# GULFSTREAM GVI (G650)

Manage Atlanta Aircraft Certification Office Central Region

. FAA 

# SEP 7 2012

DATE OF ISSUE 

# Gulfstream®

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# Gulf 

# stream

A 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 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 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, 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 31402 1-800-810-4853 , Option 3 (United States) 1-912-965-4178, Option 3 (International) 1-912-965-3520 (Fax) michael

.woods@gulfstream.com

# (}ulf<stream 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 Feb13/13 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 12/13

### GULFSTREAM 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 DESCRIPTION OF CHANGE 04-08-00 Normal Airstart -Automatic- re-write of procedure to address actions Page 04-32 taken in the event of a failed Mid Stage Check Valve (MSCV)

. 04-08-00 Manual Airstart
- Starter Assist
- re-write of procedure to address Page 04-35 actions taken in the event of a fa iled Mid Stage Check Valve (MSCV)

. 04-08-00 Manual Airstart
- Windmilling
- re-write of procedure to address Page 04-38 actions taken in the event of a failed Mid Stage Check Valve (MSCV)

.



### FAA APPROVED 

### August 12/13 LOG OF REVISIONS

### REVISION 5 Page 2 GULFSTREAM G650 AIRPLANE FLIGHT MANUAL

THIS PAGE IS INTENTIONALLY LEFT BLANK

.



### LOG OF REVISIONS FAA APPROVED August 12/13

### GULFSTREAM 

### G650 AIRPLANE FLIGHT MANUAL CHAPTER 04 - EMERGENCY PROCEDURES 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 *04-08-00 *04-08-00 *04-08-00 ·o4-08-00

' 04-08-00 *04-08-00 *04-08-00 *04-08-00

• Pages revised 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 04-10 04
- 11 04-12 04-13 04-14 04-15 04-16 04-17 04-1 8 04-19 04
-20 04-21 04
-22 04-23 04-24 04-25 04-26 04-27 04-28 04-28.1 04-28.2 04-29 04-30 04-30

. 1 04-30

.2 04-31 04-32 04-33 04-34 04-35 04-36 04-37 04-38 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 17/13 August 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 -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 04-1 3
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### GULFSTREAM G650 AIRPLANE FLIGHT MANUAL
PAGE 04-39 04-40 04-41 04-42 04-43 04-44 04-45 04-46 04-47 04-48 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 04-65 04-66 04-67 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 2 August 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 13/13 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 Revision 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 04-23-00 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 revised by Revision 5 •• Pages added by Revision 5 ••• Pages deleted by Revis i on 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 12/13

### GULFSTREAM G650 AIRPLANE FLIGHT MANUAL

THIS PAGE IS INTENTIONALLY LEFT BLANK.

LIST OF EFFECTIVE PAGES Page 4 August 12/13 • Pages revised by Revision 5 •• Pages added by Revision 5

... Pages deleted by Revision 5

### SECTION 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 04-10-20 04-10-30 GULFSTREAM G650 AIRPLANE FLIGHT MANUAL 

### CHAPTER 04
- EMERGENCY PROCEDURES TABLE OF CONTENTS SUBJECT PAGE Emergency Procedures.......

............ ....... ... ........ . 04-1 General Guidance..............................

. ...... . ....... 04-1 Electrical Power System .................................... 04-3 Dual Generator Failure (Above Altitude FL3.90)....

.. ...... .. .. ..... .. . ... ..... ... .... ...... ...... ... ... . ..... 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 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 Airstart - 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 Fire On Ground

... .. ... .... ... ... .... .. .. ...... .... 04-46 Tailpipe Fire.........

.. ........ ................................... 04-47 FAA APPROVED August 12/13 REVISION 5 Page 1SECTION 

### 04- 1 0-40

.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- 1 0
REV IS IO N 5 Page 2 SUBJEC T 

### 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 Rudde r ..... . .. .... .... .. ......... .. .. .. .. ........ . . . . 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) Fai lure - Loss of Pressure and Fluid

... ..... .. .. . . . .. .. .. .... ........ .. .... 04-69 Indicating 

### I Recording System.......................... 04-73 Pri mary Flight Display (PFD) Malfunction ........ 04-73 Suspected Erroneous 

### I Unreliable Ai rspeed Ind ications...

.... ..... .. .. ..... ...... ... . . .. . ... .. ... .. .. ...... .... 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 Gea r Down and Locked.

... . . .... .. .. .. ........ . ... . .. ... .. .. .. . . ... .. . ....... 04
-79 All Gear Up Landing Procedure

....... . ........... .. .. 04-79 Landing , Stopping and Evacuation

.......... .. ....... 04-8 1 Overweight Landing

.. ... .... ... .............................. 04-81 Ditch ing
.. ..... .. .. . ... .. .. .. .. .. .. ... .. .. . .... . ... . ... .. ... ...... . . . 04-81 Emergency Escape Routes.

.... .. . .. .. . ....... .. .... . ... 04-84 Immediate Return For Landing
............. .. ...... .. .. 04-86 Emergency Airp lane Evacuation

...... . ............ .... 04-86 Overheat 

### I Hot Cond itions

.. .. ..... ... ...... .... . . ......... 04-89 Engine Hot ............................... .. ............ .. ......... 04-89
FAA A PPROVED Augu st 1 2/1 3SECTION 

### 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 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 APPROVED August 12/13 REVISION 5 Page 3REVISION 5 

### Page 4 GULFSTREAM G650 AIRPLANE FLIGHT MANUAL

THIS PAGE IS INTENTIONALLY LEFT BLANK.

FAA APPROVED August 12/13

### GULFSTREAM G650 AIRPLANE FLIGHT MANUAL 

### 04-08-40: Manual Airstart
- Windmilling 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 (e.g., failed starter). 

# 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 NOTAUTO-ABORTAN AIRSTART FOR A TGT EXCEEDANCE.

# IWARNING 

# 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. Affected Engine ENG BLEED AIR I ECS PACK
......................OFF 

### 4. Affected Engine Generator (GEN) ............................................OFF 

### 5. L 

### I R MAIN and AL T Boost Pumps .............................................ON 

### 6. Altitude I Airspeed

........ ESTABLISH 

### 30,000 FT OR BELOW I 

### 250 KCAS MINIMUM 

### 7. Affected Engine HP RPM
..........................VERIFY ABOVE 

### 5% HP NOTE: The FADEC will not allow fuel to 

### the engine below 5% 

### HP RPM.

REVISION 5 

### Page 04-38 Continued on next page

**~** 

### Emergency Procedures 

### 04-08-00 FAA APPROVED August 12/13

### GULFSTREAM G650 AIRPLANE FLIGHT MANUAL


### 8. CONT IGN .....................................................................................ON 9. Affected Engine FUEL CONTROL.
...........................................RUN 

# I

CAUTION 

# I
THE FLIGHT CREW IS RESPONSIBLE FOR MONITORING LP, HP AND TGT DURING AIRSTARTS. THE FADEC SYSTEM WILL NOTAUTO-ABORT AN AIRSTART FORA TGT EXCEEDANCE. 

### 10. Affected Engine FF (Fuel Flow) 

### I TGT 

### I RPM

................MONITOR IF STABLE ENGINE IDLE IS ACHIEVED, PERFORM STEP 11 

## I THROUGH STEP 19. IF ENGINE FAILS TO RESTART OR ACCELERATE TO IDLE, 

## I PROCEED TO STEP 20. 11. Affected Engine OIL PRESS 

### I OIL TEMP
...........................CHECK 12. CONT IGN ....................................................................................OFF 13. 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 OFF WILL PREVENT THE POSSIBILITY OF ANOTHER ENGINE FAILURE. 

## I 14. Affected Engine ENG BLEED AIR 

### I WING ANTI ICE

..............OFF 

## I 15. ISOLATION Valve .....................................................................OPEN 

## 1 16. Affected ECS PACK 

### I GENERATOR
............................... RESTORE 

# I 17. Fuel Balance.................................................MONITOR 

### I MAINTAIN 18. TCAS ...................................................................................... TA IRA 19. 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 switch prior to placing it in the OFF position. 

### 20. Affected Engine FUEL CONTROL
............................................OFF 21. CONT IGN ....................................................................................OFF Before attempting another start , allow the engine to drain for at least thirty (30) seconds.

FAA APPROVED August 12/13 

### Continued on next page __, Emergency Procedures 04-08-00 REVISION 5 Page 04-39

### GULFSTREAM G650 AIRPLANE FLIGHT MANUAL


### 22. Procedure
......................RE-ACCOMPLISH .AT LOWER ALTITUDE 

# I 23. Nearest Suitable Airport .........................................................LAND Investigate cause of engine failure

. END 

### 04-08-50: One (1) Engine Inoperative Landing Procedure

FOR APPROACH AND LANDING, OPERATION OF LANDING GEAR, FLAPS, SPOILERS, THRUST REVERSER .AND BRAKES SHOULD BE ACCOMPLISHED AS SEPARATE EVENTS, NOT SIMULTANEOUSLY:



### 1. Autothrottle .................................................................................OFF NOTE: Use of autothrottle during single engine approaches is prohibited. 

### 2. PWR XFR UNIT (If Left Engine Failed) ......................................ON 

### 3. AUX PUMP (If Left Engine Failed) ...........................................ARM 4. Flaps ..............................................................................................20° 5. Landing Gear ......................................................DOWN I 3 GREEN 6

. .Airspeed .......................................VREF FOR 20° FLAPS +10 KCAS 7. Ground Spoilers (GND SPLR) .............................................ARMED NOTE: With left engine failed, midboard spoiler panels will be inoperative

. With right engine failed, inboard spoiler panels will be inoperative. See Section 05-11-30, Landing Field Length. 8. Brakes I Hydraulics I Brake Accumulators

.......CHECKED I 3000 PSI 9. NO SMOKE ...................................................................................ON 10. WARN INHIBIT ......................................................................INHIBIT 11. Flight Controls 1/6 Synoptic Display
........................... . .... SELECT AT FINAL APPROACH FIX: 12. FLAPS

. ....... . .................................................................. .39° (DOWN) NOTE: If the crew elects to land at flaps 20°, fly the approach at VREF 

### for flaps 20° + 

### 10 knots. See Section 5, Performance for additional information pertaining to landing distance in the flaps 20° configuration

.

REVISION 5 

### Page 04-40 Continued on next page --?


### Emergency Procedures 04-08-00 FAA APPROVED 

### August 12/13