Memory Items Flashcards
(69 cards)
1
Q
What is Vmo?
A
270 KIAS
2
Q
What is Mmo?
A
0.72 MI
3
Q
What is Va?
(maneuvering speed)
A
200 KIAS
4
Q
What is Vmca (Flaps UP)?
A
105 KIAS
5
Q
What is Vmca (Flaps TO/APPR)?
A
100 KIAS
6
Q
What is Vmcl (Flaps LDG)
A
95 KIAS
7
Q
What is Vfe (TO/APPR)
A
200 KIAS
8
Q
What is Vfe (LDG)?
A
160 KIAS
9
Q
What is Vle/Vlo?
A
200 KIAS
10
Q
What is Vsb/Msb
A
No Limit
11
Q
What is Vtire?
A
165 KTS (grondspeed)
12
Q
Maximum ITT for engine start?
A
556C
13
Q
Maximum ITT for engine idle?
A
860 C
14
Q
Allowable engine oil pressure range at idle?
A
15 to 47 PSIG
15
Q
Maximum ITT for maximum continuous thrust (MCT)
A
860C
16
Q
ITT range for takeoff thrust
A
860 - 885C
17
Q
Oil Pressure range foe takeoff
A
55 to 179 PSIG
18
Q
Tailwind limit for engine start
A
15 KTS MAXIMUM
19
Q
Ambient temperature limits for engine start
A
Minimum temp for engine start is -40C
20
Q
Starter limits (ground starts)
A
Starter Cycle
- 30 cesonds on, 30 seconds off
- 30 seconds on, 30 seconds off
- 30 seconds on, 30 minutes off
21
Q
Battery limits for ground starts
A
Minimum battery voltage… 23.5 volts
Minimum battery cold soak temp… -20C
22
Q
Generator limits
A
All operations….325 amps (continuous) each
23
Q
Maximum Ramp Weight
A
10,780 lbs
24
Q
Maximum Takeoff weight
A
10,700 lbs
25
Maximum Landing weight
9,960 lbs
26
Maximum Zero Fuel weight
8,900 lbs
27
Maximum FWD baggage compartment loading
200 lbs
28
Maximum AFT baggage compartment loading
400 lbs.
29
Minimum Flight Crew
1 pilot - must occupy left seat
must have:
* autopilot
* QRH
30
Maximum occupancy
1 pilot - 7 passenger
2 pilots - 6 passengers
31
Fuel Limitations - approved fuels
Approved fuels include JET A, JET A1, JP-8, PRC No. 3, Russion TS-1, premium grade, Ukraine TS-1
32
Fule Limitations - temperatures
-40C to 60C
33
Fuel Limitations - max. imbalance
100 lbs.
34
TO & Landing limits - surface
smooth, hard, paved only
35
TO & Landing limits - slope
+/- 2%
36
TO & landing limits - airfield pressure altitude
-1,000 to 10,000 feet
37
TO & Landing limits - Ambient temperature
-40C to +40C at sea level
38
TO & Landing limits - tailwind
10 knots
39
TO & Landing limits - crosswind
20 knots HARD LIMIT
40
Maximum altitude during single engine bleed operations
25,000 feet
41
Maximum altitude during single cabin inflow operations
25,000 feet
42
Cabin pressurization limits
* Max Differential - 9.0 PSID
* Max diff for landing - 0.3 PSID
43
External power limits
* MINIMUM 27.0 volts DC
* MINIMUM of 1,000 amps momentarily and 300 amps continuous
44
Cold weather operations for cabin/cockpit
Warm to at leaast -15C prior to takeoff if aircraft has been cold-soaked
45
Cabin/Cockpit conditions for flight
* O2 supply adequate for intended flight
* each pilot's onside audiio must be on if headsets are not worn
46
SafeTaxi & SurfaceWatch
Advisory only - not to be used for ground maneuvering
47
Weather Radar
* Do not operate on ground near ground crew
* Remain outside safe operating zone of 11 feet from antenna
48
Synthetic Vision System
Advisory only - cannot be used for navigation
49
TCAS
* Can deviate from ATC clearance for RA
* Manuevers based on TA or traffic information are not authorized
50
TAWS
Advisory only - cannot be used for navigation or terrain clearance
51
Autopilot
DO NOT manually override the AP
Min Use Heights;
* climb, enroute, or descent: 500 ft AGL
* Approach:
* Visual and non-precisions: 200 ft AGL
* Precision: 100 ft AGL
52
Yaw Damper
* Must be dsengaged for taxi, TO, and landing
* Shall be engaged in flight except ar required for TO/LDG
* Minimum use height is 50 ft AGL
53
Kinds of Operation
* VFR day and night
* IFR day and night
* RVSM
* KNown icing
54
Maximum Pressure Altitude
43,000 feet
55
Maximum altitude for landing gear extension
18,000 feet
56
Maximum altitiude for flap extension
TO/APPR...18,000 feet
LDG...18,000 feet
57
The following must be checked and operational
* Pitch trim systems - normal and standby
* Stall warning system
* Fire detection and suppression
* Switchlights
* Cockpit speakers
58
RVSM airspace requirements
* autopilot
* altitude alerting system
* ADC 1 and 2
* Pilot and copilot PFD
* Transponder 1 or 2
59
Icing limitations for ground operations
visual and tactile check required prior to TO in ground icing conditions
OAT of 5C or less or either L or R wing fuel temp cannot be determined above 0C with:
visible moisture
exposed to visible moisture since previous landing
Temp/Dewpoint spread less than 3 degrees
Water on the wing
atmospheric condisitons condusive to frost/freezing
60
Icing lmitations - ground operations
## Footnote
Take off limits
TO prohibited with any ice, snow, sluch or frost adhering to critical areas:
wings and winglet, horizontal or vertical stab, flaps and controls surfaces, engine inlets and pylons, air data probes, windshield, fuel vents, landing gear
61
Icing limitations - ground operations
Wing AI must be ON for TO in ground icing conditions
62
Icing limitations - ground operations
Approved de/anti ice fluids
Deicing - Type I and II
Anti-icing - Type IV
63
Icing limitations - ground operations
Engine AI must be on....
Enigne AI must be on in visible moisture when:
SAT is 5C to -40C
64
Icing Limitations - flight ops
Wing AI must be NORM for all operations except,
ON for TO in icing conditions
ON above FL 340 in icing conditions unless temp is below -40C
65
Icing conditions - autopilot use
Use of AP prohibited in icing conditions
66
Icing conditions - minimum thrust
Minimum thrust setting of 62% N1 except as low as 50% N1 in descent or deceleration for less than 5 minutes
67
Icing conditions - minimum speed
Minimum speed of 180 KIAS except as required for TO, APPR, and LDG.
68
Icing limitations - Flaps and LDG Gear
Remain retracted in icning conditions except for TO, APPR, LDG.
Retraction of flaps after icing encounter prohibited unless confirmed free of ice.
69
Icing limitations - wing inspection lights
Must be operable prior to fliht in known icing conditions
