Limitations Flashcards
1
Q
MAX RAMP WEIGHT
A
14,070 lbs
2
Q
MAX TAKEOFF WEIGHT
A
13,870 lbs
3
Q
MAX LANDING WEIGHT
A
12,750 lbs
4
Q
MAX ZERO FUEL WEIGHT
A
10,510 lbs
5
Q
NOSE BAGGAGE WEIGHT LIMIT
A
400 lbs
6
Q
TAIL BAGGAGE WEIGHT LIMIT
A
600 lbs
7
Q
MMO (>29,300 ft)
A
Mach .737
8
Q
VMO (8,000’ – 29,300’)
A
278 KIAS
9
Q
VMO (< 8,000’)
A
260 KIAS
10
Q
VFE (15° / 35°/ Failed at 55°)
A
200 / 161 / 140 KIAS
11
Q
VLE/VLO
A
200 KIAS
12
Q
VSB
A
No Limit
13
Q
Max speed for Autopilot Operation
A
278 KIAS / Mach .737
14
Q
Tire Limit Speed
A
165 Knots
15
Q
Minimum Speed in Icing Conditions
Flaps 0°
A
180 KIAS
16
Q
Is engine start with an ENG CNTRL FAULT L and/or R message displayed permitted?
A
Not Permitted
17
Q
Battery start limit
A
3 per hour
18
Q
One battery start = __ generator starts
A
3 generator starts
19
Q
External power start = __ battery starts
A
Zero battery starts
20
Q
What power source is used in an Air Start?
A
Battery
21
Q
Engine start duty cycles
A
3 starts per 30 minutes with 60 seconds rest between cycles.
22
Q
Abort if N1 does not indicate before __
A
25% N2
23
Q
Abort start if engine stops accelerating for
A
30 seconds
24
Q
Max time to light-off
A
10 seconds (first indication of fuel flow to increase in ITT)
25
Minimum oil temperature prior to power increase above 80% N2
10°C
26
Max elevation for battery or cross generator starts
14,000 ft
27
Max tailwind/crosswind component for engine start
10 kts
28
Minimum battery voltage for engine start
24 VDC
29
Max external power voltage for start
29 VDC
30
Min/Max external power current for start
800/1100 AMPS
31
Minimum oil temperature
-40°C
32
Minimum battery temperature
-18°C
33
If aircraft has been cold soaked below ____, the FADEC must be warmed with electrical
power for at least _ minutes followed by a power cycle with the battery switch.
-40°C; 3 minutes
34
Pitot/static heat ground time limit.
2 minutes
35
Engines above 75% N2 with wing, engine, and/or windshield anti-ice on is limited to ______ on the ground.
2 minutes
36
Wing anti-ice limited to ______ after WING ANTI-ICE COLD message has extinguished
during preflight checks.
1 minute
37
Temperature must be obtained by _______ with either/both engines running or from an
___________ when the engines are not running.
RAT on MFD; appropriate ground station
38
N1 is limited to ___ with a tailwind component greater than _____.
60%; 10 knots
39
Max takeoff/landing altitude.
14,000 ft
40
Max Tailwind Component
10 kts
41
Takeoff prohibited if:
-Any red message is displayed
-Any amber message is displayed unless the MEL is complied with
-ENG CNTRL FAULT L and/or R message is displayed
-Antiskid system is inoperative
-Battery charging amps is more than 20 amps
-Frost, ice, snow, or slush is adhering to critical areas (refer to AFM for
specifics)
42
__________ must be disengaged for takeoff/landing.
Autopilot and yaw damper
43
Cabin must be ________ prior to landing.
depressurized
44
Takeoffs/landings limited to _____ runway surfaces.
paved
45
Speed brakes must be retracted prior to ____ for landing (except where required by AFM
procedures).
50’ AGL
46
Extending ground flaps during touch-and-go landings is ________.
prohibited
47
Takeoff limited to flaps __° when Type II, III or IV anti-ice has been applied.
0
48
A visual and tactile check of the wing leading edge and upper surface when the OAT is __°C or if it cannot be determined the wing fuel temp is __°C and there is visible moisture present, or water is present on the upper wing surface, or the difference between the dew point and OAT is __°C, or the atmospheric conditions have been conductive to frost formation.
< 6; > 0; ≤ 3
49
The tactile check must be accomplished within _ minutes of takeoff.
5
50
If the aircraft is treated with deice/anti-ice fluid, the tactile check may be done anytime between _______and_____, provided the time is within the max holdover time.
the final application and takeoff
51
Max Operating Altitude
FL450
52
Max Operation Altitude with autopilot and yaw damper inop.
FL300
53
Max Altitude for flaps/landing gear extension.
FL180
54
Minimum speed in RVSM airspace.
150 KIAS
55
Minimum weight in RVSM airspace.
8,750 lbs
56
Prohibited maneuvers.
Acrobatic maneuvers including spins.
57
Intentional stalls above ______ are prohibited.
18,000 ft
58
Load factor limits @ 13,870 lbs.
Flaps 0° – -1.44 to 3.6G
| Flaps 15° or 35° – 0.0 to +2.0G
59
Takeoff with a display in _______ mode is prohibited.
reversion
60
Are CAT II approaches approved?
NO
61
Minimum autopilot use heights:
Takeoff and Climb?
Enroute and Descent?
Approaches?
350 ft AGL
1000 ft AGL
160 ft above runway
62
The V-speeds, required field length and other performance information for a specific
operation must be obtained from ________.
a single source; i.e., either the AFM, CPCalc, or FMS
| Takeoff and Landing Performance Data.
63
If the BATTERY OVERTEMP message appears on the ground, __________.
maintenance must be performed before takeoff, even if the message clears.
64
Generator Loads (max):
Ground
Air ≤ FL410
Air > FL410
200 Amps
300 Amps
250 Amps
65
Max fuel imbalance for normal ops.
200 lbs
66
Max demonstrated fuel imbalance for emergency return.
600 lbs
67
T/F, Unusable fuel (fuel remaining when fuel quantity reads 0) is not usable in flight.
True
68
Engine type
Williams International FJ44-3A turbofan
69
Engine thrust
2820 lbs. @ sea level up to 22°C
70
Approved Oils
Mobil Jet II & Mobil 254
71
Mixing of approved oils (IS / IS NOT) permissible.
Is permissible.
72
Max oil consumption
0.023 gallons / 1 hr (1 qt or L / 11 hrs)
73
Engine limited to __ seconds of continuous flight at 0 or negative Gs.
10
74
Structural cabin pressure
-0.5 to 9.0 PSI
75
What is the approved type of oxygen?
Aviator’s breathing oxygen (MIL-O-27210)
| Medical oxygen is prohibited.
76
Crew and passenger masks are not approved for use above ____ft cabin altitude.
40,000
77
Prolonged use of passenger masks above ____ft cabin altitude is not recommended.
25,000
78
Crew masks must be _______________ to qualify as quick donning.
checked and stowed properly
79
For single-pilot ops, a _________ must be available for a passenger occupying the right crew seat.
crew mask
80
If a prolonged ground cold soak (≥2 hours) at ambient temperatures of __°C or colder has
occurred, cabin temperature must be __°C for a minimum of __ minutes prior to operations
above ____ to ensure proper deployment and operation of the passenger masks.
-10; ≥ 0; 20 minutes; FL240
81
Which light must be operable for flight into know or forecast icing at night?
Wing inspection light.
82
Tail De-ice must be off when SAT is below ____.
-35°C
83
Wing and engine anti-ice may be operated in the ENG ONLY position when _______________________.
SAT is
84
Engine anti-ice must be __ during ground ops in icing conditions.
on
85
Engine anti-ice is prohibited for _____ after ground engine start.
1 minute
86
If engine anti-ice is selected before 1 minute, must be turned off for _______.
2 minutes
87
Required aircraft configuration in icing conditions.
Clean (except for approach and landing)
88
Minimum N2 for effective wing anti-ice
75% N2
89
Can the CJ3+ operate in severe icing?
No, it is prohibited.
90
Intentional selection of GROUND FLAPS (55°) in flight?
Prohibited
91
Maximum occupants
10 (including crew seats)
92
Lavatory door must be latched open for...
taxi, takeoff, and landing.
93
Lavatory max occupancy?
One
