General Flashcards
(155 cards)
1
Q
Speed, Vmo
A
259 KIAS
2
Q
Speed, Mmo (BLR Supps)
A
M 0.58
3
Q
Speed, Va
A
181 KIAS
4
Q
Speed, Vb
A
170 KIAS
5
Q
Speed, Vmca
A
92 KIAS Flaps up 250/275
87 KIAS Flaps App 250/275
6
Q
Speed, Vle (Flaps app)
A
200 KIAS
7
Q
Speed, Vfe (Flaps Down)
A
157 KIAS
8
Q
Speed, Vle Max Landing Gear Extension Speed
A
181 KIAS
9
Q
Speed, Vlo (Retraction)
A
163 KIAS
10
Q
Speed, Vx Best Angle
A
100 KIAS
11
Q
Speed, Vxse, Single Engine Best Angle
A
105 KIAS HALO 250
107 KIAS HALO 275
12
Q
Speed, Vy Best Rate
A
125 KIAS
13
Q
Speed, Vyse Single Engine Best Rate
A
116 KIAS for both
14
Q
Speed, Vso
A
75 KIAS HALO 250
77 KIAS HALO 275
15
Q
Speed, Vs1
A
82 KIAS HALO 250
84 KIAS HALO 275
16
Q
Speed, Vs
A
92 KIAS HALO 250
94 KIAS HALO 275
17
Q
Speed, Vr Max Gross Flaps Zero
A
104 KIAS HALO 250
106 KIAS HAlO 275
18
Q
Speed, Vr Max Gross Flaps App
A
98 KIAS for both
19
Q
Speed, V2 Max Gross Flaps Zero
A
113 KIAS HALO 250
116 KIAS HALO 275
20
Q
Speed, V2 Max Gross Flaps App
A
101 KIAS HALO 250
104 KIAS HALO 275
21
Q
Speed, Min Icing
A
145 KIAS HALO 250
148 KIAS HALO 275
22
Q
Speed, Vsse
A
117 knots Epic Supps
104 afm
23
Q
Speed, Max for windshield heat effectiveness
A
226 KIAS
24
Q
Speed, Max Glide
A
136 KIAS
25
Speed, Company Holding
160 KIAS
26
SHP
850 shp
27
Torque, Max Takeoff and Cont
2,230 ft-lbs
To account for power settings accuracy and steady state of inadvertent torque excursions up 2,275 ft-lbs are time limited to 7 mins
28
Torque, Max Transient
2,750 ft-lbs for 5 sec max
29
Torque, Max with Oil Pressure 60-85 PSI
1,100 ft-lbs
30
Torque, Max with Prop RPM 2,120
1,800 ft-lbs This prop rpm suggests a failure of the primary governor, overspeed governor is working
31
ITT, Max Starting
1,000C for 5 sec
32
ITT, Max Low Idle
750C Can be corrected by reducing load and/or increasing N1
33
ITT, Max Takeoff
820C
34
ITT, Max Continuous
820C
35
ITT, Max Cruise
820C
36
ITT, Max Cruise Climb and Rec (Normal Cruise)
775C
37
ITT, Max Reverse
750C
38
ITT, Max Transient
850C
39
N1, High Idle
Approx 70%
40
N1, Takeoff and Max Cont
104%
41
N1, Max Reverse
88%
42
N1, Max Transient
104%
43
N1, Min for air conditioning
62%
44
Autofeather arms at ___ N1
Approx 90% N1
45
Prop RPM, Low Idle
1,180 rpm
Placard in the plane: 700-1,150 rpm
46
Prop RPM, Max
2,000 RPM
To account for power settings accuracy and steady state of inadvertent prop excursions up 2,040 RPM are time limited to 7 mins
47
Prop RPM, Max Reverse
1,900 rpm @ 88% N1 (one min max)
| In reverse FTG is reset to approx 95% prop rpm before the prop reaches a negative pitch angle
48
Prop RPM, Max Transient
2,200 rpm for 5 sec max
49
Prop, Overspeed Governor Limit
2,120 rpm, fixed setting
50
Prop, Power Turbine Governor Limit (Acts like a Fuel Topping Governor) Max Prop Speed
Prevents prop from exceeding 2,200 rpm by reducing fuel = reduces N1 speed
51
Prop Governor Test Switch Resets the Overspeed Governor To:
1,830 to 1,910 RPM
52
Oil Pressure, Low Idle
60 PSI min
53
Oil Pressure, Normal
90 to 135 PSI
54
Oil Pressure, Transient
40 to 200 PSI
55
Oil Temp, Min on Start
-40C
56
Oil Temp, Low and High Idle
-40 to 110C
57
Oil Temp, Takeoff and Max Cont
0 to 110C
58
Oil Temp, Max Cruise
10 - 99C
59
Oil Temp, Max Reverse
0 - 99C
60
Oil Temp, Max Transient
0 to 110C
| Values above 99C limited to 10 mins
61
Oil Temp, For fuel heater operations
55C min recommended
62
Oil, Capacity
15.25 US qts
| oil tank by itself 10 US qts
63
Oil, Normal Operating quantity
Full to 4 qts low
64
Fuel, Total
544 US Gallons
65
Fuel, Mains Quantity
386 US Gallons (193 each)
66
Fuel, Aux Tank Quantity
158 US Gallons (79 each)
67
Fuel, Max Imbalance
300 lbs HALO 250 Supps. Except single engine, then max 1,000 lbs
68
Fuel, Min for Takeoff
265 lbs a side
69
Fuel, Engine Driven Fuel Pump (High Pressure Pump)
Approx 800 PSI
70
Fuel, Engine Driven Boost Pump (Low Pressure Pump)
30 PSI
71
Fuel, Standby Boost Pump
30 PSI
72
Fuel, Pressure light comes on at
10 PSI +/- 1 PSI
73
Battery Description
24v, 42Ah Lead Acid
74
Volts, Min Battery Start
23 volts
75
Volts, Min for GPU Start
20 volts
76
External Power Cart Limits
28.0v - 28.4v
1,000 amps momentary
300 amps continuous
77
Generator Volts and Amps
28.25 +/- 0.25 vDC, 250 Amps
78
Generator Amps
250 Amps
79
Current Limiter Amps
325 Amps
80
Gen Load limits, Altitude
Up to 31,000' - 100%
Above 31,000' - 88%
Ground operations - 85 %
81
GCU Does These Main Things:
PVCROD
P- paralleling, load equalization
V- voltage regulation, maintains 28v
C- cross start protection, protects current limiter by limiting gen output
R- reverse current protection, opens line contactor if a gen voltage drops low
O- over voltage protection,
D- differential voltage protection
82
Current protecting types
60 amp limiter (Current Limiter)
70 amp diode
50 amp circuit breaker
83
Number of Electrical Buses
16 on diagram QRH (17 if you count furnishings bus)
```
Ground ops bus
Hot bat bus
Main battery bus
Isolation bus
Left generator bus
Right generator bus
SFDS bus
1-4 dual fed bus
1-3 avionics bus
1 and 2 subpanel bus
```
84
Engine Model
PT6A-52
85
Starter Duty Cycle Limits
40 sec on, 60 sec off
40 sec on, 60 sec off
40 sec on, 30 mins off
86
Compressor Stages
3 axial-flow
| 1 centrifugal
87
Turbine Stages
Compressor (gas generator) turbine: Single stage axial flow reaction turbine
Power turbine: two stage axial flow reaction turbine
88
Bleed valves close approx
Hi: 92%
Low: 64%
89
Auto ignition lights go out at
Approx 400 ft-lbs
90
Weight, Max Takeoff
13,420 lbs HALO 250
| 14,000 lbs HALO 275
91
Weight, Max Landing
12,500 lbs HALO 250
| 13,500 LBS HALO 275
92
Weight, Max Ramp
13,510 lbs HALO 250
| 14,090 lbs HALO 275
93
Weight, Max Zero Fuel
11,500 lbs HALO 250 and 275
94
Weight, Max Wing Lock Max
300 lbs each, 20lbs/sq foot
95
Weight, Max rear baggage
AFM
550 lbs
Med Gear 1 - 340 lbs
Med Gear 2 - 210 lbs, 80 lbs per shelve
96
Weight, Max Upper medical gear rails
60lbs, 15 lbs pre 25 inches
97
Weight, Max Arch
25 lbs
98
Engine Anti-ice Limits
Can be open up to ISA +27° up to 13,650’ on ground or air. Above 13,650’ ISA + 15° max or close them. Watch oil temps closely.
99
Cruise Power Company
Torque 2,000 ft-lbs
Prop 1,700 rpm
ITT 775C
Fuel Flow 350 PPH
100
Max Operating Altitude
35,000'
101
OAT, Max up to FL250, above FL250
ISA +37C, above FL250 ISA +31C
102
OAT, Max above FL250
ISA +31C
103
Flight Load Factor Limit, G force
HALO 250
Flaps up: -1.25 to +3.12
Flaps Down: 0.0 to +2.0
HALO 275
Flaps up: -1.24 to +3.10
Flaps Down: 0.0 to +2.0
104
Crosswind, Max Demonstrated
25 KIAS
105
Gear Cycle Limits
1 Cycle every 5 mins, max 6 cycles. After 6 cycles a 15 min cool down is required
106
Size, Total Length
43' 10"
107
Size, Total width
57' 11" with winglets
108
Size, Aircraft height
Approx 15'
| 14' 10"
109
Size outer turning radius
41' 7"
110
Cabin Pressure, Max differential
Max 6.6 PSI (Normal 6.5 PSI +/- 0.1)
111
Duct over temp light comes on at:
300 F
112
Pneumatics, Normal System Pressure
12 - 20 PSI
113
Suction hi/low limits. Up to 15,000' and 15,000 to 35,000'
Sea level to 15,000' 4.3 to 5.9 Hg
| 15,000' to 35,000' 2.8 to 4.3 Hg
114
Pneumatics, Max Pressure
20 PSI
115
Temp, Lowest for de-ice boot operation
-40C
116
PSI Delta P switch
60 PSI
117
Bleed air waring comes on when
Rupture in line by temp exceeding approx 204F
118
Prop de-ice time to hold manual switch
90 seconds, ground school
Approx 45 sec. 5 blade supps
119
Prop amp meter should show a flicker to show switching sides approx _____ seconds
Every 90 seconds
120
Prop heat using manual, DC loadmeter should show how much increase to verify function
Approx 0.5% increase per meter
121
Prop Amp range
4 blade: 18-24 amps
122
Wind, Max Headwind Component Limit
Do not extrapolate for a headwind that exceeds 30 KIAS. Assume a 30 knot headwind when correcting takeoff field length whenever there is a 30 knot or greater headwind
123
Wind, Max Tailwind Component
Max for landing and takeoff 10 KIAS
124
Wind, Max Crosswind and Tailwind for coupled approach
Crosswind 16 knots
| Tailwind 10 knots
125
Surface De-ice, hold for how long in manual
6 seconds
126
Occupancy Max
11 including pilots
127
Brake de-ice Limits
Do not operate above 15°C
128
Altitudes, Auto Pilot mins
After takeoff 400'
Cruise 1,000'
Approach 79'
129
Altitudes, Normal Operations Max
35,000'
130
Altitudes, Yaw Damp Inop
17,000’
If duel strakes installed, no limit
131
Altitudes, on Aviation Gas
Operating Altitude - 31,000'
Either Standby Fuel Pump Inop - 20,000'
No Crossfeed Capability - 20,000'
132
Avionics For Takeoff?
ADS 1 and 2
AHS 1 and 2
PFD and MFD
Baro Settings
ADS 1 and 2 Must be operational for takeoff
AHS 1 and 2 Must be operational for takeoff
PFDs and MFD Must be operational for takeoff
Baro Settings must be in Sync for flight
133
Electric Heater Must be ______ for takeoff
Off for at least 2 mins prior to and during engine start.
| Should not be operated with pedestal floor outlet blocked or cockpit door closed
134
Squawk codes
7600 - comm failure
7700 - in-flight emerg
7500 - hijacking (switch to 7700 for immediate assistance)
135
Departure procedures meet obstacle clearance requirements and are based on the premise that on departure an aircraft will: (3)
* cross at least 35 feet above the departure end of the runway;
* climb on runway heading to 400 feet AAE before turning; and
* maintain a climb gradient of at least 200 feet per NM throughout the climb to the minimum altitude for enroute operations.
(depart uncontrolled airports RAC 7.9)
136
Distance between runway edge lighting
Max of 60m (200 feet)
1/2 mile is 2,600'
13 runway lights is 2,600'
1/4 mile is 1,200'
6 runway lights is 1,200'
137
Obstacle Clearance Mountain Regions
Region 1 and 5 - 2,000' and 5 miles
Region 2,3, and 4 - 1,500'
(RAC 8.5)
On Designated Airways and Air Routes, IFR flights may be operated at the published MEA/MOCA except that in winter when air temperatures may be much lower than those of the International Standard Atmosphere (ISA), aircraft should be operated at an altitude which is at least 1000 feet higher than the published MEA/MOCA.
CAUTION: The combination of extremely low temperatures and the effect of Mountain Waves may result in an altimeter over-reading by as much as 3000 feet. For further details, see “Pressure Altimeter”, published in the TC AIM, AIR Section.
138
Aircraft Category, Spec Vis SM
```
Aircraft Category. SPEC VIS (SM)
A - 1
B - 1.5
C - 2
D - 2
```
139
Aircraft Category, Speeds
```
A - Up to 90 knots
B - 91 to 120 knots
C - 121 to 140 knots
D - 141 to 160 knots
E - Above 161 knots
```
(RAC 9.21)
140
Aircraft Category, Circling Arc
```
A - 1.3
B - 1.5
C - 1.7
D - 2.3
E - 4.5
```
(RAC 9.23)
Approaches using expanded circling approach areas can be identified by the presence of the "C" symbol on the circling line of minima. (RAC 9.23.2)
141
TC. Hold Speed Limitation Max
Up to 6,000' - 200 knots
Above 6 000 ft up to and including 14 000 ft - 230 knots
Above 14 000 ft - 265 knots
142
RVSM Requirements
a) Before entering RVSM airspace, the status of required equipment should be reviewed. The following equipment should be operating normally:
(i) two independent altitude measurement systems;
(ii) one automatic altitude control system; and (iii) one altitude alert system.
b) The pilot must notify ATC whenever the aircraft:
(i) is no longer RVSM-compliant due to equipment failure; (ii) experiences loss of redundancy of altimetry systems; or (iii) encounters turbulence or mountain wave activity that
affects the capability to maintain the cleared flight level.
(RAC 11.7.4)
143
TC. Aircraft Speed Limit. Below 10,000'. Below 3,000' AGL and 10 NM
According to CAR 602.32, no person shall operate an aircraft in Canada:
a) below 10 000 ft ASL at more than 250 KIAS; or
b) below 3 000 ft AGL within 10 NM of a controlled airport and at more than 200 KIAS, unless authorized to do so in an air traffic control clearance.
(RAC 2.5.2)
144
Minimum Oxygen Requirements (Comm 4.11)
All crew members and 10 per cent of passengers and, in any case, no less than one passenger
(a) Entire period of flight exceeding 30 minutes at cabin-pressure-altitudes above 10,000 feet ASL but not exceeding 13,000 feet ASL
(b) Entire period of flight at cabin-pressure-altitudes above 13,000 feet ASL
(c) For aircraft operated in an air transport service under the conditions referred to in paragraph (a) or (b), a period of flight of not less than
(i) 30 minutes (Note 2), and
(ii) for flight crew members, two hours for aircraft the type certificate of which authorizes flight at altitudes exceeding FL 250 (Note 3)
(COMM 4.11.2)
145
Acceptable Deviations, Altitude
Enroute: 100' Above, 100' Below
| Mim IFR Alts: 100' Above, 0' Below
146
Acceptable Deviations, Airspeed
Briefed Approach Speed: 10 KIAS Above, 5 KIAS Below
| Vref @ 50 AGL: 10 KIAS Above, 0 KIAS Below
147
Acceptable Deviations, Vertical Speed
Enroute and Terminal Area: 3,000 FPM
Once Established on a published portion of an IAP: 1,500 FPM
FAF Inbound: 1,000 FPM
Unpressurized: 1,000 FPM
148
Acceptable Deviations, Glide Path
ILS/LPV/SCDA Approach: Half Dot Glide Slope Deflection
149
Acceptable Deviations, Track
GPS/VOR/LOC: Half Dot CDI Deflection
| NBD Approach: 5 degrees
150
Acceptable Deviations, Bank Angle
All Phases of Flight: 30 degrees or less
151
GPS scale enroute, terminal, approach
GPS enroute CDI FSD (Full Scale Deflection) is +/- 5 NM for a non WAAS GPS and +/- 2 NM for a WAAS GPS.
Terminal FSD is +/- 1 NM for both WAAS and non WAAS GPS.
2 NM to the FAF 0.3 NM
152
Max Flight Time days/hours
Comm 4.1.17 (2) medevac
7 days, 60 hours flight time
30 days, 100 hours flight time (on call)
90 days, 300 hours flight time
365 days, 1,200 hours flight time
153
Time free from duty (Comm 4.25.1)
Where the flight crew member is a flight crew member on call, one period of at least 36 consecutive hours within each 7 consecutive days or one period of at least 3 consecutive calendar days within each 17 consecutive days.
154
RVSM Required AC Equipment (4)+(1)
- 2 independent altitude measuring systems
- 1 secondary surveillance radar transponder with altitude reporting system that can be connected to the altitude measurement system in use for altitude keeping
- Altitude alerting system
- Automatic altitude control system. Max error 80 feet/25 meters and that the system must be able to hold altitude within 200ft/60m
- Preflight compare altimeters to know ground elevation, max error 75 feet
155
Glide Ratio
GlideRatio ........... 2.0 nautical miles for each 1000 feet of altitude. Decrease by 0.2 nautical miles for each 10 knots of headwind.
