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limits. Digits will appear in inverse video.
BATTERY CURRENT INDICATOR
Digital Readout . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Red. . . . . . . . . . . . . . . . . . . . . 500 to 995 amps
Amber. . . . . . . . . . . . . . . . . . . 300 to 495 amps
Green . . . . . . . . . . . . . . . . . . .-995 to 295 amps
NOTE
The pointer and digital readout will turn red or amber if outside normal operating
limits. Digits will appear in inverse video.
(Continued Next Page)
2-26 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
EICAS AND INSTRUMENT MARKINGS (Continued)
CABIN PRESSURIZATION INSTRUMENTATION
CABIN ALTITUDE
Pointer / Digital Readout
Scale Marking (Normal Mode) . . . . . . . . . . . . . . . . .Red Band . . . . . . . . . . . . . . . . . . . >10,000 Feet
Amber Band . . . . . . . . . . . 8500 to 10,000 Feet
Green Band . . . . . . . . . . . . . . . . . . <8500 Feet
Pointer / Digital Readout
Scale Marking (High Altitude Mode) . . . . . . . . . . . . .Red Band . . . . . . . . . . . . . . . . . . . >14,600 Feet
Amber Band . . . . . . . . . . 14,000 to 14,600 Feet
Green Band . . . . . . . . . . . . . . . . . <14,000 Feet
Pointer / Scale Marking (Ground) . . . . . . . . . . . . . . .Green Band . . . . . . . . . . . . . . . . . Entire Range
NOTE
• The pointer and digital readout will turn red or amber if outside normal operating
limits. Digits will appear in inverse video.
• The pressurization system will be in high altitude mode if takeoff or destination
elevation is greater than 8000 feet and airplane is below 24,500 feet.
• Cabin altitude may not be displayed when the airplane is on the ground.
CABIN ALTITUDE RATE
Scale Markings . . . . . . . . . . . . . . . . . . . . . . . . . . . . .White . . . . . . . . . . . . . . . . . . . . . . Entire Range
Digital Readout . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Green . . . . . . . . . . . . . . . . . . . . . . Entire Range
CABIN DIFFERENTIAL PRESSURE
Pointer / Digital Readout
Scale Markings . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Red Band . . . . . . . . . . . . . . . . . . 8.6 TO 10 PSI
Green Band . . . . . . . . . . . . . . . . . . . . <8.5 PSI
NOTE
The pointer and digital readout will turn red or amber if outside normal operating
limits. Digits will appear in inverse video.
OTHER INSTRUMENTS
Standby Airspeed Indicator . . . . . . . . . . . . . . . . . . . .Red Line . . . . . . . . . . . . . 250 KIAS (0.63 Mach)
Hydraulic Accumulator Pressure Indicator . . . . . . . . . . . . . . . Per Placard According to Temperature
Emergency Brake Pneumatic Pressure Indicator . . . . . . . . . . Per Placard According to Temperature
Emergency Gear Pneumatic Pressure Indicator. . . . . . . . . . . Per Placard According to Temperature
Fire Bottle Pressure Indicator . . . . . . . . . . . . . . . . . . . . . . . . . Per Placard According to Temperature
Oxygen Pressure Indicator . . . . . . . . . . . . . . . . . . . .Red Line . . . . . . . . . . . . . . . . . . . . . . . 2000 PSI
Amber Arc . . . . . . . . . . . . . . . . . . .0 to 400 PSI
510FM-07 AA 2-27
SECTION II - OPERATING LIMITATIONS MODEL 510
FAA APPROVED
U.S. Configuration
SUPPLEMENTAL OXYGEN SYSTEM
Service the oxygen system with Aviator’s Breathing Oxygen (MIL-O-27210). The use of medical
oxygen is prohibited.
For single-pilot operations, a crew oxygen mask must be available for a passenger occupying the
right crew seat. The mask must be checked during preflight and passenger briefed on its use.
The following aircraft certification requirements are in addition to the requirements of applicable
operating rules. The most restrictive requirements (certification or operating) must be observed:
1. Crew and passenger oxygen masks are not approved for use above 40,000 feet cabin
altitude. Prolonged use of passenger masks above 25,000 feet cabin altitude is not
approved.
2. The pressure-demand crew oxygen masks must be properly stowed in their containers to
qualify as a quick-donning oxygen mask.
WARNING
• Some large eyeglasses, headsets, hats and hairstyles may interfere
with the quick-donning capability of the mask. It is the crew member’s
responsibility to ensure the mask can be donned quickly.
• Passenger masks are intended for use during an emergency descent
to an altitude not requiring supplemental oxygen.
STALL WARNING AND LOW SPEED AWARENESS SYSTEMS
The low speed awareness system can be used as a reference for approach speed (VREF) at all
airplane weights, CG locations, anti-ice/deice system settings and flap positions. VREF is indicated
　
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