GULF STREAM GVI (G650) Manage

Atlanta Air craft Certification Office Central Region . FAA

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and signed by duly authorized representatives of both parties .If any provision hereof is f ound invalid or unenforceable by a court. the remainder of this Agreement shall remain v alid and enforceable.·' GulfstreamA GENERAL DYNAMICS COMPANY Gulfstream G650 Airplane Flight Manual Gulfstream Aerospace Document Number GAC-AC-G650-0PS-0001 August 12, 2013 TO: All Gulfstream G650 Operators SUBJECT: G650 Airplane Flight Manual Revis ion 5, Dated August 12, 2013 This letter to operators introduces the release of G650 Airplane 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 - Windmilling) in the event that engine fai lure 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, Option 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**Gult:~tremn** G650 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-G650-0PS-0001 FAA APPROVED Aug 12/13 RECORD OF REVISIONS REVISION 5 Page 1'' Gulfstream 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 04-3204-08-00 Page 04-3504-08-00 Page 04-38 DESCRIPTION OF CHANGE Normal Airstart -Automatic- re-write of procedure to address actions

taken in the event of a failed Mid Stage Check Valve (MSCV) . Manual Airstart - Starter Assist - re-write of procedure to address act i ons taken in the event of a fai led Mid Stage Check Valve (MSCV) . Manual Airstart - Windmilling - re-write of procedure to address actions taken in the event of a fai led Mid Stage Check Valve (MSCV) . ; j William S. Whitton, Jr. ODA Lead Administrator ODA-511131-CEDate **~·** l**~**2tJl> 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 04-04-00 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 04-04-00 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-os-oo ·o4-os-oo *04-08-00 *04-08-00 **~04-08-00** ·o4-os-oo· o4-os-oo·o4- 08-oo • Pages revised by Revision 5 •• Pages added by Revision 5 •·· Pages deleted by Revision 5

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DATE September 7/12 September 7/12

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 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 ·o4-08-oo *04-08-00 *04 -08-00 *04-08-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-10-00 04-11-00 04-11-00 04-13-00 04-13 - 0004-13-00 04-13-00 04-14-00 04-14-00 04-14-00 04-14-00 04-15-00 04-15-00 04-15-0004 -1 5 -0004-15-00 04-15-00 04-15-00 04-15-00 04-16-00 04-16-00 04-16-00 04-16 -0004-18-00 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 04-4604 -4 704-48 04-49 04-50 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 04-6504 -6604-67 04-68 04-69 04-70 04-71 04-72 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 12/13 August 12/13 August 12/13 August 12/13 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 September 7/12 September 7/12

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 2/13 February 13/13 February 13/13 February 13 /1 3 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 - 0004-19-00 04-19-00 04-20-00 04-20-00 04-21-00 04-21-00 04-23-00 04-23-00 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 rev i sed by Revis ion 5 •• Pages added by Revision 5 ••• Pages deleted by Revision 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 /1 3 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 2/1 3 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 revised by Revision 5 •• Pages added by Revision 5 ••• Pages deleted by Revision 5SECTION 04-00-00 04-00-10 04-04-00 04-04-1004- 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 04-10-20 04-10-30
GULFSTREAM G650 AIRPLANE FLIGHT MANUAL CHAPTER 04- EMERGENCY PROCEDURES TABLE OF CONTENTS SUBJECT PAGE Emergency Procedures..... ............................ ..... 04-1 Gene ral Guidance................ .... ....... .... .. ............ 04 -1 Electrical Power System .................................... 04-3 Dual Generator Failure (Above Altitude FL390).......................................................... ..... 04-3 Dua l Generator Fal lur e (Altitude FL390 or Below). ......................... . ............... ...... .... ........... 04-8 Operation On Airplane Batter ies, 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 Oil 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 Airstart -Automatic ........ ....................... 04-32 Manual Airstart - Starter Assist.... ...... ... ... .... ..... 04-35 Manual Airs tart - Wind milling... .................. .... ... 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 Fi re On Ground .. ...... .... .......... ....... .... ... 04-46 Ta ilpipe 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 Ma in 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 12/13SECTION 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 Pylon Hot ......... ............. ......... .... .. ..... .. ....... . . . . . .. 04-89 Aft Equ i pment 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 .F AA APPROVED August 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. LIR MAIN and ALT Boost Pumps ............................................. ON 4. Altitude .................................... ESTABLISH 30,000 FT OR BELOW FAA APPROVEDAugust 12/13 Continued on next page

**~** Emergency Procedures 04-08-00 REVISION 5 Page 04-35GULFSTREAM 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 ENG BLEED AIR switches must be OFF. 6. Affected ECS PACK ....... ..... ..... .................... .. .............. ..... ... .... .. OFF NOTE: If APU AIR is required to start the engine, BOTH ECS PACK swi tches must be OFF. 7. LIR WING ANTIICE ......................... .. .... ....... ......... ........ ....... .... OFF 8. Aff ected Engine Generator (GEN) ............................. SELECT OFF 9. CRANK MASTER .................................................... . ..................... ON NOTE: The Crank Master switch should illuminate, but the Start switch will not. 10. BLEED AIR Pressure ............. 35 PSI DESIRED I 20 PSI MINIMUM NOTE: APU AIR may be as low as 20 psi, but is adequate for engine start. 11. CONT IGN ... .... ......................................................... . .................... ON 12. Affected Engine ENG START .......................................... DEPRESS 13. Affected Engine FUEL CONTROL ............. RUN AT 20% HP RPM I CAUTION] THE FLIGHT CREW IS RESPONSIBLE FOR MONITORIN G LP, HP AND TGT DURING AIRSTARTS. THE FADEC SYSTEM WILL NOT AUTO-ABORT AN AIRSTART FORA TGT EXCEEDANCE. 14. Affected Engine FF (Fuel Flow) I TGT I RPM ................ MONITOR

RE VI SION 5 Page 04-36 Continued on next page --7 Emergency Procedures 04-08-00 FAA APPROV ED August 12/13GULFSTREAM G650 AIRPLANE FLIGHT MANUAL IF STABLE ENGINE IDLE IS ACHIEVED, PERFORM STEP 15 THROUGH STEP 25. IF ENGINE FAILS TO RESTART OR ACCELERATE TO IDLE, B PROCEED TO STEP 26. 15. CRANK MASTER ........................................................................ OFF 16. CONT IGN .................................................................................... OFF 17. Affected Engine SVO and IGN lcons ....................................... OUT 9 18. Affected Engine OIL PRESS I OIL TEMP ........................... CHECK II 19. 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 ENGINE AIRSTART.IN THE EVENT THE ENGINE FAILURE WAS CAUSED BY A FAILED MID

STAGE CHECK VALVE, LEAVING THE ENGINE BLEED AIR o·FF WILL PREVENT THE POSSIBILITY OF ANOTHER ENGINE FAILURE. 20. Affected Engine ENG BLEED AIR I WING ANTI ICE .............. OFF 21. ISOLATION Valve ..................................................................... OPEN 22. Affected ECS PACK I GENERATOR ............................... RESTORE 23. Fuel Balance ................................................. MONITOR I MAINTAIN 24. TCAS ...................................................................................... TA IRA 25. 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 position. 26. Affected Engine FUEL CONTROL ............................................ OFF 27. CRANK MASTER ........................................................................ OFF 28. CONT IGN .................................................................................... OFF Before attempting another s tart, allow the engine to drain for at least

thirty (30) seconds. 29. Procedure ............. RE-ACCOMPLISH AT LOWER ALTITUDE AND HIGHER AIRSPEED 30. Nearest Suitable Airport ......................................................... LAND Investigate cause of engine failure. FAA APPROVEDAugust 12/13 ENDEmergency Procedures 04-08-00 REVISION 5 Page 04-37