Sovereign 680 - Limitations and Memory Items

Environmental System Smoke or Odor

Electrical System Smoke Or Fire

Smoke Removal

Hydraulic Wheel Brake Failure

Aileron Trim Runaway

Primary Pitch Trim Runaway

Secondary Pitch Trim Runaway

Jammed Pitch Or Roll Control System

Rudder Trim Runaway

Nosewheel Steering Malfunction

Inadvertent Stall (Buffet/Roll-off)

WINDSHR

This message is displayed in the right portion of the PFD ADIS when a TAWS windshear warning alert is active, indicating an increasing tailwind or severe downdraft condition. An aural "WINDSHEAR WINDSHEAR WINDSHEAR" warning accompanies this message. Windshear escape flight guidance is not provided.

APU Fire (Red CAS message)

Battery O'Temp L and/or R (Red CAS Message)

Cabin Altitude (Red CAS Message)

DPLY (Red EICAS Indication) and EMER STOW (Switch Flashing)

Emergency Descent (Red CAS Message)

Engine Fire L and/or R (Red CAS Message)

Takeoff Above V1 or in flight at a safe Altitude at or above 400 ft AGL and conditions permit

Engine Fire L and/or R (Red CAS Message)
Takeoff below V1 or on the Ground

No Takeoff (Red CAS Message)
Speed Below V1 - Takeoff Rejected

No Takeoff (Red CAS Message)Speed Below V1 - Takeoff Continued

Engine Failure or other Emergency During Takeoff
Speed Below V1

Engine Failure or other Emergency During Takeoff
Speed at or above V1

Engine Failure During Final Approach

Dual Engine Flameout - Cruise

Dual Engine Flameout - Low Altitude

Certification Status
This Citation Sovereign is certified in accordance with 14 CFR Part_____ and JAR-_____

Certification Status
Maximum Design Ramp Weight.......................?
Maximum Design Takeoff Weight....................?
Maximum Design Landing Weight....................?
Maximum Design Zero Fuel Weight.................?
Maximum Tailcone Baggage Weight.................?
Maximum Certified Landing Weight..................?

Powerplant Limitations
Engine Type.........Pratt and Whitney Canada Inc. ______ Turbofan (producing ______lbs. thrust at sea level up to 30 C)

Attempting an engine start is prohibited with a tailwind component greater than _____knots.

FADEC
(Full Authority Digital Engine Computers)

Dispatch with an engine FADEC ______ inoperative is prohibited.
Both air data systems must be _______ for dispatch.
Maximum oil consumption is 1 quart per ____-hour period.

Engine Operating Limits

Starting ITT Limit..............................?
Max Observed ITT Limit (TO Detent)................?
Takeoff ITT Time Limit (TO Detent): .............____minutes (_____for single engine operation)
Max Continuous ITT Limit (MCT Detent)...............?

Engine Operating Limits

N1 Limit................................?
Transient N1 Limit (20 Seconds)..................?
N2 Limit...........................................?
Transient N2 Limit (20 Seconds)..................?

Engine Operating Limits

The total time during which takeoff thrust may be used is limited to ___ minutes per flight. This time may be extended to _____ minutes for one engine inoperative operation.
Oil pressure less than ___PSI but greater than or equal to _____ PSI is acceptable when the throttles are set to less than CRU detent.
After initiation of the start cycle, oil pressure should indicate an increase within ____ seconds of engine light-up indicated by a rise in N2 and ITT.

Start Cycle Limitations

Engine Starter Limitation: The rest periods between engine starts is ____ minutes after the first start attempt, ____ minutes after the second, and ____ minutes after the third.

APU Starter Limitation: ____APU start cycles per ____ minutes. ____ cycles with a ___-second rest period between cycles is permitted.

Battery Limitations

Battery Start Limitation...................____ engine starts per hour

Engine Start Source Count Against Battery
Battery Start..................................................?
GPU (greater than 1,000 amps) .....................?
GPU (less than 1,000 amps)..........................?
Cross-Generator.......................................... ?
APU-Battery Start........................................?
APU Start......................................................?

Electrical Power Systems

Status Engine Gen Limit APU Gen Limit

Ground.................?..................................?
Air........................?..................................?
> 35,000 feet........?..................................?

Electical Power Systems

The battery temperature indicating system must be operational for all ____ and _____ operations.
If the BATTERY O'TEMP L-R CAS message displays during ground operations, even if it subsequently clears, _____ is prohibited until after the proper maintenance procedures have been accomplished.
For generator cooling during ground operations, the engine must be operated at idle with the generator load less than ______ prior to engine shutdown. Otherwise, a ____ minute cooling period after engine shutdown is required prior to attempting a restart.

Auxiliary Power Unit (APU)

The maximum altitude for APU starts is .....................?
The maximum airspeed for APU starts is....................?
The maximum operating altitude for the APU is...........?
The maximum operating airspeed for the APU is _____ KIAS/ ______Mach.
APU operation is prohibited until ______ as contained in Section III, Normal Procedures.
_____APU start attempt is permitted after a dual generator failure.

Auxillary Power Unit (APU)

Following Shutdown for any reason, an APU restart must not be attempted until _____ seconds after the RPM indicator reads 0%.

Applying deice/anti-ice fluid of any type is prohibited when _______.
________ operation of the APU is prohibited.

Auxillary Power Unit (APU)

Operating the cockpit and cabin temperature controls in ______ is prohibited while APU MAX COOL is selected ON. A _______-second waiting period is required after selecting APU MAX COOL to OF before operating cockpit and cabin temperature controls in MANUAL.
The APU ________ must be inspected following an automatic shutdown of the APU.

Hydraulic Power Systems

The use of the auxiliary hydraulic pump is prohibited when the ground operating temperature is below _____.
The use of the auxiliary hydraulic pump is prohibited _______.

Ice and Rain Protection

The Anti-Ice ENGINE/STAB switches must be selected ON between the temperatures of _____ when in visible moisture. Use _____ for ground operations and ____ for in flight.
Except for the ground preflight check, maximum SAT for operation of bleed air anti-ice with the throttles above idle is ______.
Limit the ground operation of the pitot-static hear to ____ minutes to preclude damage to the pitot tubes and angle-of-attack vanes.

Ice and Rain Protection

_____ must not be used to deice surfaces prior to takeoff.
The Anti-Ice ENGINE/STAB switches must be selected ON at least ____ prior to an idle descent into an icing environment.

Operations in Severe Icing Conditions

Visual Cues
Unusually extensive ice accumulation on the airframe and windshield in areas __________.
Accumulation of ice on the upper surface of the wing aft of the protected area extending more than _______aft of the heated leading edge.

Fuel Conditions

Maximum asymmetric fuel differential for normal operations*...............................?

Minimum Single Point refueling pressure is _____PSI and maximum is ____PSI. The maximum Single Point defueling pressure is ______PSI.

*A lateral fuel imbalance of _______ has been demonstrated for emergency return.

Speed Limitations

Max. Operating Mach (MMO), above 29,833 ft........? (indicated)
Max Operating Knots (VMO), 8000 ft to 29.833 ft........?
Max. Operating Knots (VMO), below 8000ft.................?
Max Flap Extended Speed, Vfe Partial Flaps, 7 degree position...........?
Max Flap Extended Speed, Vfe Partial Flaps, 15 degree position............?
Max Flap Extended Speed, Vfe Partial Flaps, 35 degree position............?

Speed Limitations

Max. Landing Gear Operating/Extended Speed, Vle/Vlo..................?
Max Turbulent Air Penetration Speed........................?
Max Speed Brake Extension Speed....................?
Min Speed Brake Extension Speed......................?
Min Single Engine Enroute Climb Speed..................?
Max. Tire Ground Speed............................?
Min Speed For Sustained Flight in Icing Conditions..........................?

Takeoff and Landing Operational Limitations

Maximum Altitude Limit........................?
Maximum Tailwind Component...................?
Maximum Demonstrated Crosswind Component (not Limiting; with of without thrust reversers)...................?
The _________and _________ must be disengaged for takeof and landing.

Takeoff and Landing
Operational Limitations

The lavatory doors must be ______ for taxi, takeoff, and landing.
Takeoff and Landings are limited to ______ runway surfaces.
Antiskid must be operational for _________.
Except where required by AFM procedures, speed brakes,must be stowed prior to _______ for landing.

Takeoff and Landing
Operational Limitations

Takeoff is prohibited with the following forms of contamination:
With frost adhering to the following critical areas....
-________
-________
-________

Takeoff and Landing
Operational Limitations

Takeoff is prohibited with the following forms of contamination:
With ice, snow, or slush adhering to the following critical areas....

-______ -_______ -________
-______ -_______ -________
-______ -_______ -________
-______ -_______

Enroute Operational Limitations

Maximum Operating Altitude..............?
Maximum Altitude with Flaps Extended...............?

Cabin Pressurization Limitations

Normal Cabin Pressurization Limitations.............?
Pressure Relief Valve.........................................?
Pressure Gauge Redline.....................................?

Maneuver Limitations

Acrobatic maneuvers, including spins, are ______.
Intentional stalls are prohibited above _____. Intentional full stalls are limited to idle thrust only.

Passenger and Baggage Compartments

The maximum number of occupants in the passenger compartment is ______.
The baggage compartment ________ and ______ systmes must be operational if baggage is to be carried in the compartment.
The maximum floor loading distribution is ____ lbs per square foot.

Supplemental Oxygen System

Service the oxygen system with __________(MIL-O-27210).
The use of medical oxygen is _______.

Crew and passenger oxygen masks are not approved for use above ______ feet cabin altitude. Prolonged use of passenger masks above _____ feet cabin altitude is not recommended.

The pressure-demand crew oxygen masks must be _______ to qualify as a quick donning oxygen mask.

Thrust Reversers

A satisfactory preflight check of the thrust reversersmust be accomplished in accordance with Section III, Normal Procedures on _______ and on any flight that is predicated on the use of the thrust reversers for perfomance or the first flight ______ on the airplane.
Reverse thrust power must be reduced to the idle reverse detent position at ______ KIAS on landing roll.
Takeoff performance data must not be predicated on the use of the thrust reversers when the ground operating temperature is below_____.

Thrust Reversers

Deployment of the trhust reversers for more than _____ seconds with the APU operating is prohibited.
Static-ground operation of the engines is limited to _____ if the thrust reversers are deployed.
The use of thrust reversers is prohibited during ______.
The use of thrust reversers to ______ is prohibited.

Honeywell Primus Epic System

The Honeywell PRIMUS EPIC for the Cessna Citation SOVEREIGN Pilot's Guides, part numbers A28-1146-168 and A28-1146-183, Revision 1, or later applicable revision, must be ______ to the flight crew.
Dispatch is prohibited when any of the following CAS messages are displayed: __________.
Dispatch is prohibited following a flight where either a DU 1-2-3-4- O'TEMP or MAU 1-2-3-4 O'TEMP CAS Message was displayed, until O'TEMP or MAU 1-2-3-4 O'TEMP CAS Message was displayed, until _________.

Honeywell Primus Epic System

All display units must be ____________.
Dispatch with a DU in _______________ is prohibited.
Reversion of both PFDs to ___________ is prohibited.
Taxiing the airplane is prohibited until the AHRS _____ is completed.

Autopilot

One pilot must remain seated, with the seatbelt fastened, during ________.
Autopilot operation is prohibited if any of the following is true:

-________________
-________________
-________________

Autopilot

Autopilot Minimum-Use-Height:
-Enroute, and Descent ______ feet AGL.
-Precision Approach (Category I and II ILS) _____ feet AGL.
-Nonprecision Approach ______ feet AGL.
-Takeoff, Climb, and Missed Approach _____ feet AGL.

Autopilot

Autopilot operation is prohibited during in-flight engine starts using ________.
Configuring the aircraft displays to _______ fuel and weight units is prohibited.
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 reengaged.

Autopilot

For airplanes 680-0001 thru -0290 not incorporating SB680-34-20 (Epic Phase 5 Software Upgrade), the use of ______ mode to ______ transition from LNAV to VOR or ILS approach is prohibited.
HF radio transmissions are prohibited when navigation is predicated on the use of the ________.

Standby Flight Display

The standby flight disply (including ATT, ALT and ASI) and standby HSI must be ___________.

Avionics

When displayed, the geographic-referenced airplane symbol on the optional electronic charts _______ be used for navigation.
Operators with the optional electronic charts must have __________ available to the flight crew.
The Data Start Date currency __________ on the REVISION INFO window prior to use.
The flight crew is responsible for _________ of charts for the planned flight.

Ice and Rain Protection

CAUTION

Do not operate the aircraft above ______ with wing anti-ice selected on.