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Phenom > Phenom Limits & SOPs 5.0 Inc > Flashcards

Phenom Limits & SOPs 5.0 Inc Flashcards

1
Q

Max Operating Altitude

A

41,000 PA

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2
Q

Max Landing Gear Operation V LO

A

180 KIAS
(250 KIAS Emergency)

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3
Q

Max Landing Gear Extended V LE

A

275 KIAS

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4
Q

Min Control Speed - T/O
V MC

A

97 KIAS

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5
Q

Min Control speed - landing
V MC

A

86 KIAS
(97 KIAS Icing)

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6
Q

Max Operating Speed
V MO / M MO
Up to 28,000ft

A

275 KIAS - 0.70M

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7
Q

Max Operating Manoeuvring Speed
Vo

A

186KIAS

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8
Q

Max flap extend Speed
V FE
(1-4)

A

Flap 1 - 200 KIAS
Flap 2 - 160 KIAS
Flap 3 - 160 KIAS
Flap 4 - 145 KIAS

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9
Q

Max Alt Flap Extend

A

YD Operating: 15,000 ft
YD Inoperative: 12,000 ft

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10
Q

Max Tyre Ground Speed

A

139 Kts

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11
Q

Max time @ max thrust

A

10 mins

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12
Q

Max time @ TOGA

A

5 minutes

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13
Q

MAX ITT

A

Max thrust: 845°C
TOGA/CONTCLMB: 830°C

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14
Q

MAX N2 (%)

A

100.4 %

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15
Q

MAX ITT Start

A

830°C
830 - 950°C for 5 seconds

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16
Q

Minimum oil temp for engine start

A

-40°C

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17
Q

Normal Oil Temp range

A

14 - 130°C

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18
Q

Max Oil Pressure

A

170 PSI
170 - 250 PSI allowed up to 500 seconds

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19
Q

Start motor attempts vs cool down (1-4)

A

Attmpt 1: 1 min cool dwn
Attmpt 2: 1 min cool dwn
Attmpt 3: 15 min cool dwn
Attmpt 4: 30 min cool dwn

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20
Q

Min BAT VOLT for eng start

A

24 V

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21
Q

Min GPU V to charge the BATS

A

27 V

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22
Q

Max GEN load on ground

A

250 A each

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23
Q

Max GEN load in flight above 34,000’

A

250 A each

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24
Q

Max GEN load in flight below 34,000’

A

300 A each

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25
Q

Max fuel capacity

A

1292.8 Kg

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26
Q

Total unusable fuel

A

20 Kg

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27
Q

Max imbalance between tank

A

100 Kg

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28
Q

Min Fuel Tank Temp

A

– 37°C

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29
Q

Max Fuel Tank Temp (flight)

A

+ 80°C

30
Q

Max Fuel Tank Temp (ground)

A

+ 52°C

31
Q

Max Diff. Pressure

A

8.3 PSI

32
Q

Max Diff. Overpressure

A

8.6 PSI

33
Q

Max Diff. Neg Pressure

A
  • 0.4
34
Q

Max Diff. Pressure (TO/Landing)

A

0.2

35
Q

Max TO/Landing Tailwind Component

A

10 Kts

36
Q

Max x-wind component TO/Landing (inc. gusts)

A

25 Kts

37
Q

Air conditioning system operation on the ground requires 1 of either 2 criteria to be met:

A

1) GPU must be used
or
2) Both Generators operating

38
Q

YD to be engaged above __,___ ft and/or above ___ Kts

A

Above 25,000ft and/or 250 Kts

39
Q

Autopilot / YD min engagement height (duel eng)

A

500 ft AGL

40
Q

Autopilot / YD min engagement height (OEI)

A

1000 ft AGL

41
Q

Autopilot / YD min use height

A

195 ft AGL

42
Q

Autopilot / YD Altitude Loss

A

54 ft

43
Q

Spin??

A

nah lol

44
Q

Max AoB

A

60°

45
Q

Manoeuvring at AoAs near the stall, or full application of rudder, elevator and aileron is not to occcur above __ speed.

A

Vo = 186 KIAS

46
Q

G-force limitations with flaps up

A

-1.2 to +3.27 g

47
Q

G-force limitations with flaps Extended

A

0 to +2.00 g

48
Q

Runway Slope range

A

-2% to +2%

49
Q

Permissible runway surfaces

A

Paved

50
Q

Permissible runway conditions (3)

A

Dry / Wet / Contaminated

51
Q

Can we trample arrestor cables?

A

Nah

52
Q

Instrument approach category?

A

B

53
Q

Min temp for WINGSTAB operation:

A

– 40°C

54
Q

Min airspeed for WINGSTAB swith activation (Flap 0 and Gear up)

A

150 KIAS

55
Q

Min airspeed for Holding (Flap 0 and Gear up)

A

160 KIAS

56
Q

Following an aborted TO over 80 KIAS, min brake cooling time is:

A

50 mins

57
Q

Max tailwind for Engine Start

A

10 kts

58
Q

Local TRG flight Min Oxy PSI

A

1050

59
Q

Minimum Significant Weather avoidance (nm)

A

10nm

60
Q

Take-brief mnemonic:

A

T Type of TO
S Speeds from Tape
S Standard PM duties
R Rejection reasons
E Emergency intentions post V1
D Departure briefed
S Safety Alt, TA

61
Q

Max landing weight

A

4480

62
Q

Stabilised approach criteria

A

Maintaining runway centreline
On desired approach path
Between Vref and Vref +20
Appropriate trim in all axes
In briefed landing config

Must call stab by 200ft

63
Q

EFATO / SEFATO Accel Height

A

As calculated from planning tools. MIN 400 ft AGL

(1000ft requested only in FFS)

64
Q

TOGA ‘event’ Limit?

A

12 TOGA Events / per engine / per sortie

65
Q

Post Abort Actions?

A

Inform crew

F - FRCs
A - After Ldg Cxs
B - Brake Cooling Time

Consider Vacating - ATC

66
Q

Final 1000ft Climb AP Engaged Work Cycle

A

A - Altimeter - correct setting
A - ALT SEL Active, ALT armed
A - Air Speed

67
Q

NITS message format?

A

N - Nature of emergency
I - Intent
T - Time
S - Special instructions / Services required

68
Q

FL above which Windshields must be selected ON

A

Above FL150

69
Q

Min distance to go to initiate GA?

A

3000ft

70
Q

Target Storm Penetration Speed

A

180 KIAS

Phenom (4 decks)

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