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Phenom 100 > Phenom 100 Limitations > Flashcards

Phenom 100 Limitations Flashcards

1
Q

Maximum Takeoff Weight

A

10472lbs

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2
Q

Maximum Ramp Weight

A

10516lbs

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3
Q

Maximum Landing Weight

A

9766lbs

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4
Q

Maximum Zero Fuel Weight

A

8444lbs

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5
Q

Max Nose Baggage Compartment Weight

A

66lbs

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6
Q

Max Wardrobe Compartment Weight

A

55lbs

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7
Q

Max Lavatory Compartment Weight

A

33lbs

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8
Q

Max Aft Baggage Compartment Weight

A

353lbs

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9
Q

Max No of occupants

A

9

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10
Q

Max No of passengers

A

7 including 1 lap child

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11
Q

Vmo

A

275KIAS

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12
Q

Mmo

A

0.70Mach

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13
Q

Vo(maneuvering)

A

186KIAS

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14
Q

Vlo

A

180KIAS

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15
Q

Vlo (Emergency)

A

250KIAS

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16
Q

Vle

A

275KIAS

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17
Q

Vf (1)

A

200KIAS

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18
Q

Vf (2) and (3)

A

160KIAS

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19
Q

Vf (full)

A

145KIAS

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20
Q

Max flap extension altitude

A

15000 Yaw Damper operative

12000 Yaw Damper inoperative

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21
Q

Vmca

A

97KIAS

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22
Q

Vmc landing

A

86KIAS

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23
Q

Vmc landing icing conditions

A

97KIAS

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24
Q

Max Tail Wind

A

10 Knots

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25
Q

Max demostrated crosswind

A

17 knots not limiting

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26
Q

Max Tyre Speed

A

139 KIAS

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27
Q

Minimum oxygen pressure for dispatch

A

730 PSI(but consult chart in AFM for min based on no of pax for charter or rpt ops)

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28
Q

Oxy masks extend in PAX AUTO at

A

14500 +250 -500 feet

29
Q

Maximum runway slope

A

+/-2%

30
Q

Electrical system operating voltage

A

28VDC

31
Q

Battery voltage

A

24VDC

32
Q

Min battery voltage for start

A

24VDC

33
Q

GPU voltage range

A

26-29VDC

34
Q

Min GPU voltage to charge batteries

A

27VDC

35
Q

Max Generator load

A

250 AMPS but 300 AMPS permissible below FL340 in flight

36
Q

Start/Generator disengage/engage speed

A

44% N2

37
Q

ELT Battery replacement time

A

6 years or as required by the regulating authority

38
Q

Total fuel capacity

A

2850lbs

39
Q

Useable Fuel per tank

A

1403lbs

40
Q

Unuseable Fuel per tank

A

22lbs

41
Q

Max Fuel Imbalance

A

220lbs

42
Q

Min Fuel Temperature

A

-37 Deg C

43
Q

Max Fuel Temperature (Ground)

A

52 Deg C

44
Q

Max Fuel Temperature (Flight)

A

80 Deg C

45
Q

Max load limits

A

Flaps Up plus 3.27G Flaps Down plus 2G

46
Q

Yaw Damper must be on

A

Above 25000 feet or above 250 KIAS

47
Q

Static Wicks required for dispatch

A

12 (3 per aileron 2 on rudder and 2 per elevator)

48
Q

Maximum Differential Pressure

A

8.3PSI

49
Q

Maximum Negative Differential Pressure

A

-0.4PSI

50
Q

Maximum Differential Overpressure

A

8.6PSI

51
Q

Maximum Diff Press TO and LDG

A

0.2PSI

52
Q

Starter Cycle Limits

A

60 Seconds Off
60 Seconds Off
15 Minutes Off
30 Minutes Off

53
Q

Max ITT(SE)

A

845 Deg C

54
Q

Max ITT TO/GA

A

830 Deg C

55
Q

Max ITT Cont Climb

A

830 Deg C

56
Q

Max ITT start

A

830 Deg C(892 for 5 seconds)

57
Q

Max ITT Transient

A

830 Deg C
862 Deg C for 20 Seconds Normal and ATR mode
845 Deg C for ATR mode only

58
Q

Max Thrust

A

Not intended for normal operations

59
Q

Cold Start Idle Time

A

Idle Thrust for 3 minutes after oil reaches 14 Deg C

60
Q

Engine Anti Ice

A

SAT/TAT plus 5 to 10 Deg C EAI must be on
SAT/TAT below 5 Deg C Windshield.Engine and Wing anti ice must all be on
Ice Formation (despite Temperature )
Windshield, Engine and Wing anti ice must all be on

61
Q

Min Temperature to Operate Wing and Stabiliser Boots

A

-40 Deg C

62
Q

Min Speed in Icing Conditions

A

150KIAS

63
Q

Min Altitude to engage Auto Pilot (2 engines)

A

500 feet AGL

64
Q

Min Altitude to engage Auto Pilit (1 engine)

A

1000 feet AGL

65
Q

Min Auto Pilot altitude use (on approach)

A

195 feet AGL

66
Q

Max Allowable Auto Pilot Altitude Loss

A

54 feet

67
Q

Auto Pilot Use prohibited if

A
  1. Severe Icing Conditions
  2. Unusual Control force or deflection or unusually large control forces required to move flight controls
  3. Indications of frequent autopilot retrimming during straight and level flight
68
Q

Vra Turbulence Penetration (Not a Limitation)

A

230 kts at or below 28000’
230/0.59M above 28000’
SIGNS/OUTLET Switch……PED-BELTS/OFF

Phenom 100 (2 decks)

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