Limitations

Question 1

WEIGHT LIMITATIONS
Maximum Design Ramp Weight:

Answer 1

WEIGHT LIMITATIONS
Maximum Design Ramp Weight:

14,070 Pounds

Question 2

WEIGHT LIMITATIONS
Maximum Design Landing Weight:

Answer 2

WEIGHT LIMITATIONS
Maximum Design Landing Weight:

12,750 Pounds

Question 3

WEIGHT LIMITATIONS
Maximum Design Zero Fuel Weight:

Answer 3

WEIGHT LIMITATIONS
Maximum Design Zero Fuel Weight:

10,510 Pounds

Question 4

ENGINE OPERATING LIMITS
Takeoff thrust settings that are nominally limited to __
minutes duration may be used for up to ___ minutes for One Engine Inoperative operations.
The engine should not be operated above 80% N2 until oil
temperature is above ________.
.

Answer 4

ENGINE OPERATING LIMITS
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).

Question 5

ENGINE START LIMITATIONS (GROUND)
Aircraft Configuration AH

ENG CTRL SYS FAULT L/R Annunciators: ___________
Maximum Tailwind Component: _____ Knots
Maximum Crosswind Component: _____ Knots
Maximum Time to Light-off: ____ Seconds
Minimum Engine Oil Temperature (indicated on EIS): _____

Answer 5

ENGINE START LIMITATIONS (GROUND)
Aircraft Configuration AH

ENG CTRL SYS FAULT L/R Annunciators: Extinguished
Maximum Tailwind Component: 10 Knots
Maximum Crosswind Component: 10 Knots
Maximum Time to Light-off: 10 Seconds
Minimum Engine Oil Temperature (indicated on EIS): -40°C

Question 6

ENGINE START LIMITATIONS (GROUND)
Aircraft Configuration AH

Maximum Airport Elevation For Ground Battery Start: _________

Maximum Airport Elevation For External Power Start: _________

Minimum Battery Voltage For Battery Start: _________

Minimum/Maximum External Power Current Capacity For Start: _________

Answer 6

ENGINE START LIMITATIONS (GROUND)
Aircraft Configuration AH

Maximum Airport Elevation For Battery Start: 14,000 Feet

Maximum Airport Elevation For External Power Start: 14,000 Feet

Minimum Battery Voltage For Battery Start: 24 VDC

Minimum/Maximum External Power Current Capacity For Start: 800/1100 AMPS

Question 7

ENGINE START LIMITATIONS (GROUND)
If engine oil temperature is below ______, the engine must be preheated prior to conducting a start. If the battery has been cold soaked for 2 hours or longer at ambient surface temperature of _____ or lower, it must be preheated to above -18°C (0°F) prior to start. The Engine Indicating System (EIS) may take ____ minutes to become usable after power is applied when cold soaked below -10°C (+14°F).

Answer 7

ENGINE START LIMITATIONS (GROUND)
If engine oil temperature is below -40°C (-40°F), the engine must be preheated prior to conducting a start. If the battery has been cold soaked for 2 hours or longer at ambient surface temperature of -18°C (0°F) or lower, it must be preheated to above -18°C (0°F) prior to start. The Engine Indicating System (EIS) may take 1 to 6 minutes to become usable after power is applied when cold soaked below -10°C (+14°F).

Question 8

STARTER CYCLE LIMITATIONS

Three engine starts per ___ minutes. Three cycles of
operation with a ___-second rest period between cycles is
permitted.

Answer 8

STARTER CYCLE LIMITATIONS

Three engine starts per 30 minutes. Three cycles of
operation with a 60-second rest period between cycles is
permitted.

Question 9

BATTERY LIMITATIONS

The battery temperature warning system must be
operational for all ______ and ______ operations.
Battery Cycle Limitations: _____ engine starts per hour.
Three generator assisted cross starts are equal to ___
battery start. If an external power unit is used for start, __ battery cycle is counted.

Answer 9

BATTERY LIMITATIONS

The battery temperature warning system must be
operational for all ground and flight operations.
Battery Cycle Limitations: Three engine starts per hour.
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.

Question 10

GROUND OPERATION LIMITATIONS

Maximum Generator Current (per generator): ______
Limit ground operation of pitot/static heat to ____ minutes to preclude damage to the pitot tubes and angle of attack vane. Ground operation at greater than 75% N2 engine RPM with engine, wing, and/or windshield 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.

Answer 10

GROUND OPERATION LIMITATIONS
Maximum Generator Current (per generator): 200 Amperes
Limit ground operation of pitot/static heat to two minutes to two preclude damage to the pitot tubes and angle of attack vane. Ground operation at greater than 75% N2 engine RPM with engine, wing, and/or windshield anti-ice on is limited to two minutes. Do not operate with the wing anti-ice on more than one minute after the WING ANTI-ICE L/R annunciators have extinguished.

Question 11

GROUND OPERATION LIMITATIONS
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.

Answer 11

GROUND OPERATION LIMITATIONS
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.

Question 12

FUEL LIMITATIONS
Fuel Boost Pumps - ON; when FUEL LOW LEVEL L and/or R caution lights illuminate or at ____ pounds or less indicated fuel. Maximum approved fuel imbalance is ___ lbs. A fuel imbalance of 600 lbs. has been demonstrated for emergency return. EGME/DIEGME additive is _________ for use, but not required, at a concentration not to exceed 0.15 percent volume.

Answer 12

FUEL LIMITATIONS
Fuel Boost Pumps - ON; when FUEL LOW LEVEL L and/or R caution lights illuminate or at 210 pounds or less indicated fuel. Maximum approved fuel imbalance is 200 lbs. A fuel imbalance of 600 lbs. has been demonstrated for emergency return. EGME/DIEGME additive is approved for use, but not required, at a concentration not to exceed 0.15 percent volume.

Question 13

UNUSABLE FUEL LIMITATIONS
Fuel remaining in the fuel tanks when the fuel quantity indicator reads zero is ___ _______in flight.

Answer 13

UNUSABLE FUEL LIMITATIONS
Fuel remaining in the fuel tanks when the fuel quantity indicator reads zero is not usable in flight.

Question 14

SPEED LIMITATIONS
Maximum Operating Limit Speeds
MMO (Above 29,300 Feet)

Answer 14

SPEED LIMITATIONS
Maximum Operating Limit Speeds
MMO (Above 29,300 Feet)

.737 Mach (Indicated)

Question 15

SPEED LIMITATIONS
Maximum Operating Limit Speeds

VMO (Between 8000 and 29,300 Feet)

Answer 15

SPEED LIMITATIONS
Maximum Operating Limit Speeds

VMO (Between 8000 and 29,300 Feet)

278 KIAS

Question 16

SPEED LIMITATIONS
Maximum Operating Limit Speeds

VMO (Below 8000 Feet)

Answer 16

SPEED LIMITATIONS
Maximum Operating Limit Speeds

VMO (Below 8000 Feet)

260 KIAS

Question 17

SPEED LIMITATIONS
Maximum Operating Limit Speeds

Maximum Flap Extended Speed - V_FE

_{TAKEOFF AND APPROACH Position (15°)}

Answer 17

SPEED LIMITATIONS
Maximum Operating Limit Speeds

Maximum Flap Extended Speed - V_FE

_{TAKEOFF AND APPROACH Position (15°)}

200 KIAS

Question 18

SPEED LIMITATIONS
Maximum Operating Limit Speeds

Maximum Flap Extended Speed - V_FE

_{LAND Position (35°)}

Answer 18

SPEED LIMITATIONS
Maximum Operating Limit Speeds

Maximum Flap Extended Speed - V_FE

_{LAND Position (35°)}

161 KIAS

Question 19

SPEED LIMITATIONS
Maximum Operating Limit Speeds

Maximum Flap Extended Speed - V_FE

_{Maximum Speed With Flaps Failed to Ground Flaps (55°)}

Answer 19

SPEED LIMITATIONS
Maximum Operating Limit Speeds

Maximum Flap Extended Speed - V_FE

_{Maximum Speed With Flaps Failed to Ground Flaps (55°)}

140 KIAS

Question 20

SPEED LIMITATIONS
Maximum Landing Gear
Extended Speed - VLE

Answer 20

SPEED LIMITATIONS
Maximum Landing Gear
Extended Speed - VLE

200 KIAS

Question 21

SPEED LIMITATIONS
Maximum Landing Gear
Operating Speed - VLO (Retracting)

Answer 21

SPEED LIMITATIONS
Maximum Landing Gear
Operating Speed - VLO (Retracting)

200 KIAS

Question 22

SPEED LIMITATIONS
Maximum Landing Gear
Operating Speed - VLO (Retracting)

Answer 22

SPEED LIMITATIONS
Maximum Landing Gear
Operating Speed - VLO (Retracting)

200 KIAS

Question 23

SPEED LIMITATIONS
Maximum Speed Brake Operation Speed - VSB

Answer 23

SPEED LIMITATIONS
Maximum Speed Brake Operation Speed - VSB

NO LIMIT

Question 24

SPEED LIMITATIONS

Maximum Autopilot Operation Speed

Answer 24

SPEED LIMITATIONS

Maximum Autopilot Operation Speed

278 KIAS or 0.737 Mach

Question 25

SPEED LIMITATIONS

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

Answer 25

SPEED LIMITATIONS

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

180 KIAS

Question 26

GROUND FLAPS LIMITATIONS
Intentional selection of Ground Flaps in flight is _________.
The ground flaps position is not locked out in flight.
Selection of ground flaps will significantly increase ____ and ____ rate.

Answer 26

GROUND FLAPS LIMITATIONS
Intentional selection of Ground Flaps in flight is prohibited.
The ground flaps position is not locked out in flight.
Selection of ground flaps will significantly increase drag and sink rate.

Question 27

TAKEOFF AND LANDING
OPERATIONAL LIMITS
Aircraft Configuration AH
Maximum Altitude Limit

Answer 27

TAKEOFF AND LANDING
OPERATIONAL LIMITS
Aircraft Configuration AH
Maximum Altitude Limit

14,000 Feet

Question 28

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Maximum Tailwind Component

Answer 28

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Maximum Tailwind Component

10 KIAS

Question 29

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Minimum Ambient Temperature

Answer 29

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Minimum Ambient Temperature

-54°C (-65°F)

Question 30

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Cabin temperature must be held at or above 0°C (+32°F) for a minimum of ___ 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).

Answer 30

TAKEOFF AND LANDING
OPERATIONAL LIMITS

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).

Question 31

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Speed brakes must be retracted prior to ___ feet AGL before landing. Extending Ground Flaps during touch and go landings is _________. The GROUND IDLE switch must be in the _____ position when conducting touch and go landings. For normal takeoff operations, the GROUND IDLE switch must be in the ________ position.

Answer 31

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Speed brakes must be retracted prior to 50 feet AGL before landing. Extending Ground Flaps during touch and go landings is prohibited. 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.

Question 32

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Maximum Tire Ground Speed:

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

Answer 32

TAKEOFF AND LANDING
OPERATIONAL LIMITS

Maximum Tire Ground Speed:

165 Knots

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

Question 33

TAKEOFF AND LANDING
OPERATIONAL LIMITS

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 _________ 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 _______.

Answer 33

TAKEOFF AND LANDING
OPERATIONAL LIMITS

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.

Question 34

TAKEOFF AND LANDING
OPERATIONAL LIMITS

2. With ice, snow, or slush adhering to the following critical areas:
   a. ____ ______ ____ 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

Answer 34

TAKEOFF AND LANDING
OPERATIONAL LIMITS

2. With ice, snow, or slush adhering to the following critical areas:
   a. Wing 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

Question 35

TAKEOFF AND LANDING
OPERATIONAL LIMITS

3. A visual and ______ (____ __ ______) 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 that the wing fuel temperature is above 0°C (32°F) and any of the following conditions exist:

Answer 35

TAKEOFF AND LANDING
OPERATIONAL LIMITS

3. 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:

Question 36

TAKEOFF AND LANDING
OPERATIONAL LIMITS

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 ________ or less; or
d. The atmospheric conditions have been conducive to frost formation.

Answer 36

TAKEOFF AND LANDING
OPERATIONAL LIMITS

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.

Question 37

ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude

Answer 37

ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude

45,000 Feet

Question 38

ENROUTE OPERATIONAL LIMITS
Maximum Generator Current (per generator)

Up to 41,000 Feet: ___ Amperes

Above 41,000 Feet: ___ Amperes

Answer 38

ENROUTE OPERATIONAL LIMITS
Maximum Generator Current (per generator)

Up to 41,000 Feet: 300 Amperes

Above 41,000 Feet: 250 Amperes

Question 39

ENROUTE OPERATIONAL LIMITS
Maximum altitude for extension of flaps and/or
landing gear:

Answer 39

ENROUTE OPERATIONAL LIMITS
Maximum altitude for extension of flaps and/or
landing gear:

18,000 feet

Question 40

ENROUTE OPERATIONAL LIMITS
Maximum operating altitude with inoperative
Yaw Damper:

Answer 40

ENROUTE OPERATIONAL LIMITS
Maximum operating altitude with inoperative
Yaw Damper:

30,000 feet

Question 41

CABIN PRESSURIZATION LIMITATIONS
Normal Cabin Pressurization
Limitations:

Answer 41

CABIN PRESSURIZATION LIMITATIONS
Normal Cabin Pressurization
Limitations:

0.0 to 8.9 PSI ± 0.1 PSI Differential

Question 42

ICING LIMITATIONS
Icing conditions may exist when the indicated RAT in flight is ___________ 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). Icing conditions on the ground exist when the OAT or indicated RAT is _________ 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.

Answer 42

ICING LIMITATIONS
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). 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.

Question 43

ICING LIMITATIONS

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

Answer 43

ICING LIMITATIONS

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

Question 44

ICING LIMITATIONS

Minimum engine N2 speed for effective wing anti-icing:

Answer 44

ICING LIMITATIONS

Minimum engine N2 speed for effective wing anti-icing:

75% N2

Question 45

ICING LIMITATIONS

Minimum temperature for operation of tail deicing
boots (Indicated RAT):

Answer 45

ICING LIMITATIONS

Minimum temperature for operation of tail deicing
boots (Indicated RAT):

-35°C (-31°F)

Question 46

ICING LIMITATIONS

The WING/ENGINE ANTI-ICE switches must be ___ __
or _______ 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 _______ probe.

Answer 46

ICING LIMITATIONS

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.

Question 47

ICING LIMITATIONS

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 __ 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 _______% N1) to assist with shedding the accumulated ice from the spinner, fan, and stators.

Answer 47

ICING LIMITATIONS

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.

Question 48

OPERATIONS IN SEVERE ICING CONDITIONS

All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. Severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues:

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

Answer 48

OPERATIONS IN SEVERE ICING CONDITIONS

All wing icing inspection lights must be operative prior to flight into known or forecast icing conditions at night. Severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues:

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.

Question 49

OPERATIONS IN SEVERE ICING CONDITIONS

If one or more of these visual cues exist (from previous card):

1. Use of the autopilot is __________.
2. Immediately request _______ 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 _______________.

Answer 49

OPERATIONS IN SEVERE ICING CONDITIONS

If one or more of these visual cues exist (from previous card):

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.

Question 50

OPERATIONS IN SEVERE ICING CONDITIONS

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:

1. Unusual _________ trim is required while the airplane is in icing conditions.
2. Autopilot ____ ________ are encountered while the airplane is in icing conditions.

Answer 50

OPERATIONS IN SEVERE ICING CONDITIONS

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:

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.

Question 51

ROCKWELL COLLINS FCS-3000

1. One pilot must remain seated with seat belt fastened during all ________ operations.
2. Operating in the ________ mode is limited to training and display failure conditions.
3. The pilot’s PFD, copilot’s PFD and MFD must be installed and operational in the normal mode for ______.

Answer 51

ROCKWELL COLLINS FCS-3000

1. One pilot must remain seated with seat belt fastened during all autopilot operations.
2. Operating in the composite mode is limited to training and display failure conditions.
3. The pilot’s PFD, copilot’s PFD and MFD must be installed and operational in the normal mode for takeoff.

Question 52

ROCKWELL COLLINS FCS-3000

4. The FCS-3000 system must be verified to be operational by a satisfactory ________ _______ _____ (no messages on power up) prior to each flight in which the autopilot is to be used.
5. The autopilot minimum engage height, during climb following takeoff or go-around, is _____ feet AGL.

Answer 52

ROCKWELL COLLINS FCS-3000

4. The FCS-3000 system must be verified to be operational by a satisfactory automatic preflight test (no messages on power up) prior to each flight in which the autopilot is to be used.
5. The autopilot minimum engage height, during climb following takeoff or go-around, is 350 feet AGL.

Question 53

ROCKWELL COLLINS FCS-3000

The autopilot minimum use height is:

a. ILS Approach (CAT I) ____ Feet AGL
b. Non-precision Approaches ____ Feet AGL
c. Cruise 1000 Feet AGL
7. Category ___ approaches are not approved.

Answer 53

ROCKWELL COLLINS FCS-3000

The autopilot minimum use height is:

a. ILS Approach (CAT I) 180 Feet AGL
b. Non-precision Approaches 350 Feet AGL
c. Cruise 1000 Feet AGL
7. Category II approaches are not approved.

Question 54

ROCKWELL COLLINS FCS-3000

8. VOR approaches must not be conducted in the NAV mode of the flight director. Use the _____ mode, or manually track the approachcourse using the HDG mode. This limitation applies to both flight director only and autopilot coupled operation.
9. Autopilot coupled operation is prohibited during any portion of a VOR approach in which the VOR is located behind the airplane by more than ___ miles, unless the HDG mode of the flight director is being used to manually track the approach course.

Answer 54

ROCKWELL COLLINS FCS-3000

8. VOR approaches must not be conducted in the NAV mode of the flight director. Use the APPR mode, or manually track the approachcourse using the HDG mode. This limitation applies to both flight director only and autopilot coupled operation.
9. Autopilot coupled operation is prohibited during any portion of a VOR approach in which the VOR is located behind the airplane by more than 15 miles, unless the HDG mode of the flight director is being used to manually track the approach course.

Question 55

ROCKWELL COLLINS FCS-3000

10. It is _________ to display the non-coupled side Flight Director unless the coupled side Flight Director is being displayed. Failure to adhere to this limitation will result in incorrect Flight Director guidance. Use of the coupled side Flight Director by itself will operate correctly.

Answer 55

ROCKWELL COLLINS FCS-3000

10. It is prohibited to display the non-coupled side Flight Director unless the coupled side Flight Director is being displayed. Failure to adhere to this limitation will result in incorrect Flight Director guidance. Use of the coupled side Flight Director by itself will operate correctly.