Gust Factors are not limiting but should be considered at the time of...                                                   (VERBATIM)

T/O and Landing.

Gust factors must be taken into consideration when determining the usability of a Rwy at an Alternate Airport.        (VERBATIM)

CAT II MINIMUMS

Maximum X-wind Component:

CAT II MINIMUMS

Max Headwind Component:

STRUCTURAL LIMIT:

Max Taxi and Ramp Weight:

STRUCTURAL LIMITS:

Max T/O Weight:

STRUCTURAL LIMIT:

Max Landing Weight:

STRUCTURAL LIMIT:

Max Zero Fuel Weight:

Cargo Restriction;

Distance to suitable airport:

AIRSPEED and MACH LIMITS:

Turbulence Penetration:

AIRSPEED and MACH LIMITS:

Max Gear EXTENSION:

AIRSPEED and MACH LIMITS:

Max Gear ExtendED Speed:

AIRSPEED and MACH LIMITS,

Max Gear RETRACTION Speed:

AIRSPEED and MACH LIMITS,

Max Windshield WIPER operation:

AIRSPEED and MACH LIMITS,

Max W-Shield Wiper ops FAILED in the NON-Parked position:

AIRSPEED and MACH LIMITS,

Max Cruise Mach in RVSM Airspace:

AIRSPEED and MACH LIMITS,

Tire Limit GROUND Speed:

FLAPS OPERATING SPEEDS: (V_FO)

Flaps 0^o to 8^o

FLAPS OPERATING SPEEDS: (V_FO)

Flaps 8^o to 20^o

FLAPS OPERATING SPEEDS: (V_FO)

Flaps 20^o to 30^o

FLAPS OPERATING SPEEDS: (V_FO)

Flaps 30^o to 45^o

DEFINITIONS of ICING CONDITIONS:

(Cowl )

"Icing conditions exist..." 

(Verbatim)

COWL ANTI-ICE: Icing Conditions exist when... the OAT (on the ground and for T/O) or TAT (in-flight) is 10^oC or below, and

-Visible moisture in any form

(such as clouds, fog, mist, rain, snow, sleet or ice crystals) is present in flight, or below 400' AGL for Ground Operations, OR

-When operating on surfaces that are wet or contaminated.

Definition of Icing Conditions, WING:

"Icing conditions exist..."

WING ANTI-ICE: Icing conditions exist when...

-The OAT (Takeoff) is 5^oC or TAT (in flight) is 10^oC or below,  AND

-Visible moisture in any form (such as clouds, fog, mist, rain, snow, sleet or ice crystals) is present in flight or below 400' AGL for Takeoff,  OR

-The runway is wet or contaminated.          (Verbatim)

WARNING:

Do Not Hold in icing conditions with the ______ or ______ Extended.

NOTE:

ANTI-ICE will be used any time that icing conditions are expected prior to _____ reduction in the _____ ______ Check.

NOTE:

ANTI-ICE will be used any time that icing conditions are expected prior to Thrust reduction in the After Takeoff  Check.

NOTE:

Single engine taxi is prohibited when Ramps or Taxiways are contaminated with ____, _____ or ___ or during _____ Conditions.

NOTE:

Single engine taxi is prohibited when Ramps or Taxiways are contaminated with Snow, Slush or Ice or during Icing Conditions. 

NOTE:

To prevent ____ contamination from _______ jet blast operating the _____ reversers during taxi operations on wet and contaminated surfaces should be avoided. 

NOTE:

To prevent wing contamination from reverse jet blast operating the thrust reversers during taxi operations on wet and contaminated surfaces should be avoided.

TACTILE CHECK:

In addition to a visual check a tactile check of the wing _______ edge, wing _______ _____ surface and wing ____ _____ surface is required during the external ___________ inspection to determine that the wing is free from frost, ice, snow or slush, when:

-The OAT is ___ or less, or

-The wings' ____ ____ is __^oC or less, or

-The ___________ conditions have been conducive to _____ formation.

-___ and _____ may continue to adhere to wing surfaces for some time even at outside air temps above __^oC.

TACTILE CHECK:

In addition to a visual check a tactile check of the wing _______ edge, wing forward upper surface and wing rear upper surface is required during the external walk-around inspection to determine that the wing is free from frost, ice, snow or slush, when:

-The OAT is 5^oC or less, or

-The wings' fuel temp is 0^oC or less, or

-The atmospheric conditions have been conducive to frost formation.

-Ice and Frost may continue to adhere to wing surfaces for some time even at outside air temps above 5^oC.

OPERATION IN ICING CONDITIONS; COWL

Cowl Anti-ice must be ON for all...

(Verbatim)

...GROUND and FLIGHT operations when icing conditions exist 

-except-

when the inflight SAT is -40C or below,

or 

"ICE" is annunciated by the ice detection system.

(Verbatim)

OPERATION IN ICING CONDITIONS; WING

Wing Anti-ice must be ON for TAKEOFF and FLIGHT operations when...

(Verbatim)

"ICE" is annunciated by the Ice Detection System

OR

When icing conditions exist AND the airspeed is Less than 230 KIAS

EXCEPT

When the inflight SAT is -40^oC or below 

(Verbatim)

L or R WING A/ICE

_______ messages may be posted during ____ but must be verified ___ prior to _______.

L or R WING A/ICE

Caution messages may be posted during taxi but...must be verified "out" prior to T/O.

Wing anti-ice must be ON for the final ___ ______ prior to Takeoff during all ground operations, __^oC or below, unless Type ___ or __ anti-icing fluid has been applied.

(Verbatim)

Wing anti-ice must be ON for the final two minutes prior to Takeoff during all ground operations, 5^oC or below, unless Type III or IV anti-icing fluid has been applied.

(Verbatim)

During all starts do not exceed ____% N₁ for ___ minutes AFTER start

OR

Until all indications are in the ______ range, whichever is ______. 

During all starts do not exceed 75% N₁ for 2 Minutes after start

or

Until all indications are in the normal range, whichever is longer.

ENGINE OPERATING LIMITS 

Max ITT Temp:______ ^oC.

ENGINE OPERATING LIMITS 

Engine to Engine N₂ split at ground idle power should not be greater than ___% N². 

If N₂ is ___% or less with an OAT of ___^oC or __________ do not accelerate above _____.

Engine to Engine N₂ split at ground idle power should not be greater than 2% N². 

If N₂ is 57% or less with an OAT of -20^oC or WARMER do not accelerate above IDLE.

OIL PRESSURE 

T/O Power:____ PSI, Min.  

NOTE:

After _____ start, engine must remain at ____ until oil pressure returns to______range.

T/O Power: 45 PSI, Minimum. 

NOTE:

After COLD start, engine must remain at IDLE until oil pressure returns to NORMAL range.

CONTINUOUS IGNITION  

Continuous engine ignition must be used during the following:

-T/O and Landing on ___________ runways

-T/O with ____ Crosswind components (__ kts or greater)

-Flight through moderate or _______ intensity rain

-Flight through moderate or _______ intensity turbulence

-Flight in the Vicinity of ________.

(Verbatim) 

CONTINUOUS IGNITION  

Continuous engine ignition must be used during the following:

-T/O and Landing on Contaminated runways

-T/O with High Crosswind components (15 kts or greater)

-Flight through moderate or heavier intensity rain

-Flight through moderate or heavier intensity turbulence

-Flight in the Vicinity of T-storms.

(Verbatim)

ENGINE STARTER CRANKING LIMITS 

Start 1:  _____  ON, ______ Off

Start 2: ______ ON, ______ Off

Start 3: ______ ON, _______ Off.

Start 1: 1 Minute ON,  10 Secs Off

Start 2: 1 Minute ON,  10 Secs Off

Start 3: 1 Minute ON, 5 Minutes Off.

( The Starter must not be engaged if indicated N₂ RPM exceeds 55%.)

ASSOCIATED CONDITIONS: 

At initiation of thrust lever movement from SHUT OFF to IDLE: 

-ITT must be ___^oC or ____ for all ______ Starts.

(ITT=Interstage Turbine Temperature.)

(Verbatim)

ASSOCIATED CONDITIONS 

THRUST REVERSERS 

During landing, application of reverse thrust above ___% N₁ is not permitted    at airspeeds below ___ KIAS. 

Below ____ KIAS reverse thrust must be reduced to ____ 

(not above ___% N_1.)

(Verbatim)

During landing application of reverse thrust above 60% N₁ is not permitted at airspeeds below 75 KIAS.   

Below 60 KIAS reverse thrust must be reduced to IDLE 

(not above 30% N_1.)

(Verbatim)

ASSOCIATED CONDITIONS 

FUEL IMBALANCE,

Max permissible fuel imbalance between L and R WING tanks: 

T/O:  _____ lbs.

All other phases of flight: ____ lbs.

(Verbatim)

ASSOCIATED CONDITIONS 

FUEL IMBALANCE,

Max permissible fuel imbalance between L and R WING tanks

T/O:  800 lbs.

All other phases of flight: 800 lbs.

(Verbatim)

ASSOCIATED CONDITIONS

FUEL QUANTITY

(Fuel quantities are based on 6.75 lbs/US Gal.)

Pressure Refueling Gravity Refueling

Max Usable

Total Fuel Load: ________ lbs. ________ lbs.

Pressure Refueling Gravity Refueling

Max Usable

Total Fuel Load: 14,518 lbs. 13,906 lbs.

ASSOCIATED CONDITIONS

FUEL CROSSFLOW

_______Crossflow and _______ Crossflow must be ____ for T/O.

(Verbatim)

Takeoff w/ engine fuel temp indications below 5^oC (41^oF) is prohibited.

Powered Crossflow and Gravity Crossflow must be  OFF for T/O.

(Verbatim)

Takeoff w/ engine fuel temp indications below 5^oC (41^oF) is prohibited. 

APU STARTER LIMITS 

APU Start (on BATTERY)

Start            Max Time ON             Followed by

1                      30 Secs                 2 Mins OFF

2                      30 Secs               __ Mins OFF

3                      30 Secs                 2 Mins OFF

4                      30 Secs               __ Mins OFF

NOTE: 

The 2-Min delay must be ______ between _____ attempts to allow for

cooling of the ______ and ____ __________ and APU fuel drainage.

APU STARTER LIMITS 

APU Start (on BATTERY)

Start            Max Time ON             Followed by

1                      30 Secs                 2 Mins OFF

2                      30 Secs               20 Mins OFF

3                      30 Secs                 2 Mins OFF

4                      30 Secs               40 Mins OFF

NOTE: 

The 2-Min delay must be observed between cranking attempts to allow for cooling of the starter and start contactor and APU fuel drainage.

APU OPERATING RANGE 

APU Starting and operation is permitted within the following operating envelope:

Max Starting Altitude:                 ________ feet

Max Operating Altitude:              ________ feet 

APU OPERATING RANGE 

APU Starting and operation is permitted within the following operating envelope:

Max Starting Altitude:                  30,000 feet

Max Operating Altitude:               36,000 feet

APU BLEED AIR LIMITATIONS

System/Condition Limitation

Air Conditioning: Bleed Air extraction from the APU is not permitted above _________ft.

Engine Start During Ground Operations: Each engine may be started using the APU as a bleed air source.

If both engines are to be started using the APU bleed air,

operating engine's thrust must not exceed _____ N_2.

APU BLEED AIR LIMITATIONS

System/Condition Limitation

Air Conditioning Bleed Air extraction from the APU is not permitted above 15,000 ft.

Engine Start During Ground Operations: Each engine may be started using the APU as a bleed air source.

If both engines are to be started using the APU bleed air operating engine's thrust must not exceed 70% N_2.

APU DOOR OPEN LIMITATION 

With the APU door not closed or the door position is unknown, 

The airplane must be limited to:  ___ KIAS 

Or the APU must remain __  ____________ .

(Verbatim)

APU DOOR OPEN LIMITATION 

With the APU door not closed or the door position is unknown, 

The airplane must be limited to: 300 KIAS 

Or the APU must remain in operation.

(Verbatim)

AIR CONDITIONING 

Max Altitude for Single Pack Operation: ______ ft.

Use of the EMER DEPRESS switch above _______ ft is prohibited.

AIR CONDITIONING 

Max Altitude for Single Pack Operation: 25,000 ft. 

Use of the EMER DEPRESS switch above 15,000 ft is prohibited.

AUTOMATIC FLIGHT CONTROL SYSTEM 

Use of SPEED MODE (DES or IAS),  Flight Director, or Autopilot Coupled, during Approach is not permitted.

Operation with the Autopilot engaged is prohibited at altitudes below ____ft. AGL except when performing the following:

-For visual and non-precision approaches the minimum height for autopilot use is ___ AGL.

-For Precision Approaches (PAR/ILS) the minimum height for autopilot use is

___ AGL.

Cat II approach must be flown w/ the autopilot engaged.

AUTOMATIC FLIGHT CONTROL SYSTEM

Use of SPEED MODE (DES or IAS),  Flight Director or Autopilot Coupled, during Approach is not permitted.

Operation with the Autopilot engaged is prohibited at altitudes below 600' ft. AGL except when performing the following:

-For visual and non-precision approaches the minimum height for autopilot use is 400' AGL.

-For Precision Approaches (PAR/ILS) the minimum height for autopilot use is

80' AGL.

Cat II approach must be flown w/ the autopilot engaged.

RVSM AIRSPACE 

The ADC source coupled to the ______  ___ must be the same as that coupled to

the__  _______ during flight in RVSM airspace.

• In flight, prior to entering RVSM airspace, all ________  __________ for operation in RVSM airspace must be operational.
• Max cruise speed in RVSM airspace is .___ Mach.

RVSM AIRSPACE

The ADC source coupled to the Active FCC must be the same as that coupled to

the ATC Transponder during flight in RVSM airspace.

• In flight, prior to entering RVSM airspace, all Required Equipment for operation in RVSM airspace must be operational.
• Max cruise speed in RVSM airspace is .82 Mach.

RVSM REQUIRED EQUIPMENT LIST 

Equipment                            Requirements for RVSM

________                             Must be operational

________ Alerting System     Must be operational

________ Reporting Transponder (2)        

                                     ____ must be operational

Air Data Computers (2)   ____ must be operational

RVSM REQUIRED EQUIPMENT LIST 

Equipment                                   Requirements for RVSM

-Autopilot                              Must be operational

-Altitude Alerting System        Must be operational

-Altitude Reporting

           Transponder (2)         One (1) must be operational

-Air Data Computers (2)        Two (2) must be operational

PERMISSIBLE DC ELECTRICAL SYSTEM LOADS 

To protect the flight compartment ___ displays, 

the maximum permissible time for ____  _______ 

with the __ power only is __ mins.

(Verbatim)

PERMISSIBLE DC ELECTRICAL SYSTEM LOADS 

To protect the flight compartment CRT displays, 

the maximum permissible time for ground operations 

with the DC power only is 5 mins.

(Verbatim)

SLATS/FLAPS 

Enroute use of Slats/Flaps is prohibited.

Max Slats and/or Flaps EXTENDED Altitude is  _____ ft.

SLATS/FLAPS 

Enroute use of Slats/Flaps is prohibited.

Max Slats and/or Flaps extended Altitude: 15,000 ft.

FLIGHT SPOILERS\

Min Alt for Flight Spoiler Deployment:  ____ ft. AGL

To ensure adequate _______ ______ flight spoilers must not be extended inflight at airspeeds below the recommended ______ speed PLUS __ KIAS.

(Bold type, Verbatim)

FLIGHT SPOILERS

Min Alt for Flight Spoiler Deployment:  1,000 ft. AGL

To ensure adequate maneuver margins flight spoilers must not be extended in-flight at airspeeds below the recommended Approach speed PLUS 17 KIAS.

(Bold type, Verbatim)

TAXI LIGHTS 

The Taxi Lights must be ________ ___ whenever the airplane is stationary in excess of __ mins.

(Verbatim)

TAXI LIGHTS 

The Taxi Lights must be switched OFF whenever the airplane is stationary in excess of 10 mins.

(Verbatim)

WHEEL BRAKE COOLING LIMITATIONS

Min brake cooling time is __ mins and all ____ indicators

must be _____ and not ________.

(Verbatim)

WHEEL BRAKE COOLING LIMITATIONS

Min brake cooling time is 15 mins and all BTMS indicators

must be green and not increasing.

(Verbatim)

QRH Handbook

P-I-A-C-C-E

1. __ Maintains Aircraft Control

2. Identify the ___-________

3.  Accomplish Immediate ______ Items

4.  _______ Assigns PF duties

5.  Complete ___ Procedures

6.  Establish and Communicate a ____

QRH Handbook

P-I-A-C-C-E

1. PF Maintains Aircraft Control

2. Identify the Non-normal

3.  Accomplish Immediate Action Items

4.  Captain Assigns PF duties

5.  Complete QRH Procedures

6.  Establish and Communicate a Plan

When practical the FA should be informed of the T-E-S-T items:

T-_____ of Emergency

E-___

S-______ for Brace

T-Take Special ____________

When practical the FA should be informed of the T-E-S-T items:

T-Type of Emergency

E-ETA

S-Signal for Brace

T-Take Special Instructions

IMMEDIATE ACTION ITEMS (Verbatim)

Braking Loss/Asymmetry

1.  Wheel Brakes.......Release _____________

2.  PM will select _____-_____ to OFF

3.  Wheel Brakes......._______ as required 

Extreme caution is required during braking to avoid tire damage

4.  Reverse Thrust.....Apply max until _______ ______

5.  Immediate Action Items Complete.

IMMEDIATE ACTION ITEMS (Verbatim)

Braking Loss/Asymmetry

1. Wheel Brakes.......Release momentarily

2. PM will select ANTI-SKID to OFF

3. Wheel Brakes.......Reapply as required 

    Extreme caution is required during braking to avoid tire damage

4. Reverse Thrust...Apply max until stopping assured

5.  Immediate Action Items Complete.

*IMMEDIATE ACTION ITEM*

CABIN ALT Msg

-or-

Emergency Descent Procedure 

1.  O_{2 Masks..............................___ and ____}

2.  Crew Communication.......________

3.  Captain assumes __ duties.

4.  Pass Signs......................ON

5.  ATC................Declare Emergency and Advise of Descent

6.  Autopilot.........Recommended

7.  Altitude Preselector..Set to 10,000' or Lowest Safe Alt

8.  SPEED Mode....................Select

9.  Thrust Lever....................IDLE

10. FLIGHT SPOILER lever......MAX Deploy

11. Immediate Action Items complete, go to page 5-1

*IMMEDIATE ACTION ITEM*

CABIN ALT Msg

-or-

Emergency Descent Procedure 

1.  O_{2 Masks..............................Don and 100%}

2.  Crew Communication.......Establish

3.  Captain assumes PF duties

4.  Pass Signs......................ON

5.  ATC................Declare Emergency and Advise of Descent

6.  Autopilot.........Recommended

7.  Altitude Preselector..Set to 10,000' or Lowest Safe Alt

8.  SPEED Mode....................Select

9.  Thrust Lever....................IDLE

10. FLIGHT SPOILER lever......MAX Deploy

11. Immediate Action Items complete, go to page 5-1

*IMMEDIATE ACTION ITEM*

EMERGENCY DEPRESSURIZATION 

If cabin pressure is verified to be ____________ and

the airplane _________ _________ is in doubt

it is preferable to maintain __ or _____ the speed at which the malfunction occurred and avoid high __________ loads.

(Verbatim)

*IMMEDIATE ACTION ITEM*

EMERGENCY DEPRESSURIZATION 

If cabin pressure is verified to be uncontrollable and

the airplane structural integrity is in doubt

it is preferable to maintain at or below the speed at which the malfunction occurred and avoid high maneuvering loads.

(Verbatim)

*IMMEDIATE ACTION ITEM*

DOUBLE ENGINE FAILURE 

1.  CONT IGNITION..........................ON

2.  Airspeed....................................240 KIAS Minimum

3.  Engine Instruments......................Monitor N₁, N₂ & ITT

If engines continue to run down:

4.  Thrust Levers (both)....................SHUTOFF

5.  ADG manual deploy handle............PULL

When ADG power is established

6.  STAB TRIM CH 2...........................ENGAGE 

WARNING

Maintain airspeed until ready to restart engines.  Failure to maintain at least 4% N2 may preclude a successful relight.  If required increase airspeed to maintain at least 4% N2 indication.

7.  Immediate Action Items complete, assign PF, go to page 2-1. 

*IMMEDIATE ACTION ITEM*

DOUBLE ENGINE FAILURE 

1.  CONT IGNITION..........................ON

2.  Airspeed....................................240 KIAS Minimum

3.  Engine Instruments......................Monitor N₁, N₂ & ITT

If engines continue to run down:

4.  Thrust Levers (both)....................SHUTOFF

5.  ADG manual deploy handle............PULL

When ADG power is established

6.  STAB TRIM CH 2...........................ENGAGE 

WARNING

Maintain airspeed until ready to restart engines.  Failure to maintain at least 4% N2 may preclude a successful relight.  If required, increase airspeed to maintain at least 4% N2 indication.

7.  Immediate Action Items complete, assign PF, go to page 2-1. 

*IMMEDIATE ACTION ITEM*

SMOKE/FUMES

1.  O2 Masks........................___ and ____

2.  Crew Communication.....__________

3.  Immediate Action Items complete, assign PF, go to page 1-1.

The SMOKE/FUMES QRH checklist will be accomplished for any smoke or fumes related malfunction w/o an associated CAS message.

*IMMEDIATE ACTION ITEM*

SMOKE/FUMES

1.  O2 Masks........................Don and 100%

2.  Crew Communication.......Establish

3.  Immediate Action Items complete, assign PF, go to page 1-1.

The SMOKE/FUMES QRH checklist will be accomplished for any smoke or fumes related malfunction w/o an associated CAS message.

*IMMEDIATE ACTION ITEM*

STAB/TRIM RUNAWAY

1.  Control Wheel................Assume ______ Control and Override Runaway

2.  Both STAB TRIM DISC's...____, ____ & _______

3.  Captain assumes PF duties.

4.  STAB CH1 cb (2F5).................OPEN

5.  STAB CH2 cb (4A1).................OPEN

6. Immediate Action Items Complete, assign PF, go to Pg 9-1.

-If the Horizontal Stabilizer is in motion for >3 secs a clacker is activated to alert the crew of a possible horizontal stabilizer trim runaway condition.

-The trim position indicator on the EICAS screen will also show runaway trim movement.

*IMMEDIATE ACTION ITEM*

STAB/TRIM RUNAWAY

1.  Control Wheel........Assume manual Control and Override Runaway

2.  Both STAB TRIM DISC's......Push, Hold & Release

3.  Captain assumes PF duties.

4.  STAB CH1 cb (2F5).................OPEN

5.  STAB CH2 cb (4A1).................OPEN

6. Immediate Action Items Complete, assign PF, go to Pg 9-1.

-If the Horizontal Stabilizer is in motion for >3 secs a clacker is activated to alert the crew of a possible horizontal stabilizer trim runaway condition.

-The trim position indicator on the EICAS screen will also show runaway trim movement.

Not memory Items but under the 

IMMEDIATE ACTION ITEMS tab in the QRH:

L/R-A-E-R-U

Left/Rt Eng Oil LO Pressure

A______ System Jam

E______ System Jam

R______ System Jam

Uncommanded ___ Motion

Not memory Items but under the 

IMMEDIATE ACTION ITEMS tab in the QRH:

L/R-A-E-R-U

Left/Rt Eng Oil LO Pressure

Aileron System Jam

Elevator System Jam

Rudder System Jam

Uncommanded Yaw Motion

APU STARTER LIMITS

APU Start (Using DC Ground Power)

Start                 Max Time ON                   Followed By

 1                          15 Secs                          2 Mins OFF

 2                          15 Secs                        __ Mins OFF

 3                          15 Secs                          2 Mins OFF

 4                          15 Secs                        __ Mins Off

APU STARTER LIMITS

APU Start (Using DC Ground Power)

Start                 Max Time ON                   Followed By

 1                          15 Secs                          2 Mins OFF

 2                          15 Secs                        20 Mins OFF

 3                          15 Secs                          2 Mins OFF

 4                          15 Secs                        40 Mins Off

Max APU RPM:________%