Limitations Flashcards
(107 cards)
0
Q
MLW 300
A
42000LBS
1
Q
MLW 200
A
34500LBS
2
Q
MTOW 200
A
37300LBS
3
Q
MTOW 300
A
43000LBS
4
Q
Max Ramp Weight 200
A
37500LBS
5
Q
Max Ramp Weight 300
A
43200LBS
6
Q
Gear Operating Speed 200
A
158KTS
7
Q
Gear Operating Speed 300
A
163KTS
8
Q
Max Operating Speed @ 0-14,000’ 200
A
242KTS
9
Q
Max Operating Speed @ 15,000’ 200
A
239KTS
10
Q
Max Operating Speed @ 20,000’ in a 200
A
223KTS
11
Q
Max Operating Speed @ 25,000’ in a 200
A
207KTS
12
Q
What kinds of operations is the Dash 8 eligible for?
A
Day/Night VFR IFR Ops in icing conditions
13
Q
MZFW for the 200
A
32000LBS
14
Q
MZFW for the 300
A
39500LBS
15
Q
Max Operating Speed @ 0-17,000’ in a 300
A
243KTS
16
Q
Max Operating Speed @ 20,000’ in a 300
A
232KTS
17
Q
Max Operating Speed @ 25,000’ in a 300
A
214KTS
18
Q
Manoeuvring Speed in a 200
A
164KTS
19
Q
Manoeuvring Speed in a 300
A
177KTS
20
Q
Caution associated with Va
A
Rapid and large alternating control inputs in combination with changes in pitch, roll or yaw may result in structural failure at any airspeed, even below Va
21
Q
Vturb - 200
A
180KTS
22
Q
Vturb -300
A
190KTS
23
Q
Vfe F15 - 200
A
148KTS
24
Vfe F15 - 300
150KTS
25
Vfe F35 - 200
130KTS
26
Vfe F35 - 300
138KTS
27
Gear Extended Speed - 200
172KTS
28
Gear Extended Speed - 300
173KTS
29
Max Speed with Gear Doors Open (Alternate Gear Extension)
140KTS
30
Max Crosswind
36KTS
31
MTOP 200 Tq / ITT / Np / Oil Px / Oil Temp Are there any limits to this setting
107.5% (max 111%) 800°C 1212RPM 55-65psi 45-115°C Yes, 5 mins
32
MTOP 300 Tq / ITT / Np / Oil Px / Oil Temp Are there any limits to this setting
100% (max 105.6%) 800°C 1212RPM 55-65psi 45-115°C Yes, 5 mins
33
NTOP 200 Tq / ITT / Np / Oil Px / Oil Temp
99.5% (includes 2% static increase) Inflight limit is 97.5% 770°C 1212RPM 55-65psi 45-115°C
34
NTOP 300 Tq / ITT / Np / Oil Px / Oil Temp
92% (includes static increase of 2%) Inflight limit is 90% 765°C 1212RPM 55-65psi 45-115°C
35
MCP 200 Tq / ITT / Np / Oil Px / Oil Temp
97.5% for 1200Np 114.2% for 1024Np or lower 800°C 1212RPM 55-65psi 45-115°C
36
MCP 300 Tq / ITT / Np / Oil Px / Oil Temp
90% for 1200Np 96% for 1125Np or lower 800°C 1212RPM 55-65psi 45-115°C
37
Starting Limits (With reference to Temp)
\> 800°C - 20secs 840-900°C - 12secs 900-950°C - 5secs
38
Max Oil Px on starting
200psi
39
Min Oil Temp for Starting
-40°C
40
Transient Power - 200 How long is this allowed?
125% 840°C 1320RPM 200psi 125°C 20secs
41
Transient Power - 300 How long is this allowed?
115% 840°C 1320RPM 200psi 125°C Limited to 20secs
42
Max Reverse - 200
90% 770°C
43
Max Reverse - 300
90% 765°C
44
Oil Px Limits
Normal: 55-65psi Abnormal: 40-55psi (if Nh is BLW 75%) \<40psi requires shutdown
45
Oil Temp Limits
Normal: 45-115°C Abnormal: 115-125°C limited to 20mins
46
Prior to unfeathering the propeller and for power settings above flight idle, what is the minimum oil temp?
0°C
47
What is the minimum oil temp for adequate inlet splitter anti-icing?
45°C
48
Starter Cranking Limits
1: 1min on / 2min off 2: 1min on / 2min off 3: 1min on / 30min off
49
What is the normal range for the propeller?
780-1212RPM
50
What is the propeller restricted range?
500-780RPM
51
What is the Maximum refuelling Px?
50psi
52
What actions must be taken when refuelling is taking place and people on board?
Turn off the fasten seat belt signs Turn off Wx radar Do not transmit on HF SATCOM de-powered Cabin lights illuminated Emergency lights armed Do not start the APU
53
What is the useable fuel in the Mains / Auxs and Cabin Tanks?
5678LBS (planned 5400LBS) 4566LBS (planned 4400LBS) 1500LBS per 2xTanks
54
Maximum main tank fuel imbalance
600LBS
55
Maximum fuel temperature?
57°C
56
Minimum fuel temperature for takeoff
11°C
57
What are the notes associated with the Auxillary tanks? (There are 3)
1: Main tanks must be full prior to refilling Aux tanks 2: Aux fuel transfer not permitted during takeoff 3: Fuel XFR from Aux to Mains should be commenced immediately ATO
58
At what quantity in the Aux tanks can Cabin fuel XFR be started
1400LBS
59
Minimum HYD QTY for dispatch
No 1: 1.5QTS No 2: 3.0QTS
60
What is the time limit for operation of the PTU in a non-ARPS aircraft Why
5mins The hydraulic circuit in a non-ARPS aircraft is very small and therefore prone to overheating of the fluid
61
Min dispatch Px for the Sick Pusher
0°C - 940psi 20°C - 1000psi 40°C - 1060psi
62
Min dispatch Px for O2
2 crew - 1300psi 3 crew - 1800psi Cabin portable - 1100psi
63
How long should protective breathing equipment supply O2
20mins
64
Tyre Px - 200
Nose: 102psi Mains: 94psi
65
Tyre Px - 300
Nose: 62psi Mains: 101psi
66
Max operating ambient temperature for ops and APU
48.9°C or ISA+35 whichever is lower
67
Minimum operating temperature
- 54°C
68
APU Starter Cranking Limits
Same as Engines
69
After a failed APU start attempt, how long is the APU automatically disabled for?
2mins
70
What is the recommended period between APU starts Why
5mins Allows excess fuel to drain
71
Limitations of the AFCS (11) DOG CHES BEEF
1: Use of VOR w/out DME is not permitted in NAV & APP mode 2: The AP must not be manually overpowered 3: AP & FD approaches are approved for angles of 2.5°-4°. G/S angles \> 3° approved for F15 only 4: Approved for CAT I only 5: With AP engaged, the pilot must be seated at the controls with seatbelt fastened 6: An AP APPR must not be commenced with an engine inop 7: AP must be disengaged in severe icing 8: AP BCS APP not permitted 9: Min height for AP engagement is 1000' 10: AP must be disengaged by 200' ABV RWY elev 11: APP mode is not permitted with: F35 F5 with AP engaged BLW 1500' F0 with AP engaged BLW 500'
72
Limitations of the DC On the ground In the air
Ground: 0.7 Air: 1.0
73
Limitations of a TRU Ground Air
Ground: 1.0 Flight: 1.0
74
AC Generator Limitations
Ground (up to 10°C) - 1.0 Ground (above 10°C) - 0.33 Flight - 1.0
75
Inverter Limitations
Ground and Flight - 1.0
76
EFIS Limits
1: ILS not permitted when in composite 2: Primary radar display must be monitored during flight conditions that require the radar 3: OM for the EFIS must be carried on the aircraft 4: If aircraft is only fitted with 1x DME, selecting #2 VOR in MAP mode is prohibited
77
Ditching Dam Px
1400psi @ 21°C
78
Load Factors Flap 0 Flap Extended
0 - +2.5g / -1.0g Extended - 2.0g / 0.0g
79
Max Operating Altitude
25,000'
80
Max Altitude for Takeoff and Landing
10,000'
81
Maximum RWY slope
+/- 2%
82
Maximum downwind component
10KTS (measured at a height of 10m)
83
Continuous operation with fuel heater outlet temperature indication of what is prohibited
Below 11° C or above 57° C
84
Engine and Prop ground operating limitations
Max Tq 92.5% Max Tq with propeller feathered 48% Min NH - 66% Propeller continuous operation between 500 and 780 rpm is prohibited. Extended operation with propeller rpm in excess of 780 must only be carried out with airplane headed directly into wind.
85
Max Altitude with gear and flap extended
15,000'
86
Max tyre speed
165KTS
87
Normal Cabin Diff
5.5 +/- 0.3psi
88
Max Cabin Diff
5.95psi
89
Max Cabin Diff for Taxi/Takeoff/Landing
0.5psi
90
Max Cabin Altitude
8000'
91
Definition of Icing conditions
Icing conditions exist when the SAT on the ground and for take-off is 10°C or below, or SAT in flight is 5°C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). Icing conditions also exist when the SAT on the ground and for take-off is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
92
Limitation for use of HF
With HF Comm installed, use of the HF transmitter is prohibited when the ADF is used as the prime means of navigation or for position confirmation.
93
Max tyre speed
165KTS
94
Normal Cabin Diff
5.5 +/- 0.3psi
95
Max Cabin Diff
5.95psi
96
Max Cabin Diff for Taxi/Takeoff/Landing
0.5psi
97
Max Cabin Altitude
8000'
98
Definition of Icing conditions
Icing conditions exist when the SAT on the ground and for take-off is 10°C or below, or SAT in flight is 5°C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). Icing conditions also exist when the SAT on the ground and for take-off is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
99
Limitation for use of HF
With HF Comm installed, use of the HF transmitter is prohibited when the ADF is used as the prime means of navigation or for position confirmation.
101
Max Takeoff Power (MTOP) limit
5mins
102
Transient time limits
20secs
103
Max Tq with the prop feathered
57%
104
Minimum flight idle Nh
66%
105
Wet RWY limitations
All the following are prohibited \* Takeoff with 0°F \* Antiskid inop \* Unpaved/Gravel RWY \* Auto Fx inop \* Any downwind component
106
Engine - 300
PW123E 2140 with up trim of 2380 SHP
107
Engine - 200
PW123D 1950 with up trim of 2150 SHP
