Global 7500 Aircraft Limitations and Systems Flashcards

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Flashcards covering Global 7500 aircraft specifications, performance limitations, operational speeds, and hydraulic system logic based on AFM and FCOM documentation.

Last updated 7:56 PM on 8/10/26
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51 Terms

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Global 7500 Model Designation

BD-700-2A12

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Minimum Flight Crew

One pilot and one co-pilot

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Maximum Occupants

2222 people: consisting of 1919 passengers and 33 crewmembers (or the number of approved seats, whichever is less)

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Global 7500 Wingspan

104ft104\,\text{ft} (31.71m31.71\,\text{m})

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Global 7500 Length

111ft2in111\,\text{ft}\,2\,\text{in} (33.88m33.88\,\text{m})

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Maximum Tail Height

27ft27\,\text{ft} (8.24m8.24\,\text{m}) on level ground partially loaded; may reach 28ft28\,\text{ft} when empty

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Minimum Pavement Width (180° Turn)

75ft75\,\text{ft} (22.86m22.86\,\text{m}) for landing gear

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Wing Tip Clearance Width

129ft1in129\,\text{ft}\,1\,\text{in} (39.34m39.34\,\text{m})

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Maximum Ramp Weight

115,100lb115,100\,\text{lb} (52,208kg52,208\,\text{kg})

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Maximum Takeoff Weight (MTOW)

114,850lb114,850\,\text{lb} (52,095kg52,095\,\text{kg})

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Maximum Landing Weight (MLW)

87,600lb87,600\,\text{lb} (39,735kg39,735\,\text{kg})

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Maximum Zero Fuel Weight (ZFW)

67,500lb67,500\,\text{lb} (30,617kg30,617\,\text{kg})

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Minimum/Maximum Runway Slope

±2%\pm 2\%

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Unprepared Runways Limitation

Operations from unprepared runways are not conducted

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Circling Approach Configuration (Normal)

Flaps 4 at Vref+10V_{ref} + 10 (until maneuvering complete); then VrefV_{ref} on final

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Checklist Procedure Priority (High to Low)

Emergency, Normal, Caution, Advisory, and INFO messages (ground)

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Water Operation Buoyancy Limitations

Outflow valve 2 must be closed and R Pack must be OFF

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Mmo (above FL350)

0.925M0.925M

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Vmo (below 8,000 feet)

300kt300\,\text{kt}

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Turbulence Penetration Speed (High Altitude)

285kt285\,\text{kt} (from 10,000ft10,000\,\text{ft} and above) or 0.85M0.85M, whichever is lower

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Maximum Certified Operating Altitude

FL510

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Maximum Pressure Altitude (Takeoff and Landing)

10,000ft10,000\,\text{ft} pressure altitude

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Minimum Ambient Temperature (Takeoff)

40C-40^{\circ}\text{C} (40F-40^{\circ}\text{F})

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Maximum Tailwind (Engine Start)

20kt20\,\text{kt}

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Crosswind Takeoff Procedure (>18kt)

Do not exceed 60%60\% N1N_1 below 30kt30\,\text{kt}; then promptly set TO thrust

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Slats/Flaps Altitude Limit

18,000ft18,000\,\text{ft} maximum

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Landing Gear Extended Altitude Limit

20,000ft20,000\,\text{ft} (AFM Limitation)

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Flight Spoiler Retraction Altitude

300ft300\,\text{ft} minimum on approach

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MAX Spoilers Restriction

Prohibited except during emergency conditions or as required by AFM procedures

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Flap 1 Speed Limit

225kt225\,\text{kt}

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Flaps 2 and 3 Speed Limit

210kt210\,\text{kt}

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Flaps 4 Speed Limit

185kt185\,\text{kt}

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VLO (Landing Gear Operating Speed)

200kt200\,\text{kt}

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VLE (Landing Gear Extended Speed)

250kt250\,\text{kt}

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Tire Limiting Speed

195kt195\,\text{kt}

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VMCG (Flaps 2 and 3)

106kt106\,\text{kt}

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VMCA (Flaps 3 at Sea Level)

98kt98\,\text{kt}

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VMCL (Flaps 4 / Gear Down at Sea Level)

96kt96\,\text{kt}

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Normal Hydraulic Power Supply

The three "A" pumps which operate continuously

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Maximum Ground ACMP Operation (APU or External)

22 pumps

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EDP-Powered Hydraulic Systems

Systems 1 and 2 (by EDP 1A and 2A)

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Hydraulic Pressure Check Procedure (Pre-start)

Turn on the "B" and PTU pumps to pressurize the system and use the synoptic page

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Nominal Hydraulic System Pressure

3000psi3000\,\text{psi}

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Hydraulic Fluid Type

Phosphate Ester Type IV or V, low density fluid (Skydrol)

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ACMP 1B AUTO Operation Triggers

Takeoff/approach phase, EDP 1A failure, LH engine failure, or PTU operating with EDP 2A or RH engine failure

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ACMP 3B AUTO Operation Triggers

Takeoff/approach phase or failure of ACMP 3A

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Power Transfer Unit (PTU) Triggers

Takeoff/approach phase, EDP 2A/RH engine failure, or ground single engine taxi (LH engine only and Parking Brake released)

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EDP HYD SOV Closure (Manual)

L(R) HYD SOV PBA or L(R) ENG FIRE PBA is pressed

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EDP HYD SOV Closure (Automatic)

Automatically closes when reservoir detects excessive fluid temperature of 125C125^{\circ}\text{C}

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ACMP 3B Electrical Power Source

AC BUS 1

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RAM Air Turbine (RAT) Hydraulic Target

Hydraulic System 3