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 ## Footnote **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** ## Footnote 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** ## Footnote 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** ## Footnote 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 ## Footnote **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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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** ## Footnote 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.