LIMITATIONS Flashcards
1
Q
Minimum Runway Length (DRY)
A
4000’ DRY
**Minimum distances are required for release only. Upon arrival, pilots may land if the LPA computed distance is less than the landing distance available.
2
Q
OPS review required if runway length is less than what?
A
Contaminated: Less than 5500’
**Minimum distances are required for release only. Upon arrival, pilots may land if the LPA computed distance is less than the landing distance available.
3
Q
Max Crosswind for TAKEOFF?
(Normal Conditions)
A
28 kts
4
Q
Max crosswind for LANDING with NWS INOP?
A
15 kts. (operations on contaminated runways not authorized with NWS inop)
Takeoff with NWS INOP is NOT AUTHORIZED
5
Q
Max crosswind for LANDING?
(Normal Conditions)
A
24 kts
6
Q
Max crosswind for landing on a contaminated runway?
A
150 or greater runway width: 15 kts
149 or less runway width : 10 kts
7
Q
Max tailwind for takeoff and landing?
A
10 kts
8
Q
Max ramp/taxi weight.
A
40,750
9
Q
Max takeoff weight.
A
40,600
10
Q
Max Landing Weight
A
34,150
11
Q
Max Operating Altitude
A
45,000 feet
12
Q
Max turbulent air penetration speed
A
265/.75
13
Q
Max landing gear extension speed (VLO EXT)
A
250 kts.
14
Q
Max landing gear retraction speed (VLO RET).
A
200 kts.
15
Q
Max flap extension speeds?
A
Flaps 10°- 210
Flaps 20°- 210
Flaps 30°-175
16
Q
Maximum cabin differential pressure for landing.
A
1.0 psid
17
Q
Max cabin differential for ground operations.
A
0.1 psid
18
Q
APU starter limits
A
3 start attempts with 1 minute intervals (then 20 minutes cooling, 2 additional attempts, then 40 minutes cooling)
19
Q
APU airborne attempts allowed
A
ONLY 1
20
Q
EMERGENCY FUEL
A
1300 lbs.
21
Q
Max altitude for APU start
A
30,000 feet
22
Q
Max Altitude for APU operation.
A
37,000 feet
23
Q
Max airspeed for APU start.
A
285 Kts
24
Q
Min Altitude for autopilot engagement.
A
700 feet AGL
25
Min altitude for using autopilot during a precision approach (GP angle 3.5 degrees or less)
80 feet.
26
Min altitude for using autopilot during a non- precision approach (GP angle of 3.5 degrees or less) or visual approach.
200 feet.
27
Approach Category
C
28
Max time on APR
10 minutes (when automatically activated)
5 minutes (when manually activated)
29
Max time in TO thrust.
5 minutes
30
Max Zero fuel weight
28,200 lbs
31
Max takeoff and landing altitude
10,000 feet
32
Max altitude with yaw damper off
31,000
33
Max runway slope
+/- 2%
34
VMO ( Up to 8000 feet )
300 KIAS
AFM Speed Limitations
35
VMO (8001-29,475 ft)
320 KIAS
AFM Speed Limitations
36
MMO
.83 Mach
37
Max gear extension altitude
18,000 feet
38
Max gear EXTENDED speed
250 KIAS
39
Max Flap extension altitude
18,000 feet
40
Tire speed limit
182 KIAS
41
Min Oil temp for starting
-40 C
42
Min oil pressure at IDLE
28 psi
43
Min IDLE N2
46%
44
Max ground START ITT
650 C
45
Engine Starter Limits
3 starts, followed by 15 minutes cooling period.
| engine must be motored for 30 seconds after an aborted start
46
How long can the engine be motored for?
5 minutes followed by a 15 minute cooling period.
AFM Powerplant Limits.
47
Max ITT to initiate a start
350 C
48
Max ITT FADEC begins a start at
250 C
49
Minimum airspeed with spoilers extended
Vref + 8
AOM Chapter 12/ AFM System Limitations
50
Minimum altitude with spoilers extended
500 ft AGL
AOM Chapter 12/ AFM
51
When can you use EMER speed brakes?
Emergency, QRC or QRH
52
When must power/gravity crossflow be off?
Takeoff
AFM, Fuel Limitations
53
Minimum go around fuel (per wing)
500 lbs (collector tank capacity)
54
Max fuel imbalance.
250-600 lbs depending on fuel load (The higher fuel the load, the less the imbalance can be)
> 13,700------------> 250lbs
10,000-13,699-----> 315lbs
4,700-9,999--------> 450lbs
600lbs
55
Max bulk fuel temperature for takeoff
50 C
56
Minimum bulk fuel temperature for takeoff
```
JET-A = -30 C
JET-A1= -35 C
```
57
Max Altitude to use APU for electrics
30,000
58
Max altitude to use APU for ECS.
20,000 feet
59
Thrust reverser limitations
Paved surfaces only
do not deploy tr's in flight
do not use to back up airplane
do not use for touch and go's
60
Limitation for TRIM AIR ONLY.
trim air only is prohibited on ground.
61
Max cabin altitude for crew/passenger oxygen masks.
40,000 feet
prolonged passenger O2 mask ops above 25,000 feet cabin altitude is not recommended.
AFM/System Limitations/Air Conditioning and Pressurization.
62
FMS V speeds prohibited above _______
ISA +33
63
VNAV prohibited on _______ operations
QFE
64
Is FMS range/fuel info advisory only?
YES
65
When conducting an instrument approach with a T-Transition and using VNAV for descent guidance, IAS at the IAF must be _____ KTS or LESS.
210
AOM Chapter 12
66
VMCG
Flaps 10 _____
Flaps 20_____
Flaps 10: 115
Flaps 20: 114
CH 350 AFM (Collections 250)
67
VMCA (takeoff)
Flaps 10 ______
Flaps 20 ______
Flaps 10: 110
Flaps 20: 109
AOM (Limitations)
68
VMCL (landing min control speed
Flaps 10 _____
Flaps 20 _____
Flaps 30 _____
Flaps 10: 115
Flaps 20: 110
Flaps 30: 107
AOM (Limitations)
69
Icing Systems Limit: Minimum temperature- L and R WING/ENG
-40 C
AOM Chapter 12 (Ice and Rain)
70
45-minute IFR Reserve
1850 lbs.
**The DO or designee may authorize reduction of this quantity under certain circumstances.
71
Inclement weather parking Fuel.
5400 lbs. minimum
See “Parking in Inclement Weather” AOM SECTION 4.4
72
Hot Spare Fuel Load
6000 lbs.
73
Minimum Runway Width
70’
74
Max Slope (+/-)
2%
75
The Following Equipment must be operational in RVSM AIRSPACE:
* Autopilot (1)
* Altitude Alerting Device (1)
* ATC Altitude Reporting Transponder (1)
* Air Data Computers (ADC) (2)
* Pitot Probe Heaters (2) on the probes linked to the ADC in use.
76
Max Zero Fuel Weight
28,200 lbs.
77
Max Flap Extended Altitude
18,000’
78
Max Altitude for Start, Takeoff, Landing
10,000 ft.
79
Maximum Gear Extended ALTITUDE
18,000 ft.
80
VMO
320 KTS
81
MMO
.83 M
82
Max Tire Ground Speed.
182 kts
83
Minimum Control Speeds VMC
VMCG flaps 10:
VMCG flaps 20:
VMCA flaps 10:
VMCA flaps 20:
VMCL flaps 10:
VMCL flaps 20:
VMCL flaps 30:
VMCG flaps 10: 115 kts
VMCG flaps 20: 114 kts
VMCA flaps 10: 110 kts
VMCA flaps 20: 109 kts
VMCL flaps 10: 115 kts
VMCL flaps 20: 110 kts
VMCL flaps 30: 107 kts
84
Visual Inspection of the aircraft is NOT required when an over-speed event occurs under the following conditions:
* Level Flight
* No Turbulence
* Landing Gear and Flaps Retracted
* Did Not Exceed the following:
- VMO +15 KTS
- MMO +M 0.03
85
Maximum Differential (psi)
9.4 psi (S/N 20886 and before)
10.1 psi (20887 and above)
86
Maximum Negative Differential (psi)
-0.5
87
Where can you find the oxygen duration Tables?
QRH1 OXYGEN DURATION TABLES (S-21), also FCOM 2 (OXYGEN SYSTEM SECTION 08-01-5), FCOM 1 (Oxygen Duration Tables 05-12-10)
88
Max altitude to Start the Left Engine with the APU
9000 ft (pressure altitude)
89
Do not operate the APU under the following conditions
* Above 37,000 ft
* During Ground De-ice/Anti-ice procedures
90
Do not Use the APU Generator above:
30,000 feet
91
Do not use APU Bleed Air above:
20,000 feet
92
When Operating at an airport with a 5G NOTAM, Disconnect the autopilot below:
400 ft. AGL
93
Maximum Generator Load (In Flight 2 or 3 Generators operating, or on ground)
400A
94
Maximum Generator load (1 GENERATOR OPERATING)
500 A
95
Maximum TRANSIENT Generator load.
600 amps (5 Minutes)
96
Do not extend the flight spoilers below what altitude?
500 ft. AGL
97
Do not select the Flight Spoilers to EMER except during:
* Emergency conditions
* When required by a procedure
98
Pressure fueling is limited to ________ psi
55 psi
99
Max total Fuel Quantity (pressure refueling)
14,150 lbs
100
Max Total Fuel quantity ( gravity fueling)
13,000 lbs.
101
Minimum go-around Fuel
1000 lbs Total (500 lbs. per tank)
102
Maximum fuel imbalance during gravity refueling
250
103
Takeoff is PROHIBITED with the bulk fuel temperature above:
50 degrees C
104
If Bulk fuel temperature is above 45 degrees Celsius the minimum fuel quantity is:
2800 lbs
**if the fuel quantity Is less than 1000 lbs per side, do not operate engines for more than 30 minutes.
105
Cockpit Speaker mute Limits
When Cockpit speakers are muted, both pilots must use headsets.
When one pilot removes his/her headset, select COCKPIT SPEAKER MUTE- OFF
106
Operate Engine and airframe anti-icing systems on the ground and in flight when the following conditions are present:
* Visible Moisture (rain, snow, or visibility less than 1 mile)
* Operating on contaminated surfaces.
AND
On the Ground/SAT 10 C and > 5 C: L and R ENG Anti-Ice ON.
On the Ground/SAT 5 C and below: L and R ENG and WING Anti-Ice ON. (If de-iced with type 2,3,4, delay turning ON WING anti ice just prior to applying takeoff power)
IN-FLIGHT: TAT 10 C or below,
L and R ENG - ON and WING - ON ( SPEED is below 210 KTS for WING or, anytime the ICE DETECTED Amber CAS message is displayed)
107
Do not use the FMS for the following:
Navigation at latitudes South of 60 degrees South
Navigation at Latitudes North of 73 degrees North and for Canadian Northern Airspace
108
Do not Use the FMS as the primary source of navigation:
When dead reckoning (FMS DR annunciation)
109
Always retrieve approaches from ___________ database.
CURRENT
110
FMS en route and terminal operations must use __________database or _________ ___________ waypoints.
CURRENT database or
Pilot Verified waypoints
111
Do not use FPLN UPLINK ___ ___________.
In Flight
The FPLN UPLINK must complete or cancelled before taxiing.
112
Do not use FANS CPDLC FMS auto-load function to load any CPDLC clearance containing _________ constraints.
RTA
113
Do not select FANS CPDLC INSERT MOD when within ____ minutes of a TO waypoint.
2
114
Do not conduct RNAV operations when any of the following FMS messages are annunciated:
* FMS DR (PFD MFD or CDU)
* IRS ONLY (PFD MFD or CDU)
* VOR/DME ONLY (CDU) or V/D ONLY (PFD)
* VOR/DME DIST > 40.0 NM (CDU)
* CHK POS (PFD or CDU)
115
Do not conduct RNP operations when any of the following massages are displayed:
* NO APPR (FMS A1 on PFD)
* LOI (FMS A1 on PFD)
* LOSS OF INTEGRITY (on CDU)
* GNSS NOT AVAILABLE (on CDU)
* GNSS-FMS DISAGREE (on CDU)
116
Do not use Geopolitical boundaries, controlled and special use airspace on MFW MAP for _________.
NAVIGATION
117
Do not use the _____________ ______________ on digital approach and taxi charts for navigation or precision maneuvering on the ground.
Aircraft Symbol
118
Do not use the Terrain Awareness and Warning System (TAWS) for _________________.
NAVIGATION
119
Synthetic Vision System (SVS).
Do not use the SVS for airplane _____________.
Navigation
120
If SVS database is not current, DESELECT SVS prior to _______________and prior to passing the _________.
Takeoff/FAF
121
For ILS, LOC, and BC approaches, do not use _______ as the primary navigation source inside the FAF.
FMS
122
When conducting an instrument approach with a T – transition and using VNAV for descent guidance, indicated airspeed at the initial approach fix must be _______kts or less.
210
AOM Chapter 12
123
Initiate missed approach if the appropriate annunciator, or any of the following messages are displayed (related to the approach):
NO APPR
UNABLE RNP
124
For ACCURATE COMPASS READINGS, SELECT L and R WSHLD/WINDOW TO ______.
OFF
125
The following EICAS COLORS Mean what?
GREEN
RED
AMBER
CYAN
WHITE
GREEN - NORMAL (safe) operating range
RED - WARNING - Indications of hazard which may require immediate corrective action.
AMBER- Caution – indications of possible need of corrective action.
CYAN- Advisory Messages.
WHITE- Status Messages.
126
If the door actuator is operated three times in a three minute period, allow Cabin door motor to cool for _____ minutes
5
127
Minimum Oil Temperature for Takeoff?
27 degrees C
128
Minimum oil temperature to operate engines above ground Idle.
5 degrees Celsius
(AOM Chapter 12 Engine Limitations)
129
Before updating a flight plan received through CPDLC, ensure the entire flight plan is loaded in the FMS.
Before updating a flight plan received through CPDLC, ensure the entire flight plan is loaded in the FMS.
130
FMS: DO NOT accomplish the following during Flight.
1. Load Routes from PILOT ROUTE LIST.
2. Upload flight plans from ROUTE MENU (FPLN RECALL)
3. Select FPLN WIND UPDATE from the ROUTE MENU
4. Initiate a NAV RADIO SELF TEST from either the NAV radio tuning page on the FMS CDU or MFD nav radio menu.
