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Fly Exclusive > Memory items - Limitations CJ3+ > Flashcards

Memory items - Limitations CJ3+ Flashcards

1
Q

Ramp Weight

A

14,070 Pounds

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2
Q

Takeoff Weight

A

13,870 Pounds

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3
Q

Landing Weight

A

12,750 Pounds

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4
Q

Zero Fuel Weight

A

10,675 Pounds

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5
Q

ENGINE OPERATING LIMITS

A

Takeoff thrust settings that are nominally limited to 5 minutes duration may be used for up to 10 minutes for One Engine Inoperative operations.
The engine should not be operated above 80% N2 until oil temperature is above 10°C (+50°F).
Abort the start if N1 does not indicate rotation before 25% N2, or if the engine stops accelerating for 30 seconds.

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6
Q

Maximum Tailwind Component

A

10 Knots

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7
Q

Maximum Crosswind Component

A

10 Knots

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8
Q

Maximum Time to Light-off

A

10 Seconds

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9
Q

Minimum Engine Oil Temperature (indicated on EIS)

A

-40°C

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10
Q

Maximum Airport Elevation for Ground Battery start

A

14,000’

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11
Q

Maximum Airport Elevation for Ground External power start

A

14,000’

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12
Q

Minimum Battery Voltage for Battery Start

A

24 VDC

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13
Q

Minimum/Maximum External Power
Current Capacity For Start

A

800/1100 AMPS

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14
Q

ENG CTRL SYS FAULT L/R Annunciators for engine start

A

Extinguished

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15
Q

If engine oil temperature is below -40°C (-40°F), what must come first?

A

The engine must be preheated prior to conducting a start

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16
Q

If the battery has been cold soaked for 2 hours or longer at ambient surface temperature of -18°C (0°F) or lower, what must come first?

A

It must be preheated to above -18°C (0°F) prior to start.

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17
Q

How long to get the Engine Indicating System to work when the aircraft is cold soaked below -10°C (+14°F).

A

1 to 6 minutes

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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.

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19
Q

BATTERY LIMITATIONS

A
  1. The battery temperature warning system must be operational for all ground and flight operations.
  2. Battery Cycle Limitations: Three engine starts per hour.
  3. Three generator assisted cross starts are equal to one battery start.
  4. If an external power unit is used for start, no battery cycle is counted.
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20
Q

Maximum Generator Current (per generator) (ground)

A

200 Amperes

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21
Q

How long to limit ground operation of pitot/static heat to preclude damage to the pitot tubes and angle of attack vane.

A

2 Minutes

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22
Q

Ground operation at greater than 75% N2 engine RPM with engine, wing, and/or windshield anti-ice on is limited to how long?

A

2 minutes. Do not operate with the wing anti-ice on more than one minute after the WING ANTI-ICE L/R annunciators have extinguished.

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23
Q

Where must the temperature be obtained during ground operations?

A

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 SAT display is unreliable on the ground.

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24
Q

FUEL LIMITATIONS - When must the fuel pumps be on?

A

Fuel Boost Pumps – ON; when FUEL LOW LEVEL L and/or R caution lights illuminate or at 210 pounds or less indicated fuel.

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25
Q

Fuel imbalance

A

Maximum approved fuel imbalance is 200 lbs. A fuel imbalance of 600 lbs. has been demonstrated for emergency return.

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26
Q

Fuel additives

A

EGME/DIEGME additive is approved for use, but not required, at a concentration not to exceed 0.15 percent volume.

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27
Q

UNUSABLE FUEL LIMITATIONS

A

Fuel remaining in the fuel tanks when the fuel quantity indicator reads zero is not usable in flight

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28
Q

MMO (Above 29,300 Feet)

A

0.737 Mach (Indicated)

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29
Q

VMO (Between 8000 and 29,300 Feet)

A

278 KIAS

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30
Q

VMO (Below 8000 Feet)

A

260 KIAS

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31
Q

Maximum Flap Extended Speed – VFE (TO & approach position (15°)

A

200 KIAS

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32
Q

Maximum Flap Extended Speed – VFE (landing position (35°)

A

161 KIAS

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33
Q

Maximum Speed with Flaps Failed to Ground Flaps (55°)

A

140 KIAS

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34
Q

Maximum Landing Gear Extended Speed – VLE

A

200 KIAS

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35
Q

Maximum Landing Gear Operating Speed – VLO (Extending)

A

200 KIAS

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36
Q

Maximum Landing Gear Operating Speed – VLO (Retracting)

A

200 KIAS

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37
Q

Maximum Speed Brake Operation Speed – VSB

A

No Limit

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38
Q

Maximum Autopilot Operation Speed

A

278 KIAS or 0.737 Mach

39
Q

Minimum Speed for Sustained Flight in Icing Conditions (except takeoff approach and landing)

A

180 KIAS

40
Q

GROUND FLAPS LIMITATIONS - Intentional selection of Ground flap operation in flight?

A

Intentional selection of Ground Flaps in flight is prohibited.

41
Q

Is the Ground Flap inaccessible during flight?

A

The ground flaps position is not locked out in flight. Selection of ground flaps will significantly increase drag and sink rate.

42
Q

Max altitude for TO&L

A

14,000’

43
Q

Maximum Tailwind Component

A

10 Knots

44
Q

Minimum Ambient Temperature for TO&L

A

-54°C (-65°F)

45
Q

How long and to what temperature must the cabin be heated to before take off?

A

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 (two hours or longer) at ambient temperatures of -10°C (+14°F) or colder (refer to Normal Procedures, COLD WEATHER OPERATIONS).

46
Q

Auto pilot and yaw damper use during TO&L

A

The autopilot and yaw damper must be OFF for takeoff and landing

47
Q

Engine synchronizer use during TO&L operations

A

Engine synchronizer must be OFF for takeoff and landing.

48
Q

Is take off allowed if the anti skid system is inoperable?

A

Takeoff is prohibited if the antiskid system is inoperative

49
Q

Cabin pressurization during TO&L

A

Cabin must be depressurized for takeoff and landing.

50
Q

Can we use a grass field for TO&L?

A

Takeoffs and landings are limited to paved runway surfaces

51
Q

Can we use speed brakes during TO&L?

A

Speed brakes must be retracted prior to 50 feet AGL before landing

52
Q

Can we use ground flaps during touch and go operations?

A

Extending Ground Flaps during touch and go landings is prohibited

53
Q

What position must the GROUND IDLE switch be in for touch and go operations? Normal TO operations?

A

The GROUND IDLE switch must be in the HIGH position when conducting touch and go landings. For normal takeoff operations, the GROUND IDLE switch must be in the NORMAL position.

54
Q

Maximum Tire Ground Speed

A

165 Knots

55
Q

What position must the flaps be in when using type II, III, and IV anti-ice fluids?

A

Takeoff is limited to the flaps up configuration when Type II, III, or IV anti-ice fluid has been applied to the airplane.

56
Q

May a take off be conducted with a warning annunciator displayed?

A

Takeoff may not be initiated with a warning annunciator displayed. Takeoff may not be initiated with a caution annunciator displayed unless the associated system or component has been deferred per an approved Minimum Equipment List (MEL). When dispatching in this manner, if the procedure associated with the caution annunciator includes “Land as soon as practical” as a step, the step may be ignored.

57
Q

Take off prohibited with Frost in which areas?

A

Wing Leading Edge
Upper Wing Surface
Windshield

58
Q

Take off prohibited with snow, ice, or slush on which areas?

A

a. Wind Leading Edge and Upper Wing Surface
b. Flight Control Surfaces including all hinge gaps
c. Horizontal Stabilizer
d. Vertical Stabilizer
e. Engine Inlets
f. Top of Engine Pylons
g. Top of Fuselage
h. Windshield
i. All Pitot Probes and Static Ports
j. Angle of Attack Vanes
k. Upper surface of nose forward of the windshield

59
Q

How would you go about checking for icing on the aircraft?

A

A visual and tactile (hand on surface) 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 10°C (50°F) or if it cannot be determined that the wing fuel temperature is above 0°C (32°F) and any of the following conditions exist:
a. There is visible moisture present (rain, drizzle, sleet, snow, fog, etc.); or
b. Water is present on the upper wing surface; or
c. The difference between the dew point and the outside air temperature is 3°C (5°F) or less; or
d. The atmospheric conditions have been conducive to frost formation.

60
Q

Enroute operational limits - Maximum Operating Altitude

A

45,000’

61
Q

Maximum Generator Current (per generator in flight)

A

300 Amperes Up to 41,000 Feet
250 Amperes Above 41,000 Feet

62
Q

Maximum altitude for extension of flaps and/or landing gear

A

18,000 Feet

63
Q

Maximum operating altitude with inoperative Yaw Damper

A

30,000 Feet

64
Q

Normal Cabin Pressurization Limitations

A

-0.5 to 9.0 PSI

65
Q

Where can icing conditions exist in flight?

A

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 (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals).

66
Q

Where can icing conditions exist on the ground?

A

Icing conditions on the ground exist when the OAT or indicated RAT is +10°C (+50°F) or below and, where surface snow, slush, ice or standing water may be ingested by the engines or freeze on engine nacelles, or engine sensor probes.

67
Q

Can flaps be used in icing conditions?

A

In icing conditions, operating the airplane at other than flaps 0 for an extended period of time (except approach and landing) is prohibited.

68
Q

What is the minimum N2 speed for effective wing anti-icing?

A

75% N2

69
Q

What is the minimum temperature for operation of the tail deicing boots?

A

Minimum temperature for operation of tail deicing boots (Indicated RAT): -35°C (-31°F)

70
Q

When do the WING/ENGINE ANTI-ICE switches need to be on in flight?

A

The WING/ENGINE ANTI-ICE 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. Failure to observe this limitation may result in ENG CTRL SYS FAULT L/R annunciations due to ice accumulation on the engine PT2/TT2 probe.

71
Q

When do the WING/ENGINE ANTI-ICE switches need to be on - on the ground?

A

Engine anti-ice must be ON during ground operations in icing conditions, except selection of anti-ice on is prohibited for 1 minute after ground engine start (to ensure accurate RAT for takeoff). If engine anti-ice was inadvertently turned ON prior to 1 minute of engine operation, the anti-ice must be turned off for 2 minutes before turning it back on. If minor engine vibrations are felt or heard during ground operations, the crew must momentarily increase engine speed (typically 20-30% N1) to assist with shedding the accumulated ice from the spinner, fan, and stators.

72
Q

Can 1 wing inspection light be inop when flight at night in known icing be allowed?

A

All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night.

73
Q

Severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues:

A
  1. Unusually extensive ice accumulation on the airframe and windshield in areas not normally observed to collect ice.
  2. Accumulation of ice on the upper surface of the wing that extends more than 12 to 18 inches aft of the heated leading edge.
74
Q

If one ore more of these visual cues exist while in severe icing conditions, what shall the pilot do?

A
  1. Use of the autopilot is prohibited.
  2. Immediately request priority handling from Air Traffic Control to facilitate a route or altitude change to exit the icing conditions.
  3. Leave flaps in current position, do not extend or retract.
  4. Avoid abrupt and excessive maneuvering that may exacerbate control difficulties.
  5. If unusual or uncommanded roll control movement is observed, reduce angle-of-attack.
75
Q

Since the autopilot, when installed and operating, may mask tactile cues that indicate adverse changes in handling characteristics, use of the autopilot is prohibited when?

A
  1. Unusual lateral trim is required while the airplane is in icing conditions.
  2. Autopilot trim warnings are encountered while the airplane is in icing conditions.
76
Q

Nose Baggage Compartment

A

400 Pounds

77
Q

Aft Baggage Compartment

A

600 Pounds

78
Q

GROUND OPERATIONAL LIMITS

A
  1. Limit ground operation of pitot-static heat to 2 minutes to prevent damage to the pitot tubes and angle-of-attack vane.
  2. Do not operate with wing anti-ice on more than 1 minute after the WING A/I COLD message has cleared.
  3. At least one engine must be running before the RAT indication on the MFD is used for ambient surface temperature.
  4. Do not exceed 60% N1 with a tailwind component greater than 10 knots.
79
Q

Can takeoff be allowed if battery charging is more than 20 amps?

A

Takeoff is prohibited until the battery charging amps is 20 amps or less.

80
Q

RVSM OPERATIONS LIMITS

A

Airspeed Limits - Minimum speed in RVSM airspace: 150 KIAS
Weight Limits - Minimum weight in RVSM airspace: 8,750 Pounds

81
Q

MANEUVER LIMITS

A

Acrobatic maneuvers, including spins, are prohibited.
Intentional stalls are prohibited above 18,00 feet.

82
Q

ANGLE OF ATTACK AND STALL WARNING SYSTEM

A

The angle-of-attack system may be used as a reference but does not replace the airspeed display in the PFD as a primary instrument.

83
Q

HF RADIO

A

Navigation based solely on the ADF is prohibited during HF radio transmissions. Alternate primary means of navigation should be selected prior to HF radio use.

84
Q

RED BATTERY OVERTEMP CAS message

A

Do not take off until the proper maintenance procedures have been accomplished, even if the message subsequently clears.

85
Q

OXYGEN SYSTEM

A
  1. Crew and passenger oxygen masks are not approved for use above 40,000 feet cabin altitude. Prolonged use of passenger masks above 25,000 feet cabin altitude is not recommended.
  2. Prior to flight, the crew oxygen mask must be checked and stowed properly in its receptacle to qualify as a quick donning oxygen mask.
  3. For single pilot operations, a crew oxygen mask must be available for a passenger occupying the right crew seat. The mask must be checked during preflight and passenger briefed on its use.
  4. Cabin temperature must be held at or above 0°C (+32°F) for a minimum of 20 minutes prior to operations above FL240 after a prolonged ground cold soak period (two hours or longer) at ambient temperatures of -10°C (+14°F) or colder. This temperature ensures proper deployment and operation of the passenger oxygen masks. This limitation does not apply if there are no passengers in the cabin.
86
Q

PASSENGER COMPARTMENT

A

The lavatory door or curtain must be latched open for taxi, takeoff, and landing.
The lavatory is limited to one occupant.

87
Q

GARMIN G3000 INTEGRATED AVIONICS SYSTEM - General Limits

A

All display units must be operational. Takeoff with a display in reversion mode is prohibited.
· The fuel quantity, fuel required, fuel remaining, and gross weight estimate functions of the G3000 are supplemental information only and must be verified by the flight crew.
· Do not use data link weather information shown on any display for maneuvering in or near areas of hazardous weather. The data link weather information is intended to assist in avoiding hazardous weather. The actual age of the weather phenomena may be significantly older than the indicated age of the data link weather product.

88
Q

GARMIN G3000 INTEGRATED AVIONICS SYSTEM - Autopilot Limits

A
  1. One pilot must remain seated with the seat belt fastened during all autopilot operations.
  2. Autopilot minimum use height:
    A. Takeoff and Climb – 350 feet above runway
    B. Enroute and descent – 1000 feet AGL
    C. Approach (all Modes) – 160 feet above runaway
89
Q

GARMIN G3000 INTEGRATED AVIONICS SYSTEM - Navigation Limits

A

Takeoff is prohibited with the GEO LIMITS system message displayed.
· Instrument approaches using FMS guidance must be retrieved from the navigation database. The navigation database must be up to date. Inserting waypoints into a published approach is prohibited.
· Use of FMS as primary guidance is prohibited on the final approach segment of ILS, LOC, LOC-BC, SDF, or any other approach not approved for GPS overlay.
· Prior to the FAF, make sure that the ILS or VOR auto-selected course (as appropriate) matches the final approach course on the published approach.
· Use of AP or FD coupled to GS for LDA-GS approaches is prohibited. The GS mode may not capture the glideslope on LDA approaches.

90
Q

GARMIN G3000 INTEGRATED AVIONICS SYSTEM - Synthetic Vision Technology

A
  1. Aircraft maneuvering in any flight phase shall not be based solely on information from the SVT. SVT shall not be used as the primary means of terrain, obstacle or traffic avoidance.
  2. The SVT shall not be used for primary flight guidance.
  3. Descent below published IFR minimums shall not be predicated upon the use of SVT.
91
Q

GARMIN G3000 INTEGRATED AVIONICS SYSTEM - Takeoff and Landing Data (TOLD)

A

The current database must be used when takeoff/landing performance data is obtained from the FMS.
· The V-Speeds, required field length and other performance information for a specific operation MUST be obtained from a single source, either ARM, CPCalc or FMS.
· It is the responsibility of the crew to verify all inputs regarding airplane configuration, weight, runway information and ambient conditions.

92
Q

Engine Operation During Low-g Maneuvering Flight

A

The engine is limited to 10 seconds of continuous flight at zero- or negative-g

93
Q

Engine type

A

Williams international FJ44-3A

94
Q

Minimum maneuvering speed

A

Clean - Vref+30
Flap 15 - Vref+20
Flap 30 - Vref +10

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