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Limitations > Praetor 500 > Flashcards

Praetor 500 Flashcards

1
Q

Maximum aircraft weights

A

MAX Ramp Weight (MRW) … 37,699
MAX Takeoff Weight (MTOW) … 37,567 (42,858 - 600)
MAX Landing Weight (MLW) … 34,172
MAX Zero Fuel Weight (MZFW) … 25,959

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2
Q

MAXIMUM FLAP EXTENDED SPEEDS (VFE)

A

Flap 1…………………210 KIAS ………. 200 KIAS
Flap 2…………………185 KIAS ………. 175 KIAS
Flap 3…………………185 KIAS……….. 175 KIAS
Flap FULL……………170 KIAS……..… 160 KIAS

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3
Q

MAXIMUM ALTITUDE FOR FLAP EXTENDED

A

20,000 ft

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4
Q

LANDING GEAR OPERATION/EXTENDED SPEED (Vlo AND Vle)

A

Vlo … 250 kias
Vle … 250 kias

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5
Q

MAXIMUM TIRE GROUND SPEED

A

182 kias

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6
Q

Maximum Takeoff and Landing Tailwind Component

A

10 kts

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7
Q

MAXIMUM CROSSWIND LIMITATIONS
CONTAMINATED RUNWAY

A

Contaminated …….. 20 kts
Compacted snow … 20 kts
Wet ice ………………… 15 kts

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8
Q

MINIMUM CREW

A

2 pilots

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9
Q

BAGGAGE LOADING

A

Forward Cabinet…………………………………. 88 lb
Stowage Compartment………………………… 330 lb
Cargo Compartment……………………………. 880 lb

Floor loading … 75 lb/ft²

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10
Q

POSITIVE/NEGATIVE MANEUVERING FLIGHT LOAD FACTORS

A

Flaps up ….….. 2.5 g / -1.0 g
Flaps down …. 2.0 g / 0.0 g

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11
Q

RUNWAY SLOPE/SURFACE

A

Slope ……… -2.0% to +2.0%
Surface ….. Paved

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12
Q

KINDS OF OPERATION

A

IFR
VFR
Icing Conditions
Extended Overwater
CAT 1

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13
Q

CABIN INTERIOR DOORS

A

During taxi, takeoff and landing, cabin interior doors must be secured in the open position.

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14
Q

DIVAN SEATS

A

During taxi, takeoff and landing, the divan cannot be occupied by persons with the following characteristics:
– Under 15 years old;
– With shoulder height shorter than backrest height;
– Holding an infant, even with lap-held belt.

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15
Q

COCKPIT POCKET DOOR

A

If the door becomes jammed, push it or kick it until it breaks free.

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16
Q

TOWING

A

Towbarless towing is prohibited, unless it is conducted in accordance with the procedures presented in the AMM.

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17
Q

PILOT TABLE

A

During taxi, takeoff and landing, the pilots foldable tables must be stowed.

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18
Q

TERRAIN AWARENESS AND WARNING SYSTEM (TAWS)

A

– Navigation must not be predicated upon the use of the TAWS.
– To avoid giving unwanted alerts, the TAWS must be inhibited when
landing at an airport that is not included in the airport database.
– The use of TAWS functions should be manually inhibited during
QFE operations if GPS data is unavailable or inoperative.

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19
Q

TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) II
MANEUVERING LIMITATIONS

A

– Maneuver as necessary to comply with a Resolution Advisory (RA).
– Do not maneuver for a Traffic Advisory (TA) or on information presented in the traffic display.

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20
Q

SATELLITE WEATHER RADIO SYSTEM (XM
WEATHER)

A

The XM Weather should not be used as a primary source of weather data.

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21
Q

FUEL SPECIFICATION

A

JET A (-40°C) and JET A1(-47°C)

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22
Q

MAX FUEL TANK TEMPERATURE FOR TAKEOFF

A

52°C (125.6°F)

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23
Q

CROSSFEED OPERATION

A

The FUEL XFEED Knob must be set to OFF during takeoff, go-around, and landing.

24
Q

APU UNSUCCESSFUL START ATTEMPTS
With time between attempts

A

Up to 3 consecutive unsuccessful start attempts are allowed, with 30 second intervals between attempts.

25
Q

TAKEOFF / GO AROUND THRUST TIME LIMITED

A

Maximum TO/GA thrust for (AEO)……………… 5 minutes
Maximum TO/GA thrust for (OEI)………………. 10 minutes

26
Q

ENGINE OIL TEMPERATURE LIMIT

A

MIN ….. 15° C
MAX …. 138° C

– between 5°C and 15°C no thrust above maximum continuous
– between -40°C and 5°C no thrust above ground idle

27
Q

ENGINE OIL PRESSURE LIMIT

A

– ENG 1 (2) OIL LO PRESS CAS message together with red EICAS
oil pressure indication is displayed whenever engine oil pressure is
below the limits while engine running.
– ENG 1 (2) EXCEEDANCE CAS message together with red EICAS
oil pressure indication is displayed whenever engine oil pressure is
above the limits while engine running.

28
Q

Maximum Crosswind Component for Takeoff

A

35 kts

For takeoff with crosswind components above 25 kt, the N1 is limited to 80% maximum with speeds below 40 KIAS. Do not stabilize N1 between 45% and 70% in crosswinds above 25 kt.

29
Q

STARTING AND MOTORING LIMITS

A

Max Accumulated Time - 5 min
Max Consecutive Cycles - 3
15 minutes of cool down after whichever occurs first

30
Q

Starting Duty Maximum Time

A

80 Seconds

31
Q

THRUST REVERSER

A

Backing the airplane with reverse thrust is prohibited.
Upon landing, thrust reversers should be stowed at 40 KIAS.

32
Q

PRESSURIZATION

A

Maximum Differential Pressure (6000 ft cabin altitude)…… 9.64 psid
Maximum Differential Pressure (5800 ft cabin altitude)…… 9.73 psid
Maximum Differential Overpressure……………………………….. 10.4 psid
Maximum Differential Negative Pressure…………………………. -0.5 psid
Maximum Differential Pressure for Takeoff and Landing….. 0.2 psid

33
Q

AUTOBRAKE

A

AUTOBRAKE must be set to OFF for emergency and abnormal procedures.

34
Q

ANTI-ICING FOR TAKEOFF

A

• If OAT is greater than 10° C, Ice protect Knob set to AUTO.
• If visible moisture is present and OAT is less than 10° C but greater than 5° C Ice protect Knob set to ENG.
• If visible moisture is present and OAT is less than 5° C Ice protect Knob set to ALL.

35
Q

Maximum Operating Altitude for Anti-ice w/ Single Bleed

A

20,000 ft

36
Q

AUTOPILOT MIN ENGAGE HEIGHTS

A

Minimum Engagement Height………………. 400 ft
Minimum Use Height:
With Vertical Path Reference……..…….. 80 ft
Without Vertical Path Reference………. 180 ft

37
Q

AUTOTHROTTLE
Planning Adjustments

A

When planning to land with autothrottle engaged:
– Add 5 KIAS to VREF;
– Multiply the associated flaps unfactored landing distance by 1.1

38
Q

MIN ALTITUDE FOR USE OF ONBOARD MAINTENANCE SYSTEM

A

Minimum Altitude for Use In-Flight ……….. 10000 ft AGL
NOTE: Troubleshooting is not permitted in-flight.

39
Q

Cargo compartment fire extinguishing bottles agent duration

A

Either 78 or 110 minutes

40
Q

OPERATIONAL ENVELOPE
FOR T.O. & LANDING

A

Min T.O. & Landing Temperature….. -40°C

Min T.O. & Landing Altitude ………… -1,000 ft
Max T.O. & Landing Altitude ……….. 9,600 ft
With HALTO
Max T.O. & Landing Altitude………….. 13800 ft

41
Q

OPERATIONAL ENVELOPE
FOR SPEED/ALT

A

Vmo up to 10,000 ft ……….. 300 kias
Vmo 10,000 to 29,475 ft …. 320 kias
MMO Above 29,475 ft …….. 0.83 mach
MAX ALT …………………..…….. 45,000 ft

42
Q

TURBULENT AIR PENETRATION SPEEDS

A

At or below 10,000 ft ……….. 230 kias
Above 10,000 ft ……………….. 265 kias / 0.77 M

43
Q

MAX ITT LIMITS °C

A

Engine start …………… 650° C
Max continuous …….. 950° C
Takeoff power
Steady ………….. 955° C
Transient ……… 970° C

44
Q

DRY MOTORING

A

Required when starting within 15 to 180 minutes from engine shutdown.

Engines should be motored one at a time until N2 reaches between 19 to 23 percent, or 15 seconds, whichever occurs first.

ENGINE START SEQUENCE CAN BE INITIATED ANY TIME AFTER 3 MINUTES AND BEFORE 40 MINUTES HAVE ELAPSED.

45
Q

Is single-engine taxi authorized?

A

No

46
Q

APU INFLIGHT LIMITATIONS

A

Max start alt ………….. 31,000 ft
Min start temp ………. -37° C
Max elec usage ……… 31,000 ft
Max eng start assist . 23,000 ft
Max pneumatic ……… 20,000 ft

47
Q

APU ROTOR SPEED AND TEMP LIMITS

A

Rotor spd ….. 106%
Start ………….. 985° C
Continuous .. 757°C

48
Q

ENGINE START WITH ITT ABOVE 450° C?

A

Motor engine for 30 seconds prior to start.

49
Q

MIN BATTERY VOLTAGE FOR ENGINE START?

A

23 V DC

50
Q

MINIMUM GPU VOLTAGE FOR BATTERY CHARGING

A

28 V DC

51
Q

MAXIMUM USABLE FUEL PER TANK

A

Left and right wing - 6,526 lbs
Total - 13,052 lbs

52
Q

UNUSABLE FUEL PER TANK

A

Left and right tank - 7 gal (45 lbs)
Total - 14 gal (90 lbs)

53
Q

MAXIMUM FUEL CAPACITY

A

Left and right - 981 gal (6,573 lbs)
Total - 1,962 gal (13,142 lbs)

54
Q

MAX IMBALANCE BETWEEN TANKS

A

510 lbs

55
Q

At what cabin altitude will PAX O2 automatically deploy?

A

14,500 +/- 300 feet

56
Q

RAT min speed for operation?

A

140 kts

Limitations (1 decks)

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