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Flexjet EMB 545/550 > Limitations > Flashcards

Limitations Flashcards

1
Q

What is the Length of the 450/500/600

A

450: 64’07
500: 64’07
600: 68’05

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2
Q

What is the Width of the 450/500/600

A

450: 66’05”
500: 70’06”
600: 70’06

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3
Q

What is the Height of the 450/500/600

A

450/500/600:

21’03”

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4
Q

What is the min pavement width for the main gear to make a 180deg turn on each type

A

450: 52’06”
500: 52’05”
600: 56’

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5
Q

What is the wall to wall wingtip length for each type

A

450: 97’06”
500: 102”03
600: 104’06”

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6
Q

What kinds of operations is the aircraft authorized to conduct

A

1) VMC
2) IMC
3) Day
4) Night
5) Icing
6) Extended Overwater
7) Category 1

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7
Q

Max VMO/MMO?

A

1) Up to to 10,000’: 300KIAS
2) 10000 to 29,475: 320KIAS
3) MMO above 29,475: .83M

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8
Q

Minimum Mach Operating Speed

A

1) SAT from -57C to -60C: .40M
2) SAT from -60C to -65C: .55M
3) SAT from -65C to -70C: .67M

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9
Q

VA

A

1) Up to PA of 20,000 ft: 205 KIAS

2) Higher than 20,000 ft: See chart 2-10 in AOM

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10
Q

Turbulent Air Penetration Speed

A

1) If possible avoid severe turbulence.
2) At or below 10,000’: 230KIAS
3) Above 10,000’: lower of 265KIAS/.77M

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11
Q

Max Gear Operating Speeds?

A

VLO and VLE: 250KIAS

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12
Q

Max Flap Extended Speeds (Flexjet)

A

Flap 1 - 200 KIAS
Flap 2- 175 KIAS
Flap 3- 175 KIAS
Flap Full - 160 KIAS

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13
Q

Max Altitude for Flap Extension

A

20,000’

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14
Q

Max Tire Speed (GS)

A

182 KIAS

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15
Q

Max Demonstrated X-Wind for T/O

A

35 kts
For takeoff with X wind above 25kts, N1 is limited to 80% maximum with speeds below 40KIAS. D not stabilize N1 between 45% and 70% in crosswinds above 25kts.

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16
Q

Contaminated Runway X Wind Components

A

Contaminated: 20kts
Compacted Snow: 20kts
Wet Ice: 15kts.

When landing with a crosswind, brakes must be applied as soon as nose gear touches down

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17
Q

Min T/O and LDG altitude

A

-1000’

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18
Q

Max T/O and LDG Altitude

A

1) 9,600ft

2) With the HALTO SB - 13,800’

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19
Q

Max Tailwind Component

A

10 kts

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20
Q

Max Runway Slopes approved for T/O and LDG

A

+- 2%

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21
Q

Max Pressure Altitude

A

45,000 ft

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22
Q

Maximum Baggage Loading

A

1) FWD Cabinet: 88lbs
2) Stowage Compartment: 330lbs
3) Cargo Compartment: 880lbs

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23
Q

Steep Approaches

A

Not authorized

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24
Q

Category II Ops

A

Not Authorized

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25
Q

Maneuvering Load Factors

A

1) Flaps Up: +2.5 to -1 G
2) Flaps extended: +2.0 to 0.0G
3) Flaps 3 and Full above MLW: 1.5G limit

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26
Q

Cabin Interior Doors

A

Must be secured open for Taxi, takeoff and Landing

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27
Q

Praetor 500 and 600 Emergency Exit Considerations

A

The emergency exit is in the LAV so the LAV door on these aircraft must be secured open for all taxi, takeoff and landing ops.

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28
Q

Who cannot occupy Divan Seats

A

1) Pax under 15 years old
2) pax with shoulder height shorter than backrest height
3) Adult holding and infant (even with lap-held belt)

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29
Q

What do you do if a brake is applied during towing operations:

A

DON’T DO THIS, a detailed inspection for damage to the nose landing gear and affected regions shall be performed prior to the next flight.

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30
Q

TAWS considerations:

A

1) Navigation should not be predicated on the use of TAWS
2) must be inhibited when landing at an airport that is not included in the database
3) should be inhibited during QFE ops if GPS data is unavailable

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31
Q

TCAS II Considerations:

A

1) Deviation from ATC is authorized to the extent necessary to comply with and RA
2) Maneuvers must not be based solely on a TA or information on the traffic display.

32
Q

XM Weather

A

Should not be used a the primary source of weather data

33
Q

Total Fuel Capacity for each model

A

1) 450: 12,220 lbs
2) 500: 13,150 lbs
3) 600: 16,262 lbs

34
Q

Max Fuel Tank Temp

A

52 deg C

35
Q

Max PA to start APU in flight

A

31,000ft

36
Q

Min Temp to start APU in flight

A

-37C

37
Q

Max PA for APU operation (Electrical Power Limit)

A

31,000 ft

38
Q

Max PA for for APU operation (In-Flight Assisted Engine Start)

A

23,000 ft

39
Q

Max PA for APU operation (ECS)

A

20,000 ft

40
Q

Max APU Rotor Speed

A

106%

41
Q

Max APU EGT for Start

A

985C

42
Q

Max APU Continuous EGT

A

757C

43
Q

APU Unsuccessful Start Attempts

A

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

44
Q

Max ITT for Ground Start

A

650C

45
Q

Max ITT for Inflight Start with ITT is less than 250C and N2 is less than 18%

A

400C

46
Q

Max ITT for Inflight Start in all other start conditions

A

800C

47
Q

Max ITT and Time Limit with T/O power when OEI

A

1) Steady: 10 mins/ 955C

2) Transient: 2 mins / 970C

48
Q

Max ITT and Time limit with T/O power with AEO and WAI OFF

A

1) Steady: 5 mins/ 955C

2) Transient: 2 mins/ 970C

49
Q

Max ITT and Time limits with T/O power and WAI ON

A

1) Steady: 5 mins/ 955C

2) Transient: 2 mins/ 970C

50
Q

Max Continuous Steady ITT

A

950C

51
Q

Min Oil Temp

A

15C

52
Q

Max Oil Temp

A

138C

53
Q

What exceptions are there to the oil temp limits:

A

1) Temps between 5C and 15C allowed if TLs are not above Max Continuous Thrust
2) Temps between -40 and 5C allowed is TLs are not above ground idle.

54
Q

Max Accumulated Time and Cycles for Starting and Motoring

A

5 mins and 3 cycles

55
Q

Cool down time required prior to additional starting or motoring

A

15 mins after reaching 5 mins of accumulated time or 3 cycles whichever comes first.

56
Q

Starting Duty Max Cycle Time

A

80 secs

57
Q

Autobrake

A

Must be off for emergency and abnormal procedures.

58
Q

Max operating PA when anti-ice single bleed operation

A

20,000ft

59
Q

Max Differential Pressure 6000ft and 5800ft Cabin Alt

A

1) 9.64 PSID

2) 9.73 PSID

60
Q

Max Differential Overpressure

A

10.4 PSID

61
Q

Max Differential Negative Pressure

A

-0.5 PSID

62
Q

Max Differential Pressure for T/O and LDG

A

0.2 PSID

63
Q

Min Engagement Height for Autopilot

A

400ft

64
Q

Min use heights for Autopilot

A

1) With Vertical Path Reference: 80 ft

2) Without Vertical Path Reference: 180 ft.

65
Q

Landing with Autothrottle

A

1) Add 5KIAS to VREF

2) Multiply the associated flaps un-factored landing distance by 1.1

66
Q

Max Latitude for Stationary Alignment

A

78.25 (Northern and Southern Hemisphere)

67
Q

Min Altitude for use of on board MX system for use in flight

A

10,000 ft (troubleshooting not permitted in flight)

68
Q

Cargo Compartment Fire Protection

A

Either 78 or 110 mins (placard installed in Cargo Compartment)

69
Q

Min Equipment Required for ops in RVSM airspace

A

1) 2 RVSM Air Data Systems
2) 1 Autopilot with Alt. Hold Mode Operative
3) 1 Altitude Alerter
4) 1 Transponder

70
Q

Max T/O and LDG Altitude

A

13,800ft

71
Q

Min T/O and LDG Temp

A

-40C

72
Q

Max Temp for T/O

A

52C

73
Q

Max Demonstrated X-Wind for Landing on a dry runway

A

25 Kts

74
Q

Max Ramp Weight (Praetor 500)

A

37,699

75
Q

Max TO Weight (Praetor 500)

A

37,567

76
Q

Max Zero Fuel Weight (Praetor 500)

A

25,959

77
Q

Max Landing Weight (Praetor 500)

A

34,172

Flexjet EMB 545/550 (24 decks)

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