Limits Flashcards
1
Q
MIN CREW
A
ONE PILOT
2
Q
PAX SEATING LIMITATIONS
A
15 PAX MAX
3
Q
LOAD FACTOR FLAPS DOWN NEGATIVE
A
0 Gs
4
Q
LOAD FACTOR FLAPS DOWN POSITIVE
A
1.1 Gs
5
Q
LOAD FACTOR FLAPS UP NEGATIVE
A
-1.24 Gs
6
Q
LOAD FACTOR FLAPS UP POSITIVE
A
3.1 Gs
7
Q
MAX OPERATING ALTITUDE WITH AVGAS AND BOTH STBY BOOST PUMPS OPERATIVE
A
35,000 FT
8
Q
MAX OPERATING ALTITUDE
A
35,000 FT
9
Q
MAX OPERATING ALTITUDE AVGAS EITHER STBY BOOST PUMT INOP
A
FLIGHT PROHIBITED
10
Q
MAX ALLOWABLE TAKEOFF WEIGHT
A
15,000 LBSOR AS LIMITED BY:-TAKEOFF CLIMB REQUIREMENTS-TIRE SPEED-BRAKE ENERGY-TAKEOFF FIELD LENGTH
11
Q
MAX LANDING WEIGHT
A
15,000 LBSOR AS LIMITED BY:-MAX LANDING WIEGHT TO ACHIEVE CLIMB GRADIENTS-MAX LANDING DISTANCE - FLAPS DOWN
12
Q
MAX RAMP WEIGHT
A
15,100 LBS
13
Q
MAX ZERO FUEL WEIGHT
A
12,500 LBS
14
Q
EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP BEST ANGLE OF CLIMB (VXSE)
A
125 KIAS
15
Q
EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP BEST RATE OF CLIMB (VYSE)
A
125 KIAS
16
Q
EMERGENCY AIRSPEEDS (15,000 LBS)ONE ENGINE INOP ENROUTE CLIMB
A
125 KIAS
17
Q
EMERGENCY AIRSPEEDS (15,000 LBS)AIR MIN CONTROL SPEED (VMCA): FLAPS UP
A
94 KIAS
18
Q
EMERGENCY AIRSPEEDS (15,000 LBS)AIR MIN CONTROL SPEED (VMCA): FLAPS APPROACH
A
93 KIAS
19
Q
EMERGENCY AIRSPEEDS (15,000 LBS)EMERGENCY DESCENT SPEED
A
184 KIAS
20
Q
EMERGENCY AIRSPEEDS (15,000 LBS)MAX RANGE GLIDE SPEED
A
135 KIAS
21
Q
MAX DEMO’D CROSSWIND
A
20 KTS
22
Q
MAX TAILWIND
A
10 KTS
23
Q
SINGLE ENGINE ENROUTE CLIMB
A
125 KIAS
24
Q
MANEUVERING SPEED (VA)
A
184 KTS
25
MAX FLAP EXTENSION/EXTENDED SPEED (VFE) APPROACH
202 KIAS
26
MAX FLAP EXTENSION/EXTENDED SPEED (VFE) FULL
158 KIAS
27
MAX LANDING GEAR EXTENDED SPEED (VLE)
184 KIAS
28
MAX LANDING GEAR OPERATING SPEED (VLO) EXTENSION
184 KIAS
29
MAX LANDING GEAR OPERATING SPEED (VLO) RETRACTION
166 KIAS
30
AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS UP
96 KIAS
31
AIR MIN CONTROL SPEED (VMCA) PROP FEATHERED FLAPS APPROACH
94 KIAS
32
MAX OPERATING SPEED (VMO)
263 KIAS/0.58 MACH
33
AIRCRAFT HEIGHT
14' 4"
34
AIRCRAFT LENGTH
46' 8"
35
AIRCRAFT WINGSPAN
57' 11"
36
AFT FACING SEATS TAKEOFF RESTRICTION
IF OCCUPIED FOR T/O, HEADRESTS MUST BE FULLY EXTENDED
37
AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR BACK COURSE
70°
38
AUTOPILOT MAX COUPLED INTERCEPT ANGLE FOR NAV/LOC
LESS THAN 90°
39
AUTOPILOT MIN ALT FOR APPROACH
79 FT AGL
40
AUTOPILOT MIN ALT FOR CRUISE
1,000 FT AGL
41
AUTOPILOT MIN ALT FOR STEEP APPROACH
160 FT AGL
42
Below ______ volts, battery must be recharged prior to attempting engine start.
20 VDC
43
EXTERNAL POWER AMPS LIMITS: MOMENTARY
1,000 AMPS
44
EXTERNAL POWER AMPS LIMITS: CONTINUOUS
300 AMPS
45
EXTERNAL POWER VOLTAGE RANGE
28 TO 28.4 VOLTS
46
GENERATOR LOAD LIMITS ABOVE 34,000 FT
95%
47
GENERATOR LOAD LIMITS IN GROUND AT 62%-70% N1
75%
48
GENERATOR LOAD LIMITS IN GROUND AT 70%-100% N1
100%
49
GENERATOR LOAD LIMITS SL TO 34,000 FT
100%
50
MIN BATTERY VOLTS FOR BATTERY START
23 VDC
51
STARTER DUTY CYCLE
-30 SEC ON/5 MIN OFF-30 SEC ON/5 MIN OFF-30 SEC ON/30 MIN OFF
52
For fuel system, fill the _______ tanks first.
MAIN
53
For fuel system, do not takeoff if fuel gauges in the ______ arc or indicate less than _____ lbs in each wing system.
YELLOW265
54
FUEL CROSSFEED PERMITTED ONLY WHEN
ONE ENGINE INOP
55
MAX FUEL IMBALANCE
300 LBS
56
AUX SYSTEM FUEL QUANTITY
79.5 U.S. GAL / 533 LBS
57
MAIN SYSTEM FUEL QUANTITY
190 U.S. GAL / 1,273 LBS
58
TOTAL USABLE FUEL QUANTITY
539 U.S. GAL / 3,611 LBS
59
WHEN IS ENGINE ANTI-ICE REQUIRED?
+5° C IN VISIBLE MOISTURE...NOT permitted for T/O operations above 10C
60
MIN TEMP FOR DEICING BOOTS OPERATIONS
-40° C
61
MIN AIRSPEED FOR SUSTAINED OPS IN ICING
140 KTS
62
MAIN LANDING GEAR STRUT EXTENSION (INCHES)
3.23 TO 3.49 INCHES
63
NOSE LANDING GEAR STRUT EXTENSION (INCHES)
3.77 TO 4.06 INCHES
64
BRAKES DEICE TEMP OPERATION LIMITE
NOT ABOVE 15° C
65
LANDING GEAR CYCLE LIMITS
1 CYCLE (UP/DOWN) EVERY 5 MIN FOR TOTAL OF 6 FOLLOWED BY 15 MIN COOL-DOWN
66
MAX CABIN PRESSURE DIFFERENTIAL
6.6 PSI
67
CABIN DIFFERENTIAL PRESSURE (GREEN ARC)
0 TO 6.6 PSI
68
CABIN DIFFERENTIAL PRESSURE (RED ARC)
6.6 PSI AND UP
69
When does the "CABIN ALTITUDE" light illuminate?
ABOVE 10,000 FT CABIN ALT
70
When does the "CABIN ALTITUDE HI" light illuminate?
ABOVE 12,000 FT CABIN ALT
71
When do the passenger mask automatically deploy?
ABOVE 12,500 FT CABIN ALT
72
Cabin altitude is limited to _____ Ft as long as air is coming into pressure vessel.
13,000 FT
73
The "CABIN DIFF HI" light illuminates at what PSID?
6.9 PSID
74
ENGINE MODEL NUMBER AND TYPE
PT6A-60A, TURBOPROP
75
PROPELLER TYPE
CONSTANT-SPEED, FULL-FEATHERING, REVERSING, COUNTER-WEIGHTED, AND HYDRAULICALLY ACTUATED
76
MAX N1 CRUISE CLIMB
104%
77
N1
62% MIN
78
MAX N1 MAX CRUISE
104%
79
MAX TRANSIENT N1
104%
80
MAX ITT CRUISE
820° C
81
MAX ITT CRUISE CLIMB
785° C
82
MAX ITT IDLE
750° C
83
MAX CONTINUOUS ITT
820° C
84
MAX ITT REVERSE
760° C
85
ENGINE STARTING MAX TRANSIENT ITT
1,000° C FOR 5 SEC
86
MAX TAKEOFF ITT
820° C
87
ENGINE MAX ITT TRANSIENT
850° C FOR 20 SEC
88
NORMAL OIL PRESSURE FOR CRUISE CLIMB
90 TO 135 PSI
89
ENGINE OIL PRESSURE IDLE
60 PSI MIN
90
MAX CONTINUOUS OIL PRESSURE
90 TO 135 PSI
91
MAX CRUISE OIL PRESSURE
90 TO 135 PSI
92
MAX REVERSE OIL PRESSURE
90 TO 135 PSI
93
ENGINE OIL PRESSURE STARTING
0 TO 200 PSI
94
NORMAL TAKEOFF OIL PRESSURE
90 TO 135 PSI
95
ENGINE OIL PRESSURE TRANSIENT
200 PSI
96
ENGINE OIL TEMP CRUISE CLIMB
0° TO 110° C
97
ENGINE OIL TEMP IDLE
-40° TO 110° C
98
MAX CONTINUOUS OIL TEMP
0 TO 110° C
99
ENGINE OIL TEMP MAX CRUISE
0 TO 110° C
100
ENGINE OIL TEMP MAX REVERSE
0 TO 99° C
101
ENGINE OIL TEMP MIN FOR FUEL HEAT AT T/O
55° C (RECOMMENDED)
102
ENGINE PROP RPM (N2) CRUISE CLIMB
1,700 (UP TO 1,735 FOR 7 MINUTES)
103
ENGINE PROP RPM (N2) IDLE
1,050 MIN
104
ENGINE PROP RPM (N2) MAX CONTINUOUS
1,700 RPM (UP TO 1,735 FOR 7 MINUTES)
105
MAX CRUISE N2
1,700 RPM (UP TO 1,735 FOR 7 MINUTES)
106
MAX REVERSE N2
1,650 RPM
107
MAX TAKEOFF N2
1,700 RPM (UP TO 1,735 FOR 7 MINUTES)
108
MAX TRANSIENT N2
1,870 RPM FOR 20 SEC
109
ENGINE TORQUE% MAX CONTINUOUS
100% (UP TO 102% FOR 7 MINUTES)
110
MAX TORQUE% FOR TAKEOFF
100% (UP TO 102% FOR 7 MINUTES)
111
ENGINE TORQUE LIMITE BELOW 1,000 RPM N2
62%
112
If the shaft to the primary governor were to shear, what would happen to the propeller?
It would feather
113
What is the range of the primary governor?
1,450 to 1,700 RPM
114
The overspeed governor governs to _____.
1,768 RPM
115
how many stby fuel pumps required for T/O
1 when using rec engine fuels...crossfeed will be unavailable from side without operative STBY pump
116
engine anti ice shall be off for T/O in temps above
+10C
117
de ice boots shall not be operated in temps below
below -40C
118
brake de ice shall not be used above
15C
119
electric heat must be turned off ___ prior to engine start
2 min
