Limitations Flashcards
(115 cards)
1
Q
Engine Dry-Motoring Cycle
1st
A
The dry-motoring cycle (with thrust lever at IDLE) may be used for engine ground starts and engine airstarts.
Maximum 90 seconds ON, followed by 5 minutes OFF
2
Q
*Engine Starter Duty Cycle
3rd through 5th*
A
Maximum 90 seconds ON (ground), 120 seconds ON (in flight)
Followed by…
5 minutes OFF
3
Q
APU Operational Limits
EGT - Continuous
A
717°C
4
Q
RVSM Altimeter Tolerance
Standby Altimeter in RVSM
A
Does not meet altimeter accuracy requirements of RVSM.
5
Q
Maximum Runway Slope for Autolands (up hill, down hill)
A
+1%, -1%
6
Q
When operating the ICE PROTECTION in manual mode:
A
CAUTION
Do not rely on visual airframe icing cues to select engine anti-ice ON.
Use temperature and visual moisture criteria specified in this section.
Delaying the use of engine anti-ice until ice buildup is visible from the flightdeck may result in severe engine damage and/or flameout.
7
Q
N1 Max RPM
A
100%
8
Q
Autopilot Use During Landing
A
Unless executing an autolanding with AUTOLAND 1 engaged, turn off autopilot PRIOR to 50 feet AGL.
9
Q
APU Operational Limits
Rotor Speed
A
108%
10
Q
Engine and Wing Anti-Ice Operations
A
During taxi out and takeoff, the MCDU TO DATASET MENU REF A/I must be set to ALL when OAT is 10°c or below and icing conditions exist or are anticipated.
11
Q
Engine Maximum Continuous Max ITT
A
960°C
12
Q
APU Operational Limits
Altitude for Start
A
30,000 feet
13
Q
Turbulent Airspeed (below 10,000 feet)
A
250 KIAS
14
Q
Maximum Relief Differential Pressure
Above 37,000 feet
A
8.3 psi
15
Q
Definition of Icing Conditions
A
- OAT (on the ground and for takeoff) or TAT (inflight) is 10°C or below, and
- Visibile moisture in any form is present such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals, or
- When operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush may be ingested by engines and freeze on engines, nacelles, or engine sensor probes.
16
Q
Autoland Weight Limitations
Maximum
A
97,000 lbs
17
Q
Maximum Gear Extension Speed (Vlo)
A
265 KIAS
18
Q
Maximum Weights
Taxi & Ramp
A
114,500 lbs
19
Q
Engine Caution Range
A
Amber
20
Q
FMS Bank Angles for Single Engine Operations
A
There is no automatic bank angle protection for an engine out situation.
21
Q
Maximum Gear Retraction Speed (Vlor)
A
235 KIAS
22
Q
Turbulent Airspeed (at or above 10,000 feet)
A
270 KIAS/.76M
23
Q
Maximum Weights
Zero Fuel (MZFW)
A
90,150 lbs
24
Q
Engine Normal Operating Range
A
Green
25
Maximum Flap Operating Speeds Vfe(KIAS)
Flaps 2
215
26
Maximum Airspeed for Windshield Wiper Operation Failed in the Non-Parked Position
320 KIAS
27
FMS Speed
Not authorized for takeoff.
28
Engine Normal Takeoff & Go Around Max ITT
947°C
29
Tire Limit Ground Speed
195 kts
30
APU Operational Limits
*Altitude for Operation: ELECTRICAL*
33,000 feet
31
Approved Fuel
Primary
Jet A and A-1
Mixing of fuels is permitted.
32
Engine Maximum Takeoff & Go Around Max ITT*
*Automatically engaged mode in one engine inoperative or wind shear conditions with the thrust lever in the TOGA position.
983 °C
33
Maximum operating limit speeds (Vmo/Mmo) shall...
not be deliberately exceeded in any regime of flight.
34
Engine and Wing Anti-Ice Temperature Limits
There is no temperature limitation for anti-ice system automatic operation.
35
Fuel Density
6.77 lbs/gal
36
*APU Starter Limit*
3rd Start cycle
5 minutes OFF
37
*APU Starter Limit*
1st and 2nd Start cycle
60 seconds OFF
38
*Reverse Thrust Use*
Reverse thrust is for GROUND USE only.
Thrust reverser are intended for use during full stop landings.
39
Crossfeed Operation
The XFEED Selector must be set to OFF during takeoff and landing.
40
*Maximum Airspeed for Windshield Wiper Operation*
250 KIAS
41
Flaps Maneuvering Load Acceleration Limits
Flaps UP
-1.0 to 2.5 G
42
TAS, TAT and SAT
Information are only valid above 60 KIAS.
43
*Engine Starter Duty Cycle
1st and 2nd*
Maximum 90 seconds ON (ground), 120 seconds ON (in flight)
Followed by...
10 seconds OFF
44
“When using Jet A type of fuel with ambient temperatures of _______ , the fuel temperature prior to flight must be verified to be ________ “
-30°C (-22°F) is below
At or above -29°C (-21°F)
45
*Maximum Headwind for CAT II/III Approaches*
25 kts
46
Maximum Relief Differential Pressure
Up to 37,000 feet
7.8 psi
47
Brakes Cooling Limitation
Do NOT takeoff with amber brake temperature indicators.
48
*Maximum Crosswind for Landing Vis <4000 or 3/4*
15 kts (A)
49
Flaps Maneuvering Load Acceleration Limits
Flaps Down (1,2,3,4,5 and Full)
0.0 to 2.0 G
50
*Maximum Wind for Takeoff and Landing (including gusts)*
50 kts (A)
51
Minimum Fuel Temperature
-40°C
52
Maximum Airspeed to Open Flightdeck Window
160 KIAS
53
Maximum Takeoff and Landing Altitude
8,000 feet
54
Evacuation Slides
Whenever occupants are in the cabin, the escape slides must be armed during taxi, takeoff, and landing.
55
Electrical Circuit Breaker Reset
There is no operational situation in which it would be necessary to reset a tripped fuel boost pump or fuel indicating system circuit breaker.
WARNING
Resetting a tripped fuel boost pump or fuel indicating system circuit breaker is prohibited.
56
Unusable Fuel
101.5 lbs per tank
57
Maximum Runway Slope (up hill, down hill)
+2.0%, -2.0%
58
Minimum Operating Limit Speed
Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for non-routine flight or training operations.
59
APU Operational Limits
Temperature (min and max)
Min: -54°C
Max: ISA + 35°C
60
*Maximum Operating Altitude*
41,000 feet
61
Minimum SAT for Takeoff, Landing and Ground Start
-40°C
62
Maximum Flap Operating Speeds Vfe(KIAS)
Flaps 5
180
63
Engine Type
CF-34-10E
64
Maximum Flight Operating Latitude
72° North (A)
| 59° South (A)
65
“During takeoff or go around, do NOT turn the autopilot on until ...”
Above 400 feet AGL
66
*Maximum Operating Mach Number*
.82 (Mmo)
67
Reverse Thrust Go Around WARNING
Do NOT attempt a go around maneuver after deployment of the thrust reversers.
68
Engine Dry-Motoring Cycle
2nd through 5th
The dry-motoring cycle (with thrust lever at IDLE) may be used for engine ground starts and engine airstarts.
Maximum 30 seconds ON, followed by 5 minutes OFF
69
Maximum Flap Operating Speeds Vfe(KIAS)
Flaps 1
230
70
RVSM Altimeter Tolerance
*Maximum Allowable In-Flight Difference Between Captain and First Officer Displays for RVSM Operation*
200 feet
71
Terrain/Obstacle Awareness Alerting functions ...
Should be manually inhibited within 15nm on approach to an airport that is not in the EGPWS airport database to avoid unwanted alerts.
72
Flight Load Acceleration Limitation WARNING
Rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) may result in structural failures at any speed.
73
Reverse Thrust During Landing
*Application of __________, is not permitted at airspeeds _________.
Below _____ _______ reverse thrust to _____.”
Maximum reverse thrust; below 60 KIAS
60 KIAS; reduce; IDLE
74
*Maximum Altitude for Single Pack Operation*
31,000 feet
75
APU Operational Limits
*Altitude for Operation: BLEED*
15,000 feet
76
Pressurization Door Opening WARNING
Prior to opening any of the aircraft doors, the aircraft must be completely depressurized.
77
Autoland Weight Limitations
Minimum
69,500 lbs
78
Maximum Flap Operating Speeds Vfe(KIAS)
Flaps 3
200
79
RVSM Altimeter Tolerance
Primary Altimeter Readings
On the ground, must be within 75 feet of each other and within 75 feet of field elevation.
80
*Maximum Altitude With Flaps Extended*
20,000 feet
81
APU Operational Limits
*Altitude for Operation: To Assist ENGINE START*
21,000 feet
82
Maximum SAT for Takeoff, Landing and Ground Start
52°C
83
Maximum Weights
*Landing (MLW)*
97,000 lbs
84
*Maximum Crosswind (including gusts) for Autoland*
15 kts (A)
85
Maximum Useable Fuel
14,400 lbs, per tank
86
*Maximum Fuel Imbalance*
Between left and right main tanks during all phases is 800 lbs.
87
Oil Temperature Max
155°C
88
Maximum Flap Operating Speeds Vfe(KIAS)
Flaps Full
165
89
Reverse Thrust WARNING
After applying thrust reverser, do not move the throttle back to the forward thrust range, unless the REV icon on the EICAS is shown in amber or green.
90
Maximum Airspeed for RAT Operation
Vmo/Mmo
91
Enroute Use of Flaps/Slats ...
Is prohibited.
92
*Maximum Takeoff and Landing Tailwind Component*
10 kts
93
Engine Dry Motoring Cycle After 5th Start
After five sequential motorings, cycle may be repeated following a 15 minute cool down period.
94
*Design Maneuvering Speed*
Full application of rudder and aileron controls, as well as maneuvers that involve angle of attack near the stall, must be confined to speeds below
*240 KIAS*
95
“In the event of a landing below ____ , the aircraft may not takeoff without further maintenance inspection.”
-40°C
96
Minimum Flight Crew
Captain and First Officer
97
*Maximum Operating Airspeed*
Vmo
98
*Engine Maximum and Minimum Limitations*
Red
99
APU Operational Limits
EGT - Start
1032°C
100
Normal and Maximum Takeoff & Go Around Engine Temperature Limit
Are limited to 5 minutes during a 10 minute period.
101
Icing Conditions with Flaps/Slats Extended...
Do NOT hold in icing conditions with flaps/slats extended.
102
N2 Max RPM
100%
103
Approved Fuels
Alternate
JP-8
Mixing of fuels is permitted.
104
Maximum Differential Overpressure
8.7 psi
105
Maximum Gear Extended Speed (Vle)
265 KIAS
106
*Maximum Crosswind (including gusts) for Takeoff and Landing*
28 kts (A)
107
Maximum Differential Pressure for Takeoff and Landing
0.2 psi
108
Maximum Flap Operating Speeds Vfe(KIAS)
Flaps 4
180
109
Maximum Weights
Take (MTOW)
114,150 lbs
110
Maximum Negative Differential Pressure
-0.5 psi
111
Oil Pressure Minimum
25 psi
112
Flightdeck Door Access System Check
Must be accomplished prior to the first flight of the day.
113
*Memory Item*
(YAW or ROLL) TRIM Runaway
AP/TRIM DISC ... PRESS and HOLD
114
*Memory Item*
Nosewheel Steering Runaway
STEER DISC ... PRESS
115
*Memory Item*
PITCH TRIM Runaway
AP/TRIM DISC ... PRESS and HOLD
