APPENDIX 1 - Operator Differences Requirements GEX (BD-700-1A10) to G5000 (BD-700-1A11)

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
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