AirSprint US CJ2+ Limitations Flashcards
Memorize Aircraft Limitations for the CJ2+
1
Q
Maximum Design Ramp Weight
A
12,625 Pounds
2
Q
Maximum Design Takeoff Weight
A
12,500 Pounds
3
Q
Maximum Design Landing Weight
A
11,525 Pounds
4
Q
Maximum Design Zero Fuel Weight
A
9,700 Pounds
5
Q
Takeoff Weight is Limited by the Most Restrictive of the Following Requirements:
A
- Maximum Certified Takeoff Weight
- Maximum Takeoff Weight Permitted by Climb Requirements
- Takeoff Field Length
6
Q
Landing Weight is Limited by the Most Restrictive of the Following Requirements:
A
- Maximum Certified Landing Weight
- Maximum Landing Weight Permitted by Climb Requirements or Brake Energy Limits
- Landing Distance
7
Q
Maximum Time Above 840 degrees C ITT
A
30 Seconds
8
Q
Maximum Time Above 900 degrees C to 1000 degrees C ITT
A
15 Seconds
9
Q
ENG CTRL SYS FAULT L/R Annunciators
A
Extinguished
10
Q
Maximum Tailwind Component
A
10 KNOTS
11
Q
Maximum Crosswind Component
A
10 KNOTS
12
Q
Maximum Time to Light-Off
A
10 Seconds
13
Q
Minimum Engine Oil Temperature
A
-40 degrees C
14
Q
Maximum Airport Elevation for Ground Battery Start
A
14,000 Feet
15
Q
Maximum Airport Elevation for Ground External Power Start
A
14,000 Feet
16
Q
Minimum Battery Voltage for Battery Start
A
24 VDC
17
Q
Minimum/Maximum External Power Current Capacity for Start
A
800/1100 AMPS
18
Q
Starter Cycle Limitations
A
Three engine starts per 30 minutes. Three cycles of operation with a 60 - Second rest period between cycles is permitted.
19
Q
Battery Limitations
A
- The battery temperature warning system must be operational for all ground and flight operations
- The battery temperature warning system preflight test in section III, normal procedures, must be satisfactorily completed
- if the BATT O’TEMP or BATT FAULT light illuminates during ground operation, do not take off until the proper maintenance procedures have been accomplished.
- Battery Cycle Limitations: Three engine starts per hour
20
Q
Battery Limitations - Cycles
A
- Three generator assisted cross starts are equal to one battery start
- If an external power unit is used for start, no battery cycle is counted
21
Q
Ground Operations
Maximum Generator Current per generator
A
200 AMPS
22
Q
Ground Operations
Limit pitot-static heat to____
A
2 minutes
23
Q
Ground Operation
with N2 at 75% RPM or greater limit engine, wing, and/or windshield anti-ice to_______
A
2 minutes
24
Q
Ground Operations
Do not operate with the wing anti-ice for more than _______ after the WING ANTI-ICE L/R annunciators have extinguished.
A
1 minute
25
Ground Operations
Ambient surface temperature must be obtained from the RAT display at the bottom of each PFD, with either or both engines operating, or from an appropriate ground station. The _____ display is unreliable on the ground.
SAT
26
Use _______ isopropyl alcohol for windshield anti-ice
TT-I-735
27
Use ________________ type hydraulic Fluids only
MIL-PRF-83282
28
Fuel Boost Pumps - ON; when L and/or R FUEL LOW LEVEL caution lights illuminate or at ___________ pounds or less indicated fuel
220 + or - 40 Pounds
29
Approved Fuels
```
JET A
Jet A1
Jet 3
JP-8
RT
TS-1
```
30
Approved Oils
| Can they be mixed?
Mobil Jet II
Mobile 254
Yes
31
Maximum Operating Limit Speeds
1. Mmo (Above 29,123 Feet)
2. Vmo (Between 8,000 and 29,123 Feet
3. Vmo ( Below 8,000 Feet)
1. 0.737 Mach
2. 278 KIAS
3. 260 KIAS
32
Maximum Flap Extnded Speed - Vfe
1. Takeoff and Approach (15)
2. Land position (35)
3. Maximum Speed With Flaps Failed to Ground Flaps (60)
1. 200 KIAS
2. 161 KIAS
3. 140 KIAS
33
Full application of rudder and aileron controls, as well as maneuvers that involve angle-of-attack near the stall should be confined to speeds below _____________ speed. Refer to LOAD FACTOR limitations for pitch maneuvering limitations.
Maximum Maneuvering
34
Maximum Landing Gar:
1. Extended Speed - Vle
2. Operating Speed - Vlo (Extending)
3. Operating Speed - Vlo (Retracting)
1. 200 KIAS
2. 200 KIAS
3. 200 KIAS
35
Maximum Speed Brake Operation Speed Vsb
No Limit
36
Maximum Autopilot Operation Speed
278 KIAS or Mach 0.737
37
Maximum Tire Ground Speed
165 Knots
38
Intentional selection of ground flaps in flight is ______
Prohibited
39
The ground flaps position is _____ locked out in flight. Selection of ground flaps will significantly increase drag and sink rate.
not
40
Takeoff and landing Operational Limits
Maximum Altitude Limit
14,000 feet
41
Takeoff and landing Operational Limits
Maximum Tailwind Component
10 Knots
42
Takeoff and landing Operational Limits
Minimum Ambient Temperature
-54 degrees C
43
Takeoff and landing Operational Limits
The maximum asymmetric fuel differential is _____ pounds, however controllability for safe return and landing has been demonstrated with an emergency asymmetrical difference of ______ pounds.
200 Pounds
600 Pounds
44
Cabin temperature must be held at or above _________ for a minimum of 20 minutes prior to takeoff, after a prolonged ground soak period (two hours or longer) at ambient temperatures of ________ or colder.
What is this limitation effect?
0 degrees C (+32 degrees F)
-10 degrees C (+14 degrees F)
Passenger oxygen masks deployment and operation.
45
Prior to takeoff, Channels A and B of the L and R FADECs must be _________
Operational
46
Takeoff is _________ with and ENG CTRL SYS FAULT L/R light illuminated prior to takeoff.
Prohibited
47
The Autopilot and yaw damper must be ______ for takeoff and landing.
OFF
48
The following systems must be operational and must have satisfactorily completed the preflight checks in Section III, Normal Procedures:
1. Rudder Bias
2. Angle of Attack
3. Electric Elevator Trim
4. Flaps
5. Flight Controls
6. Stall Warning System
49
Engine synchronizer must be _____ for takeoff and landing.
Off
50
Takeoff is prohibited when antiskid is inoperative and flaps are in the _____ position
Up
51
Takeoffs and landings are limited to _______ runway surfaces.
Paved
52
___________ must be retracted prior to 50 feet AGL before landing
Speedbrakes
53
Cabin must be _______ for takeoff and landing
depresurized
54
Extending Ground Flaps during touch and go landings is _____________.
Prohibited
55
The GND IDLE switch must be in the _________ position when conducting touch and go landings. For normal takeoff operations, the GND IDLE switch must be in the _____ position.
HIGH
NORMAL
56
Takeoff is limited to the Flaps ________ position when Type II, Type III, or Type IV anti-ice fluid is on the airplane.
UP (0degrees)
57
Takeoff is prohibited with the following forms of contamination:
With frost adhering to the following critical areas:
1.
2.
3.
1. Wing leading edge
2. Upper Wing Surface
3. Windshield
58
```
Takeoff is prohibited with the following forms of contamination:
With ice, snow or slush adhering to the following critical areas:
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
```
1. Wing Leading Edge and Upper Wing Surface, Flight Control Surfaces including all hinge gaps.
2. Horizontal Stabilizer
3. Vertical Stabilizer
4. Engine Inlets
5. Top of Engine Pylons
6. Top of Fuselage
7. Windshield
8. All Pitot Probes and Static Ports
9. Angle of Attack Vanes
10. Upper surface of nose forward of the windshield
59
Takeoff is prohibited with the following forms of contamination:
A visual and tactile check of the wing leading edge and wing upper surface must be performed to ensure the wing is free from frost, ice, snow, or slush when the outside air temperature is less than _______ or if it cannot be determined wing fuel temperature is above _____ and :
a. There is ____________ present (rain, drizzle, sleet, snow, fog, etc.)
b. Water is ____ on the wing upper surface.
c. The difference between the ______ and the outside temperature is 3 degrees C (5 degrees F) or less.
d. The atmospheric conditions have been conducive to ____ formation.
10 degrees C (50 degrees F)
0 degrees C (32 degrees F)
a. Visible Moisture
b. present
c. dew point
d. frost
60
Minimum airspeed for sustained flight in icing conditions (except approach and landing) is _________
160 KIAS
61
In icing conditions, operating the airplane at other than flaps 0 degrees for an extended period of time (except approach and landing is ________.
prohibited
62
Minimum engine N2 speed for effective wing anti-icing is ____________
80% N2
63
Minimum temperature for operation of tail deicing boots (indicated RAT)
-35 degrees C (-31 degrees F)
64
After an icing encounter with inoperative tail deice boots, maximum flap deflection is _________.
15 degrees
65
Maximum Operating Altitude.
45,000 Feet
66
Maximum Generator Current (per Generator) Airborne
300 Amperes up to 41,000 Feet
| 250 Amperes above 41,000 Feet
67
Maximum altitude for extension of flaps and/or landing gear
18,000 Feet
68
The Williams FJ44-3A-24 engines each produce _____ pounds of static takeoff thrust at sea level, flat-rated to 22 degrees C (72 degrees F)
2416
69
During in-flight windmilling, the engine will vent oil overboard. Typical consumption is approximately _____ gallons per hour.
0.02
70
Fuel anti-icing additive ______ required.
is not
71
Flight through severe turbulence should be avoided if possible. The following procedures are recommended for flight in severe turbulence.
1. airspeed ________
2. Maintain a constant ________ without chasing the altitude. Avoid sudden large control movements.
3. Operation of ______ is recommended in basic modes only (ROL and PIT only)
1. approximately 180 KIAS
2. attitude
3. autopilot
72
Takeoff performance is degraded when Type II, Type III, or Type IV anti-ice fluid is on the airplane. The fluid that remains on the airplane during takeoff causes the _____ forces at rotation to be increased and the takeoff distance to be increased.
elevator
72
Maximum allowable luggage forward compartment is__________
400 pounds
73
Maximum allowable luggage aft storage compartment is____________
600 pounds.
73
Maximum allowable luggage aft storage compartment is____________
600 pounds.
