MC-12 | Limitations Flashcards
1
Q
Auto Pilot Limitation
AP/YD must not be used for _______ or ________.
A
Take off or Landing
2
Q
Auto Pilot Limitation
Max Coupled intercept angles
Nav and Loc = _________*
A
< 90*
3
Q
Auto Pilot Limitation
Max Coupled intercept angles
Nav and Loc Back Course = _________*
A
< 70*
4
Q
Auto Pilot Limitation
Operation w/ Pitch Trip Malfunction is ______________.
A
Prohibited
5
Q
Auto Pilot Limitations
Minimum Engage Height After Takeoff
A
400 ft. AGL
6
Q
Auto Pilot Limitations
Minimum use height during approach
A
79 ft. AGL
7
Q
Auto Pilot Limitations
Minimum use height during cruise
A
1000 ft. AGL
8
Q
Auto Pilot Limitations
Minimum use height during steep approach
A
160 ft. AGL
9
Q
AutoPilot Limitation
Rudderboost must be _____________.
A
Must be operational for all flights.
10
Q
Brake De-Ice Limitations
Don’t use above______ * Celsius
More than ____ Minutes w/ wheels retracted
A
15* Celcius
10 Minutes
11
Q
Climb Speed
A
135 KIAS SL - 35K
12
Q
DC Power Limitations
Flight Operations (MEK)
34,000 - 35,0000
A
95%
13
Q
DC Power Limitations
Flight Operations (MEK)
Sea Level - 34,000
A
100%
14
Q
DC Power Limitations
Flight Operations (NOMEK)
21-26K
A
90%
15
Q
DC Power Limitations
Flight Operations (NOMEK)
26-30K
A
80%
16
Q
DC Power Limitations
Flight Operations (NOMEK)
30-32K
A
75%
17
Q
DC Power Limitations
Flight Operations (NOMEK)
32-35K
A
70%
18
Q
DC Power Limitations
Flight Operations (NOMEK)
Max Single Engine all Altitudes
A
90%
19
Q
DC Power Limitations
Flight Operations (NOMEK)
SL-21K
A
100%
20
Q
DC Power Limitations
Ground Operations (MEK)
55-70% N1
A
55%
21
Q
DC Power Limitations
Ground OPS (NOMEK)
70-100% N1
A
100%
22
Q
DC Power Limitations
Ground OPS -(NOMEK)
62-70% N1
A
75%
23
Q
External Power Limits
Continuous
A
300 Amps
24
Q
External Power Limits
Momentary
A
1000 Amps
25
External Power Limits
Normal
28-28.4
26
Fuel System Limitations
ER Fuel Capacity
118 Gal Ea (236 Total)
27
Fuel System Limitations
Max Imbalance
300 lbs.
28
Fuel System Limitations
Max Range
2300 NM or 8 Hrs
29
Fuel System Limitations
Max useable fuel quantity.
775 gal / 5192 lb
30
Fuel System Limitations
Max with fuel pressure light on
10 hrs.
31
Fuel System Limitations
Minimum in each main for takeoff.
265 lbs.
32
G Load Limitations
Flaps Down
0.0 - 2.0
33
G Load Limitations
Flaps Up
-1.21 - 3.01
34
Gear Cycle Limits
___ cycles at ___ every ____ Minutes
___ minutes rest after ___ cycles
Gear Cycle Limits
6 cycles at 1 every 5 Minutes
15 minutes rest after 6 cycles
35
Gyro Suction Gage Limits
Normal - 15K ft. - 35K Ft.
2.8 - 4.3 in
36
Gyro Suction Gage Limits
Normal - SL - 15K Ft.
4.3 - 5.9 in
37
Icing Limitations
EO/IR Turret must be __________(MC-12V)
Retracted
38
Icing Limitations
Vader radar & cooling sys must be ____________. (MC-12V)
Shut Down
39
Icing Limitations
When should you activate Engine De-Ice?
ENGINE ANTI-ICE, LEFT and RIGHT, shall be ON
in ambient temperatures of +____°C or below, in ________ -__________.
Should also be off for Take-off above _____* C.
ENGINE ANTI-ICE, LEFT and RIGHT, shall be ON in ambient temperatures of +5°C or below, in visible moisture.
Should also be off for Take-off above 10* C.
40
ITT Limits (MEK & NOMEK)
Max Transient Starting
(Time Limited)
1000* Celcius for 5 seconds
41
ITT Limits
Cruise Climb
NOMEK | MEK
NOMEK 785* Celsius
| MEK 840* Celsius
42
ITT Limits
Max Continuous
NOMEK | MEK
NOMEK 820* Celsius
| MEK 840* Celsius
43
ITT Limits
Max Cruise
NOMEK | MEK
NOMEK 820* Celsius
| MEK 840* Celsius
44
ITT Limits
Max Low Idle
NOMEK / MEK
NOMEK 750* Celsius
| MEK 750* Celsius
45
ITT Limits
Max Reverse
NOMEK | MEK
NOMEK 760* Celsius
| MEK 760* Celsius
46
ITT Limits
Takeoff
NOMEK | MEK
NOMEK 820* Celsius
| MEK 850* Celsius
47
ITT Limits
Throttle PUSH
870* (100% Q for 5 minutes)
NOMEK ONLY During ENG Failure
48
ITT Limits
Transient
NOMEK | MEK
(Time Limit)
NOMEK 850* Celsius
MEK 870* Celsius
20 seconds
49
Max Operating Altitude
Normal Operations
35k ft.
50
Oil Pressure Limits (PSI)
Caution Range (Limits Tq to ____%)
60-90 PSI
62% Q
51
Oil Pressure Limits (PSI)
Max Starting
200 PSI
52
Oil Pressure Limits (PSI)
Normal Operating Range
90-135 PSI
53
Oil Pressure Limits (PSI)
Oil pressure below ___ psi is unsafe and requires engine shutdown or landing at nearest suitable airport.
*Fluctuations of +/- ____ psi are acceptable.
Oil pressure below 60 psi is unsafe and requires engine shutdown or landing at nearest suitable airport.
*Fluctuations of +/- 10 psi are acceptable.
54
Oil Pressure Limits (PSI)
Starting, Low Idle
60 PSI
55
Oil Temp Limits
Max Trans ( ___ Min) Ground ONLY
NOMEK | MEK
NOMEK 99-110* Celsius for 10 Minutes
| MEK 111-115* Celsius for 10 Minutes
56
Oil Temp Limits
Normal
NOMEK | MEK
NOMEK 0 - 99* Celsius
MEK 0 - 110* Celsius
57
Oil Temp Limits
Rec for fuel heater ops at T/O
55* Celcius
58
Oil Temp Limits
Starting, Low Idle
-40 - 110* Celcius
59
Pneumatic Pressure Limits
Max
20 PSI
60
Pneumatic Pressure Limits
Normal Operating Range
12 - 20 PSI
61
Propeller De-Ice Ammeter Limitations
Normal Range
26 - 32 amps
62
Props (N2 RPM) Limits
*All other conditions
1700
63
Props (N2 RPM) Limits
Avoid During Ground Operations
400 - 1050 RPM
| NOMEK Only
64
Props (N2 RPM) Limits
Inadvertent Excusions (Time Limited)
1735 RPM (7 Minutes)
| NOMEK Only
65
Props (N2 RPM) Limits
Max
1700 RPM
66
Props (N2 RPM) Limits
Max Reverse
1650 RPM
67
Props (N2 RPM) Limits
Max Transient (Time Limited)
1870 RPM for 20 Seconds
68
Props (N2 RPM) Limits
Minimum Idle
1050 RPM (NOMEK Only)
69
Props (N2 RPM) Limits
Normal Operating Range
1450 - 1700 RPM
70
Starter Limitations
30 seconds ON - 5 minutes OFF
30 seconds ON - 5 minutes OFF
30 seconds ON - 30 minutes OFF
71
Surface De-Ice Limits (Pneumatic Boot Operations)
No Operations Below
Activate when ice accumulates...
-40* C
__________
1/2 Inch
72
Temp Limits
Max Above 25k ft.
ISA + 31* C
73
Temp Limits
Max Below 25k ft.
ISA + 37* C
74
Torque Limits
Max TQ Props above 1700 RPM
96%
75
Torque Limits
| Normal Operating Range
1000-1700 rpm
0-100%
76
Torque Limits
| Transient (NOMEK
Time LImited)
102% (NOMEK Only)
| 7 Minutes
77
Torque Limits
| Transient Limit
Time Limited
156%
| 20 Seconds
78
Turbine Tach (N1 Speed) Limits
Max
104%
79
Turbine Tach (N1 Speed) Limits
Min Flight (MEK)
64%
80
Turbine Tach (N1 Speed) Limits
Min idle Ground (MEK)
55%
81
Turbine Tach (N1 Speed) Limits
Min Low Idle (NOMEK)
62%
82
Turbine Tach (N1 Speed) Limits
Transient
104%
83
V Speed
VX
135 KIAS
84
V Speed
Max Windshield De-Icing
226
85
V Speed
Maximum Glide Range
135 KIAS
86
V Speed
Minimum for Reversing
40 KIAS
87
V Speed
Minimum Sustained Icing Speed
15K lbs or less
140 KIAS
88
V Speed
Minimum Sustained Icing Speed
> 15K lbs
150 KIAS
89
V Speed
Mmo (Above 24K ft.)
.58
90
V Speed
Va (Flaps Up)
182 KIAS
91
V Speed
Vb (Turbulence Penatration)
170 KIAS
92
V Speed
Vfe (Flaps Approach)
202 KIAS
93
V Speed
Vfe (Full Down)
158 KIAS
94
V Speed
Vlo (Extension)
182 KIAS
95
V Speed
Vlo (Retraction)
164 KIAS
96
V Speed
Vmca (Flaps Approach)
99 KIAS
97
V Speed
Vmca (Flaps Up)
103 KIAS
98
V Speed
Vmo (Below 24K ft.)
245
99
V Speed
Vmo MX-15 extended (and >1,500' AGL)
MC12V (AFMS)
180 KIAS
100
V Speed
VSSE ( Intentional OEI)
135 KIAS
101
V Speed
Vy
135 KIAS
102
V Speed
VYSe
135 KIAS
103
Weight Limits
Max Bag Compartment Weight
550 lbs.
104
Weight Limits
Max landing Weight
15,675 lbs.
105
Weight Limits
Max Ramp Weight
16,600 lbs.
106
Weight Limits
Max Takeoff Weight
16,500 lbs.
107
Weight Limits
Max weight on airstair door.
One Person
108
Weight Limits
Max Zero Fuel Weight (M, G, W)
13,000 lbs
109
Weight Limits
Max Zero Fuel Weight (V)
13,430 lbs
110
What is the Maximum Cabin Differential?
6.6 PSIG
111
Yaw Damn System ( 2 part question)
Max Altitude inoperable (Dual Strakes)
Must be on above ____________ except for
__________ & ___________.
19,000' MSL
(Must be on above 19K except for takeoff and Landing)
**Check REL**
