Q400 Limitations Flashcards
(124 cards)
0
Q
Vmo - 10,000’
A
282 kts
1
Q
Vmo - 8,000’
A
245 kts
2
Q
Vmo - F180
A
286 kts
3
Q
Vmo - F200
A
275 kts
4
Q
Vmo - F250
A
248 kts
5
Q
Starting Limits
A
Start 1 - 70 sec on - 2 mins off
Start 2 - 70 sec on - 2 mins off
Start 3 - 70 sec on - 30 mins off
6
Q
Maximum Number of Occupants
Flight Crew
A
2
7
Q
Maximum Number of Occupants
Observers?
A
1
8
Q
Maximum Number of Occupants
Observer?
A
1
9
Q
Maximum Number of Occupants
Cabin Passengers
A
74
10
Q
Maximum Number of Occupants
Infants?
A
6
11
Q
Maximum Number of Occupants
Total
A
85
12
Q
Weight Limit - Forward Baggage Compartment
A
413 kg
13
Q
Weight Limit - Aft Baggage Compartment 1
A
1724 kg
14
Q
Weight Limit - Aft Baggage Compartment 2
A
454 kg
15
Q
Weight Limit - Aft Baggage Compartment 1 and 2 Combined
A
1724 kg
16
Q
Manoeuvring Limit Load Factors
Flaps Retracted
A
+2.5 & -1.0 g
17
Q
Manoeuvring Limit Load Factors
Flaps Extended
A
+2.0 & -0.0 g
18
Q
Maximum Operating Altitude
A
25000 ft
19
Q
Maximum Operating Altitude for Take off and Landing
A
10000 ft
20
Q
Maximum runway slope for Take off and Landing
A
+/- 2%
21
Q
Maximum Temperature
A
+50 DegC or IAS +35 whichever is lower
22
Q
Ambient Temperature - Flight and Ground
Minimum Temperature
A
-54 degC
23
Q
Crosswind and Tailwind
Hard Dry Runway
A
32 kts crosswind - 10 kts tailwind
24
Crosswind and Tailwind
Contaminated runway
Stand Water, Slush or Loose Snow
14 kts crosswind - Nil Tailwind
25
Crosswind and Tailwind
Contaminated runway
Compacted Snow
20 kts Crosswind - Nil Tailwind
26
Setting takeoff power prior to brakes release, with the nose of the aircraft more than 45 deg out of the wind, is prohibited for wind speeds greater than:
8 kts
27
Vmca - Flap 0
113 kts
28
Vmca - Flap 5
98 kts
29
Vmca - Flap10
95 kts
30
Vmca - Flap 15
91 kts
31
Vmcl - Flap 5
100 kts
32
Vmcl - Flap 10
99 kts
33
Vmcl - Flap 15
96 kts
34
Vmcl - Flap 35
92 kts
35
Vmcg
Flap 5, 10 & 15 - 89 kts
36
Manoeuvring Speed (Va)
204 kts
37
Turbulence Penetration Speed (Vb)
210 kts
38
Max Flap Extension Speed
Flap 5
200 kts
39
Max Flap Extension Speed
Flap 10
181 kts
40
Max Flap Extension Speed
Flap 15
172 kts
41
Max Flap Extension Speed
Flap 35
158 kts
42
Max Landing gear Operation Speed (Vlo) - (Gearspeed)
200 kts
43
Max Landing gear Extended Speed (Vle)
215 kts
44
Max Tyre Speed
182 kts
45
Max tq - MTOP
106%
46
Max Tq - NTOP
90.3% (90 or 91 indicated)
47
Max Tq - Transient
135% (20 sec max)
48
Max Tq - Reverse
35%
49
Max Tq - Max Continous
100%
50
Max ITT - MTOP
880 degC
51
Max ITT - NTOP
822 degC (varies with temp -check graph)
52
Max ITT - Max Continous
880 degC
53
Max ITT - Starting
920 degC
54
Max ITT - Transient
920 degC
55
Max ITT - Reverse
880 degC
56
Max Np
MTOP, NTOP, Max Cont, and Max Reverse
| 1020 rpm
57
Max Np - Transient
1173 rpm
58
Max Continuous Np overspeed
1071 rpm
59
Oil Press PSID
MTOP, NTOP, Max Cont, and Max Reverse
61 to 72 psi
60
Oil Press PSID - Starting
100 psi Max
| 165 psi, discing with oil temp < 0 deg
61
Oil Press - Transient
44 to 61 psi
| 72 to 100 psi
62
Oil Temp
| MTOP, NTOP, Max Cont, and Max Reverse
0 to 107 degC
63
Min Oil Temp
| Starting
-40 degC
64
Max Oil Temp - Transient
125 degC - 5 sec max for torque values above flight idle and less than 55%
65
Ground operations with wind speeds greater than 50 kts must:
be reported to maintenance within 24 hrs
66
Max power setting for Ground Static Operation with 36 to 50 kts (gusts to 55 kts)
Disc
67
Hyd Qnty for dispatch
System 1, 2 and 3 - 50%
68
Min Dispatch - O2
| Crew Fixed System
1300 psi
69
Min Dispatch - O2
| Cabin Crew Supp O2 - 121 lt
1600 - 1800 @ 21 deg
70
Min Dispatch - O2
| Supp O2 - 311 lt
1600 psi at 21 degC
71
Normal Press Differential Limit
5.46 psi
72
Max Press Differential Limit
5.95 psi
73
Max Cabin Press Differential Limit during Taxiing, Take-off and Landing
0.5 psi
74
Max Cabin Alt (for pressurised flight)
8000 ft
75
Max Tyre Pressure - Main Wheels
140 psi
76
Max Tyre Pressure - Nose Wheels
92 psi
77
The Crew Fixed Oxygen system is capable of supplying at least _____ min of protective breathing O2 to each crew member
15
78
Gravity refuelling is not permitted when:
the APU is running
79
Continuous operation of the APU throughout the refuelling process, requires:
sufficient fuel in the left main fuel tank
80
The fuel truck must be parked at least ______ mt ( _____ ft) from the APU exhaust outlet
9.2 mt (30 ft)
81
In the case of fuel spillage at the adaptor or the fuel tank vents:
refuelling must be stopped immediately
82
At ports not accustomed to refuelling Dash8 aircraft:
the re-fueller must be advised that the APU will be running.
83
Pressure Error Correction (PEC) for a precision approach is
20 ft
84
Max battery load meter reading for take-off is
0.1
85
Min battery temperature for take-off is?
-20 degC
86
When Ice is detected the AIRFRAME MODE selector must
be positioned to FAST or SLOW
87
During auto pilot operation, a pilot must:
be seated at the controls with seat belts fastened
88
In severe Icing conditions, the autopilot:
must be disengaged
89
In APP mode, use of the VOR without:
associated DME is not permitted
90
With one engine inoperative, the Autopilot must be disengaged:
prior to extension of the landing gear or 1000 ft, whichever occurs first
91
Autopilot and Flight director only approaches are approved for glideslope angles of:
2.5 to a max of 4 deg
92
On approach the autopilot must be disengaged by ______ ft above runway elevation
200
93
After take off or go-round, the minimum height for autopilot engagement is
1000 ft agl
94
The AFCS is approved for autopilot approaches to:
CAT 1 limits only
95
Unless the baggage compartments are empty, the aircraft must not be operated more than:
1 hours flight time from an airport suitable for landing.
96
When the ADF is used as the prime means of navigation or for confirming position, use of the:
HF transmitter is prohibited!
97
What distance = 1 hr flight time with OEI
276 nm
98
With the Integrated Standby Instrument fitted, what is the maximum fight duration that can be flown from a airport suitable for landing?
1 hr flight time
99
The DHC8 Model 402 is eligible for _____ and _____ VFR, _____ and operation in_______ _______
day and night, IFR, icing conditions
100
Minimum Flight crew is
Two pilots
101
The Engine Model in the Q400 is
Pratt and Whittney - PW 150A
102
Minimum operating Temperature is
-54 degC
103
Maximum airstart altitude is
20000 ft
104
Automatic Take-offpower uptrim is?
10% tq (nominal)
105
Maximum Torque for ground operations is?
100%
106
Minimum NH is?
64.2 %
107
With wind speeds of 36 to 50 kts (gusts of 55 kts) and the nose of the aircraft more that 30 deg out of the wind, the max pwr setting is
Disc
108
With wind speeds of 21 to 35 kts and the nose of the aircraft more that 30 deg out of the wind, the max pwr setting is
flight idle
109
With wind speeds of 9 to 20 and the nose of the aircraft more that 30 deg out of the wind, the max pwr setting is?
60 deg PLA
110
Minimum SAT for engine relight is
-40 degC
111
What inflight operation of the power levers is prohibited
aft of the FLT IDLE gate
112
Q400 total usable fuel?
11724 lbs / 5318 kg
113
Max Fuel imbalance
600 lbs / 272 kg
114
The AUX pumps must be ON for?
Take off and landing.
115
Continuous operation with the fuel heater outlet temperature indication:
below 0 degC and above 71 degC is prohibited
116
Fuel weights are based on a specific gravity of:
0.795 at 15 degC
117
The engine Intake bypass doors must be ______ for engine operation in icing conditions
open
118
During ground operations in icing conditions the _______ _______ and the _______ _______ _______ must also be on
pitot static and the stall warning heat
119
The max permitted WED of contaminate is?
15 mm
120
The maximum permitted depth of contaminant is?
60mm
121
For WED greater then 3mm:
Power levers aft of disc is prohibited
122
Minimum oil temp to ensure engine inlet ice protection is?
55 degC
123
Minimum oil temperature required to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power, is?
65 degC
