Operating Limitations Flashcards

1
Q

Max Zero Fuel Weight (MZFW) - E135

A

35,274 LBS

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2
Q

Max Ramp Weight (MRW) - E135

A

44,312 LBS

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3
Q

Max Takeoff Weight (MTOW) - E135

A

44,092 LBS

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4
Q

Max Landing Weight (MLW) - E135

A

40,785 LBS

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5
Q

Max Zero Fuel Weight (MZFW) - E145

A

40,564 LBS

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6
Q

Max Ramp Weight (MRW) - E145

A

50,044 LBS

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7
Q

Max Takeoff Weight (MTOW) - E145

A

49,823 LBS

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8
Q

Max Landing Weight (MLW) - E145

A

43,651 LBS

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9
Q

Takeoff/Landing Minimum Altitude

A

-1000’

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10
Q

Takeoff/Landing Maximum Altitude

A

8,000’

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11
Q

Maximum Operating Altitude

A

37,000’

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12
Q

Mmo

A

Mach .78

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13
Q

Vmo

A

250 KIAS to 8000’ / 320 KIAS above 10,000’

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14
Q

Vlo for Extension

A

250 KIAS

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15
Q

Vlo for Retraction

A

200 KIAS

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16
Q

Vle

A

250 KIAS

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17
Q

Va

A

200 KIAS

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18
Q

Turbulent Air Penetration Below 10,000’

A

200 KIAS

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19
Q

Turbulent Air Penetration Above 10,000’

A

250 KIAS / .63M whichever is lower

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20
Q

Vfe - Flaps 9

A

250 KIAS

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21
Q

Vfe - Flaps 18/22

A

200 KIAS

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22
Q

Vfe - Flaps 45

A

145 KIAS

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23
Q

Maximum Altitude for Flap Extension

A

20,000’

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24
Q

Max A/S for Windshield Wiper Operation

A

170 KIAS

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25
Max A/S After Takeoff/During Climb Without Trimming
160 KIAS
26
Max Recommended A/S to Remove DV Windows
140 KIAS
27
Max Crosswind Dry/Wet Runway
30 KIAS
28
Max Takeoff/Landing Tailwind Component
10 KIAS
29
Maximum Load on Main Generator
400 A
30
Maximum Load on APU Generator up to 30,000'
400 A
31
Maximum Load on APU Generator above 30,000'
300 A
32
Maximum Battery Temperature
70° C
33
Usable Wing Fuel Per Tank
5,717 LBS
34
Unusable Fuel Per Tank
39 LBS
35
Unusable Quantity Per Fuel Tank (Elec Pump INOP)
365 LBS
36
Maximum Imbalance Between Wing Tanks
800 LBS
37
Min Fuel Tank Temp
-40° C
38
Max Fuel Tank Temp
52° C
39
Min Fuel Temp @ FCOC Without Icing Inhibitor
4° C
40
Maximum Altitude for Start
30,000'
41
Max Operating Altitude
37,000'
42
Maximum Rotor Speed
108%
43
Rotor Speed for Automatic Shutdown
104%
44
Maximum EGT for Start
884° C
45
Maximum Continous EGT
680° C
46
Maximum Continous EGT for 5 Min Max
717° C
47
Minimum Battery Temperature for Start
-20° C
48
Cooling Period Between First Three Start Attempts
1 min off
49
Cooling Period Between Two Series of Three Start Attempts
30 Mins off
50
Maximum N1
100%
51
Maximum N2 (Steady State)
102.4%
52
Max ITT for Start
800° C
53
Max ITT Takeoff (5 Min Max)
948° C
54
Max Continous ITT
901° C
55
Min Oil Press Below 88% N2
34 PSI
56
Min Oil Pressure Above 88% N2
50 PSI
57
Max Oil Press (Steady State Temp >21° C)
95 PSI
58
Max Oil Press (Transient 5 Min)
110 PSI
59
Min Oil Temp for N2 Above 83%
40° C
60
Min Oil Temp for Starting
-40° C
61
Min Oil Temp Cont Ops
21° C
62
Max Oil Temp Cont Ops
126° C
63
Min/Max Fuel Temp
-40/+52° C
64
Eng Dry Motoring Ops
5 min on / 5 min off
65
Eng Start Limits (1st - 4th Cycles)
1 min on / 1 min off
66
Eng Start Limits (5th Cycle)
1 min on / 5 min off
67
Eng Warm-Up
4 min for cold eng / 2 min for warm eng
68
Engine is considered cold if shutdown for more than
90 mins
69
Min Oil Temp to Increase N2 Above 83%
40° C / or run eng for 8 mins / or static runup to 88% N2 and ensure oil pressure is equal or less than 83 PSI
70
Cold Weather Ops Restriction
Idle RPM max until press < 95 PSI
71
Eng Cool Down
1 min @ idle/taxi speed before shutdown
72
Maximum Differential Pressure
7.8 PSI
73
Maximum Differential Overpressure
8.1 PSI
74
Maximum Differential Negative Pressure
-0.3 PSI
75
Maximum Temp for Anti-Icing Operations
10° C
76
Minimum Temp for Manual Anti-Icing Operation
-40° C
77
Single Engine or Single Bleed Max Altitude in Icing Conditions
15,000'
78
Holding in Icing Conditions
Landing gear-up / Flaps up / Min airspeed 200 KIAS
79
Icing Conditions
10° C or less and visible moisture
80
APU Bleed as Pneumatic Source for Anti-Icing System
Do not use
81
Maximum Airspeed for Windshield Wiper Operation
170 KIAS
82
Min Engagement Height After Takeoff
500'
83
Autopilot Coupled Approaches Approved Down to
200'
84
Descent Below MDA on Non-Precision Approach with A/P Engaged
Prohibited
85
Single Engine Go-Around With Autopilot Engaged
Prohibited