Limitations Flashcards
(123 cards)
1
Q
AIRSPEED - Mmo 26,750 to 37,000 feet
A
0.81 M
2
Q
AIRSPEED - Mmo 37,000 to 43,000 feet
A
0.81 to 0.78 M
3
Q
AIRSPEED - Mmo 43,000 feet and above
A
0.78 M
4
Q
AIRSPEED - Mmo Mach Trim inoperative & A/P disengaged
A
0.77 M
5
Q
AIRSPEED - Vmo up to 8,000 feet
A
300 KIAS
6
Q
AIRSPEED - Vmo 8,000 to 20,000 feet
A
340 KIAS
7
Q
AIRSPEED - Vmo 20,000 to 23,000 feet
A
340 to 330 KIAS
8
Q
AIRSPEED - Vmo 23,000 to 26,750
A
330 KIAS
9
Q
Vle
A
260 KIAS
10
Q
Vlo
A
200 KIAS
11
Q
Vfe (Flaps 8)
A
250 KIAS
12
Q
Vfe (Flaps 20)
A
200 KIAS
13
Q
Vfe (Flaps 40)
A
165 KIAS
14
Q
Vmca (Flaps 8)
A
120 KIAS
15
Q
Vmca (Flaps 20)
A
110 KIAS
16
Q
Vmcg (Rudder Boost ON)
A
95 KIAS
17
Q
Vmcg (Rudder Boost OFF)
A
116 KIAS
18
Q
Turbulent Air Penetration
A
250 KIAS / 0.73 M
19
Q
Max Demonstrated Crosswind
A
29 knots
20
Q
Tailwind Component for T/O & Landing
A
10 knots
21
Q
Main Tire Limiting Speed (Ground Speed)
A
182 knots
22
Q
Maximum Pressure Altitude
A
51,000 feet
23
Q
Runway Water / Slush on Runway
A
3/4 inch (19 mm)
24
Q
Spoilers Inoperative
A
38,000 feet
25
Maximum Pressure Altitude T/O & Landing (Temperature)
13,700 feet (+50 / -54)
26
Fuel Load Balance: Takeoff and Landing
Balanced within 200 pounds
27
Fuel Load Balance: En-route
Balanced within 500 pounds
28
Limit Maneuvering Load Factors: Flaps Up
+3.0g to -1.0g
29
Limit Maneuvering Load Factors: Flaps Down
+2.0g to 0.0g
30
Maximum Ramp Weight
23,750 pounds
31
Maximum Certified Takeoff Weight
23,500 pounds
32
Maximum Certified Landing Weight
19,500 pounds
33
Maximu Zero Fuel Weight
17,000 pounds
34
Maximum Takeoff Weight with anti-skid OFF or inoperative
18,500 pounds
35
Aviation Gasoline
The use of aviation gasoline is prohibited
36
Unusable Fuel in Fuselage Tank with Gravity Transfer
350 pounds (approx)
37
“LOW FUEL” Annunciator
410 pounds in either wing
38
Fuel Anti-Icing Additive
Anti-icing additive is not a requirement
39
“L & R FUEL PRESS” annunciators illuminate
2.75 psi or less
40
Fuel Capacity (SPPR)
7,800 pounds
41
Fuel Capacity (over wing refueling)
7,910 pounds
42
What activates the fuel scavenge pumps?
Pressing the Lights Test Switch or either wing fuel < 410 pounds
43
What turns on the standby fuel pumps?
START Cycle, Manually Selected or FILL
44
Maximum Thrust
4,600 pounds @ sea level
45
Maximum Continuous ITT
785 degrees
46
Max Transient ITT (20 SEC)
825 degrees
47
Maximum ITT on Start
950 degrees
48
FADEC will terminate start at _____________?
1000 degrees ITT or < 200 degrees ITT after 15 seconds
49
Maximum time APR or Thrust Levers in T/O position
5 mins
50
Engine idle speed (ground)
52% N2 (PMA powers FADEC @ 52%)
51
Engine idle speed (in-flight)
65% N2
52
Engine Computers / Annunciators
Engine Computers must be in AUTO MODE and annunciators must be extinguished
53
Starter Limits
After Start attempt: Wait:
1 3 mins
2 15 mins
3 30 mins
54
Hydraulic AUX PUMP Usage (0.5 GAL per minute)
| 1000 - 1125 psi
3 minutes ON, 20 minutes OFF
55
Normal Hydraulic Pressure
1500 psi
56
Hydraulic Pressure Relief Valve
Opens at 1750 psi
57
GEAR AIR & BRAKE AIR Pressure
1800 - 3000 psi (Nitrogen or Dry Air)
58
Hydraulic Accumulators
2 Accumulators
1 for Thrust Reversers
1 for rest of the hydraulic system
750 psi (MINIMUM), 850 psi (PRECHARGE)
59
Hydraulic Fluid Type
MIL-5606
60
“L & R HYDR PRESS” Annunciators illuminate at what psi?
150 psi from respective engine driven pump (2)
61
Secondary Flight Controls are _________?
Electrically controlled & hydraulically actuated (FLAPS, SPOILERONS, and AUTOSPOILERS)
62
Oil Capacity Per Engine
1.95 gallons
63
Check Oil Level
10 minutes after shutdown
64
Type of Oil
Type II oils conforming to Pratt and Whitney Canada PWA521
65
“L & R OIL PRESS” Annunciator illuminates at ________?
Less than 20 psi
66
What drives the accessory gear box?
Tower Shaft
67
Minimum Fuel required for APU / from which fuel tank
100 pounds / Left fuel tank
68
When does the APU shut down in the event of a fire?
At first indication of a fire
69
How would you detect an APU fire during a walk-around?
By a horn from the left main wheel well
70
How can an APU fire be extinguished?
Automatically from 10-17 seconds of fire indication or manually pressing FIRE button on APU control panel
71
Primary Power is from what?
Two engine -driven START/GENERATORS RATED TO 30 VCD, 400 AMPS
72
Secondary Power
Two 24-volt lead acid, NICAD or Concorde (MAINT FREE) batteries
73
AC Power (What Converts 28VDC to 115 AC)
Two 115-volt, solid-state inverters
74
GPU Limitations
500-1500 amps, regulated to 28 VDC, over-voltage protection at 32 VDC
75
Generator Limits
325 amps ground operations, 400 amps flight operations
76
Emergency Battery Duration
EMER BAT 1 = 3.1 hours
| EMER BAT 2 = 99.2 hours
77
What types of circuit breakers are installed?
Thermal and magnetic.
| All A/C circuit breakers are magnetic.
78
How are emergency bus items identified on the circuit breaker panel?
Red ring around the circuit breaker
79
How are AC items identified on the circuit breaker panel?
White ring around the circuit breaker
80
Maximum Cabin Altitude
| Unless Landing 8000 feet PA or Higher
8,000 feet +/- 250 feet
81
Maximum Cabin Altitude
| Cabin Outflow Valves Close
13,700 feet +/- 500 feet
82
Maximum Differential Pressure
9.8 psig
83
When does the “PRESS SYS” annunciator illuminate?
AUTOMATIC MODE - 8,600 feet +/- 250 feet
| MANUAL MODE - 8,750 feet +/- 250 feet
84
When does the “EMER PRESS” annunciator illuminate?
9,500 feet +/- 250 feet
85
When does the cabin altitude warning horn and (if installed) CABIN HI annunciator activate?
10,100 feet +/- 250 feet
86
Passenger Oxygen Masks automatically deploy when?
14,500 feet +/- 250 feet cabin altitude
87
What mode must be used for takeoff and landing above 8,000 feet PA?
AUTO (All cautions and warnings reset to 14,500 feet except cabin altitude limiters)
88
What fire extinguishing agent is used?
HALON 1301
89
Fire Bottle Pressure Gauge
600 psi
90
How do you check the smoke detector (CABIN FIRE)?
Press either the Pilot’s or Copilot’s Lights Test Switch
91
Normal Oxygen Pressure Gauge
1550-1850 psig
92
Crew and Passenger Oxygen masks are not approved above ___________?
Above 40,000 feet cabin altitude
93
Passenger Masks will not provide sufficient oxygen above _________?
Above 34,000 feet cabin altitude
94
Prolonged operation with passengers on board is not recommended above _____________?
25,000 feet cabin altitude
95
A missing Green Discharge Disc mean _____________?
An over pressurization of 2700-3000 psi in the oxygen bottle
96
What are the crew oxygen mask settings?
Scott ATO crew masks:
Normal, 100% and Emergency
Puritan Bennett Sweep-On 2000 crew masks:
EMER, 100% and NORM
97
When will the crew oxygen masks deliver 100% oxygen regardless of altitude?
Above 35,000 feet cabin altitude
98
Anti-Ice ON in what conditions?
10 degrees or below, visibility 1 mile or less with visible moisture of any kind (such as rain, snow, sleet, ice crystals, clouds or fog)
99
Type of alcohol used?
Methanol O-M-232
100
Alcohol Reservoir Capacity / Duration?
2.35 gallons / 45 minutes
101
Do not operate NAC HT With Associated Engine OFF
More than 5 seconds
102
Do not operate NAC HT above 15 degrees
More than 30 seconds
103
Do not apply NAC HT with thrust above
65% N1 except for takeoff
104
Failed STAB HT On the Ground (Ground Test)
Flashing “STAB HT” annunciator
105
Failed STAB HT in-flight
Steady “STAB HT” annunciator
106
What System is Lost During Emergency Pressurization?
Wing and windshield anti-ice
107
What Anti-Ice Systems are lost during EMER BATT conditions?
All anti-ice systems are lost except nacele heat
108
What items are heated with the pitot heat switches?
Left switch heats the pilot’s pitot tube and stall vane.
Right switch heats the stand-by pitot tube, copilot’s pitot tube, stall vane, pressurization static port, TAT probe, galley drain and lavatory sink drain.
109
Use of thrust reverse to back up the aircraft is ____________?
Prohibited
110
How are the thrust reversers deployed?
Electrically controlled and hydraulically actuated?
111
Thrust reverse is limited to idle ______________________
Below 50 KIAS
112
Thrust reverse approved for what runways?
Paved surfaces only
113
How are thrust reversers stowed during an inadvertent T/R deployment?
Automatically via the FADEC
114
The autopilot / flight director system is approved for what ILS approaches?
Category I ILS approaches
115
Operation of the autopilot with the red TRIM FAIL light illuminated is __________?
PROHIBITED
116
Autopilot pitch and roll axis must not be used for _______________?
Takeoff and Landing
117
The minimum altitude for use of the autopilot is ____________?
Approach Configuration - 200 feet AGL
En route Configuration - 1000 feet AGL
Minimum Engage Height - 1000 feet AGL
118
How many static wicks are installed and how many wicks are required?
19 total and 14 required for flight (Check MEL)
119
No Intentional Stalls
Above 18,000 feet
120
Yaw Damper for Takeoff or Landings
OFF for takeoff
| Optional for landings
121
Check of Trim Systems
Required daily before first flight
122
If you exceed brake energy limits?
Aircraft must be parked for 20 minutes minimum and a visual inspection of main gear tires, wheel and brakes for condition must be made before next takeoff attempt
123
What prerequisites are needed to follow the Through-Flight Checklist?
There has been no change in flight crew personnel.
No maintenance has been performed on the aircraft. Routine line servicing is not considered maintenance.
No more than three (3) hours have elapsed between engine shutdown and engine start.
Extreme weather conditions (heavy precipitation, ice, snow, extreme cold, etc. have not occurred which would change the preflight status of the aircraft.
