Praetor 500

Question 1

Maximum aircraft weights

Answer 1

MAX Ramp Weight (MRW) … 37,699
MAX Takeoff Weight (MTOW) … 37,567 (42,858 - 600)
MAX Landing Weight (MLW) … 34,172 (37,479 - 600)
MAX Zero Fuel Weight (MZFW) … 25,959

Question 2

MAXIMUM FLAP EXTENDED SPEEDS (VFE)

Answer 2

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

Question 3

MAXIMUM ALTITUDE FOR FLAP EXTENDED

Answer 3

20,000 ft

Question 4

LANDING GEAR OPERATION/EXTENDED SPEED (Vlo AND Vle)

Answer 4

Vlo … 250 kias
Vle … 250 kias

Question 5

MAXIMUM TIRE GROUND SPEED

Answer 5

182 kias

Question 6

Maximum Takeoff and Landing Tailwind Component

Answer 6

10 kts

Question 7

MAXIMUM CROSSWIND LIMITATIONS
CONTAMINATED RUNWAY

Answer 7

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

Question 8

MINIMUM CREW

Answer 8

2 pilots

Question 9

BAGGAGE LOADING

Answer 9

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

Floor loading … 75 lb/ft²

Question 10

POSITIVE/NEGATIVE MANEUVERING FLIGHT LOAD FACTORS

Answer 10

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

Question 11

RUNWAY SLOPE/SURFACE

Answer 11

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

Question 12

KINDS OF OPERATION

Answer 12

IFR
VFR
Icing Conditions
Extended Overwater
CAT 1

Question 13

CABIN INTERIOR DOORS

Answer 13

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

Question 14

DIVAN SEATS

Answer 14

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.

Question 15

COCKPIT POCKET DOOR

Answer 15

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

Question 16

TOWING

Answer 16

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

Question 17

PILOT TABLE

Answer 17

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

Question 18

TERRAIN AWARENESS AND WARNING SYSTEM (TAWS)

Answer 18

– 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.

Question 19

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

Answer 19

– 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.

Question 20

SATELLITE WEATHER RADIO SYSTEM (XM
WEATHER)

Answer 20

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

Question 21

FUEL SPECIFICATION

Answer 21

JET A (-40°C) and JET A1(-47°C)

Question 22

MAX FUEL TANK TEMPERATURE FOR TAKEOFF

Answer 22

52°C (125.6°F)

Question 23

CROSSFEED OPERATION

Answer 23

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

Question 24

APU UNSUCCESSFUL START ATTEMPTS
With time between attempts

Answer 24

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

Question 25

TAKEOFF / GO AROUND THRUST TIME LIMITED

Answer 25

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

Question 26

ENGINE OIL TEMPERATURE LIMIT

Answer 26

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

Question 27

ENGINE OIL PRESSURE LIMIT

Answer 27

– 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.

Question 28

Maximum Crosswind Component for Takeoff

Answer 28

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.

Question 29

STARTING AND MOTORING LIMITS

Answer 29

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

Question 30

Starting Duty Maximum Time

Answer 30

80 Seconds

Question 31

THRUST REVERSER

Answer 31

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

Question 32

PRESSURIZATION

Answer 32

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

Question 33

AUTOBRAKE

Answer 33

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

Question 34

ANTI-ICING FOR TAKEOFF

Answer 34

• 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.

Question 35

Maximum Operating Altitude for Anti-ice w/ Single Bleed

Answer 35

20,000 ft

Question 36

AUTOPILOT MIN ENGAGE HEIGHTS

Answer 36

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

Question 37

AUTOTHROTTLE Planning Adjustments

Answer 37

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

Question 38

MIN ALTITUDE FOR USE OF ONBOARD MAINTENANCE SYSTEM

Answer 38

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

Question 39

Cargo compartment fire extinguishing bottles agent duration

Answer 39

Either 78 or 110 minutes

Question 40

OPERATIONAL ENVELOPE FOR T.O. & LANDING

Answer 40

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

Question 41

OPERATIONAL ENVELOPE FOR SPEED/ALT

Answer 41

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

Question 42

TURBULENT AIR PENETRATION SPEEDS

Answer 42

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

Question 43

MAX ITT LIMITS °C

Answer 43

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

Question 44

DRY MOTORING

Answer 44

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.

Question 45

Is single-engine taxi authorized?

Answer 45

No

Question 46

APU INFLIGHT LIMITATIONS

Answer 46

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

Question 47

APU ROTOR SPEED AND TEMP LIMITS

Answer 47

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

Question 48

ENGINE START WITH ITT ABOVE 450° C?

Answer 48

Motor engine for 30 seconds prior to start.

Question 49

MIN BATTERY VOLTAGE FOR ENGINE START?

Answer 49

23 V DC

Question 50

MINIMUM GPU VOLTAGE FOR BATTERY CHARGING

Answer 50

28 V DC

Question 51

MAXIMUM USABLE FUEL PER TANK

Answer 51

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

Question 52

UNUSABLE FUEL PER TANK

Answer 52

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

Question 53

MAXIMUM FUEL CAPACITY

Answer 53

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

Question 54

MAX IMBALANCE BETWEEN TANKS

Answer 54

510 lbs

Question 55

At what cabin altitude will PAX O2 automatically deploy?

Answer 55

14,500 +/- 300 feet

Question 56

RAT min speed for operation?

Answer 56

140 kts