Eclipse Aerospace MSB 500-31-019: Revision B, text

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Page 1Open in PDF

ECLIPSE Service Bulle tin NUMBER:

SB 5 00 - 31 - 019 , R e v B Mandat ory M ODEL:

E CLIP SE E A5 00 www .ECLIPSE.aer o S UBJE C T :

A ir c r af t C om p u t e r S y s t e m ( A C S) S o f t w ar e U pd at e t o 5 .1.

PLANNING

INFORMA TION A.

Ef f ectivity Aircraft Serial Numbers:

000001 through 000104, 0001 13 through 0001 15, 000120 and 000123 through 000124 when modified by SB 500 - 99 - 002, A vionics Upgrade to A VIO NG Configuration AND NOT modified by SB 500 - 99 - 005, A vionics Upgrade T o A vio NG +

1.5 Configuration.

Aircraft Serial Numbers 000105 through 0001 12, 0001 16 through 0001 19, 000121, 000122 and 000125 through 000265 NOT modified by SB 500-99-005, A vionics Upgrade T o A vio NG +

1.5 Configuration.

NOTE :

Applies to Aircraft in the A vio NG configuration.

R eason Aircraft Computer System (ACS) software upgrade for enhanced functionality and product improvement.

Revision B Changes:

Clarified ef fectivity .

Description This Service Bulletin (SB) updates the ACS software version for A vio NG configured aircraft.

R ele v ant Publications None E.

Compliance Eclipse Aerospace Incorporated considers this to be a mandatory upgrade that should be accomplished within 90 days or 50 hours whichever comes first.

F .

Appr o v al This Service Bulletin is based on engineering data that is F AA-approved, and the modification herein complies with the applicable regulations.

Labor R equir ements The following information is for planning purposes only .

(1) Estimated labor hours to perform:

Suggested number of personnel:

1 ACS Software loading:

4.0 Hours T otal labor hours:

4.0 Hours The above is an estimate based on properly equipped and experienced personnel complying with this Service Bulletin.

Actual labor hours may vary depending on workforce experience, concurrent maintenance, discovery of other discrepancies, etc.

(2) Qualification of personnel:

• A person properly authorized to perform aircraft maintenance under 14 CFR 43 or equivalent approved by the Civil A viation Authority having jurisdiction.

• A vio Maintenance Computer (AMC) trained.

I s su ed:

SB 5 00 - 31-019 P a g e 1 o f 9

Page 2Open in PDF

ECLIPSE Service Bulle tin H.

So f tw ar e A ccomplishment Summary Upgrade ACS software to version

5.1.06 using the A vio Maintenance Computer (AMC) with software version

2.4.00 or greater .

R e f er ences Aircraft Maintenance Manual (AMM) P/N 06-1 17751, latest revision.

Publications A f f ect ed Aircraft Flight Manual, P/N 06-122204, Revision 4 or higher must be used after completion of this Service Bulletin.

Export Contr ol These commodities, technology or software were exported from the United States in accordance with the Export Administration Regulations.

These commodities, technology or software are intended for use only in the End User ’ s country .

An export license from the U.S.

Department of Commerce may be required before these products can be re-exported, transferred, transshipped on a non-continuous voyage, or otherwise disposed of in any other country , either in their original form or after being incorporated into an end item.

Diversion of this end-item or its use contrary to any applicable U.S.

government license or to U.S.

law is prohibited.

MA TERIAL

INFORMA TION A.

Mat erials No parts and/or kits need to be ordered for this Service Bulletin.

T ooling The following special tooling/support equipment is required to accomplish this Service Bulletin.

Nomenclature Part Number Use A vio Maintenance Computer (AMC) with software version

2.4.00 or later 20-120576-1001 or 20-121926-1001 T o load ACS software.

ACS J08 T -harness 99-1 17120-2001

ACS/AMC Connection AMC ACS Software Download Box 87-120876-1003

ACS/AMC Connection USB to Ethernet Adapter SMC2209 Aircraft Interface Ethernet Cable Aircraft Interface C.

P art R e-identification Enter the new SW version (ACS_5.1.06) on the ACS software label.

I s su ed:

SB 5 00 - 31-019 P a g e 2 o f 9

Page 3Open in PDF

ECLIPSE Service Bulle tin

A CC O

MPLISHMENT INS

TRUCTIONS A.

Job Se tup Sign Off

(1) Power up the AMC, select T ab 31, Software Revision drop down and verify that ACS Software version

5.1.06 is available.

NOTE :

If ACS Software version

5.1.06 is not listed contact Eclipse Aerospace Service Engineering, T el.

toll free

(877) 375–7978.

(2) Make the aircraft safe for maintenance.

Refer to AMM 20 - 00 - 01 MAKE SAFE FOR MAINTENANCE.

A CS So f tw ar e Updat e

(1) Using SUBT ASK AMM - 31 - 40 - 00 - 021 - 921 - 001, prepare ACS computers for installation of

5.1.06 software upgrade.

CAUTION :

MAKE SURE

ELECTRICAL POWER IS OFF WHEN

CONNECTING ACS J08 T -HARNESS.

(2) AMC to ACS connection.

NOTE :

Both ACSs will need to be loaded;

this will require performing this procedure for both the Left and Right ACS.

Step

3.B.(2)(a) provides instructions for connecting the AMC to the left ACS and Step

3.B.(2)(b) provides instructions for connecting the AMC to the right ACS.

I s su ed:

SB 5 00 - 31-019 P a g e 3 o f 9

Page 4Open in PDF

ECLIPSE Service Bulle tin Sign Off

(a) Connect AMC to left ACS as follows:

Refer to Figure 1 .

Left ACS - AMC Connection Figure 1

Disconnect aircraft harness connector 39A01P08 (7, Figure

1) from left APC connector 39A01J08 (8, Figure

1) .

Connect APC J08 T -Harness (9, Figure

1) to left APC connector 39A01J08 (8, Figure

1) .

Connect APC J08 T -Harness (4, Figure

1) to aircraft harness connector 39A01P08 (7, Figure

1) .

Connect AMC ACS Download Box (3, Figure

1) to APC J08 T -Harness (4, Figure

1) .

Connect AMC ACS Download Box USB connector (1, Figure

1) to USB port on AMC (1, Figure

1) .

Make sure that the Program Enable switch on the AMC ACS Download Box (3, Figure

1) is in the OFF position.

Continue to step B.(3) .

I s su ed:

SB 5 00 - 31-019 P a g e 4 o f 9

Page 5Open in PDF

ECLIPSE Service Bulle tin Sign Off

(b) Connect AMC to right ACS as follows:

Refer to Figure 2 .

Right ACS - AMC Connection Figure 2

Disconnect aircraft harness connector 39A02P08 (9, Figure

2) from right APC connector 39A02J08 (8, Figure

2) .

Connect APC J08 T -Harness (7, Figure

2) to right APC connector 39A02J08 (8, Figure

2) .

Connect APC J08 T -Harness (4, Figure

2) to aircraft harness connector 39A02P08 (9, Figure

2) .

Connect AMC ACS Download Box (1, Figure

2) to APC J08 T -Harness (4, Figure

2) .

I s su ed:

SB 5 00 - 31-019 P a g e 5 o f 9

Page 6OCROpen in PDF

ECLIPSE ECLPSE Service Bulletin AEROSPACE Sign Off

5. Connect AMC ACS Download Box USB connector (6, Figure 2) to USB port on AMC (5, Figure 2).

6. Make sure that the Program Enable switch on the AMC ACS Download Box (1, Figure 2) is in the OFF position.

Continue to step B. (3).

NOTE: Both ACSs will need to be loaded; this will require performing this procedure for both the left and right ACS.

(3) Power up the aircraft by setting the SYS BATT and START BATT switches to ON and the BUS TIE to AUTO. (Clear any MASTER WARNINGS/CAUTIONS as needed.)

NOTE: If use of external power is required, Refer to AMM - 24-40-00-051-801 - EXTERNAL POWER - MAINTENANCE PRACTICES.

(4) On the AMC, select Tab 31 and wait for the AMC to connect. Refer to Figure 3.

AVIO Maintenance Computer VerinA, 2400 Feb 27 18:21:00 UTC X Copyright Eclipse Aerospace 8 Weigh 22 Autopilot 30 De-Ice 32 Ldg Gear 34 Nav/Pitot 72 Engine 73 Fuel Ctrl JACS

- ACS

- Left ACS Data Right ACS Data -Load ACS Software Revision SW Rev ACS_V_5.0.00 SW Rev ACS_V_5.1.06 CRC 5590C8AA CRC Load SW Ldr Rev LDR_V_4.0.00 Ldr Rev CRC F942772F CRCI Fuel Data Ok • Fuel Data Г CCS Data Ok • CCS Data

• Config Data Ok • Config Data Г W&B Data Ok • W&B Data Copy to Right Copy to Left -USB Flash Drive Init Left Data Init Right Data Write Maint Mode Off 5131673 Batt: 4:15 L-ACS R-ACS AMC Tab 31 - For Reference Only Figure 3 NOTE: AMC Screenshot is for reference only and may vary with the AMC software revision.

(5) Connection on lower right corner of AMC will show L-ACS or R-ACS box in green, which ever is applicable.

Page 7OCROpen in PDF

ECLIPSE ECLPSE Service Bulletin AEROSPACE Sign Off

(6) On Load ACS dropdown box select ACS_V_5.1.06 and select the Load SW button, follow the AMC prompts after selecting the load SW button.

NOTE: Software load should take approximately five minutes.

• When software load is complete, the status box will show Loading...done.

(7) On AMC verify software ACS CRC is C2968A62. Refer to Figure 4.

AVIO Maintenance Computer Version AMC_2.4.00 Feb 27 18:30:55 UTC X Copyright Eclipse Aerospace 8 Weigh 21 Air Cond 22 Autopilot 24 Elec Pwr 27 FIt Ctrls 28 Fuel 30 De-Ice 31 Instr 32 Ldg Gear 34 Nav/Pitot 72 Engine 73 Fuel Ctrl ACS

- ACS

- Left ACS Data - Right ACS Data - Load ACS Software Revision SW Rev ACS_V_5.1.06 SW Rev ACS_V_5.1.06 CRC C2968A62 CRC Load SW Ldr Rev LDR_V_4.0.00 Ldr Rev CRC F942772F CRC Load ACS V 5.1.06 27-Feb 2013 18:22:26 S-rec file... verified Fuel Data Ok • Fuel Data Clear ACS memory... done

• CCS Data Ok • CCS Data Loading... done CRC Expected: C2968A62 Г Config Data Ok • Config Data Г W&B Data Ok Г W&B Data Copy to Right Copy to Left - USB Flash Drive Init Left Data Init Right Data Write Maint Mode Off Batt: 4:21 L-ACS R-ACS AMC Tab 31 - For Reference Only Figure 4 NOTE: AMC Screenshot is for reference only and may vary with the AMC software revision.

(8) Power down the aircraft by setting the SYS BATT and START BATT switches to OFF and the BUS TIE to OPEN.

CAUTION: AIRCRAFT MUST BE POWERED DOWN PRIOR TO

DISCONNECTING/CONNECTING THE T-HARNESS FROM THE ACS. DAMAGE TO EQUIPMENT COULD OCCUR.

(9) Disconnect AMC from ACS.

(a) For left ACS:

Remove APC J08 T-Harness from the left APC connector 39A01J08 and aircraft harness connector 39A01P08. Reconnect connector 39A01P08 to left APC connector 39A01J08.

Page 8Open in PDF

ECLIPSE Service Bulle tin Sign Off

(b) For right ACS:

Remove APC J08 T -Harness from the right APC connector 39A02J08 and aircraft harness connector 39A02P08.

Reconnect connector 39A02P08 to right APC connector 39A02J08.

(10) W rite the new software version

(5.1.06) on the ACS software label with a permanent ink marker .

1) Perform software update on right ACS, do step B.(2).(b) , and repeat steps B.(3) thru B.(10) .

(12) Perform aircraft configuration update.

Note installed options, activate and configure as required.

Refer to AMM 31 - 40 - 00

AIRCRAFT

COMPUTER

SYSTEMS -

MAINTENANCE PRACTICES.

(13) Do adjustment/test of the left and right APCs (for software update).

Refer to AMM - 31 - 40 - 00 - 071 - 801 -

AIRCRAFT

COMPUTER

SYSTEMS -

ADJUSTMENT/TEST .

(14) Remove all tools, equipment, and unwanted material from work area.

(15) If no further maintenance is required, return the aircraft back to service.

Refer to AMM - 20 - 00 - 02 - 051 - 801 - RETURN T O SER VICE (AFTER MAINTENANCE).

Limit ations and Pr ocedur es A vio Maintenance Computer (AMC) must have software version

2.4.00 or higher in order to load ACS software

5.1.06.

Remove AFM TR-016 (installed by SB 500-31-026 Software Configuration Update).

Cos t Contact Eclipse Aerospace Customer Care for cost and availability .

REC ORD OF C O

MPLIANCE Upon completion of this Service Bulletin, make an appropriate maintenance-record entry specifying the Service Bulletin number .

TIFYING

ECLIPSE AER OSP A CE On completing this service bulletin, the operator/maintainer shall complete the attached Compliance Record and send it to Eclipse Aerospace via regular mail, fax, or e-mail.

Mailing Address Eclipse Aerospace Incorporated A TTN:

Customer Care 2503 Clark Carr Loop SE Albuquerque, NM 87106 Fax 1-505-241-8802 E-mail sbcompliance@eclipse.aero I s su ed:

SB 5 00 - 31-019 P a g e 8 o f 9

Page 9Open in PDF

SER VICE

BULLETIN

COMPLIANCE RECORD MODEL _________

AIRPLANE S/N ________ REG.

NO.

_________ T OT AL TIME ______ (HOURS) OWNER NAME:

______________________________________________________________________ ADDRESS:

______________________________________________________________________ ______________________________________________________________________

TELEPHONE NO.

(___) __________________________ F AX NO.

(___) ______________________

COMPLIANCE WITH SB 500-31-019, Rev B Description of W ork Performed (Inspection | Modification | Repair | Option Installation | Defect or Damage Found, if applicable) _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ _________________________________________________________________________________ DA TE _______________ WORK

PERFORMED BY ____________________________________________________________ (PRINTED) __________________________________________________________ (SIGNA TURE) COMP ANY __________________________________________________________

ADDRESS __________________________________________________________ __________________________________________________________

TELEPHONE ________________________________ F AX_______________________________