G650 Airplane Flight Manual Supplement No. G650-2019-03
Gulfstream Aerospace G650 · Pilot's Operating Handbook
Overview
This document is a supplement to the Gulfstream G650 Airplane Flight Manual, specifically for aircraft with serial numbers 6001 and subsequent that do not have ASC 134. It provides updated limitations, procedures, and performance information that supersede the basic manual.
- Applies to G650 airplanes SN 6001 and subsequent without ASC 134.
- Limits operating envelope to below 250 KCAS / 0.925M unless in an emergency.
- Maximum altitude with rudder or yaw damper inoperative is 20,000 ft.
- Maximum operating limit speed is 250 KCAS / 0.925M, except for emergencies.
- Revised procedures for rudder failure include immediate autopilot disconnection.
- Maintain airspeed below 200 KCAS to reduce roll oscillations during rudder failure.
- Landing should be performed as soon as practicable in case of rudder failure.
- Use smooth roll inputs to minimize lateral-directional oscillations.
Document
Source
Originally published by regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Year ·
- 2019
- File size ·
- 215 KB
- Publisher ·
- regulations.gov
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Max speed kcas ·
- 250
- Max speed mach ·
- 0.925
- Max operating altitude (ft) ·
- 20000
Performance
- Max operating speed kcas ·
- 250
- Max operating speed mach ·
- 0.925
V-speeds
- VMO_KCAS ·
- 250
What is the G650 Airplane Flight Manual Supplement No. G650-2019-03?
The G650 Airplane Flight Manual Supplement No. G650-2019-03 is a pilot's operating handbook for the Gulfstream Aerospace G650, dated 2019.
Where does the G650 Airplane Flight Manual Supplement No. G650-2019-03 come from?
This copy of the G650 Airplane Flight Manual Supplement No. G650-2019-03 was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.
What year was the G650 Airplane Flight Manual Supplement No. G650-2019-03 published?
The G650 Airplane Flight Manual Supplement No. G650-2019-03 — the Gulfstream Aerospace G650 pilot's operating handbook on file — is dated 2019.
Most owners only have the POH. Here's the essential set for the Gulfstream Aerospace G650.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
PREFACE
This section introduces the supplement and specifies its applicability to certain G650 aircraft, noting limitations on operating speeds.
LIMITATIONS
Details maximum operating altitudes and airspeed limitations, including specific conditions for rudder and yaw damper inoperative scenarios.
NORMAL PROCEDURES
No changes are made to the normal procedures outlined in the basic Airplane Flight Manual.
ABNORMAL PROCEDURES
Revisions to procedures for handling rudder failure, emphasizing immediate actions to mitigate roll/yaw oscillations.
EMERGENCY PROCEDURES
No changes are made to the emergency procedures outlined in the basic Airplane Flight Manual.
PERFORMANCE
No changes are made to the performance information in the basic Airplane Flight Manual.
Safety notes
- Do not delay disconnecting the autopilot to prevent undesirable roll/yaw oscillations.
- Maintain airspeed below 200 KCAS to minimize roll oscillations during rudder failure.
- Select the longest and widest runway available for landing in case of rudder failure.
Full document text
GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 Gulfstream Aerospace Corporation Supplement No. G650-2019-03 P.O. Box 2206 Savannah, Ga. 31402-2206 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR GULFSTREAM MODEL G650 REGISTRATION NUMBER: SERIAL NUMBER: This Supplement must be attached to the FAA Approved GVI (G650) Airplane Flight Manual, dated September 7, 2012, for G650 airplanes Serial Number (SN) 6001 and subsequent not having ASC 134. The information contained herein supplements or supersedes the information of the basic Airplane Flight Manual. For Limitations, Normal Procedures, Abnormal Procedures, Emergency Procedures and Performance information not contained in this supplement, consult the basic Airplane Flight Manual. FAA APPROVED: �ill%fl-Robert Glasscock ODA Lead Administrator Gulfstream Aerospace Corporation ODA-511131-CE DATE: IJovern/a�v 4, ZOI 1I This page intentionally left blank. GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 FAA APPROVED BASIC ISSUE Nov 04/19 Page i LOG OF REVISIONS Revision Number Affected Pages Description of Revision GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 BASIC ISSUE FAA APPROVED Page ii Nov 04/19 This page intentionally left blank. GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 FAA APPROVED BASIC ISSUE Nov 04/19 Page 1 SECTION 0 PREFACE Introduction / General This Airplane Flight Manual Supplement applies only to G650 airplanes Serial Number (SN) 6001 and subsequent not having ASC 134 incorporated. This supplement limits the Operating Envelope of these aircraft below 250 KCAS / 0.925M unless responding to an emergency procedure where a higher airspeed is required for continued safe flight, such as loss of pressurization or high engine vibrations. Revised abnormal procedures are provided for loss of rudder or yaw damper. GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 BASIC ISSUE FAA APPROVED Page 2 Nov 04/19 SECTION 1 LIMITATIONS 01-03-30: Maximum Operating Altitudes Add Item 6: 6. Rudder and/or Yaw Damper Inoperative Altitude: The maximum altitude when operating with a failed rudder (as indicated by Rudder Fail (caution) CAS message) and/or yaw damper inoperative is 20,000 ft. 01-03-40: Airspeed Limitations Revise Items 6 and 7: 6. Maximum Operating Limit Speed (VMO / MMO): Maximum operating limit speed shall not be deliberately exceeded in any regime of flight (climb, cruise, or descent). The maximum operating envelope is limited to 250 KCAS / 0.925M, unless higher speed (340 KCAS / 0.925M) is necessary to comply with emergency procedures requiring rapid descents. See Figure 2: Altitude / Mach Flight Envelope on the next page. 7. Rudder and/or Yaw Damper Inoperative Speed: The maximum speed when operating with a failed rudder (as indicated by Rudder Fail (caution) CAS message) and/or yaw damper inoperative is 250 KCAS / 0.9M. GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 FAA APPROVED BASIC ISSUE Nov 04/19 Page 3 Figure 2. Altitude / Mach Flight Envelope TIL-056241 Pressure Altitude - FT Mach Number MMO 0.9M 0.85M 0.8M 51000 ft, Mach 0.925 35000 ft, 0.925M 29380 ft, 0.875M VMO=340 KCAS 300 KCAS 250 KCAS Emergency Descent Only Takeoff & Landing Takeoff & Landing NOTE: • Airplane S/Ns 6003 through 6019 = 14500 airport pressure altitude • Airplane S/Ns 6001, and 6020 and subs = 15000 airport pressure altitude 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 -10000 0 10000 20000 30000 40000 50000 60000 -5000 5000 15000 25000 35000 45000 55000 GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 BASIC ISSUE FAA APPROVED Page 4 Nov 04/19 SECTION 2 NORMAL PROCEDURES No change to the Airplane Flight Manual. SECTION 3 ABNORMAL PROCEDURES 03-25-10: Crew Alerting System (CAS) Caution Messages and Procedures Revise Corrective Action column for amber Rudder Fail CAS message to read: 03-13-200: Rudder Failure Replace the procedure in its entirety to read: An inoperative rudder will result in the loss of the FCS yaw damper function; therefore, encountering turbulence and gusting wind conditions may cause lateral-directional oscillations. Use smooth roll inputs during all phases of flight to the maximum extent practicable to minimize sideslip buildup. CAUTION DO NOT DELAY DISCONNECT OF AUTOPILOT TO PREVENT THE POSSIBLE ONSET OF UNDESIRABLE ROLL/YAW OSCILLATIONS. NOTE: If EBHA actuator is still operative, the FCC may control rudder directly through use of the MCE and message may be caused by both REUs being failed. Rudder trim indication may respond to trim inputs without corresponding rudder surface motion. Apply small rudder pedal inputs and observe airplane response to verify surface operational status. CAS MESSAGE POSSIBLE CAUSE(S) CORRECTIVE ACTION Rudder Fail Both REUs and/or actuators on rudder flight control surface are inoperative. (1) Autopilot – IMMEDIATELY OFF (2) Airspeed – WITHOUT USING SPEED BRAKES, SLOW IMMEDIATELY BELOW 200 KCAS AND MAINTAIN BELOW PITCH LIMIT INDICATOR. GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 FAA APPROVED BASIC ISSUE Nov 04/19 Page 5 1. Autopilot ............................................................. IMMEDIATELY OFF 2. Airspeed .................................. WITHOUT USING SPEED BRAKES, SLOW IMMEDIATELY BELOW 200 KCAS AND MAINTAIN BELOW PITCH LIMIT INDICATOR 3. FLT CTRL RESET Switch ...................................................... PRESS IF CAS MESSAGE CLEARS, AND RUDDER CONTROL RESPONSE RETURNS, CONTINUE NORMAL FLIGHT. IF SIGNIFICANT, REPEATED ROLL OSCILLATIONS ARE PRESENT: 4. Wheel Inputs ........... USE SUFFICIENTLY LARGE WHEEL INPUTS TO MAINTAIN BANK ANGLE OF APPROXIMATELY ± 10 DEG NOTE: Roll oscillations are significantly reduced if airspeed can be slowed below 200 KCAS and oscillations may cease below
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20,000 ft. Maintain below Pitch Limit indicator while slowing. When roll oscillations cease, cruise flight below 250 KCAS and 20,000 ft can be performed. 5. Altitude ............DESCEND WHILE REMAINING BELOW 200 KCAS .......................... UNTIL REPEATED ROLL OSCILLATIONS CEASE 6. Altitude / Airspeed .... REMAIN BELOW 250 KCAS AND 20,000 FT FOR REMAINDER OF FLIGHT 7. Autopilot ...................................................................... AS DESIRED 8. Airport ..................................... LAND AS SOON AS PRACTICABLE NOTE: Select longest and widest runway available, based on minimum crosswind less than 10 knots; use asymmetric thrust to facilitate runway alignment on approach to landing, if required. 9. Landing Controllability Check ........................................ PERFORM See 03-13-10: Landing Controllability Check. GULFSTREAM AEROSPACE G650 AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. G650-2019-03 BASIC ISSUE FAA APPROVED Page 6 Nov 04/19 10. Approach / Landing .............................................AUTOPILOT OFF NOTE: Plan for long, shallow final approach; use smooth roll inputs to minimize roll/yaw oscillations, maximum extent practicable. 11. Yaw .......................... USE DIFFERENTIAL THRUST IF REQUIRED 12. Airspeed ...................................................................... VREF +10 KTS 13. Landing Flare ......................... MAINTAIN ASYMMETRIC THRUST DIFFERENTIAL DURING THROTTLE REDUCTION UNTIL AFTER NOSEWHEEL TOUCHDOWN TO MINIMIZE YAW EXCURSIONS LANDING: 14. Speed Brakes ..................................................................... EXTEND NOTE: Ground spoilers will not extend until both throttles are at idle position. 15. Nose Wheels....................... LOWER TO GROUND IMMEDIATELY 16. Differential Braking and Nosewheel Steering ................................ .......................COORDINATE USE FOR DIRECTIONAL CONTROL 17. Throttle...................... RETARD REMAINING THROTTLE TO IDLE END SECTION 4 EMERGENCY PROCEDURES No change to the Airplane Flight Manual. SECTION 5 PERFORMANCE No change to the Airplane Flight Manual.