GULFSTREAM G650 Model Guide
GULFSTREAM G650 · Model Guide
Overview
GULFSTREAM G650 is a large twin-engine turbofan business jet. Its flight manual limits it to 22 occupants, of which 19 may be passengers, and to a 51,000 ft maximum operating altitude. The wider Gulfstream GVI family is listed at up to 7,000 nm range and 488 kt cruise. Those are family maxima, not G650 figures. The G650ER variant has higher weights and more fuel.
- Max takeoff weight is 99,600 lbs for the G650 and 103,600 lbs for the G650ER. Max landing weight is 83,500 lbs for both.
- Fuel capacity is 44,200 lb (6,558 gal) on the G650 and 48,200 lb (7,152 gal) on the G650ER.
- Takeoff is prohibited in any flight control law other than Normal, and with frost, ice, snow or slush on critical surfaces.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 49 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Fuel capacity (gal) ·
- 6,558
- Fuel capacity (lb) ·
- 44,200
- Max operating altitude (ft) ·
- 51,000
- Max fuel imbalance takeoff (lb) ·
- 1,000
- Max operating altitude single pack (ft) ·
- 48,000
Performance
- Max tailwind (kt) ·
- 10
- Demonstrated crosswind (kt) ·
- 28
- Max airfield pressure altitude (ft) ·
- 15,000
V-speeds
- VA_KTS ·
- 206
- VLE_KTS ·
- 250
- VFE_FLAPS_10_KTS ·
- 250
- VFE_FLAPS_20_KTS ·
- 220
- VFE_FLAPS_39_KTS ·
- 190
- VMCG_SEA_LEVEL_KTS ·
- 105
- VMO_ABOVE_8000FT_KTS ·
- 340
- VMO_BELOW_8000FT_KTS ·
- 300
Weight & balance
- Max ramp weight (lb) ·
- 100,000
- Max landing weight (lb) ·
- 83,500
- Max takeoff weight (lb) ·
- 99,600
- Max zero fuel weight (lb) ·
- 60,500
How many people can the GULFSTREAM G650 carry?
The GULFSTREAM G650 flight manual limits total occupants to 22, with no more than 19 passengers. The wider GVI family is listed with up to 24 passengers, but that is a family maximum.
What is the difference between G650 and G650ER weights?
For the GULFSTREAM G650, max takeoff weight is 99,600 lbs and max ramp is 100,000 lbs. The G650ER is 103,600 lbs and 104,000 lbs. Max landing weight (83,500 lbs) and max zero fuel weight (60,500 lbs) are the same.
What should I check in the records of a GULFSTREAM G650?
Check that the flight control computer software update (ASC 037) is done, along with the open and recurring ADs, such as AD 2020-11-01 on the primary flight control actuation software. Also confirm the AFM revision and engine and APU times.
What is the GULFSTREAM G650 Model Guide?
The GULFSTREAM G650 Model Guide is a model guide for the GULFSTREAM G650, dated 2026.
What year was the GULFSTREAM G650 Model Guide published?
The GULFSTREAM G650 Model Guide — the GULFSTREAM G650 model guide on file — is dated 2026.
Common. More common than 94% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the GULFSTREAM 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
Operating limits to know
Max tailwind is 10 kts. Demonstrated crosswind is 28 kts, or 25 kts above 10,000 ft. Max airfield pressure altitude is 14,500 ft for s/n 6003 through 6019 and 15,000 ft for s/n 6001 and above 6020, so check the serial number. Max operating altitude is 51,000 ft, or 48,000 ft with a single air-conditioning pack.
Flight control software (ASC 037)
ASC 037 Rev A updates the flight control computer software from v5.44 to v6.24. It adds range and cruise improvements, auto-brake provision and production yaw trim. It applies to s/n 6001 to 6164, takes about 51 labor-hours, and is done only at authorized Gulfstream facilities. FAA operators need AFM Revision 10 or later. Confirm it is incorporated.
Records and AD status
The sample Master AD/SI report for s/n 6101 shows two BR725A1-12 engines and an APU. It shows 1245.8 hours and 507 AFL as of 23-Apr-2020. Most ADs show as complied with. AD 2020-11-01 (primary flight control actuation software update) was listed with 27-JUL-2022 as its next-due date. Ask for the current AD/SI report for the specific aircraft.
Safety notes
- The RAT may not be deployed when normal AC power is available, except in emergencies or as an abnormal or emergency checklist directs.
- Flight into known icing is prohibited when the flight control law is Alternate, Direct or Backup. Exit icing if the law degrades.
- Landing-gear and flap speeds are limited. VFE is 250 KCAS at flaps 10, 220 at flaps 20 and 190 at flaps 39.
Full document text
GULFSTREAM G650 Model Guide GULFSTREAM G650 is a large twin-engine turbofan business jet. Its flight manual limits it to 22 occupants, of which 19 may be passengers, and to a 51,000 ft maximum operating altitude. The wider Gulfstream GVI family is listed at up to 7,000 nm range and 488 kt cruise. Those are family maxima, not G650 figures. The G650ER variant has higher weights and more fuel. • Max takeoff weight is 99,600 lbs for the G650 and 103,600 lbs for the G650ER. Max landing weight is 83,500 lbs for both. • Fuel capacity is 44,200 lb (6,558 gal) on the G650 and 48,200 lb (7,152 gal) on the G650ER. • Takeoff is prohibited in any flight control law other than Normal, and with frost, ice, snow or slush on critical surfaces. Operating limits to know Max tailwind is 10 kts. Demonstrated crosswind is 28 kts, or 25 kts above 10,000 ft. Max airfield pressure altitude is 14,500 ft for s/n 6003 through 6019 and 15,000 ft for s/n 6001 and above 6020, so check the serial number. Max operating altitude is 51,000 ft, or 48,000 ft with a single air-conditioning pack. Flight control software (ASC 037) ASC 037 Rev A updates the flight control computer software from v5.44 to v6.24. It adds range and cruise improvements, auto-brake provision and production yaw trim. It applies to s/n 6001 to 6164, takes about 51 labor-hours, and is done only at authorized Gulfstream facilities. FAA operators need AFM Revision 10 or later. Confirm it is incorporated. Records and AD status The sample Master AD/SI report for s/n 6101 shows two BR725A1-12 engines and an APU. It shows 1245.8 hours and 507 AFL as of 23-Apr-2020. Most ADs show as complied with. AD 2020-11-01 (primary flight control actuation software update) was listed with 27-JUL-2022 as its next-due date. Ask for the current AD/SI report for the specific aircraft. Safety notes: • The RAT may not be deployed when normal AC power is available, except in emergencies or as an abnormal or emergency checklist directs. • Flight into known icing is prohibited when the flight control law is Alternate, Direct or Backup. Exit icing if the law degrades. • Landing-gear and flap speeds are limited. VFE is 250 KCAS at flaps 10, 220 at flaps 20 and 190 at flaps 39.