Limitations Flashcards
(103 cards)
1
Q
Max Taxi Weight
A
29,300
2
Q
Max TO Weight
A
29,000
3
Q
Max Landing Weight
A
28,500
4
Q
Max Zero Fuel Weight
A
26,500
5
Q
Cargo 1
A
1125
6
Q
Cargo 2
A
850
7
Q
Cargo 1 and 2 Total
A
1725
8
Q
Usable Fuel
A
5690
9
Q
Max Fuel Imbalance
A
200
10
Q
TO Power + APR or Go Around
TRQ% and ITT Deg C
A
TRQ 107
ITT Deg C 940
11
Q
Max ITT Temp time at 940 Deg C
Max ITT Temp time at 950 Deg C
A
Time at 940 Deg C is 5 mins
Time at 950 Deg C is 2 mins
12
Q
TO Power TRQ% and ITT Deg C
A
100
917 (927)
13
Q
Max ITT time at 917 Deg C is
Max ITT time at 927 Deg C
A
5 mins
2 mins
14
Q
When can normal TO ITT be exceeded
A
IAW Supplement 24
15
Q
Max Continuous (OEI) TRQ% and ITT Deg C
A
100
940
16
Q
Transient except TO TRQ% and ITT Deg C
A
112
965
Max 12 Secs
17
Q
Max ITT time at 965 Deg C
A
12 sec
18
Q
Engine Start Max ITT Deg C
A
965
19
Q
Engine Anti-Icing will be turned on when
A
SAT or OAT +10 Degrees C or colder AND Visible moisture OR Standing water, slush, snow on ramps, taxiways or runways
20
Q
After leaving Icing conditions, how long must Anti-Ice must be left on
A
At least 5 mins
21
Q
Wing and Stab Deicing Boots are turned on when
A
SAT or OAT +5 Degs C or colder with visible moisture present OR the uncertainty of ice accumulation OR Any amount of ice observed on any part of the aircraft
22
Q
Wing and Stab Boots may be used below ______ feet above TO field elevation only at the first sign of ice
A
400 feet
23
Q
If SAT is below _____ Degs C only use _____ if ice is observed on aircraft
A
-40 Degs C
boots
24
Q
Deicing boots can be turned off if
A
OAT or SAT of +5 Degs C and no ice on wipers and NO moisture with 3 cycles (9 mins) to be completed after leaving visible moisture. Time may be shortened to complete boot inflation before landing flare or if entering SAT below -40 Degs C
25
Prop Deicing is turned on when SAT or OAT Degs C is
-5 Deg C and below with visible ice accretion
26
Prop Deicing Norm Selection:
| Temps
-5 to -12 Degs C
27
Prop Deice Max Selection:
| Temps
- 13 or colder unless vibration occur at warmer temps
| * Use caution in MAX mode as runback ice may occur
28
Flap 7 or 15
175 KIAS
29
Flaps 20
165KIAS
30
Flaps 35
140 KIAS
31
Max Flap Altitude
14,000'
32
Max Landing Gear Retraction VLOR
150 KIAS
33
Max Landing Gear Extention VLOE
200 KIAS
34
Max Landing Gear extended VLE
200 KIAS
35
Max Landing Gear Emergency Extention VLOEE
200 KIAS
36
VMO to 16,000 feet
| VMO at 25,000 feet
250 KIAS
210 KIAS
*May not be deliberately exceeded in flight
37
Max VA
180 KIAS
| *Full deflection and maneuvers near critical angle of attack must be performed below VA
38
Define VMM (min maneuvering speed)
Min speed used for maneuvering portion of approach or departure, weight dependent speed required to maintain 1.3 Vs margin at 30 degs bank
39
Vmm Flaps 0 degree
Vref 20+30
| Vref 35+35
40
Vmm Flaps 7
Vref 20+20
| Vref 35+25
41
Vmm Flaps 15
Vref 20+15
| Vref 35+20
42
Vmm Flaps 20
Vref 20+10
43
Vmm Flaps 35
Vref 35+10
44
Prior to reaching Vmm do not exceed___ degrees of bank
15 Degrees
45
Max Rough Air Penetration Speed
190 KIAS up to 21,000 feet, ISA above this altitude, reduce speed as indicated by the VMO pointer by 30 KTS
46
Flaps Retracted Load Factor
+2.75 to -1.0
47
Flap Extended Load Factor
+2.0 to +/-0.0
48
Wheel Braking cooling limits, abort/ Normal Braking
Contact dispatch and inform them of the abort with no need for MX
15 Mins since RTO
49
Min Airspeed in Icing Climbing above MSA, Cruise, Descent, Holding and Approach (Flaps 0)
160 KIAS
50
Airport Pressure Altitude
-1000 to 8000 feet
51
Max TO and Landing Tailwind
10 KTS
52
Max Operating Altitude
25,000 feet
53
Use of Flight Director during TO
Is not authorized until gear handle is in the up position
54
Autopilot not Authorized
* Below 500 feet AGL or Acceleration Alt, whichever is lower
* Below 500 feet on Visual Approach
* Below 200 feet AGL on precision Approach
* Below 200 feet on Go Around
* Below MDA
55
Yaw Damper not Authorized for
Takeoff
Go-around
Landing
56
Windshield Wiper Speeds Low and High
Low Mode 130 KIAS
High Mode 160 KIAS Max
*Never Operate on Dry Windshields
57
Main Battery Temp
| No Battery Start
57 Degs C
58
Main Battery Temp
| No Cross Gen Start
61 Degs C
59
Main Battery Temp
| Max for TO
64 Degs C
60
Main Battery Temp
| Battery Hot Light
71 Degs C
61
High Energy Abort
* Make an entry in the logbook
* Contact Dispatch
* MX will determine the need for Inspection
62
Climb (no maneuvering)
VCLEAN +15
63
Climb (maneuvering) below Minimum Safe Altitude (MSA)
VMM+10
64
Climb above MSA, cruise,descent, holding, and Approach (Flaps 0)
160 KIAS
65
Corrected VREF
VREF+10
66
Final Approach (Maneuvering)
VMM+10
67
Missed Approach/Go Around below MSA
VREF+20
68
Starter Duty Cycle:(s)
Two start attempts with 3 minutes cooling between, then 25 minutes cooling before subsequent starts.
69
Motoring:
Three 30-second ventilations with 3 minutes cooling between each, then a one-hour cooling period before subsequent starts or motoring.
70
Time to light-off (from initial Ng rotation to ITT rise),
20 seconds maximum (for direct start operations only), and 10 seconds from introducing fuel to light off (for motoring start only).
71
Maximum time with engaged starter is ___ seconds of which max___seconds plain motoring.
70 sec
| 30 sec
72
BAT start is not allowed if the battery temperature is below
-20°C
73
Minimum voltage for any battery start is ___ volts.
24 volts
74
Minimum time between engine starts when starting subsequent engines is___minute. This applies to all start types. The___minute wait begins when the associated GEN light extinguishes following engine start and the subsequent engine start flow.
one min
| one min
75
Minimum oil temperature for engine start with type II oil is______. Mixing of Type I and II oils is allowed but not recommended.
-40ºC (-40ºF)
76
_____ and _____ switches shall be OFF and CLOSED during takeoff and landing in normal operation.
XFEED
| CONN VALVE
77
The FUEL TEMP LOW light must be____for takeoff
off
78
Fuel Temp, (°C) Operating Limits
min-40°C
max+43°C
max pressure altitude 31,000
79
Ice Speed function of Stall Warning System will activate when
Either Engine Anti-Ice switch is turned ON.
80
Runway Slope, Landing
-2% to +2%
81
Runway Slope, Takeoff
- 2% to +1.5%
82
Maximum Differential Pressure
7.5 psi
83
CABIN PRESSURIZATION
| Auto Mode Schedule
7.1 psi
84
Crosswind Takeoff and Landing
35 KTS
85
During initialization on ground the aircraft must not be moved. Takeoff is not permitted if:
1. If attitude difference between the attitude displayed on both EFIS EADls and the standby attitude indicator is three (3) degrees or more (bank and pitch).
2. If the heading on the compass card is slewing away from the aircraft heading.
86
Reverse taxi operations or power-backs are
STRICTLY PROHIBITED
87
Prop Normal operating range RPM is
1150-1396 RPM
88
Minimum Emergency Battery Temp for TO
-18 Degs C
89
Captain ONLY TO and Landing with less than 100 Hrs as FO
| CRAMVX
```
Contaminated RWY
RWY less than 5000 feet
Airports (Special)
MEL specifies
Vis less than 4000 RVR or 3/4 SM
Xwind exceeding 15kts
```
90
Captain ONLY TO and Landings
| WFBL
Winshear reported in vicinity
Flaps in 0 position
Breaking action less than good
Lower than standard TO mins
91
Max tire speed
165 kts
92
Icing conditions exist whenever:
| The outside air temperature (OAT) or static air temperature (SAT) is ___C or colder and:
+10°
1. There is any type of visible moisture present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, ice crystals), or
2. When on the ground, there is standing water, slush, or snow (hard packed snow excluded) on the ramps, taxiways, or runways
93
Minimum oil temp. for ground operations, and after Takeoff for maximum 5 minutes
25°C
94
Minimum Emergency Lighting Battery Temperature for takeoff
-18°C
95
Derivative Takeoff Power takeoffs are prohibited if any of the following conditions exist: (Reduced Power)
1. The Anti-Skid system is inoperative
2. CTOT inoperative
3. Wind shear
4. Tailwind
5. Contaminated RWY
6. De-icing fluid applied
96
In instrument conditions final configuration must be accomplished prior to reaching _________with the exception of circling approaches, single engine operations, or in order to comply with ATC speed restrictions.
the final approach fix
97
In visual conditions, final configuration must be accomplished no later than_____.
In visual conditions, final configuration must be accomplished no later than 500ft. AGL.
98
For single engine Nonprecision Approaches, final flaps will be delayed until
landing is assured
99
For circling approaches, final flaps will be selected when
leaving the MDA.
100
TO with Auto Coarsen INOP is
Not authorized on contaminated RWY
101
Reverse thrust is prohibited below
60kts
102
Standby pitot must be on______mins before TO
5 mins
103
Windshield heat must be on_____mins before TO
6mins
