Limitations Flashcards
(111 cards)
1
Q
WEIGHT LIMITATIONS
Maximum Design Ramp Weight:
A
WEIGHT LIMITATIONS
Maximum Design Ramp Weight:
30,550 Pounds
2
Q
WEIGHT LIMITATIONS
Maximum Design Takeoff Weight:
A
WEIGHT LIMITATIONS
Maximum Design Takeoff Weight:
30,300 Pounds
3
Q
WEIGHT LIMITATIONS
Maximum Design Landing Weight:
A
WEIGHT LIMITATIONS
Maximum Design Landing Weight:
27,100 Pounds
4
Q
WEIGHT LIMITATIONS
Maximum Design Zero Fuel Weight:
A
WEIGHT LIMITATIONS
Maximum Design Zero Fuel Weight:
20,800 Pounds
5
Q
WEIGHT LIMITATIONS
Minimum Flight Weight:
A
WEIGHT LIMITATIONS
Minimum Flight Weight:
17,345 Pounds
6
Q
WEIGHT LIMITATIONS
Maximum Tailcone Weight:
A
WEIGHT LIMITATIONS
Maximum Tailcone Weight:
1,000 Pounds
7
Q
UNUSABLE FUEL LIMITATIONS
Fuel remaining in the fuel tanks when the fuel quantity indicator reads ____. This fuel is ___ _______in flight.
A
UNUSABLE FUEL LIMITATIONS
Fuel remaining in the fuel tanks when the fuel quantity indicator reads zero. This fuel is not usable in flight.
8
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Altitude Limit
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Altitude Limit
14,000 Feet
9
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Tailwind Component
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Tailwind Component
10 Knots
10
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Demonstrated Crosswind Component
(Not Limiting; with or without thrust reversers)
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Demonstrated Crosswind Component
(Not Limiting; with or without thrust reversers)
25 Knots
11
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The autopilot and yaw damper must be _________ for takeoff and landing.
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The autopilot and yaw damper must be disengaged for takeoff and landing.
12
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
A satisfactory precheck flight of each of the following systems must be accomplished in accordance with Section III, Normal Procedures, prior to take off:
- Angle-of-Attack and ____ _______
- Bleed Air System
- Glareshield Cooling Fans
- Rudder Bias
- Standby Power
- Stabilizer Trim
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
A satisfactory precheck flight of each of the following systems must be accomplished in accordance with Section III, Normal Procedures, prior to take off:
- Angle-of-Attack and Stall** **Warning
- Bleed Air System
- Glareshield Cooling Fans
- Rudder Bias
- Standby Power
- Stabilizer Trim
13
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The lavatory doors must be latched and _______ for takeoff and landing.
Takeoff and landings are limited to _______ runway surfaces.
Antiskid must be operational for _______.
Except where otherwise specified by AFM procedures, speedbrakes must be stowed prior to ____ feet AGL for landing.
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The lavatory doors must be latched and open for takeoff and landing.
Takeoff and landings are limited to paved runway surfaces.
Antiskid must be operational for takeoff.
Except where otherwise specified by AFM procedures, speedbrakes must be stowed prior to 500 feet AGL for landing.
14
Q
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is prohibited with a ____ message displayed. Takeoff is prohibited with an amber message displayed unless relief is specifically authorized in a Minimum Equipment List (MEL).
Takeoff is limited to the flaps ____ configuration when Type II, III, or IV anti-ice fluid has been applied to the airplane.
A
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is prohibited with a red message displayed. Takeoff is prohibited with an amber message displayed unless relief is specifically authorized in a Minimum Equipment List (MEL).
Takeoff is limited to the flaps 7º configuration when Type II, III, or IV anti-ice fluid has been applied to the airplane.
15
Q
ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude
For operations above FL410, the following conditions must be met:
- Both ENG BLD AIR selectors must be selected to _____ or HP and both engine bleed air sources must be available.
- The PRESS SOURCE selector must be selected to ______.
A
ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude
47,000 Feet
For operations above FL410, the following conditions must be met:
- Both ENG BLD AIR selectors must be selected to NORM or HP and both engine bleed air sources must be available.
- The PRESS SOURCE selector must be selected to NORM.
16
Q
ENROUTE OPERATIONAL LIMITS
Maximum Altitude with Flaps Extended
The Mach trim system must be operations for speeds above Mach ____ with the autopilot disengaged.
A
ENROUTE OPERATIONAL LIMITS
Maximum Altitude with Flaps Extended
18,000 feet
The Mach trim system must be operations for speeds above Mach 0.77 with the autopilot disengaged.
17
Q
POWERPLANT LIMITS
Engine Type-
Pratt and Whitney Canada Inc. PW306C Turbofan (producing ____ lbs thrust at sea level up to 30º C)
Continuous static-ground operation of the engine at takeoff thrust is limited to a maximum of ___ minutes.
Attempting an engine start is prohibited with a tailwind component greater than ___ knots.
.
A
POWERPLANT LIMITS
Engine Type-
Pratt and Whitney Canada Inc. PW306C Turbofan (producing 5770 lbs thrust at sea level up to 30º C)
Continuous static-ground operation of the engine at takeoff thrust is limited to a maximum of 2 minutes.
Attempting an engine start is prohibited with a tailwind component greater than 10 knots.
18
Q
APPROVED OILS
Maximum oil consumption is 1 quart per ___ flight hours. When oil consumption is greater that 1 quart per ___ flight hours, refer to the Airplane Maintenance Manual.
Oil types or brands may not be ______ unless specifically approved in the PW306C Maintenance Manuals.
A
APPROVED OILS
Maximum oil consumption is 1 quart per 8 flight hours. When oil consumption is greater that 1 quart per 8 flight hours, refer to the Airplane Maintenance Manual.
Oil types or brands may not be mixed unless specifically approved in the PW306C Maintenance Manuals.
19
Q
ENGINE OPERATING LIMITS
TAKEOFF (TO DETENT)
Two Engines: ________ Minutes
One Engine: ________ Minutes
A
ENGINE OPERATING LIMITS
TAKEOFF (TO DETENT)
Two Engines: 5 Minutes
One Engine: 10 Minutes
20
Q
ENGINE OPERATING LIMITS
MAXIMUM CONTINUOUS (MCT DETENT):
_______________
A
ENGINE OPERATING LIMITS
MAXIMUM CONTINUOUS (MCT DETENT):
CONTINUOUS
21
Q
ENGINE OPERATING LIMITS
MAXIMUM CRUISE (CRU DETENT):
_______________
A
ENGINE OPERATING LIMITS
MAXIMUM CRUISE (CRU DETENT):
CONTINUOUS
22
Q
ENGINE OPERATING LIMITS
REVERSE THRUST:
____ Minutes
A
ENGINE OPERATING LIMITS
REVERSE THRUST:
5 Minutes
23
Q
ENGINE OPERATING LIMITS
Max Observed ITT ºC
TAKEOFF (TO DETENT)
___ ºC
A
ENGINE OPERATING LIMITS
Max Observed ITT ºC
TAKEOFF (TO DETENT)
920 ºC
24
Q
ENGINE OPERATING LIMITS
Max Observed ITT ºC
MAXIMUM CONTINUOUS (MCT DETENT)
___ ºC
A
ENGINE OPERATING LIMITS
Max Observed ITT ºC
MAXIMUM CONTINUOUS (MCT DETENT)
920 ºC
25
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
MAXIMUM CRUISE (CRU DETENT)
\_\_\_ ºC
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
MAXIMUM CRUISE (CRU DETENT)
**_920_** ºC
26
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
REVERSE THRUST
\_\_\_ ºC
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
REVERSE THRUST
**_920_** ºC
27
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
STARTING
\_\_\_ ºC
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
STARTING
**_950_** ºC
28
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
TRANSIENT
\_\_\_ ºC
**ENGINE OPERATING LIMITS**
Max Observed ITT ºC
TRANSIENT
**_950_** ºC
29
**START CYCLE LIMITS**
Engine Starter Limit...
The rest period between engine starts is ___ minutes after first start attempt, ___ minutes after the second, and ___ after the third.
**START CYCLE LIMITS**
Engine Starter Limit...
The rest period between engine starts is **_2_** minutes after first start attempt, **_5_** minutes after the second, and **_30_** after the third.
30
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
Batteries Only
\_\_\_ seconds
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
Batteries Only
**_20_** seconds
31
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
Batteries with generator assist
\_\_\_ seconds
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
Batteries with generator assist
**_15_** seconds
32
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
External Power (1000 amps)
\_\_\_ seconds
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
External Power (1000 amps)
**_15_** seconds
33
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
External Power (1500 amps)
\_\_\_ seconds
**START CYCLE LIMITS**
Engine Starter Motoring Limit (not engine start)
External Power (1500 amps)
**_7_** seconds
34
**START CYCLE LIMITS**
## Footnote
APU Starter Limit
Three APU start cycles per ____ minutes. Three cycles with a 90-second rest period between cycles is permitted.
**START CYCLE LIMITS**
## Footnote
APU Starter Limit
Three APU start cycles per **_30_** minutes. Three cycles with a 90-second rest period between cycles is permitted.
35
**START CYCLE LIMITS**
## Footnote
Battery Start Limit
\_\_\_\_ engine starts per hour. Nine APU start cycles per hour.
**START CYCLE LIMITS**
## Footnote
Battery Start Limit
**_Three_** engine starts per hour. Nine APU start cycles per hour.
36
**START CYCLE LIMITS**
## Footnote
Three engine external power starts (available external power current greater than or equal to 1000 amps) are equivalent to ___ engine battery start.
**START CYCLE LIMITS**
## Footnote
Three engine external power starts (available external power current greater than or equal to 1000 amps) are equivalent to **_one_** engine battery start.
37
**START CYCLE LIMITS**
## Footnote
One engine external power starts (available external power current less than 1000 amps) is equivalent to ___ engine battery start.
**START CYCLE LIMITS**
## Footnote
One engine external power starts (available external power current less than 1000 amps) is equivalent to **_one_** engine battery start.
38
**START CYCLE LIMITS**
## Footnote
Three generator-assisted cross starts are equivalent to ___ engine battery start.
**START CYCLE LIMITS**
## Footnote
Three generator-assisted cross starts are equivalent to **_one_** engine battery start.
39
**START CYCLE LIMITS**
## Footnote
Three APU battery starts are equivalent to ___ engine battery start.
**START CYCLE LIMITS**
## Footnote
Three APU battery starts are equivalent to **_one_** engine battery start.
40
**EXTERNAL POWER LIMITS FOR STARTING**
Maximum Current ____ A
Maximum Voltage \_\_\_\_V
**EXTERNAL POWER LIMITS FOR STARTING**
Maximum Current **_1500_** A
Maximum Voltage **_28_**V
41
**SPEED LIMITATIONS**
**Maximum Operating Limit Speeds**
MMO (Above 29,833 Feet)
## Footnote
**\_\_\_\_ Mach (Indicated)**
**SPEED LIMITATIONS**
**Maximum Operating Limit Speeds**
MMO (Above 29,833 Feet)
**_.80_ Mach (Indicated)**
42
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
VMO (Between 8000 and 29,833 Feet)
**_\_\_\_\__ KIAS**
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
VMO (Between 8000 and 29,833 Feet)
**_305_ KIAS**
43
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
VMO (Below 8000 Feet)
**\_\_\_\_ KIAS**
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
VMO (Below 8000 Feet)
**_270_ KIAS**
44
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
Maximum Flap Extended Speed - VFE
Partial Flaps Position - 7° Position
**\_\_\_\_\_ KIAS**
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
Maximum Flap Extended Speed - VFE
Partial Flaps Position - 7° Position
**_250_** **KIAS**
45
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
Maximum Flap Extended Speed - VFE
Partial Flaps Position - 15° Position
**\_\_\_\_\_ KIAS**
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
Maximum Flap Extended Speed - VFE
Partial Flaps Position - 15° Position
**_200_** **KIAS**
46
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
Maximum Flap Extended Speed - VFE
Full Flaps Position - 35° Position
**\_\_\_\_\_ KIAS**
**SPEED LIMITATIONS
Maximum Operating Limit Speeds**
Maximum Flap Extended Speed - VFE
Full Flaps Position - 35° Position
**_175_** **KIAS**
47
**SPEED LIMITATIONS**
Maximum Landing Gear
Extended/Operating Speed - VLE/VLO
\_\_\_\_\_ KIAS
**SPEED LIMITATIONS**
Maximum Landing Gear
Extended/Operating Speed - VLE/VLO
**_210_ KIAS**
48
**SPEED LIMITATIONS**
Maximum Turbulent Air Penetration Speed
\_\_\_\_\_ KIAS/Mach \_\_\_\_
**SPEED LIMITATIONS**
Maximum Turbulent Air Penetration Speed
**_225_** KIAS/Mach **_0.73_**
49
**SPEED LIMITATIONS**
Maximum Speed Brake Operation Speed - VSB
**SPEED LIMITATIONS**
Maximum Speed Brake Operation Speed - VSB
**NO LIMIT**
50
**SPEED LIMITATIONS**
Maximum Tire Ground Speed
\_\_\_\_ Knots
**SPEED LIMITATIONS**
Maximum Tire Ground Speed
**_165_** Knots
51
**SPEED LIMITATIONS**
Minimum Speed for Sustained Flight In Icing Conditions
(except takeoff, approach and landing)
\_\_\_\_ KIAS
**SPEED LIMITATIONS**
Minimum Speed for Sustained Flight In Icing Conditions
(except takeoff, approach and landing)
**_180_** KIAS
52
**ELECTRICAL POWER SYSTEMS**
**Ground**
Engine Generator Limit _____ Amps
APU Gen Limit _____ Amps
**ELECTRICAL POWER SYSTEMS**
**Ground**
Engine Generator Limit **_300_** Amps
APU Gen Limit **_275_** Amps
53
**ELECTRICAL POWER SYSTEMS**
**Air**
Engine Generator Limit _____ Amps
APU Gen Limit _____ Amps
**ELECTRICAL POWER SYSTEMS**
**Air**
Engine Generator Limit **_300_** Amps
APU Gen Limit **_275_** Amps
54
**ELECTRICAL POWER SYSTEMS**
**\> 35,000 feet**
Engine Generator Limit _____ Amps
APU Gen Limit _____ Amps
**ELECTRICAL POWER SYSTEMS**
**\> 35,000 feet**
Engine Generator Limit **_275_** Amps
APU Gen Limit **N/A**
55
**AUXILIARY POWER UNIT (APU)**
The maximum altitude for APU starts is \_\_\_\_\_\_.
**AUXILIARY POWER UNIT (APU)**
The maximum altitude for APU starts is **_FL200_**.
56
**AUXILIARY POWER UNIT (APU)**
The maximum airspeed for APU starts is ______ KIAS.
**AUXILIARY POWER UNIT (APU)**
The maximum airspeed for APU starts is **_250_** KIAS.
57
**AUXILIARY POWER UNIT (APU)**
The maximum operating altitude for operating the APU is \_\_\_\_\_\_.
**AUXILIARY POWER UNIT (APU)**
The maximum operating altitude for operating the APU is**_FL300_**.
58
**AUXILIARY POWER UNIT (APU)**
The maximum operating airspeed for the APU is
\_\_\_\_\_\_ KIAS/Mach \_\_\_\_\_.
**AUXILIARY POWER UNIT (APU)**
The maximum operating airspeed for the APU is
**_305_** KIAS/Mach **_0.80_**.
59
**AUXILIARY POWER UNIT (APU)**
\_\_\_\_ APU start is permitted after a dual generator failure.
**AUXILIARY POWER UNIT (APU)**
**_One_** APU start is permitted after a dual generator failure.
60
**AUXILIARY POWER UNIT (APU)**
Following shutdown for any reason, an APU restart must not be attempted until ____ after RPM indicator reads 0%.
**AUXILIARY POWER UNIT (APU)**
Following shutdown for any reason, an APU restart must not be attempted until **_30 seconds_** after RPM indicator reads 0%.
61
**AUXILIARY POWER UNIT (APU)**
Applying deice/anti-ice fluid of any type is _________ when the APU is operating.
**AUXILIARY POWER UNIT (APU)**
Applying deice/anti-ice fluid of any type is **_prohibited_** when the APU is operating.
62
**AUXILIARY POWER UNIT (APU)**
\_\_\_\_\_\_\_\_\_ operation of the APU is prohibited.
**AUXILIARY POWER UNIT (APU)**
**_Unattended_** operation of the APU is prohibited.
63
**AUXILIARY POWER UNIT (APU)**
The APU compartment must be _________ following an automatic shutdown of the APU.
**AUXILIARY POWER UNIT (APU)**
The APU compartment must be **_inspected_** following an automatic shutdown of the APU.
64
**AUXILIARY POWER UNIT (APU)**
Operating the cockpit and cabin temperature controls in MANUAL is ________ while APU MAX COOL is selected ON. A _________ waiting period is required after selecting APU MAX COOL to OFF before operating cockpit and cabin temperature controls in MANUAL.
**AUXILIARY POWER UNIT (APU)**
Operating the cockpit and cabin temperature controls in MANUAL is **_prohibited_** while APU MAX COOL is selected ON. A **_30-second_** waiting period is required after selecting APU MAX COOL to OFF before operating cockpit and cabin temperature controls in MANUAL.
65
**FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)**
Dispatch with an engine FADEC channel inoperative is \_\_\_\_\_\_\_\_.
**FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)**
Dispatch with an engine FADEC channel inoperative is **_prohibited_**.
66
**FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)**
Exceeding the time interval for a cyan ENGINE DISPATCH LIMIT L and/or R message is \_\_\_\_\_\_\_\_.
**FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)**
Exceeding the time interval for a cyan ENGINE DISPATCH LIMIT L and/or R message is **_prohibited_**.
67
**FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)**
Both air data systems must be ________ for dispatch.
**FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)**
Both air data systems must be **_operational_** for dispatch.
68
**HYDRAULIC POWER SYSTEM**
The use of the auxiliary hydraulic pump is prohibited when the ground operating temperature is below ________ .
**HYDRAULIC POWER SYSTEM**
The use of the auxiliary hydraulic pump is prohibited when the ground operating temperature is below -**_40 ºC_**.
69
**HYDRAULIC POWER SYSTEM**
The use of the auxiliary hydraulic pump in flight is \_\_\_\_\_\_\_\_\_\_.
**HYDRAULIC POWER SYSTEM**
The use of the auxiliary hydraulic pump in flight is **_prohibited_**.
70
**ICE AND RAIN PROTECTION**
ANTI-ICE ENGINE/STAB buttons must be selected ___ between the temperatures of +10 ºC to -35 ºC when in visible moisture. Use SAT for ground operations and RAT for in flight.
**ICE AND RAIN PROTECTION**
ANTI-ICE ENGINE/STAB buttons must be selected **_on_** between the temperatures of +10 ºC to -35 ºC when in visible moisture. Use SAT for ground operations and RAT for in flight.
71
**ICE AND RAIN PROTECTION**
Except for the ground preflight check, maximum SAT for operation of bleed air anti-ice with the throttle above idle is \_\_\_\_\_.
**ICE AND RAIN PROTECTION**
Except for the ground preflight check, maximum SAT for operation of bleed air anti-ice with the throttle above idle is **_+20 ºC_**.
72
**ICE AND RAIN PROTECTION**
Limit the ground operation of the pitot-static heat to __ minutes to preclude damage to the pitot tubes and angle-of-attack vanes.
**ICE AND RAIN PROTECTION**
Limit the ground operation of the pitot-static heat to **_2_** minutes to preclude damage to the pitot tubes and angle-of-attack vanes.
73
**ICE AND RAIN PROTECTION**
Anti-ice systems must not be used to deice surfaces prior
to \_\_\_\_\_\_\_.
**ICE AND RAIN PROTECTION**
Anti-ince systems must not be used to deice surfaces prior
to **_takeoff_**.
74
**ICE AND RAIN PROTECTION**
Anti-ice wing buttons must be selected ______ for operations above FL410.
**ICE AND RAIN PROTECTION**
Anti-ice wing buttons must be selected **_OFF_** for operations above FL410.
75
**BOUNDARY LAYER ENERGIZERS**
\_\_\_\_ boundary layer energizers (BLEs) must be present for dispatch (nine per wing).
**BOUNDARY LAYER ENERGIZERS**
**_All_** boundary layer energizers (BLEs) must be present for dispatch (nine per wing).
76
**CABIN PRESSURIZATION LIMITS**
Normal Cabin Pressurization Limits:
**CABIN PRESSURIZATION LIMITS**
Normal Cabin Pressurization Limits:
**_0.0 to 9.3 (+/-0.1) PSID_**
77
**CABIN PRESSURIZATION LIMITS**
Pressure Relief Valve:
**CABIN PRESSURIZATION LIMITS**
Pressure Relief Valve:
**_9.6 (+/-0.1) PSID_**
78
**CABIN PRESSURIZATION LIMITS**
Pressure Gauge Redline:
**CABIN PRESSURIZATION LIMITS**
Pressure Gauge Redline:
**_9.7 PSID_**
79
**CABIN PRESSURIZATION LIMITS**
When the PRESS SOURCE selector is selected L or R, and ENG BLD AIR selector is selected \_\_\_\_, or an engine bleed air source is unavailable, the BAGGAGE HEAT button must be selected \_\_\_\_.
**CABIN PRESSURIZATION LIMITS**
When the PRESS SOURCE selector is selected L or R, and ENG BLD AIR selector is selected **_OFF_**, or an engine bleed air source is unavailable, the BAGGAGE HEAT button must be selected **_OFF_**.
80
**PASSENGER COMPARTMENT**
The maximum number of occupants in the passenger compartment is \_\_\_\_.
**PASSENGER COMPARTMENT**
The maximum number of occupants in the passenger compartment is **_12_**.
81
**PASSENGER COMPARTMENT**
The lavatory door must be latched ____ for taxi, takeoff and landing.
**PASSENGER COMPARTMENT**
The lavatory door must be latched **_open_** for taxi, takeoff and landing.
82
**PASSENGER COMPARTMENT**
The use of the lavatory is ______ for taxi, takeoff, and landing and is lmited to ____ occupant in flight.
**PASSENGER COMPARTMENT**
The use of the lavatory is **_prohibited_** for taxi, takeoff, and landing and is lmited to **_one_** occupant in flight.
83
**BAGGAGE COMPARTMENT**
The baggage compartment smoke detection and extinguishing systems must be _________ if baggage is to be carried in the compartment.
**BAGGAGE COMPARTMENT**
The baggage compartment smoke detection and extinguishing systems must be **_operational_** if baggage is to be carried in the compartment.
84
**BAGGAGE COMPARTMENT**
The maximum total weight of baggage in the tailcone baggage compartment is _____ pounds. Total weight includes baggage in the forward and aft compartments plus any on the coat rod.
**BAGGAGE COMPARTMENT**
The maximum total weight of baggage in the tailcone baggage compartment is **_1000_** pounds. Total weight includes baggage in the forward and aft compartments plus any on the coat rod.
85
**BAGGAGE COMPARTMENT**
The maximum floor loading distribution is ____ pounds per square foot.
**BAGGAGE COMPARTMENT**
The maximum floor loading distribution is **_150_** pounds per square foot.
86
**THRUST REVERSERS**
Reverse thrust must be reduced to the idle reverse detent position at ___ KIAS on landing roll.
**THRUST REVERSERS**
Reverse thrust must be reduced to the idle reverse detent position at **_65_** KIAS on landing roll.
87
**THRUST REVERSERS**
Deployment of the thrust reversers for more than ___ seconds with the APU operation is prohibited.
**THRUST REVERSERS**
Deployment of the thrust reversers for more than **_30_** seconds with the APU operation is prohibited.
88
**THRUST REVERSERS**
Static-ground operation of the engines is limited to _____ if the thrust reversers are deployed.
**THRUST REVERSERS**
Static-ground operation of the engines is limited to **_IDLE_** if the thrust reversers are deployed.
89
**THRUST REVERSERS**
The use of thrust reversers is ________ during touch-and-go landings.
**THRUST REVERSERS**
The use of thrust reversers is **_prohibited_** during touch-and-go landings.
90
**THRUST REVERSERS**
The use of thrust reversers to ________ the airplane is prohibited.
**THRUST REVERSERS**
The use of thrust reversers to **_reverse_** the airplane is prohibited.
91
**THRUST REVERSERS**
Takeoff performance data must not be predicated on the use of the thrust reversers when the ground operating tempeature is below ____ (\_\_\_\_ for Airplanes 680-0001 thru -0035 not incorporating SL680-78-01, Replacement of Thrust Reverser Door Seals).
**THRUST REVERSERS**
Takeoff performance data must not be predicated on the use of the thrust reversers when the ground operating tempeature is below **_-40 ºC_** (**_-15 ºC_** for Airplanes 680-0001 thru -0035 not incorporating SL680-78-01, Replacement of Thrust Reverser Door Seals).
92
**STANDBY FLIGHT DISPLAY**
The standby flight display (including attitude, altitide, and airspeed) and standby HSI ____ be functioning prior to takeoff.
**STANDBY FLIGHT DISPLAY**
The standby flight display (including attitude, altitide, and airspeed) and standby HSI **_must_** be functioning prior to takeoff.
93
**HONEYWELL PRIMUS EPIC SYSTEM**
Ground operation with EICAS and/or avionics selected on without conditioned air is limited to ____ minutes when the OAT is greater than 47 ºC.
**HONEYWELL PRIMUS EPIC SYSTEM**
Ground operation with EICAS and/or avionics selected on without conditioned air is limited to **_30_** minutes when the OAT is greater than 47 ºC.
94
**HONEYWELL PRIMUS EPIC SYSTEM**
Dispatch is prohibited when any of the following amber messages are displayed: DU 1-2-3-4 O'TEMP or \_\_\_\_\_\_\_\_\_\_\_\_.
**HONEYWELL PRIMUS EPIC SYSTEM**
Dispatch is prohibited when any of the following amber messages are displayed: DU 1-2-3-4 O'TEMP or **_MAU 1-2-3-4 O'TEMP_**.
95
**HONEYWELL PRIMUS EPIC SYSTEM**
Dispatch is prohibited following a flight where either an amber ________ or MAU 1-2-3-4 O'TEMP message was displayed, until the condition is identified and corrected.
**HONEYWELL PRIMUS EPIC SYSTEM**
Dispatch is prohibited following a flight where either an amber **_DU 1-2-3-4 O'TEMP_** or MAU 1-2-3-4 O'TEMP message was displayed, until the condition is identified and corrected.
96
**HONEYWELL PRIMUS EPIC SYSTEM**
Reversion of both PFDs to DU2 and DU3 is \_\_\_\_\_\_\_\_\_.
**HONEYWELL PRIMUS EPIC SYSTEM**
Reversion of both PFDs to DU2 and DU3 is **_prohibited_**.
97
**HONEYWELL PRIMUS EPIC SYSTEM**
Taxiing the airplane is prohibited until the attitude/heading ground alignment is completed (approximately ___ seconds for AHRS/\_\_\_ minutes with optional IRS).
**HONEYWELL PRIMUS EPIC SYSTEM**
Taxiing the airplane is prohibited until the attitude/heading ground alignment is completed (approximately **_90_** seconds for AHRS/**_6_** minutes with optional IRS).
98
**HONEYWELL PRIMUS EPIC SYSTEM**
One piliot must remain seated, with the seatbelt fastened, during all _________ operations.
**HONEYWELL PRIMUS EPIC SYSTEM**
One piliot must remain seated, with the seatbelt fastened, during all **_autopilot_** operations.
99
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot operation is prohibited if any of the following is true:
(1) Any comparison monitor annunciation is activated.
(2) Either _____ is in ATT or HDG reversion.
(3) Either attitude heading source is failed.
Use of barometric VNAV vertical guidance is ____________ when the barometric altitude is corrected to the landing field election (QFE operation).
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot operation is prohibited if any of the following is true:
(1) Any comparison monitor annunciation is activated.
(2) Either **_PFD_** is in ATT or HDG reversion.
(3) Either attitude heading source is failed.
Use of barometric VNAV vertical guidance is **_prohibited_** when the barometric altitude is corrected to the landing field election (QFE operation).
100
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Enroute and Descent: _____ feet AGL
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Enroute and Descent: **_1000_** feet AGL
101
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Precision Approach (ILS/LPV): _____ feet AGL
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Precision Approach (ILS/LPV): **_80_** feet AGL
102
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Non-recision Approach: _____ feet AGL
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Non-recision Approach: **_200_** feet AGL
103
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Takeoff, Climb, and Missed Approach: _____ feet AGL
**HONEYWELL PRIMUS EPIC SYSTEM**
Autopilot Minimum Use Height:
Takeoff, Climb, and Missed Approach: **_400_** feet AGL
104
**HONEYWELL PRIMUS EPIC SYSTEM**
\_\_\_\_\_\_\_\_ operation is prohibited during in-flight engine starts using starter assist.
**HONEYWELL PRIMUS EPIC SYSTEM**
**_Autopilot_** operation is prohibited during in-flight engine starts using starter assist.
105
**HONEYWELL PRIMUS EPIC SYSTEM**
Configuring the airplane displays to ______ fuel and weight units is prohibited.
**HONEYWELL PRIMUS EPIC SYSTEM**
Configuring the airplane displays to **_metric_** fuel and weight units is prohibited.
106
**HONEYWELL PRIMUS EPIC SYSTEM**
When the flight director or autopilot is coupled to VOR or ILS, ____ mode must be selected (HDG bug synced to current heading) prior to switching navigation frequencies. When the next VOR or ILS frequency is satisfactorily received, _____ mode may be re-engaged.
**HONEYWELL PRIMUS EPIC SYSTEM**
When the flight director or autopilot is coupled to VOR or ILS, **_HDG_** mode must be selected (HDG bug synced to current heading) prior to switching navigation frequencies. When the next VOR or ILS frequency is satisfactorily received, **_NAV_** mode may be re-engaged.
107
**HONEYWELL PRIMUS EPIC SYSTEM**
HF radio transmission are _______ when navigation is predicated on the use of the automatic direction finder.
**HONEYWELL PRIMUS EPIC SYSTEM**
HF radio transmission are **_prohibited_** when navigation is predicated on the use of the automatic direction finder.
108
**AIRPLANES WITH ELECTRONIC CHARTS**
When displayed, the geographic-referenced airplane symbol on the optional electronic charts must not be used for \_\_\_\_\_\_\_\_.
**AIRPLANES WITH ELECTRONIC CHARTS**
When displayed, the geographic-referenced airplane symbol on the optional electronic charts must not be used for **_navigation_**.
109
**AIRPLANES WITH ELECTRONIC CHARTS**
Operators with the optional electronic charts must have ________ \_\_\_\_\_\_\_ available to the flight crew.
**AIRPLANES WITH ELECTRONIC CHARTS**
Operators with the optional electronic charts must have **_back-up_** **_charts_** available to the flight crew.
110
**AIRPLANES WITH ELECTRONIC CHARTS**
The Data Start Date currency must be verified on the REVISION INFO window _____ to use.
**AIRPLANES WITH ELECTRONIC CHARTS**
The Data Start Date currency must be verified on the REVISION INFO window **_prior_** to use.
111
**AIRPLANES WITH ELECTRONIC CHARTS**
The _____ \_\_\_\_\_ is responsible for verifying availability of charts for the planned flight.
**AIRPLANES WITH ELECTRONIC CHARTS**
The **_flight_** **_crew_** is responsible for verifying availability of charts for the planned flight.
