Limitations Flashcards
(89 cards)
1
Q
Max Design Ramp Weight
A
14,070 lbs
2
Q
Max Design Takeoff Weight
A
13,870
3
Q
Max Design Landing Weight
A
12,750
4
Q
Max Design Zero Fuel Weight
A
10,510
5
Q
How long is takeoff thrust limited to?
A
5 minutes. May be used up to 10 minutes for One Engine Inoperative Operations.
6
Q
Engine Start Limitations Ground:
ENG CTRL SYS FAULT L/R Annunciators
A
Extinguished
7
Q
Engine Start Limitations Ground:
Maximum tailwind and crosswind component
A
10 knots
8
Q
Engine Start Limitations Ground:
Maximum time to light off
A
10 seconds
9
Q
Engine Start Limitations Ground:
Minimum Engine Oil Temperature (indicated on EIS)
A
-40°C
10
Q
Maximum Airport elevations for batter or external power start?
A
14,000 Feet
11
Q
Maximum Battery Voltage For Battery Start?
A
24 VDC
12
Q
Minimum/Maximum External Power Current Capacity For Start
A
800/1100 Amps
13
Q
If the engine oil temperature is below -40°C, what must be done in order to start?
A
Engine must be preheated
14
Q
If the battery has been cold soaked for 2hrs or longer at ambient surface temperature of -18°C (0°F) what must be conducted prior to a start?
A
The battery must be preheated to above 18°C
15
Q
The EIS may take ___ to ___ minutes to become usable after power is applied when cold soaked below ___?
A
1 to 6 minutes. Below -10°C (+14°F)
16
Q
Three engine starts per ___ minutes. Three cycles of operation with a ___ second rest period between cycles is permitted
A
30 mins. 60 secs
17
Q
The battery temperature warning system must be operational for all ____ and ____ operations.
A
Ground and Flight
18
Q
The battery cell is limited to how many starts per hour?
A
Three
19
Q
How many generator assisted starts are equal to a battery start?
A
Three
20
Q
If an EPU cart is used, how many battery cycles are counted?
A
None
21
Q
Maximum Generator Current Per Generator on the ground
A
200 Ampres
22
Q
Limit ground operation of pitot/static heat to ___ minutes to preclude damage to the pitot tubes and angle of attack vane.
A
Two
23
Q
Ground operation at greater than 75% N2 engine RPM with engine RPM with engine, wing, and/or winshield anti-ice on is limited to ___ minutes. Do not operate with the wing anti-ice on more than ___ minute after the WING ANTI-ICE L/R annunciators have extinguished
A
Two Minutes. One Minute
24
Q
Ambient surface temperature must be obtained from the _____ display at the bottom of each _____, with either or both engines operating, or from an appropriate ground station. The SAT display is unreliable on the ground
A
RAT. PFD
25
Fuel Boost Pumps - ON; when FUEL LOW LEVEL L and/or R cautions lights illuminate or at ___lbs or less of indicated fuel.
210
26
Maximum approve fuel imbalance is ___lbs. A fuel imbalance of ___lbs has been demonstrated for emergency return.
200lbs. 600lbs.
27
EDME/DIEGME additive is _____for use, but not required, at a concentration not to exceed 0.15% volume
Approved
28
What is considered unusable fuel in flight?
Fuel remaining in the fuel tanks when the fuel quantity indicator reads zero is not usable in flight.
29
What is the maximum operating limit speed at altitudes above 29,300 feet?
0.737 Mach (Indicated)
## Footnote
This speed is referred to as MMo.
30
What is the VMO for altitudes between 8,000 and 29,300 feet?
278 KIAS
## Footnote
VMO stands for Maximum Operating Limit Speed.
31
What is the VMO for altitudes below 8,000 feet?
260 KIAS
## Footnote
VMO is critical for maintaining aircraft safety at lower altitudes.
32
What is the maximum flap extended speed for the TAKEOFF AND APPROACH position (15°)?
200 KIAS
## Footnote
This speed is crucial for safe takeoff and approach procedures.
33
What is the maximum flap extended speed for the LAND position (35°)?
161 KIAS
34
What is the maximum speed with flaps failed to Ground Flaps (55°)?
140 KIAS
## Footnote
This is an important speed to consider in case of flap malfunction.
35
Maximum Landing Gear Extended Speed - VLE
200 KIAS
36
What is Landing Gear Operating/Retracrting Speed - VLo (Extending)
200 KIAS
37
What is the Maximum Altitude Limit for takeoff and landing?
14,000 Feet
38
Speed brakes must be retracted before landing at what altitude?
Speed brakes must be retracted prior to 50 feet AGL before landing.
39
Extending Ground Flaps during touch and go landings
Extending Ground Flaps during touch and go landings is prohibited.
40
GROUND IDLE switch position for touch and go landings
The GROUND IDLE switch must be in the HIGH position when conducting touch and go landings.
41
Takeoff prohibition with frost
Takeoff is prohibited with frost adhering to critical areas such as Wing Leading Edge, Upper Wing Surface, and Windshield.
42
Maximum Speed Brake Operation Speed - VsB
No Limit
43
Maximum Autopilot Operation Speed
278 KIAS or 0.737 Mach
44
Minimum Speed for Sustained Flight in Icing Conditions
180 KIAS
45
Maximum Tailwind Component
10 Knots
46
Minimum Ambient Temperature For Takeoff
-54°C (-65°F)
## Footnote
Cabin temperature must be held at or above 0°C (+32°F) for a minimum of 20 minutes prior to takeoff after a prolonged ground cold soak period.
47
Maximum Tire Ground Speed
165 Knots
48
Takeoff limitation with anti-ice fluid
Takeoff is limited to the flaps up configuration when Type II, III, or IV anti-ice fluid has been applied.
49
Takeoff prohibition with ice, snow, or slush
Takeoff is prohibited with ice, snow, or slush adhering to critical areas including Wing Leading Edge, Flight Control Surfaces, and Windshield.
50
Intentional selection of Ground Flaps in flight
Intentional selection of Ground Flaps in flight is prohibited.
51
Autopilot and yaw damper for takeoff and landing
The autopilot and yaw damper must be OFF for takeoff and landing.
52
Engine synchronizer for takeoff and landing
Engine synchronizer must be OFF for takeoff and landing.
53
Takeoff prohibition if antiskid system is inoperative
Takeoff is prohibited if the antiskid system is inoperative.
54
What is the cabin depressurization for takeoff and landing
Cabin must be depressurized for takeoff and landing.
55
Takeoffs and landings surface limitation
Takeoffs and landings are limited to paved runway surfaces.
56
Takeoff initiation with warning or caution annunciator
Takeoff may not be initiated with a warning annunciator displayed.
57
What must be performed prior to flight when the outside temperature is below 10°C (50°F) or it cannot be determined if the wing fuel temp is above 0°C
A visual and tactile check of the wing leading edge and upper surface must be performed to ensure it is free from frost, ice, snow, or slush when conditions are met.
58
What are the operational limits for takeoff regarding visible moisture when the OAT is above 10°C?
A Tactile inspection is required when visible moisture is present (rain, drizzle, sleet, snow, fog, etc.); or water is present on the upper wing surface; or the difference between the dew point and the outside air temperature is 3°C (5°F) or less; or atmospheric conditions are conducive to frost formation.
59
What is the maximum operating altitude for the CE-525B Citation CJ3?
45,000 Feet
60
What is the maximum generator current per generator up to 41,000 feet?
300 Amperes
61
What is the maximum generator current per generator above 41,000 feet?
250 Amperes
62
What is the maximum altitude for extension of flaps and/or landing gear?
18,000 Feet
63
What is the maximum operating altitude with an inoperative yaw damper?
30,000 Feet
64
What are the normal cabin pressurization limitations for the CE-525B Citation CJ3?
0.0 to 8.9 PSI + 0.1 PSI Differential
65
What conditions indicate potential icing in flight?
Icing conditions may exist when the indicated RAT in flight is +10°C (+50°F) or below, and visible moisture in any form is present.
66
What are considered icing conditions while on the ground?
Icing conditions exist when the OAT or indicated RAT is +10°C (+50°F) or below and surface snow, slush, ice, or standing water may be ingested by the engines.
67
What is the minimum airspeed for sustained flight in icing conditions?
180 KIAS
68
What is the minimum engine N2 speed for effective wing anti-icing?
75% N2
See note——70% high idle with icing on??????
69
What is the minimum temperature for operation of tail deicing boots?
-35°C (-31°F)
70
What must be done with the WING/ENGINE ANTI-ICE switches in icing conditions?
The switches must be ENG ON or WING/ENG for operations with indicated RAT of +10°C (+50°F) or below when flight free of visible moisture cannot be assured.
71
What is the procedure for engine anti-ice during ground operations in icing conditions?
Engine anti-ice must be ON during ground operations in icing conditions, except for 1 minute after ground engine start.
72
What should be done if minor engine vibrations are felt during ground operations?
Momentarily increase engine speed (typically 20-30% N1) to assist with shedding accumulated ice.
73
What must be operative prior to flight into known or forecast icing conditions at night?
All wing icing inspection lights
74
What are the visual cues for severe icing conditions?
1. Unusually extensive ice accumulation on the airframe and windshield. 2. Accumulation of ice on the upper surface of the wing extending more than 12 to 18 inches aft of the heated leading edge.
75
What actions should be taken if visual cues for severe icing conditions are observed?
1. Use of the autopilot is prohibited. 2. Request priority handling from Air Traffic Control. 3. Leave flaps in current position. 4. Avoid abrupt maneuvering. 5. Reduce angle-of-attack if unusual roll control movement is observed.
76
When is the use of the autopilot prohibited in icing conditions?
When unusual lateral trim is required or autopilot trim warnings are encountered.
77
What is required regarding the pilot's seating during autopilot operations?
One pilot must remain seated with seat belt fastened during all autopilot operations.
78
What must be verified prior to each flight in which the autopilot is to be used?
The FCS-3000 system must be verified to be operational by a satisfactory automatic preflight test.
79
What is the autopilot minimum engage height during climb following takeoff or go-around?
350 feet AGL
80
What is the autopilot minimum use height for ILS Approach (CAT I)?
180 Feet AGL
81
What is the autopilot minimum use height for Non-precision Approaches?
350 Feet AGL
82
What is the autopilot minimum use height for Cruise?
1000 Feet AGL
83
Are Category II approaches approved?
No, Category II approaches are not approved.
84
What mode must VOR approaches not be conducted in?
MUST NOT BE CONDUCTED IN NAV mode of the flight director. This limitation applies to both flight director only and autopilot coupled operation
## Footnote
Use the APPR mode, or manually track the approach course using the HDG mode.
85
When is autopilot coupled operation prohibited during a VOR approach?
When the VOR is located behind the airplane by more than 15 miles, unless using the HDG mode.
86
What is prohibited regarding the non-coupled side Flight Director?
The non-coupled side Flight Director must not be displayed unless the coupled side Flight Director is being displayed.
## Footnote
Failure to adhere will result in incorrect Flight Director guidance.
87
What conditions must exist to require a tactile inspection of the wing for ice?
OAT < 10°C (50°F)
Cannot be determined if the wing fuel temp is above 0°C
There is moisture present (rain, sleet, snow, fog, etc)
Water is present on the upper wing surface
The difference between the dew point and OAT is 3°C or less
Atmospheric Conditions have been conducive to frost formation
88
What is max fuel quantity?
4710lbs
89
What is the maximum batter temperature?
63°C/145°F - BATT OTEMP and MASTER WARNING
71°C/160°F - BATT OTEMP flashes
160°C + rapid voice and MASTER WARNING
