E55P Initial > Limitations > Flashcards

Limitations Flashcards

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1
Q

How much fuel for 45 minute IFR reserve?

A

1121 LBS

FL300 @ .74M 16,800LBS

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2
Q

How much fuel for Hot Spare?

A

3600 LBS

The DO or ADO on duty may authorize reduction of these quantities under certain conditions.

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3
Q

Emergency Fuel

A

759 LBS

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4
Q

Fuel onboard when parking in inclement weather?

A

3600 LBS

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5
Q

Minimum runway length

A

3500 FT

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6
Q

Minimum runway width

A

60 FT

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7
Q

Max runway slope

A

+ / - 2%

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8
Q

When is an ops review required for runway performance?

A

Contaminated runway LESS THAN 5500 FT

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9
Q

Max crosswind on takeoff

A

Static : 18KT
Rolling : 25KT

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10
Q

Max landing crosswind

A

28KTS

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11
Q

What are the crosswind limits when operating from a contaminated runway?

A

150ft wide or greater - 15kts
149ft wide or less - 10kts

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12
Q

Max tailwind component on takeoff

Can you use instantaneous winds?

A

10KT

The use of instantaneous winds for the purposes of takeoff and landing when standard reported winds indicate otherwise is prohibitied. - FOM 2.11.4

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13
Q

What kinds of equipment are required for operations in RVSM airspace?

A

1) Autopilot (1)
2) Altitude alerting device (1)
3) ATC altitude alerting transponder (1)
4) Air Data Computer (2)
5) Pitot tube heaters (2) on the probes linked to the ADC in use

Mnemonic: AATAP -> Autopilot, Altitude alerting device, ATC altitude alerting transponder, Air Data Computer, Pitot tube heaters.

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14
Q

Max takeoff weight?

A

18,387 LBS (300)
18,551LBS (300E)

See AOM 12.2.1 for further guidance

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15
Q

Max landing weight

A

17,042LBS (300)
17,272LBS (300E)

See AOM 12.2.2 for further guidance

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16
Q

Max ramp & taxi weight

A

18,497 LBS - 300
18,617 LBS - 300E

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17
Q

Zero fuel weight

A

14,440 LBS - 300
14,263 LBS - 300E

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18
Q

Max allowable baggage

A

Forward - 110
Aft - 463

See FOM 2.7.6 for standard weights

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19
Q

Maximum operating altitude

A

FL450

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20
Q

Maximum altitude flaps extended

A

FL180

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21
Q

Maximum altitude with OEI in icing conditions

A

15,000ft

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22
Q

Maximum altitude for engine start, takeoff and landing

A

14,000ft

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23
Q

​Maximum altitude for takeoff and landing in icing conditions

A

10,000ft

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24
Q

Lowest altitude for engine start, takeoff and landing

A

-1000ft

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25
Minimum operation speed
26
Max operating speed (Vmo)
320KTS
27
Max operating Mach (Mmo)
.78 Mach 300 .80 Mach 300E
28
Turbulent air penetration speed
232KTS / .65M
29
Maneuvering speed
205KTS
30
Max landing gear operating speed
250KTS
31
max tire speed
182KTS
32
Max speed Flaps 1
180KTS
33
Max speed Flaps 2/3
170KTS
34
max speed flaps full
160KTS
35
Minimum speed in icing conditions WING STAB anti-ice systems inhibited (flaps and gear up)
165Kts
36
Minimum speed in icing conditions - WING STAB anti-ice uninhibited (flaps and gear up)
150KTS
37
Max speed in icing - (Yaw Damp OFF)
180KTS
38
Max cabin differential pressure
9.4psi
39
max allowable overpressure
9.6psi
40
max negative differential
-0.3psi
41
Max takeoff and landing differential pressure
0.2psi ## Footnote **THE CABIN MUST BE DEPRESSURIZED PRIOR TO OPENING THE MAIN CABIN DOOR**
42
Minimum altitude for AP or YD engagement
Minimum ENGAGEMENT height- 600ft / 1000ft OEI Minimum USE hight - 195ft / 220FT OEI ## Footnote Do not use the AP or YD for T/O or LDG. Do not manually override the AP during normal ops.
43
Minimum voltage for a battery start
24V
44
Minimum GPU voltage for batt charging
27V
45
Max generator load in flight
390A
46
Max generator load on ground
330A
47
Fuel capacity
300 - 5401 300E - 5427.6
48
Max pressure refueling pressure
pressure fueling is limited to 10-50PSI
49
Maximum fuel imbalance (all flight regimes)
220 LBS
50
When do icing conditions exist?
* OAT is 10C or below * Visable moisture (rain, snow, or visability less than 1sm) * Operating on contaminated surfaces ## Footnote FLIGHT IN FREEZING DRIZZLE OR FREEZING RAIN OF ANY INTENSITY IS PROHIBITED - AOM 12.15.1
51
# ICING SYSTEM OPERATION LIMITATIONS Minimum temperature - landing
-38C
52
# ICING SYSTEM OPERATION LIMITATIONS Minimum temp allowable for automated operating of wing stab heat (below 16,000 ft)
-40C
53
# ICING SYSTEM OPERATION LIMITATIONS Automated operating envelope or wing stab heating (at or above 16,000ft)
-45C
54
When is the use of A/P prohibited?
* ice accumulation aft of protected area on wing * unusual lateral trim imputs or A/P trim warning
55
What approach category are we
Certified CAT B | CAT C if approach speeds exceed 120 - AOM 12.18.3
56
What does a GOLDEN CAS message indicate? Are they actually golden?
GOLDEN CAS is displayed in color of severity in inverse video. Golden CAS indicates root cause.
57
Maximum thrust time limit
10 mins
58
Takeoff thrust time limit
5 mins
59
Maximum continuous thrust time limit
5 mins when in level flight
60
Max transient N1
102%
61
Max Transient N2
103%
62
Max transient ITT
765 C
63
Max transient time limt
20 sec
64
Transient oil pressure limits (20 sec)
0-20 PSI
65
Transient oil pressue limts (400 Sec)
20-270 PSI
66
Starter limitations
67
Coldest allowable temp for BATT temp for starting
-18 degrees Celsius
68
Per AOM 4.2.2 Anti-Ice System Operation guidelines, when operating in visible moisture what system needs to be ON when OAT are between 5 - 10 degrees?
ENG A/I 1 & 2
69
Per AOM 4.2.2 Anti-Ice System Operation guidelines, what system needs to be ON at 5 degrees or colder when operating in visible moisture?1
Everything ON
70
What actions are required when the ICE CONDITION CAS illuminates?
All A/I ON
E55P Initial
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