LIMITATIONS Flashcards
(91 cards)
1
Q
MINIMUM TEMPERATURE
A
-54°
2
Q
MAXIMUM TEMPERATURE
A
ISA + 35°C
3
Q
A/C OFF (2 min) / RADIO MASTER ON
A
ISA + 15°C
4
Q
A/C OFF / RADIO MASTER OFF
A
ISA + 35°C
5
Q
MAX ALTITUDE
EEC ON, BOTH ENGINE BLEEDS OPEN
A
FL 320
6
Q
MAX ALTITUDE
EEC ON, ONE ENG BLEED CLOSED OR BOTH ENG BLEEDS CLOSED W/APU BLEED OPEN
A
FL 250
7
Q
MAX ALTITUDE
EEC OFF, BOTH ENG BLEEDS OPEN
A
FL 250
8
Q
MAX ALTITUDE
EEC OFF, ONE ENGINE BLEED CLOSED OR BOTH ENG BLEEDS CLOSED W/APU BLEED OPEN
A
FL 200
9
Q
T.O & LDGS ABOVE 8,000’ PRESS ALT PERMITTED
A
ONLY WITH EECS IN MANUAL POSITION
10
Q
REQUIRED POWER T.O’S CONTAMINATED RUNWAY
A
NOT PERMITTED
11
Q
MAX T.O. PRESS ALT
A
10,000’
12
Q
MAX LDG PRESS ALT.
A
10,000’
13
Q
MAX RUNWAY SLOPE
A
2% RUNWAY LENGTH
14
Q
RUNWAY SURFACE
A
PAVED
15
Q
MAX TAILWHEEL COMPONENT T.O. & LDG
A
10 KTS
16
Q
MAX TAILWHEEL COMPONENT REDUCED POWER T.O.
A
3 KTS
17
Q
X-WIND COMPONENT BRAKING GOOD
X-WIND COMPONENT BRAKING FAIR
X-WIND COMPONENT BRAKING POOR
A
30 KTS DEMONSTRATED
15 KTS MAX
10 KTS MAX
18
Q
MANEUVERING SPEED (Va)
A
200 KTS
19
Q
TURBULENT AIR PENETRATION SPEED (SL - 15,000’
A
180 KTS
20
Q
TURBULENT AIR PENETRATION SPEED (Above 15,000’)
A
160 KTS
21
Q
MAX OPERATING LIMIT SPEED
A
.52 MACH 272 KTS
22
Q
(EMB-120 RT)
MAX RAMP WEIGHT (MRW)
A
25,529 lbs
23
Q
(EMB-120 RT)
MAX TAKE OFF WEIGHT (MTOW)
A
25,353 lbs
24
Q
(EMB-120 RT)
MAX LANDING WEIGHT (MLW)
A
24,802 lbs
25
(EMB-120 RT)
| MAX ZERO FUEL WEIGHT (MZFW)
23,148 lbs
26
(EMB-120 ER)
| MAX RAMP WEIGHT (MRW)
26,609 lbs
27
(EMB-120 ER)
| MAX TAKE OFF WEIGHT (MTOW)
26,433 lbs
28
(EMB-120 ER)
| MAX LANDING WEIGHT (MLW)
25,794 lbs
29
(EMB-120 ER)
| MAX ZERO FUEL WEIGHT (MZFW)
24,030 lbs
30
The T.O. Weight (Start of T.O. Roll) is limited by the most restrictive of Max T.O. weights for:
Attitude & Temperature
T.O. Field length requirements
Brake energy requirments
Obstacle Clearance
31
The Landing weight is limited by the most restrictive of:
Landing field length requirements
| Max approach climb weight for altitude & temperature
32
Maneuvering flight load limits
Flaps Retracted
Flaps Extended
-1 g - 2.80g
| 0g - 2.00g
33
Max differential cabin pressure
7.2
34
Normal differential cabin pressure
7.0
35
Cabin Altitude (SL - FL16,800')
Sea Level
36
Cabin Altitude (16,800' - FL320
8000'
37
All Take offs will be made with engine Bleeds _____
Closed
38
Do not open RAM air inlet w/ AC Packs ______
ON
39
Max Operating altitude w/ one pack:
FL 250
40
APU
| Max Operating Temperature
ISA + 38°C
41
APU
| Max EGT During Start
760°C
42
APU
| Max EGT during steady state operations
680°C
43
APU
| In flight EGT between ____° - _____° for up to 5 mins
680°C - 730°C
44
APU
Inflight starting speed limits:
Surface - 5000'
5000' - 20,000'
100 - 250 kts
| 100 - 220 kts
45
APU
| From 5,000' - 20,000' Decrease ___ kts p/1000' for max speed of _____ at 20,000'
2 kts
| 220 kts
46
APU
| Do not attempt to star APU above ______
FL 200
47
APU
| During ground deicing iperations insure the APU bleed is _____.
Closed
48
A/P & Yaw Damper
| The AP / YD must be ______ during T.O. / LDG
OFF
49
A/P & Yaw Damper
| Minimum ALT for AP & YD engagement after T.O. is:
500' AGL
50
A/P & Yaw Damper
| Minimum airspeed for AP / YD operation single engine
120 kts
51
A/P & Yaw Damper
| Minimum ALT for AP / YD operation on ILS coupled approaches:
200' AGL
52
A/P & Yaw Damper
| Min ALT for AP / YD on coupled non-prec approach
50' below MDA
53
A/P & Yaw Damper
| Min ALT for AP / YD all other approaches
500' AGL
54
```
A/P & Yaw Damper
ALT loss during AP malfunction:
1. Cruise
2. Maneuvering
3. ILS approch
4. Single Engine ILS approach
```
1. 80'
2. 70'
3. 80'
4. 90'
55
```
ELECTRICAL SYSTEM
Main Generator Operations (Max Loads)
1. On Ground OAT > ISA + 27°C
2. On Ground OAT < ISA + 27°C
3. In flight up to FL270
4. In flight above FL 270
```
1. 380 amps
2 400 amps
3. 400 amps
4. 380 amps
56
ELECTRICAL SYSTEM
Aux Generator Ops (Max Loads)
1. Up to FL180
2. FL180 & Above
1. 150 amps
| 2. 140 amps
57
```
ELECTRICAL SYSTEM
APU Generator Ops (Max Loads)
1. On the ground
2. Up to 16,000' MSL
3. 16,000' MSL & Above
Max Batt Temp
```
1. 370 amps
2. 400 amps
3. 290 amps
4. 70°C
58
```
OPERATING PARAMETERS
Engine start (Including APU) not possible when operating in ____ moade (Auto Transfer)
```
EMERGENCY MODE (Auto Transfer)
59
OPERATING PARAMETERS
| ____ will supply power to ____ for 30 mins in case of loss of all generators.
Main Batt
| Emergency DC Buses
60
OPERATING PARAMETERS
| ____ suitable to feed ____ for 30 mins after total failure of ELEC DC system
Backup Batt
| Standby Horizon
61
```
FLIGHT CONTROLS
Flap Extended Speed
1. Flaps 15°
2. Flaps 25°
3. Flaps 45°
```
200 KTS
150 KTS
135 KTS
62
FUEL SYSTEM
1. Max Usable each tank
2. Unusable each tank
3. Add ____ to unusable in corresponding tank when ____ ____ ____ ____ is inoperative.
4. When fuel quantity reads ____ in level attitude. Any fuel remaining in tank can / cannot be used safely in flight.
1. 2866 lbs
2. 24 lbs
3. 796 lbs (Main Elec Boost pump)
4. Zero / Cannot
63
FUEL SYSTEM
| Max Demonstrated imbalance
600 lbs
64
FUEL SYSTEM
| Usable fuel types
Jet A, A-1, B, JP-4, 5, 8
65
FUEL SYSTEM
| Fuel X-feed should be ____ for all T.O. & Ldg.
OFF
66
ICE & RAIN PROTECTION
| Min Nn for Pneumatic Deicing System operation
80%
67
ICE & RAIN PROTECTION
| Max speed for windshied wiper operations
160 kts
68
INSTRUMENTS & AVIONICS
| Do not operate Wx Radar
Near people during refueling or near fuel spilts
69
INSTRUMENTS & AVIONICS
| Do not operate aircraft unless:
Heading & ALT info are valid on both pilots EFIS.
70
INSTRUMENTS & AVIONICS
| Approaches must be made with EFIS in ____ mode
Angular
71
LANDING GEAR & BRAKES
| Gear Operating speed (Vlo)
200 kts
72
LANDING GEAR & BRAKES
| Gear Extend Speed (Vle)
200 kts
73
LANDING GEAR & BRAKES
| After overweight landing, T.O. must not be made for ____ mins.
26
74
LANDING GEAR & BRAKES
| For T.O. & Ldgs with Anti-skid INOP:
Appropriate performance decreasing must be applied.
75
OXY SYSTEM
| Min crew portable oxy cylinder pressure for dispatch
1800 psi
76
OXY SYSTEM
| Min attendant's portable oxygen cylinder pressure for dispatch:
1200 psi
77
POWERPLANT
| May be extended during T.O. up to ____ for ____ min.
876°C
| 5
78
POWERPLANT
| Above ____°C up to ____°C time limited to 20 secs
816°C
| 850°C
79
POWERPLANT
| Above ____°C up to ____°C time limited to 5 secs
850°C
| 950°C
80
POWERPLANT
| May be exceeded during T.O. up to ____% for ___ mins.
100
| 5
81
POWERPLANT
| Up to this value, time limited to ____.
20 secs
82
POWERPLANT
| Max Np speed control tolerance is ____ to ____
100. 0
| 100. 7
83
POWERPLANT
| Stead state operation after selection of ____
Reverse
84
POWERPLANT
| Oil temp must be monitored above ____ for ____
45°C
| Intake Strut de-icing & prevent fuel icing
85
POWERPLANT
| Operation between ____ & ____ PSID only if Nh is below ____%.
140
55
75%
86
POWERPLANT
| Operation between ____ & ____ allowed for ____.
100
| 115 20 mins
87
POWERPLANT
| Reverse thrust for ____ use only.
Ground
88
POWERPLANT
| Max Reverse Not approved
Wet runways w/areas of standing water
89
```
POWERPLANT
Max reverse allowable cruise power:
1. 100% NP
2. 90% Np
3, 85% NP
```
Torque
1. 72%
2. 80%
3. 84%
90
STARTER DUTY CYCLES
First Cycle
Second Cycle
Third Cycle
30 secs on - 3 mins off
30 secs on - 3 mins off
30 secs on - 30 mins off
91
POWERPLANT
1. Propeller Manufacturer
2. Propeller Model Number
3. Propeller Diameter
4. Number of Prop blades
5. During ground operations, prop should not be operated above ____% n
6. Inflight ops at power settings __ __ __ not approved.
7. Autofeather system must be ____ for T.O.
1. Hamilton Standard
2. 14 RF-19
3. 105' (32m)
4. 4
5. 60^
6. Below flight idle
7. Operative
