Operator Differences Requirements
GEX (BD-700-1A10) to G5000 (BD-700-1A11)
| DIFFERENCE AIRCRAFT: G5000 (BD-700-1A11)
BASE AIRCRAFT: GEX (BD-700-1A10) APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT
CHAR |
PROC
CHNG |
LVL
A |
LVL
B |
LVL
C |
LVL
D |
CHK | CURR |
| 20 Aircraft General | Fuselage
Length: 96 ft. 10 in. (29.49 m)Decrease of 32 in(.81 m)Removal of two side windows Wingspan: 94 ft. (28.65 m)No change Tailspan: 31ft. 9 in. (9.68 m)No change Height (SATCOM): 25 ft. 6 in. (7.77 m)No change |
No | No | HO | A | A | |||
| 20 Aircraft General | Performance
Max T.O. Weight: 87,700 lb. (39,780 kg) Decrease of 10,300 lb. (4,672 kg) Max Landing Weight: 78,600 lb. (35,655 kg)No change Fuel Capacity: 36,200 lb. (16,425 kg) Decrease of 7,350 lb. (3,325 kg) (GEX) Decrease of 8,900 lb. (4,000 kg) (GEX certified to 98,000 lb. (44,452 kg) Max T.O. Weight with increased centre tank fuel capacity) |
No | No | HO | A | A | |||
| 20 Aircraft General | Wheel Base
Nose to Main Wheels: 40 ft, 2 in. (12.25 m)Decrease of 2 ft 8 in (.81 m) |
No | No | HO | A | A | |||
| 28 Fuel | Removal of aft fuel tank | No | No | HO | A | A | |||
| 28 Fuel | Fuel recirculation is now an automatic system | No | See note | HO | A | A | |||
| 31 Indicating / Recording Systems | New fuel synoptic page | No | No | HO | A | A | |||
Note: The fuel recirculation, which is currently a manual system on the GEX, becomes an automatic system on the G5000 and later production GEX aircraft.
| DIFFERENCE AIRCRAFT: G5000 (BD-700-1A11)
BASE AIRCRAFT: GEX (BD-700-1A10) APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| TRAINING | CHKG/CURR | ||||||||
| SYSTEM | REMARKS | FLT
CHAR |
PROC
CHNG |
LVL
A |
LVL
B |
LVL
C |
LVL
D |
CHK | CURR |
| 28 Fuel | Reduction in centre tank capacity
Decrease of 5,050 lb. (2,300 kg) (GEX) Decrease of6,600 lb. (2,975 kg) (GEX certified to 98,000 lb. Max T.O. Weight (44,452 kg) with increased centre tank fuel capacity) |
No | No | HO | A | A | |||
| 28 Fuel | Minor EICAS/Synoptic page changes | No | No | HO | A | A | |||
| 28 Fuel | Fuel control panel, deletion of switches and switch labels changed | No | See note | HO | A | A | |||
| 28 Fuel | Refueling panel, deletion of switches and switch labels changed | No | No | HO | A | A | |||
Note: The Fuel RECIRC switches become an inhibited function vice an ON/OFF one
| DIFFERENCE AIRCRAFT: G5000 (BD-700-1A11)
BASE AIRCRAFT: GEX (BD-700-1A10) APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT
CHAR |
PROC
CHNG |
LVL
A |
LVL
B |
LVL
C |
LVL
D |
CHK | CURR |
| Taxi | Very slight decrease in taxi turning radius. 2 FT 8 IN (.82M) | No | No | HO | A | A | |||
Operator Differences Requirements
G5000 (BD-700-1A11) to GEX (BD-700-1A10)
| DIFFERENCE AIRCRAFT: GEX (BD-700-1A10)
BASE AIRCRAFT: G5000 (BD-700-1A11) APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| TRAINING | CHKG/CURR | ||||||||
| DESIGN | REMARKS | FLT
CHAR |
PROC
CHNG |
LVL
A |
LVL
B |
LVL
C |
LVL
D |
CHK | CURR |
| 20 Aircraft General | Fuselage
Length: 99 ft. 5 in. (30.30 m)Increase of 32 in (.81 m)Addition of two side windows Wingspan: 94 ft. (28.65 m)No change Tailspan: 31ft. 9 in. (9.68 m)No change Height (SATCOM): 25 ft. 6 in. (7.77 m)No change |
No | No | HO | A | A | |||
| 20 Aircraft General | Performance
Max T.O. Weight: 98,000 lb. (44,452kg) Increase of 10,300 lb. (4,672 kg) Max Landing Weight: 78,600 lb. (35,655 kg)No change GEX Fuel Capacity: 43,550 lb.(19,750 kg)Increase of 7,350 lb.(3,325 kg) GEX certified to 98,000 lb. Max T.O. Weight (44,452 kg) with increased centre tank fuel capacity: 45,100 lb.(20,425 kg);Increase of 8,900 lb.(4,000 kg) |
No | No | HO | A | A | |||
| 20 Aircraft General | Wheel Base
Nose to Main Wheels: 42 ft, 10 in. (12.25 m)Increase of 2 ft 8 in (.81 m) |
No | No | HO | A | A | |||
| 28 Fuel | Addition of aft fuel tank | No | No | HO | A | A | |||
| 28 Fuel | Fuel recirculation is now a manual system | No | See note | HO | A | A | |||
| 31 Indicating / Recording Systems | New fuel synoptic page | No | No | HO | A | A | |||
Note: The fuel recirculation, which is currently a manual system on the GEX, becomes an automatic system on both the G5000 and for later production GEX aircraft.
| DIFFERENCE AIRCRAFT: GEX (BD-700-1A10)
BASE AIRCRAFT: G5000 (BD-700-1A11) APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| TRAINING | CHKG/CURR | ||||||||
| SYSTEM | REMARKS | FLT
CHAR |
PROC
CHNG |
LVL
A |
LVL
B |
LVL
C |
LVL
D |
CHK | CURR |
| 28 Fuel | Increase in centre tank capacity
Increase of 5,050 lb. (2,300 kg) (GEX) Increase of6,600 lb. (2975 kg) (GEX certified to 98,000 lb. Max T.O. Weight (44,452 kg) with increased centre tank fuel capacity) |
No | No | HO | A | A | |||
| 28 Fuel | Minor EICAS/Synoptic page changes | No | No | HO | A | A | |||
| 28 Fuel | Fuel control panel, addition of switches and switch labels changed | No | See note | HO | A | A | |||
| 28 Fuel | Refueling panel, addition of switches and switch labels changed | No | No | HO | A | A | |||
Note: The Fuel RECIRC switches become an ON/OFF function vice an inhibited one
| DIFFERENCE AIRCRAFT: GEX (BD-700-1A10)
BASE AIRCRAFT: G5000 (BD-700-1A11) APPROVED BY (POI)____________________________ |
COMPLIANCE METHOD | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| TRAINING | CHKG/CURR | ||||||||
| MANEUVER | REMARKS | FLT
CHAR |
PROC
CHNG |
LVL
A |
LVL
B |
LVL
C |
LVL
D |
CHK | CURR |
| Taxi | Very slight increase in taxi turning radius 2 ft. 8 in. (.82m) | No | No | HO | A | A | |||