upgrade TCM EDI-200 Light Weight FADEC Data Recorder Installation. For information only. All Liberty XL-2 Aircraft SN 0001 & up. This procedure installs a Teledyne Continental Motors Engine Data Interface model 200 (EDI-200) on a Liberty Aerospace model XL2 aircraft. INSTALLATION AND TEST PROCEDURE: 1.1 Instrument Console Assembly Preparation Objective: Figure 1 - EDI-200 Assembly This section prepares the aircraft instrument console to receive the EDI-200 mounting bracket hardware Parts Required: Part Number Part Description Supplier Qty CCR244CS-3-02 Rivet, Blind, Nut Plate, 100 Flush Head 286 CRES Liberty 8 MS219- Nut, Self Locking, Plate, Two Lug, Floating #6-32 Liberty Place the master switch in the OFF position Place the FADEC B switch (SW0) in the OFF position Locate on the circuit breaker panel CB 001, 70A, BATT and pull to the open position Open and remove circuit breaker panel assembly 135A to gain clear access to the instrument panel console floor. NOTE: The CB panel will remain out of the aircraft until a later step in the EDI-200 installation process. ISSUE Day Year REVISION Day Year Page 1

2 SIL--0 CAUTION: Do not attempt drilling of EDI-200 mounting bracket holes with the CB panel in place. Wire damage may result Prepare EDI-200 mounting bracket hardware holes in the instrument console as shown in Figure 2. Figure 2 - EDI-200 Mounting Bracket Hardware Holes Install EDI-200 mounting bracket nut plate hardware in locations shown in Figure 3 ISSUE Day Year REVISION Day Year Page 2

3 SIL--0 Figure 3 - EDI-200 Mounting Bracket Nut Plate Installation Instrument console assembly preparation complete ISSUE Day Year REVISION Day Year Page 3

4 SIL EDI-200 Installation Objective: This section installs the EDI-200 unit, bracket and wire harness in the aircraft Parts Required Part Number Part Description Supplier Qty 135A EDI Bracket Assembly Liberty 1 135A EDI Cable Liberty EDI-200 (TCM PN ) Aerosance 1 MS x0.500 Pan Head Screw Corrosion Resistant Liberty 8 NAS1149N632R Flat Washer #6.149 ID x OD x 0.32 TH Liberty 4 MS CABLE TIE, BLACK Liberty Connect power wire F62A20 ring terminal to aircraft power terminal block TB01.1 as shown in Figure Connect power wire F61A20 ring terminal to aircraft power terminal TB01.3 as shown in Figure Connect ground wire F63A20N quick disconnect to aircraft ground GL01 cluster 20 as shown in Figure 4. Figure 4 - EDI-200 Power Wire Installation NOTE: Ground wire F63A20N is shown routed to ground terminal cluster 20. If cluster 20 is not available, connection to a nearby cluster is permitted. ISSUE Day Year REVISION Day Year Page 4

5 SIL Record EDI-200 data plate information below for later aircraft log book entry: NAME DATA Model Name Part Number Serial Number Software Install the EDI-200 unit on its mounting bracket using four 6-32 pan head screws. Be sure to position the EDI- 200 data plate outward so that it may be read when the CB panel is open as shown in Figure 5. Figure 5 - EDI-200 Console Installation ISSUE Day Year REVISION Day Year Page 5

6 SIL Feed the EDI-200, lead wire and bracket assembly up through the instrument panel console into location and secure with 6-32 x 3/8 pan head screws and washers as indicated in Figure Locate and connect EDIJ1 to EDIP1 as shown in figure 5 securing the connection by tightening connector locking screws (2) Secure power wires, EDIJ1 and EDIP1 with wire ties to adjacent console wire harnesses routed as shown in Figure Verify all EDI wires are clear of adjacent structure and will not interfere with CB Panel installation to follow Position circuit breaker panel 135A in front of the instrument console permitting access to connector SDP Referring to Figure 5, connect EDI wire harness connector EDIP2 to SDP001 securing the connection by tightening connector locking screws (2) Route and secure EDIP2 and SDP001 with wire ties to adjacent console wire harnesses routing clear of the CB panel installation to follow Complete installation of circuit breaker panel 135A CAUTION: When installing the circuit breaker panel care must be taken to assure wire harnesses are free and clear of all near by structures within the console. Do not force the circuit panel into position. If the panel will not easily fit into position check for wire harness interference EDI-200 installation complete. ISSUE REVISION Page Day Year Day Year 6

7 SIL--0 2 EDI-200 SETUP AND TEST 2.1 Flash Card Memory Installation Objective: The EDI-200 stores data for flight time in proportion to the size of a compact flash memory card inserted. For example a 8 MB card stores in excess of 150 hours of data. With a 1GB CF card storage will exceed 1,500 hours. This section will install a 1Gb card in preparation for functional testing Parts Required: TCM Part Number Part Description Supplier Qty Memory Card TCM Remove EDI-200 cover screws and open access to the flash memory slot. Refer to Figure 6 below. CAUTION Flash memory cards are ESD sensitive devices. Follow proper ESD procedures to prevent inadvertent damage by static discharge. Figure 6 - EDI-200 Flash Memory Card Installation Remove the memory card with a gentle pull motion forward out of the EDI-200 assembly Record the following data from the memory card label ISSUE Day Year REVISION Day Year Page 7

8 SIL--0 NAME VALUE AEROSANCE PART NUMBER TCM PART NUMBER DATE CODE Mark the flash card data label with the following information: Aircraft registration number Aircraft serial number Hobbs hours at installation Installation date Insert memory card with the white label towards the LED indicators in the EDI-200 flash memory slot until it fully seated. Fully seated the card will extend beyond the EDI face place by approximately ¼ inch. CAUTION: The flash memory card may only be inserted one way. Do not force insertion. Properly aligned, the card will slide easily becoming fully seated with only slight finger pressure. Antistatic procedures are to be followed when handling the flash card memory Install the flash card cover and secure with two socket head screws. Tighten screws to 1 to 5 inch pound of torque Flash card memory installation complete. ISSUE REVISION Page Day Year Day Year 8

9 SIL Initialization Test Objective: The EDI-200 begins and completes a self-test as completely as practicable depending on the aircraft operational state when power is applied to the EDI. This test will power the EDI up and verify a valid initialization state is achieved Parts Required: Part Number Part Description Supplier Qty NA Inspection mirror Any Locate on the circuit breaker panel CB 001, 70A, BATT and push to the closed position Verify all circuit breakers are closed and ready to support aircraft power up. NOTE: In the following steps EDI-200 normal operation will be verified by reading status LEDs located in the EDI-200 face plate When verifying correct status, refer to the following table for a description of each LED condition observed. Green LED EDI-200 Indicating Lamp Code Red LED Flashing, Alternately With Red - Initializing OFF - Unit Fault Or Unit Powered Off On Steady Receiving Data Flashing Unit OK, Not Receiving Data Flashing Alternately With Green - Initializing Off - Not Recording Or Unit Powered Off On Steady - Recording Flashing - Disk Error (CF disk full, file corrupted, etc.) Apply power to the aircraft by closure of the master switch Using an inspection mirror view the EDI-200 LEDs and verify expected status listed below: SB Flashing, Alternately With Red Initializing - Process will take approximately 30 seconds Flashing Alternately With Green Initializing - Process will take approximately 30 seconds SB Flashing Unit OK, Not Receiving Data OFF Not Recording ISSUE REVISION Page Day Year Day Year 9

10 SIL--0 verify expected status listed below: SB On Steady Receiving Data Off - Not Recording Power up FADEC B by closing FADEC PWR switch B. Using an inspection mirror view the EDI LEDs and verify expected status listed below: SB On Steady Receiving Data Off - Not Recording Place FADEC PWR A and FADEC PWR B switches in the OFF state. Using and inspection mirror view the EDI LEDs and verify expected status listed below SB Flashing Unit OK, Not Receiving Data Off - Not Recording Remove power from the aircraft by deactivation of the master switch. Using an inspection mirror, view the EDI LEDs and verify expected status listed below: SB OFF - Unit Fault Or Unit Powered Off Off - Not Recording Or Unit Powered Off EDI-200 Initialization Test Complete 2.3 Engine Data Recording Indication Test Objective: Once the EDI-200 has initialized it is ready to start recording engine data. EDI-200 recording will not begin until the engine speed is 300 RPM or greater. This test will verify the EDI-200 does indicate recording of data with the engine running Parts Required: Part Number Part Description Supplier Qty NA Inspection mirror Any Perform a normal start of the engine and set the throttle to idle (850 to 950 RPM) Using an inspection mirror, observe the EDI-200 LEDs and verify expected status listed below: SB On Steady Receiving Data On Steady - Recording Perform an engine shutdown leaving power applied through the master switch, FADEC PWR A and FADEC PWR B Switches. ISSUE REVISION Page Day Year Day Year 10

11 SIL Using an inspection mirror, observe the EDI-200 LEDs and verify expected status listed below. SB On Steady Receiving Data Off - Not Recording Power off the aircraft by toggling the FADEC A and B switches to the OFF position followed by a toggling of the master switch to the OFF position EDI-200 engine data recording indication test complete. 3 MAINTENANCE RECORD Record completion of modifications performed under this procedure in the appropriate aircraft maintenance logs and records. ISSUE REVISION Page Day Year Day Year 11

12 SIL--0 The costs of all compliance actions identified in this Service Document will be covered under the XL-2 warranty to be determined at time of installation. Please complete and return this page by scanned , regular mail, or FAX, indicating that this SIL--0 has been received and all actions have been taken to comply with it. This document shall be returned to Liberty Aerospace. Regular Mail: ATTN: Technical Support Liberty Aerospace, Melbourne, FL Or FAX: LIBERTY AIRCRAFT SERIAL NUMBER AIRCRAFT TACH HOURS AT TIME OF MODIFICATION MODIFICATION COMPLETION DATE Owner/Operator s Name Owner/Operator s Address Telephone Numbers Owner/Operator s Signature ISSUE REVISION Page Day Year Day Year