GULFSTREAM GVI (G650) Manage Atlanta Aircraft Certification Office Centra l Regi on. FAA

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u nenfor ce ab le by a co u rt. th e re ma ind er of this A g ree men t sha ll r em ain va lid and e nfo r ceabl e,.. GulfstreamA GENERAL DYNAMICS COMPANY Gulfstream G650 Airplane Flight Manual Gulfstream Aerospace Document Number GAC-AC-G650-0PS-0001 August12,2013 TO: All Gulfstream G650 Operators SUBJECT: G650 Airplane Flight Manual Revision 5, Dated August 12, 2013 This letter to operators introduces the release of G650 Ai rplane Flight Manual Revision 5, dated August 12, 2013 . The purpose of this revision is to address and identify procedures for inflight air starts (Normal Airstart - Automatic, Manual Airstart - Starter Assist , and Manual Airstart - Windmill i ng) in the event that engine failure was caused by a failed Mid Stage Check Valve (MSCV) . To incorporate this revision, use the List of Effective Pages to ensure the inclusion of all sections . If any missing pages are noted while incorporating this revision, please contact Flight Crew Technical Information at 1-800-810-4853 , Option 3 (United States) or 1-912-965-4178, Opt i on 3 (International) . Thank you for the opportunity to better serve you. (over, please)Sincerely , Michael Woods , Senior Technical Writer Flight Crew Technical Information Gulfstream Aerospace P.O. Box 2206, M/S SW7 (C-20) Savannah, GA 314021-800-810-4853, Option 3 (United States) 1-912-965-4178, Option 3 (International) 1-912-965-3520 (Fax) michael. woods@gulfstream. com.• Gulf.'3trerun (}650 AIRPLANE FLIGHT MANUAL RECORD OF REVISIONS Revision No: Dated: Inserted By: Date: Basic Issue Sep 07/12 Gulfstream Sep 07/12 Revision 1 Oct 16/12 Revision 2 Feb 13/13 Revision 3 May 02/13 Revision 4 Jul17/13 Revision 5 Aug 12/13 Gulfstream Aerospace Document Number GAC-AC-GSSO-OPS-0001 FAA APPROVED Aug 12/13 RECORD OF REVISIONS REVISION 5 Page 1'. Gulfstre£rm G650 AIRPLANE FLIGHT MANUAL OWNER INFORMATION Name: Address: City: State: Country: Postal (ZIP) Code: Telephone: Email: Company: Registration No.: REVISION 5 Page 2

Gulfstream Customer Support United States : (800) 81 0-GULF (4853) International : (912) 965-4178

RECORD OF REVISIONS FAA APPROVED Aug 12/13GULFSTREAM G650 AIRPLANE FLIGHT MANUAL LOG OF REVISION 5 Listed below are the highlights of Revision 5, along with their respective Chapter , Section and Page numbers. Remove and insert all affected pages as listed in the List of Effective Pages and enter Revision 5 dated August 12 , 2013 to the Record of Revision Sheet. ATA \PAGES

04 - 08 - 00 Page 04-32 04-08-00 Page 04-35 04-08-00 Page 04-38 DESCRIPTION OF CHANGE Normal Ai rstart - Automat ic- re - write of procedure to address act i ons

taken in the event of a fa il ed Mid St age Check Valve (MSCV) . Manua l Ai rstart - Starter Ass ist - re -w ri te of pr ocedure to address act i ons taken in the eve nt of a fai led Mid Stage Check Valve (MSCV) . Manua l Ai rstart - Windm i lling - re-write of procedure to address act i ons taken in the event of a fai led Mid Stage Check Va l ve (MSCV) . ! I I . . ". ' . I **JJ~**
**~**·L **/**.:b. William S. Whitton, Jr. ODA Lead Administrator ODA-511131-CEDate **~·** l**~~** 20 (_3, FAA APPROVEDAugust 12/13 LOG OF REVISIONS REVISION 5 Page 1REVISION 5 Page 2

GULFSTREAM G650 AIRPLANE FLIGHT MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK . LOG OF REVISIONS FAA APPROVED August 12/13GULFSTREAM G650 AIRPLANE FLIGHT MANUAL CHAPTER04-EMERGENCYPROCEDURES LIST OF EFFECTIVE PAGES ATA 04-00-00 04-00-00 04-04-0004 - 04-00 04-04-00 04-04 - 00 04-04-00 04-04-00 04-04-00 04-04-00 04-04-00 04-04-00 04-04-00 04-04-00 04-04-00 04-04-00 04-06-00 04-06 - 00 04-06 - 00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-06-00 04-07-00 04-07-00 04-07-00 04-07-00 ·o4-08-oo ·o4-08-oo *04-08-00 ·o4-08-oo* 04-08-00 *04-08-00* 04-08-00 * 04-08-00 • Pages rev i sed by Revision 5 •• Pages added by Revision 5 ••• Pages deleted by Revision 5

PAGE 04-1 04-2 04-3 04-4 04-5 04-6 04-7 04-8 04-9 04-1004 - 1104-12 04-13 04-14 04-15 04-16 04-17 04-18 04-19 04-20 04-21 04-22 04-2304 - 2404-25 04-26 04-27 04-28 04-28.1 04-28 .204-29 04-30 04-30.1 04-30 .2 04-31 04-32 04-33 04-34 04-35 04-36 04-37 04-38

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Februa ry 13/13 February 13 / 13 February 13/13 February 13/13 February 13/13 February 13/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13August 12/13 August 12/13 August 12/13 August 12/13 August 12/13 August 12/13 August 12/13 August 12 / 13 LIST OF EFFECTIVE PAGES Page 1 August 12/13ATA"04 -08-00 "04-08-00 *04-08-00* 04-08-0004 - 10-00 04-10-00 04-10-0004 - 10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-11-00 04-11-00 04-13-00 04-13-00 04-13-00 04-13-00 04-14-00 04-14-00 04-14-00 04-14-00 04-15-00 04-15-00 04-15-00 04-15 - 0004-15-00 04-15-00 04-15-00 04-15-00 04-16-00 04-16-00 04-16-00 04-16-00 04-18-00 04-18-00 04-18-00 04-18-00 04-19 - 00 04 - 19-00

GULFSTREAM G650 AIRPLANE FLIGHT MANUAL PAGE 04-39 04-40 04-41 04-42 04-43 04-44 04-45 04-46 04-47 04-4804 - 4904-50 04-51 04-52 04-53 04-54 04-55 04-56 04-57 04-58 04-59 04-60 04-61 04-62 04-63 04-64 04-65 04-66 04-67 04-68 04-69 04-7004 - 7104-72 04-73 04-74 04-75 04-76 04-77 04-78 04-79 04-80 04-81 04-82 LIST OF EFFECTIVE PAGES Page 2August 12/13

DATE August 12/1 3 August 12/13 August 12/13 August 12/13 July 17/ 13 July 1 7/13 July 1 7/13 July 17/13 July 1 7./13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13 July 17/13

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February 13/13 February 13/13 February 13/13 February 13/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2 /13February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 • Pages revised by Revision 5 .. Pages added by Rev i sion 5 ••• Pages deleted by Revision 5ATA 04-19-00 04-19-00 04-19-00 04-19-00 04-19-00 04-19-00 04-20-00 04-20-00 04-21-00 04-21-00 04-23 - 0004-23-00 04-24-00 04-24-00 04-25-00 04-25-00 04-25-00 04-25-00 04-25-00 04-25-00 04-25-00 04-25-00 • Pages revised by Revision 5 •• Pages added by Rev i sion 5 ... Pages deleted by Rev i sion 5

GULFSTREAM G650 AIRPLANE FLIGHT MANUAL PAGE 04-83 04-84 04-85 04-86 04-87 04-88 04-89 04-90 04-91 04-92 04-93 04-94 04-95 04-96 04-97 04-98 04-99 04-100 04-101 04-102 04-103 04-104

DATE February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 February 13/13 May 2/13 May 2/13 September 7/12 September 7/12 September 7/12 September 7/12 September 7/12 September 7/12 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 May 2/13 LIST OF EFFECTIVE PAGES Page 3 August 12/13GULFSTREAM G650 AIRPLANE FLIGHT MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK . LIST OF EFFECTIVE PAGES Page 4August 12/13 • Pages rev ise d by Rev isi on 5 **~** Pages added by Revision 5 ••• Pages de l eted by Rev isi on 5SECTION 04-00-00 04-00-10 04-04-00 04-04-10 04-04-20 04-04-30 04-06-00 04-06-10 04-06-20 04-06-30 04-06-40 04-06-50 04-06-60 04-06-70 04-07-00 04-07-10 04-07-20 04-07-30 04-07-40 04-07-50 04-08-00 04-08-10 04-08-20 04-08-30 04-08-40 04-08-50 04-08-60 04-10-00 04-10-10 04-10-2004 - 10-30

GULFSTREAM G650 AIRPLANE FLIGHT MANUAL CHAPTER 04- EMERGENCY PROCEDURES TABLE OF CONTENTS SUBJECT PAGE Emergency Procedures............ .. ..... ........ ........... 04-1

General Gu i dance... ..... . ......................... .. ......... 04-1 Electrical Power System........... ......... .... ............ 04-3 Dual Generator Failure (Above Altitude FL390).. .. . . . ..... ..... .... ....... ..... .. .... .... ........ ............ 04-3 Dual Generator Failure (Altitude FL390 or Below)............. .... .................. .. .................... ...... 04-8 Operation On Airplane Batteries, EBHA and UPS Batteries Only (RAT Unavailable)............ 04-14 Engine Failure ..................................................... 04-17 Engine Failure Considerations ......................... 04-17 Engine Failure Below V1 ............. ........ ............. 04-18 Engine Failure Above V1...... .......... .............. .... 04-18 Dual Engine Flameout.................... ........ .......... 04-22 Inadvertent Engine (One Or Both) Shut Down ... .................... . .................................. . ...... 04-24 Dual Engine Failure - Mid Altitude........... .... .... 04-25 Dual Engine Out Landing Procedure .... ...... ..... 04-26 Engine Operating Parameters ........................... 04-29 High O il Temperature ............... . ........................ 04-29 Low Oil Pressure. .... ..... ........ .............. ............ .. 04-30 Low Fuel Pressure ....... ............ .. ...... ..... .... ........ 04-30 Fuel Tank Temperature. ... ... .... ....... . ....... ... ........ 04-30 Engine Exceedance .......................................... 04-30.1 Engine Shutdown I Airstart I Single Engine Procedures........................................................... 04-31 Engine Shutdown in Flight.. .............................. 04-31 Normal Airs tart -Automatic............................... 04-32 Manual Airstart - Starter Assist.......... . ......... . .... 04-35 Manual Airstart - Windmilling ... ...... ............... .... 04-38 One (1) Engine Inoperative Landing Procedure.. .... ...... .... ... ... ............................. .. .... 04-40 One (1) Engine Inoperative Go-Around Procedure ............... ...................... .................... 04-41 Fire: Engine I APU I Electrical/ Airplane Interior.................................................................. 04-43 Engine Fire In Flight......................................... 04-43 Engine Fire On Ground . .... .... .... ...... .... .. .... .... ... 04-46 Tailpipe Fire... . .................................................. 04-47 FAA APPROVEDAugust 12/13 REVISION 5 Page 1SECTION 04-10-40 04-10-50 04-11-00 04-11-10 04-13-00 04-13-10 04-13-20 04-13-30 04-13-40 04-13-50 04-13-60 04-14-00 04-14-10 04-15-00 04-15-10 04-15-20 04-16-00 04-16-10 04-16-20 04-18-00 04-18-10 04-18-20 04-18-30 04-18-40 04-18-50 04-18-60 04-19-00 04-19-10 04-19-20 04-19-30 04-19-40 04-19-50 04-20-00 04-20-10 REVISION 5 Page 2

SUBJECT GULFSTREAM G650 AIRPLANE FLIGHT MANUAL PAGE APU Fire ........... ..... ........... .... ............................ 04-48 Airplane Interior Fire I Smoke I Fumes............ 04-49 Fire Detection System ........................................ 04-55 Engine Fire Warning System Malfunction ........ 04-55 Flight Controls System............................... ........ 04-57 Jammed Aileron ................................................ 04-57 Jammed Elevator........ ...................................... 04-57 Jammed Rudder .... ............. . ............................. 04-58 Jammed Spoiler(s).......... .... ........ ................ ...... 04-59

Ground Spoiler Failure in Flight....................... 04-60 Ground Spoiler Failure On Landing... .............. 04-60 Fuel System......................................................... 04-61 Fuel Leak In Flight....... ..... . ..... .......................... 04-61 Hydraulic System................................................ 04-65 Dual Hydraulic System (L SYS and R SYS) Failure............................................................... 04-65

Left Hydraulic System (L SYS) Failure - Loss

of Pressure and Fluid .. .. ... .... ..... ....... ..... .. .. . . . .... 04-69 Indicating I Recording System.......................... 04-73 Primary Flight Display (PFD) Malfunction........ 04-73 Suspected Erroneous I Unreliable Airspeed Indications ........................................... .... .......... 04-73 Landing Gear System......................................... 04-77 Braking Using the PARKING BRAKE............... 04-77 Nose Gear Retracted, Both Main Gear Down

and Locked ...... .... . ..... ....... .... ..... ............ .... .. .. .. . 04-78 One Main Gear and Nose Gear Down and Locked, Opposite Main Gear Retracted ........... 04-78 One Main Gear Only Down and Locked .......... 04-79 Both Main Gear Retracted, Nose Gear Down

and Locked.......................................... . ............ 04-79

All Gear Up Landing Procedure............. ......... . 04-79 Landing, Stopping and Evacuation................... 04-81 Overweight Landing.. ...... .................................. 04-81 Ditching................ . .... .. ................ .. .................... 04-81 Emergency Escape Routes ......... .... ... . . ..... ....... 04-84

Immediate Return For Landing............ .. ........... 04-86 Emergency Airplane Evacuation ....................... 04-86 Overheat I Hot Conditions ................................. 04-89 Engine Hot. ....................................................... 04-89 FAA APPROVED August 12113SECTION 04-20-20 04-20-30 04-20-40 04-21-00 04-21-10 04-21-20 04-21-30 04-23-00 04-23-10 04-23-20 04-23-30 04-24-00 04-24-10 04-25-00 04-25-10 04-25-20

SUBJECT GULFSTREAM G650 AIRPLANE FLIGHT MANUAL PAGE Py lon Hot ... . . . . . .. . ..... .. . . . . . .. ... ... . .. . . . . . . . . . . . . . . . . . . . . .. . . 04-89 Aft Equipment Hot ....... .......... .... . . . . ...... . ....... . . . . . 04-90 Aft Floor Hot ..... ... ... ...... ..... ... .. .. ............ ... . . ....... 04-90 Pressurization Control System.......................... 04-91 Loss of Pressurization.. .... . ............................... 04-91 Emergency Descent Procedure.. ......... ... .......... 04-91

Automatic Emergency Descent Mode (EDM) .. 04-92 Thrust Reverser System.......... ... ........................ 04-93 Thrust Reverser Unlock or Deploy During Takeoff .... ............ ... ....... ........ ............. ...... ..... .... 04-93

Thrust Reverser Unlock or Deploy During Flight...... . .......... ... ..... .... ...... .. ... ..... ...... .. ....... ..... 04-93 Thrust Reverser Failure ....... . ............. .. ............. 04-94 Windshield I Door System ........... ...................... 04-95 Main Entrance Door Not Secure .. . . . . . . . . . . . . ........ 04-95 Red Warning Messages and Annunciations .... 04-97 Crew Alerting System (CAS) Warning Messages and Procedures ............................... 04-97 Other Warning Annunciations and Procedures ........... ............ ............................ ....... ....... 04-100 FAA APPROVEDAugust 12/13 REVISION 5 Page 3REVISION 5 Page 4

GULFSTREAM G650 AIRPLANE FLIGHT MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK . FAA APPROVED August 12/13GULFSTREAM G650 AIRPLANE FLIGHT MANUAL 8. ISOLATION Valve ..................................................................... OPEN 9. PWR XFR UNIT (if Left Engine Failed) ........... ON (IF REQUIRED) 10. AUX Pump (if Left Engine Failed) ........................................... ARM 11. TCAS .................................................................................... TA ONLY 12. Fuel Load Balance ....................................... MONITOR I MAINTAIN See Section 01-03-80, Maximum Fuel Imbalance. END 04-08-20: Normal Airstart- Automatic I CAUTION I IF POWER LEVER IS NOT AT IDLE, A THROTTLE CONFIGURATION, L·R MESSAGE WILL BE DISPLAYED ON CAS. THE START WILL CONTINUE AND THE ENGINE WILL ACCELERATE TO THE THRUST SELECTED BY THE POWER LEVER. THIS IS NOT RECOMMENDED. ALWAYS ENSURE THAT THE POWER LEVER IS AT IDLE DURING STARTING. THE FLIGHT CREW IS RESPONSIBLE FOR MONITORING LP, HP AND TGT DURING AIRSTARTS. THE FADEC SYSTEM WILL NOT AUTO-ABORT AN AIRSTART FORA TGT EXCEEDANCE. I wARNING I VERIFY PROPER ENGINE: LEFT OR RIGHT. 1. INOPERATIVE Engine Power Lever ....................................... .IDLE NOTE: The flight crew shall agree on the correct (affected) FUEL CONTROL prior to placing it in the OFF position. 2. Affected Engine FUEL CONTROL ............................................ OFF 3. L I R MAIN and ALT Boost Pumps ............................................. ON 4. Altitude ............................. ....... ESTABLISH 30,000 FT OR BELOW REVISION 5 Page 04-32

Continued on next page

**~** Emergency Procedures 04-08-00 FAA APPROVED August 12/13GULFSTREAM G650 AIRPLANE FLIGHT MANUAL

I CAUTION I IF BOTH BLEEDS AND BOTH ECS PACKS ARE TO BE SHUT OFF FOR ENGINE START, BOTH CREW MEMBERS SHALL DON OXYGEN MASKS. 5. Affected Engine ENG BLEED AIR ............................................ OFF NOTE: If APU AIR is required to start the engine , BOTH**~NG** BLEED AIR switches must be OFF . 6. Affected ECS PACK ................................................................... OFF NOTE: If APU AIR is required to start the engine, BOTH ECS PACK switches must be OFF. 7. L I R WING ANTIICE .................................................................. OFF 8. Affected Engine Generator (GEN) ............................................ OFF 9. START MASTER ........................................................................... ON 10. BLEED AIR Pressure ............. 35 PSI DESIRED I 20 PSI MINIMUM NOTE: If using APU AIR to start engine in flight, BLEED AIR pressure will not be available while ENG START is depressed. NOTE: If the START button is not held long enough, the red Engine Fail L-R will illuminate and the start will be aborted. START MASTER must be cycled OFF-ON prior to another start attempt. 11. Affected Engine ENG START Switch ............................. DEPRESS NOTE: The FADEC determines if starter assist is required for engine start based on airspeed. The threshold speed for a windmill versus starter assisted airstart is 250 KCAS. 12. Affected Engine FUEL CONTROL. ........................................... RUN

FAA APPROVEDAugust 12/13 Continued on next page -7 Emergency Procedures 04-08-00 REVISION 5 Page 04-33GU L FSTREAM G650 AIRPLANE FLIGHT MANUAL

I CAUTION I THE FLIGHT CREW IS RESPONSIBLE FOR MONITORING LP , HPAND TGT DURINGAIRSTARTS . THE FADEC SYSTEM WILL NOT AUTO-ABORT AN AIRSTART FOR A TGT EXCEEDANCE . 13. Affected Engine FF (Fuel Flow) I TGT I RPM .... ....... . .... MONITOR 1 IF STABLE ENGINE IDLE IS ACHIEVED , PERFORM STEP 14 THROUGH STEP 24. IF ENGINE FAILS TO RESTART OR ACCELERATE TO IDLE , PROCEED TO STEP 25. 14. START MASTER ............ . ........... . ............ ... ..................... ....... .. ... OFF 15. Affected Engine SVO and IGN Icons ... ...... ..... ........... ....... ... .... OUT 1 16. Affected Engine OIL PRESS I OIL TEMP .. ......................... CHECK 17. Stabilized Engine ....... . ...... ALLOW ENGINE TO IDLE 5 MINUTES THEN ACCELERATE SLOWLY TO DESIRED POWER SETTING I CAUTION I DO NOT SELECT THE AFFECTED ENGINE BLEED AIR ON AFTER THE ENGINEAIRSTART.INTHE EVENTTHE ENGINE FAILURE WAS CAUSED BY A FAILED MID

STAGE CHECK VALVE , LEAVING THE ENGINE BLEED AIR OFF WILL PREVENT THE POSS IBI LITY OF ANOTHER ENGINE FAILURE . 1 18. Affected Engine ENG BLEED AIR I WING ANTI ICE .............. OFF 19. ISOLATION Valve ........ . ......................................... . .................. OPEN 20. Affected ECS PACK I GENERATOR ............................... RESTORE 21. Fuel Balance ........................ . .................... .... MONITOR I MAINTAIN 22. TCAS .............................................. . .... . ...... . ........................... TA IRA 23. FLT CTRL RESET Switch ...... ..... ........ ..... .. PRESS (IF REQUIRED) I 24. Nearest Suitable Airport ..... .. ... ... ..... ........ ..... ... ...... ..... ... .. .... ... LAND Investigate cause of engine failure . IF THE ENGINE FAILS TO RESTART OR ACCELERATE TO IDLE: NOTE: The flight crew shall agree on the correct (affected) FUEL CONTROL prior to placing it in the OFF pos iti on . 25. Affected Engine FUEL CONTROL ........................ . ................... OFF 26. START MASTER .... ..... .................................... .... .. ........ . ............. OFF 27. Procedure ..... ..... .... ........ RE-ACCOMPLISH AT LOWER ALTITUDE REVISION 5 Page 04-3 4 Continued on next page --7 Emergency Procedu r es

04 - 08 - 00 FAA APPROVEDA u gus t 12/ 13I GULFSTREAM G650 AIRPLANE FLIGHT MANUAL 28. Nearest Suitable Airport ........ . ............. . .... ...... ... ... ........ ..... ..... LAND Investigate cause of engine failure . END 04-08-30: Manual Airstart -Starter Assist NOTE: This procedure is to be followed if specifically directed by another procedure or if airplane conditions preclude performing 04-08-20, Normal Airstart- Automatic . I CAUTION I IF POWER LEVER IS NOT AT IDLE, A THROTTLE CONFIGURATION, L-R MESSAGE WILL BE DISPLAYED ON CAS. THE START WILL CONTINUE AND THE ENGINE WILL ACCELERATE TO THE THRUST SELECTED BY THE POWER LEVER. THIS .IS NOT RECOMMENDED. ALWAYS ENSURE THAT THE POWER LEVER IS AT IDLE DURING STARTING. THE FLIGHT CREW IS RESPONSIBLE FOR MONITORING LP, HP AND TGT DURING AIRSTARTS . THE FADEC SYSTEM WILL NOT AUTO-ABORT AN AIRSTART FORA TGT EXCEEDANCE. I WARNING I VERIFY PROPER ENGINE: LEFT OR RIGHT. 1. Inoperative Engine Power Lever ............................................ .IDLE NOTE: The flight crew shall agree on the correct (affected) FUEL CONTROL prior to placing it in the OFF position. 2. Affected Engine FUEL CONTROL .... . ....................................... OFF 3. L I R MAIN and ALT Boost Pumps ............................... . ............. ON 4. Altitude .................................... ESTABLISH 30,000 FT OR BELOW

FAA APPROVEDAugus t 12/13

Continued on next page -7 Emergency Procedures 04-08-00 REVISION 5 Page 04-35