Term
| The EA500 is approved for the following types of operations when the appropriate instruments and equipment are installed? |
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Definition
- VFR Day
- VFR Night
- IFR
- Reduced Vertical Separation Minimum (RVSM)
- Icing (according to Icing Conditions in AFM)
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Term
For aircraft not certified for flight in icing, flight into icing conditions is
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Definition
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Term
| ENGINE Anti-ice must be selected ON for all ground and flight operations when the outside air temperature is |
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Definition
10o C or colder when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush is present. |
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Term
| When operating the engines at IDLE on the ground in freezing fog and visible moisture, the engine speed must |
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Definition
Be increased once every 5 minutes to 65% N1 to avoid ice on the spinner |
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Term
| The following equipment must be operational for RVSM operations |
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Definition
- Autopilot
- Altitude Alerting System
- Altitude Reporting - Transponder 1
- Air Data Systems - ADC 1 and ADC 2
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Term
| RVSM Flight envelope is limited from Mach _____ to Mach _____ in level flight |
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Definition
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Term
| Minimum Fight Crew of One provided the following; |
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Definition
- Pilot occupies left seat
- Autopilot is operative
- Use of Headset mounted microphone
- Ident button on sidestick works
- QRH is available to pilot
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Term
| If operations require two pilots, the following must be installed; |
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Definition
| Quick-don Oxygen Masks with built-in microphones for both pilot and copilot |
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Term
| All pilots operating the Eclipse 500 must be trained and qualified in accordance with |
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Definition
| The FAA Accepted/Approved Eclipse Aerospace Training program or equivalent FAA Accepted/Approved program |
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Term
| Maximum Occupant Seating is |
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Definition
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Term
| Seat belts and shoulder harnesses must be worn by all occupants during |
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Definition
| Taxiing, Takeoff, and Landing |
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Term
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Definition
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Term
| Maximum Certified Takeoff Weight is |
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Definition
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Term
| Takeoff weight is limited by the most restrictive of the following; |
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Definition
- Maximum Certified Takeoff Weight
- Maximum Weight Permitted by Climb
- Takeoff Distance
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Term
| Maximum Certified Landing Weight is |
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Definition
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Term
| Landing weight is limited by the most restrictive of the following; |
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Definition
- Maximum Certified Landing Weight
- Landing Distance
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Term
| Maximum Zero Fuel Weight is |
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Definition
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Term
| Maximum Weight in baggage area is |
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Definition
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Term
| It is the responsibility of the ________ to ensure the aircraft is loaded properly and within the Center of Gravity Limitations Envelope |
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Definition
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Term
| Maxium Operating Airspeed (Vmo) is |
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Definition
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Term
| Maximum Operating Mach (Mmo) is |
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Definition
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Term
| Operating Manuevering Speed (Vo) is |
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Definition
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Term
| Maximum Operating Altitude is |
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Definition
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Term
| Maximum Takeoff and Landing Altitude is |
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Definition
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Term
| Aerobatic Manuevers including spins are |
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Definition
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Term
| Maximum positive G-load with flaps UP is |
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Definition
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Term
| Maximum positive G-load with flaps T/O is |
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Definition
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Term
| Maximum negative G-load with flaps UP is |
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Definition
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Term
| Maximum negative G-load with flaps T/O is |
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Definition
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Term
| Type of Runway surfaces for takeoffs and landings are limited to |
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Definition
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Term
| Maximum Engine ITT for starting is |
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Definition
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Term
| Maximum Engine ITT for Takeoff, APR, and MCT is |
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Definition
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Term
| Maximum %N2 for Takeoff, APR, and MCT is |
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Definition
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Term
| Maximum %N1 for Takeoff, APR, and MCT is |
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Definition
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Term
| Maximum time limit for engine opertaion in Takeoff is |
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Definition
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Term
| Maximum time limit for engine operation in APR is |
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Definition
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Term
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Definition
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Term
| Fuel System Icing Inhibitors (i.e. Prist) are ____________ for all operations |
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Definition
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Term
| Normal Engine oil pressure range for ground, flight, takeoff, APR, and MCT is |
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Definition
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Term
| Time limit for Negative 'G' is limited to |
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Definition
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Term
| A list of Approved Oil grades can be found in |
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Definition
AFM Section 2 - Limitations |
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Term
| Maximum Total Engine Oil capacity is |
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Definition
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Term
| An oil quantity check is required prior to |
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Definition
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Term
| Engine starts are not permitted at an oil temperature below |
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Definition
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Term
| Engine starts at oil temperatures between ____ and ____ must be accomplished with a GPU |
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Definition
| -20 degrees C and +5 degrees C |
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Term
| Minimum battery voltage for engine starts is |
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Definition
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Term
| The engine starter is limited to the following operating cycles and cool down periods; |
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Definition
| Three 30 second starts with a 60 second spool-down/ cool-down period in between followed by a 30 minute spool-down and cool-down period |
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Term
| Maximum crosswind limit for engine operations on the ground is |
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Definition
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Term
| Maximum tailwind limit for engine operations on the ground is |
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Definition
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Term
| Maximum tailwind limit for engine operations on the ground with N1 above 75% is |
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Definition
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Term
| Following the loss of both ADC 1 and 2, the use of ADC 3 as sole reference for airspeed and altitude is limited to |
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Definition
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Term
| Due to the AHRS system limitations, operation in charted areas requiring reference to true North is |
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Definition
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Term
| Minimum altitude for autopilot use during climb, enroute, or descent is |
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Definition
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Term
| Minimum altitude for autopilot use during approach is |
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Definition
| 150 ft AGL (Precision), 250 ft AGL (Non-Precision) |
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Term
| The Air Conditioner must be operating if the avionics are ON on the ground for more than 30 minutes and the cockpit temperature is more than |
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Definition
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Term
| Headsets must be used by the flight crew after |
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Definition
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Term
| The Passenger Address (PA) system is |
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Definition
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Term
| The stall protection system and stick pusher must be successfully tested prior to |
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Definition
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Term
| Maximum Airspeed with Yaw Damper OFF is |
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Definition
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Term
| Maximum Altitude with Yaw Damper OFF is |
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Definition
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Term
| For not installed equipment, the corresponding ECB (if one exists) must be |
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Definition
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Term
| Maximum Cabin pressure differential (dP) is |
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Definition
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Term
| Landing with the cabin pressurized is |
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Definition
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Term
| Flight is not permitted if the aircraft batteries are stored at temperatures colder than |
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Definition
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Term
| During ground-idle operations with the VCS operating, the __________ may indicate a discharge. |
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Definition
Start Battery
Increasing Right Engine N2 speed between 52%-54% will ensure 60 minutes of battery power |
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Term
| The generator amperage limitation for gound operations is |
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Definition
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Term
| The generator amperage limitation for flight up to 35,000 ft is |
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Definition
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Term
| The generator amperage limitation for flight above 35,000 ft is |
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Definition
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Term
| Maximum flap extension speed (Vfe) for flaps T/O is |
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Definition
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Term
| Maximum flap extension speed (Vfe) for flaps LDG is |
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Definition
(Aircraft 001-265 not modified by SB 500-99-004)
120 KEAS
(Aircraft 266 & above, or 001-265 with SB 500-99-004)
140 KEAS
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Term
| Maximum altitude for flap operation is |
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Definition
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Term
| Total fuel capacity (Usuable plus Unusuable) is |
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Definition
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Term
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Definition
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Term
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Definition
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Term
| Maximum fuel imbalance for takeoff, landing and flight is |
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Definition
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Term
| Maximum fuel sump temperature for takeoff is |
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Definition
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Term
| The use of the wing deice (boots) is |
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Definition
Prohibited for aircraft not modified by SB 500-99-004
(All 4 wing deice ECBs must be collared) |
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Term
| The use of Windshield Heat is |
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Definition
Prohibited for aircraft not modified by SB 500-99-004
(Both Windshield Heat ECBs must be collared) |
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Term
| Maximum airspeed in order to lower the gear (Vlo) is |
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Definition
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Term
| Maximum airspeed with the gear down and locked (Vle) is |
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Definition
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Term
| Maximum altitude for gear operation is |
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Definition
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Term
| Landing gear actuation shall be limited to _____ cycles in _____ minutes |
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Definition
| 3 cycles within 10 minutes |
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Term
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Definition
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Term
| For aircraft modified by Service Bulletin 500-99-004 the use of Windshield heat high (HI) mode during takeoff or landing is |
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Definition
Prohibited
(It's use is limited to clearing ice accretion only)
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