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General
Required Flight Crew
- Pilot, Co-Pilot
- (Captain, First Officer)
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General
Types of Aircraft Operations
This aircraft meets the airworthiness requirements of FAR's Part 25 (Airworthines Standards, Transport Category Airplanes) and Part 36 (Noise Standards). When the appropriate equipment and instruments, as required by the airworthiness and operating regulations are approved, installed and in operable condition, flight in the following conditions are approved:
- Day and Night
- VFR and IFR
- Flight in Icing conditions
(WARNING) This aircraft is not certified for ditching, because the safety equipment specified by the applicable regulations is not installed)
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General
RVSM operations must not be commenced or continued unless all of the required equipment specified below is operational.
Equipment Required for RVSM
- (1) Autopilot .....................Must be Operational
- (1) Alt. Alerting System......Must be Operational
- (2) Alt. Reporting Transponder ......(1) Must be Operational
- (2) Air Data Computers ....(2) Must be operational
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General
When on RVSM airspace, the ADC source must be the same as?
- Must be the same as that coupled to ATC transponder during flight in RVSM airspace,
- (FL 290 to FL 410)
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General
Runway Slope %, for Takeoff and Landing
-2% to +2%
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General
Tailwind Component for Takeoff and Landing
10 kts.
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General
Flight Maneuvering Load Acceleration Limits for:
Flaps Up
Flaps Down
Flaps up.......................+2.5g to -l.0g
Flaps down..................+2.0g to 0g
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General
Side-Slip Maneuvers caution
Avoid unnecessary and large side-slip maneuvers during low speed, high altitude cruise.
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Air - Cabin Pressurization
Max. Differential Pressure
8.7 psi
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Air - Cabin Pressurization
Max. Negative Differential Pressure
- 0.5 psi
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Air - Cabin Pressurization
During taxi, takeoff and landing, the pressure differential must not exceed,
0.1 psi
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Air - Cabin Pressurization
The aircraft must be completely depressurized prior to,
Opening any of the aircraft doors.
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Air - Cabin Pressurization
The maximum altitude for single pack operation is
FL 310
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Air
If the APU is the bleed source in Manual Mode, the use of Wing and/or Cowl anti-ice with APU in Manual Mode...
WING and/or COWL anti-ice selection is Prohibited with the APU as a bleed source in manual mode.
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Air
Use of the EMER DEPRESS above 15,000 ft.
To preclude possible crew and/or passenger ear damage, use of the EMER DEPRESS switch above 15,000 ft. is Prohibited.
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Airspeeds - Maximum Allowable Airspeeds
Maximum Operating - VMO/MMO
335/.85 Mach
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Airspeeds - Maximum Allowable Airspeeds
Maximum Operating from FL 250 to FL 410 - VMO/MMO
Red Line
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Airspeeds - Maximum Allowable Airspeeds
Maximum Operating (KIAS) from 8,000 ft. MSL to FL 250 - VMO
Red Line/335
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Airspeeds - Maximum Allowable Airspeeds
Maximum Operating (KIAS) up to 8,000 ft. MSL - VMO
Red Line/330
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Airspeeds - Maximum Allowable Airspeeds
Maximum Turbulence Penetration Speed - VB/MB
280/.75 MACH (whichever is Lower)
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Airspeeds - Maximum Allowable Airspeeds
Maximum Maneuvering Speed at Sea Level @ 75,000 lb. - VA
253 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Landing Gear Extension - VLOE
220 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Landing Gear Extended - VLE
220 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Landing Gear Retraction - VLOR
200 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Flap Placard Speeds - VFE Flaps 1°, 8°, 20°
230 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Flap Placard Speeds - VFE Flaps 30°
185 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Flap Placard Speeds - VFE Flaps 45°
170 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Maximum Wiper Operating Speed
250 Kts.
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Airspeeds - Maximum Allowable Airspeeds
Maximum ADG Operating Speed - VMO/MMO
335/.85 MACH
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Airspeeds - Maximum Allowable Airspeeds
Maximum Tire Limit Speed
182 Kts.
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Airspeeds - Maximum Allowable Airspeeds
RVSM Maximum Cruise Mach Number
Mach 0.83
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Airspeeds - Design Maneuvering Speed
Full application of rudder and aileron controls as well as maneuvers that involve angle of attack near the stall, must be confined to speeds below VA.
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Altitude - Maximum Operating Altitude
FL 410
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Altitude - Minimum Takeoff And Landing Pressure Altitude
-1,000 ft.
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Altitude - Maximum Takeoff And Landing Pressure Altitude
9,600 ft.
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Temperature - Maximum ambient air temperature for takeoff and landing
- ISA + 35°C
- (15°C) + 35°C = 50°C (122°F)
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Temperature
Minimum ambient temperature approved for Takeoff & Landing from -1,000 ft. to 9,600 ft. Pressure Altitude
-40°C (-40°F)
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APU - Starting
Ambient Temperature Limit:
(ground) and (flight)
EGT Limit:
- Minimum -40°C (ground) and -65°C (flight)
- EGT Limit: Red Line
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APU - Starting
Maximum EGT:
1038°C, Not to be exceeded under ANY conditions.
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APU - Starting
Altitude Limit for APU Start:
FL 370
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APU - Starting
Airspeed Limit:
VMO/MMO
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APU - Starting
Starter Limitations:
How many Starts or Start Attemps?
3 Starts or Start attempts per 60 minutes, with a minimum of two minutes delay between cranking attempts to allow for cooling of the starter, starter contactor and for APU drainage.
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APU - Operating Range
RPM Limit:
Red line (106%)
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APU - Operating Range
EGT Limit:
Red line
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APU - Operating Range
Generator Loading Limit Altitude:
FL 410
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APU - Operating Range
Bleed Air Extraction Limit Altitude:
FL 250
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APU - Operating Range
Bleed Air Extraction (On Ground):
No Limit
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APU - Operating Range
Bleed Air Engine Start Limit Altitude:
FL 210
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APU - Operating Range
Airspeed Limit:
VMO/MMO
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APU - Starting
On the Ground Starting Altitude Limit:
15,000 ft.
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APU - Operating Range
Max EGT, APU on-speed
(dependant upon altitude and temperature):
Ground:
In flight:
- Ground: 682° C to 789° C
- In flight: 773° C to 806° C
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Autoflight - Minimum Use Heights
On Takeoff
600 ft. AGL
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Autoflight - Minimum Use Heights
Non Precision Approach:
400 ft. AGL
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Autoflight - Minimum Use Heights
Precision Approach with a GPA ≤ 3.5° degrees:
80 ft. AGL
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Autoflight - Minimum Use Heights
Precision Approach with a GPA > 3.5°; ≤ 4°
120 ft. AGL, provided that the airport elevation is below 4,000’. Above 4,000’ elevation, the use of the autopilot is prohibited.
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Autoflight - Minimum Descent Altitude
When setting the MDA marker using the DA / knob:
The MDA is adjusted to the next highest 10 ft. increment on a Precision Approach and the next highest 100 ft. on a Non-Precission Approach.
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Electrical - AC System:
Max. load on either main Generator up to 41,000 ft.
40 kVA
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Electrical - AC System:
Max. load on APU Generator up to 41,000 ft.
40 kVA
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Electrical - DC System: In Flight Operation:
Max. continuous load on each TRU
120 amps.
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Electrical - DC System Ground Operation:
Max permissible time for ground operations with DC (battery) power to protect the cockpit CRT displays:
5 minutes on DC (battery power).
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Electrical - Circuit Breaker Reset (In Flight)
- A circuit breaker must not be reset or cycled:
- Unless doing so is consistent with explicit procedures specified on AOM Vol.1, or unless in the judgment of the Captain, that resetting or cycling of the circuit breaker is necessary for the safe completion of the flight.
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Engines
What is the N1 value for Engine Start?
N/A
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Engines
What is the ITT value for Engine Start?
Red Line
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Engines
What is the N2 value for Engine Start?
0%-45%
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Engines
What is the OIL Temp value for Engine Start?
-40°C (minimum)
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Engines
What is the OIL Pressure value for Engine Start?
Amber value for a max. of 10 minutes
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Engines
What is the N1 value for Engine @ Idle?
20% - 25%
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Engines
What is the ITT value for Engine @ Idle?
N/A
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Engines
What is the N2 value for Engine @ Idle?
55% - 65%
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Engine Operating Limits
Max Time in TO/GA
5 Minutes
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Engine Operating Limits
Max Time in APR
10 Minutes - 1 Engine
5 Minutes - 2 Engines
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Engines
ITT temperature before Attempting to start an engine on the ground:
Below 120°C
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Engines
ITT temperature before Attempting to air start an engine:
Below 90°C
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Engines
Max oil pressure:
156 psi when oil temp transient is less than 60°C.
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Engines
Oil pressures should show
Positive value during start and may peak beyond 182 psi (max display value)
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Engines
How is Oil pressure displayed above 182 psi?
Is displayed as amber dashes.
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Engines
Max. time Oil pressure may be greater than 95 psi?
For a max. of 10 minutes.
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Engines
Low Oil Pressure (25 - 45 PSI) when above IDLE;
Low oil pressure (amber values) when above IDLE require oil temperature monitoring.
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Engines - APR Thrust
Pilot initiated APR Thrust
(MAX POWER detent or HIGH PWR SCHEDULE switchlight)
- Is Prohibited:
- For the first 30 minutes after any engine start at altitudes below 7,500 MSL
At all times Above 7,500 MSL
(note) This limitation does not prohibit the pilot from selecting APR as required for safety of flight. If subsequently restarted in flight, the engine will reset the FADEC and the 30 minute warm up time limit re-applies.
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Engines
ITT EXCEED B(B1)(C) Status Message
Any ITT EXCEED B(B1)(C) status message must be logged in the AML.
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Engines - Thrust Management Data
With the engines running and bleeds configured for takeoff:
The crew must verify that the target N1 values correspond to the data presented in the TPS message and the thrust setting charts (+1.0%) Refer to the TPS message or CRJ-700 Flip Cards.
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Engines - Thrust Management Data
With the thrust levers set for takeoff;
The target and actual N1 values should match.
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Engines - Takeoff Method
Method “A”, “B” or “C”.
- 30° either direction from aircraft nose; no wind speed limit
- OR
- >30° either direction from aircraft nose; <5 kts. wind speed.
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Engines - Takeoff Method
Method “B” or “C”.
(Do NOT exceed 75% N1 before brake release)
>30° either direction from aircraft nose, between 5 and 30 kts. wind speed.
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Engines - Takeoff Method
Method “C” only.
>30° either direction from aircraft nose, >30 kts. windspeed.
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Engines - Aircraft Cold Soak
Before the first flight of the day, when the aircraft is cold-soaked at an ambient temperature of -30°C or below for more than eight hours:
The engines must be motored for 60 seconds and the fan rotation must be verified on the N1 indicator before an engine start is initiated.
The thrust reversers must be actuated until the deploy and stow cycles are two seconds or less.
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Engines - Continuous Ignition
Continuous ignition must be used during the following:
- Takeoffs and landings on a contaminated runway
- Flight through moderate or heavier intensity rain
- Flight through moderate or heavier intensity turbulence
- Flight in the vicinity of thunderstorms.
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Engines - Warm Up
The engines must remain at IDLE until oil pressure reaches normal operating range.
During all starts, do not exceed 75% N1 for two minutes after start, or until all operating indications are in the normal range, whichever is longer.
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Engines - Thrust Reversers
Thrust reversers are approved for ground use only, activation of the reverse thrust levers in flight is..
Prohibited
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Engines - Thrust Reversers
The thrust reversers are intended for use during full stop landings. Do not attempt a go-around maneuver after...
Deployment of the thrust reversers.
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Engines - Thrust Reversers
Takeoff with any thrust reverser icon of the EICAS warning and/or caution message displayed is...
Prohibited
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Engines - Starter Limits
The starter must not be used if indicated N2 RPM exceeds
45% N2
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Engines - Starter Limits
Engine Start (Ground)
(Thrust Lever has been advanced to IDLE)
1st and 2nd cycles
90 seconds ON, 10 sec OFF
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Engines - Starter Limits
Engine Start (Ground)
(Thrust Lever has been advanced to IDLE)
3rd through 5th cycles
90 seconds ON, 5 mins OFF
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Engines - Starter Limits
Engine Start or Motoring (Flight)
1st cycle
2 Minutes ON, 10 sec OFF
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Engines - Starter Limits
Engine Start or Motoring (Flight)
2nd through 5th cycles
1 Minute ON, 5 mins OFF
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Engines - Starter Limits
Motoring (Ground)
(Thrust Lever remains at SHUTOFF)
1st cycle
90 seconds ON, 5 mins OFF
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Engines - Starter Limits
Motoring (Ground)
(Thrust Lever remains at SHUTOFF)
2nd through 5th cycles
30 seconds ON, 5 mins OFF
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Engine Relight
Starter Assisted
Altitude from 21,000 to sea level
Speed from VREF up to Vmo and from 0 to 45% N2
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Engine Relight
Special All Engine Out (AEO) Rapid Relight
Altitude from 10,000 to Sea Level
FADEC rapid relight capability has been demonstrated at 200 kias for up to 15-second fuel interruptions.
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Engine Relight
Windmilling
10,000 feet to Sea level
Speed 250 KIAS to Vmo and 7.2% N2 minimum.
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Engine Relight
Windmilling
21,000 feet to 10,000 feet
Speed 290 KIAS to Vmo and 7.2% N2 minimum
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Engines - Starter Limits
CAUTION
Motoring Cycle limits may not be combined with Starting Cycle limits.
Any time the Thrust Lever has been advanced to IDLE, Motoring Cycle limits cannot be applied.
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Flight Controls - Slats/Flaps
Enroute use of slats/flaps is;
Prohibited.
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Flight Controls - Slats/Flaps
Use of slats/flaps during holding is...
Prohibited
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Flight Controls - Slats/Flaps
Maximum altitude for slats/flaps extension is
15,000 feet.
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Flight Controls - Flight Spoilers
Flight spoilers must not be extended in flight below an altitude of...
500 feet AGL.
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Flight Controls - Flight Spoilers
To ensure adequate maneuver margins, flight spoilers must not be extended in flight at airspeeds below...
The recommended approach speed plus 10 KIAS.
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Flight Controls - Ground Lift Dumping
The GND LIFT DUMPING switch must always be selected to...
AUTO during takeoffs and touch-and-go landings.
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Flight Controls - Horizontal Stab Trim
Horizontal stabilizer trim position indications...
Must be checked before each flight.
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Flight Instruments - Integrated Standby Instrument
When NAV 1 is tuned to a valid ILS frequency, the ISI will display localizer and glide slope deviation while on the backcourse approach. Use of the ISI localizer and backcourse information is...
Prohibited during backcourse approaches.
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Flight Instruments
Attitude and Heading Reference System
The aircraft must not be moved until...
All attitude and heading information presented on PFD is valid.
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Flight Management System (FMS)
General
The Flight Management System (FMS) must be operated...
In accordance with this Aircraft Operating Manual.
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Flight Management System (FMS)
Enroute and Terminal
IFR enroute and terminal navigation is...
Prohibited unless the pilot verifies the currency of the database and verifies waypoints for accuracy by reference to current publications (Jeppesen).
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Flight Management System (FMS)
Enroute and Terminal
The VNAV System information is not temperature compensated. FMS generated altitudes and V-paths...
are not corrected for non-ISA conditions.
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Flight Management System (FMS)
Enroute and Terminal
FMS range, fuel management and altitude/speed capability information is...
Advisory only.
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Flight Management System (FMS)
Approach
ILS, LOC, LOC-BC, LDA, SDF and MLS approaches using the FMS are..
Prohibited
Only Non-Precision Approches are approved.
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Flight Management System (FMS)
Approach
Instrument approaches must be accomplished..
- Instrument approaches must be accomplished with Instrument Approach Procedures that are retrieved from the FMS database.
- The FMS must incorporate the current update cycle. The pilot must verify approach waypoints for accuracy by reference to current publications (Jeppesen).
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Flight Management System (FMS)
Approach
Operations with a VNAV final approach glidepath angle that exceeds 4.0° are...
Prohibited.
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Flight Management System (FMS)
Approach
The approach must not be continued past the final approach fix, if...
an FMS "NO APPR" message is displayed on the PFD.
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Fuel - Temperature
Takeoff with engine fuel temperature indications below 5°C is...
Prohibited, L (R) FUEL LO TEMP caution message will be displayed.
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Fuel - Temperature
Takeoff with bulk fuel temperature indications below the limits stated is...
Prohibited.
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Fuel - Temperature
During flight, bulk fuel temperature must remain....
Above the applicable bulk fuel freezing point.
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Fuel - Temperature
Fuel Type:
Bulk Fuel Temp Takeoff Limit:
Bulk Fuel Temp during Flight Limit:
Fuel - JET A
Bulk Fuel Temp Takeoff Limit - (-30°C)
Bulk Fuel Temp during Flight Limit - (-40°C)
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Fuel - Quantity
Takeoff with a fuel load in excess of _______ lbs. in the center tank is not permitted unless each main wing tank is above ________ lbs.
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Fuel - Quantity
The minimum fuel quantity for go-around is ______ lbs. per wing (with the aircraft level) and assuming a maximum aircraft climb attitude of 10° nose up.
600 lb.
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Fuel - Imbalance
The max. permissible fuel imbalance between the contents of the left main tank and the right main tank,
During takeoff _____ lbs.
During all other phases of flight _______ lbs.
- During takeoff......300 lb.
- All other phases of flight.....800 lb.
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Fuel - Crossflow
Power and Gravity Crossflow must be
Off for takeoff
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Global Positioning System (GPS)
General
When flying to an airport where a GPS stand-alone approach is intended and is the only suitable approach, prior to dispatch...
the crew must verify that the predictive RAIM at the destination is AVAILABLE during the ETA.
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Ice and Rain
Ice Protection Procedures
TAXI
Ground Contamination or Visible Moisture
TEMP: OAT 10°C or colder
IAS:N/A
ANTI-ICE:________
ANTI-ICE: COWL
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Ice and Rain
Ice Protection Procedures
TAKEOFF
Ground Contamination or Visible Moisture
TEMP: OAT 10°C or colder
IAS:N/A
ANTI-ICE:________
ANTI-ICE: COWL
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Ice and Rain
Ice Protection Procedures
TAKEOFF
Ground Contamination or Visible Moisture
TEMP: OAT 5°C or colder
IAS:N/A
ANTI-ICE:_________
ANTI-ICE: COWL and WING
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Ice and Rain
Ice Protection Procedures
IN FLIGHT
Visible Moisture
TEMP: Between SAT -40°C and TAT 10°C
IAS: >230
ANTI-ICE: _______
ANTI-ICE: COWL
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Ice and Rain
Ice Protection Procedures
IN FLIGHT
Visible Moisture
TEMP: Between SAT -40°C and TAT 10°C
IAS: <230
ANTI-ICE: _______
ANTI-ICE: COWL and WING
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Ice and Rain
Ice Protection Procedures
Ground contamination definition:
Ramps, taxiways or runways with surface snow, ice, slush or standing water.
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Ice and Rain
Ice Protection Procedures
Visible moisture definition:
Visibility of one mile or less, clouds, snow, ice crystals, sleet or rain
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Ice and Rain
Ice Protection Procedures
When Type II or Type IV Anti-icing Fluids have been applied:
WING anti-ice, if required, must be selected ON just prior to thrust increase for take-off.
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Ice and Rain
Severe Icing – Super-Cooled Large Droplet Icing
Continued operation in areas of Severe Icing conditions is...
Prohibited
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Ice and Rain
Severe Icing – Super-Cooled Large Droplet Icing
Severe Icing conditions are indicated by ice accretion on...
the cockpit side windows
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Ice and Rain
Severe Icing – Super-Cooled Large Droplet Icing
If severe Icing is encountered:
- WING and COWL Anti-Icing Systems must be ON
- Leave icing conditions
- NOTE
- Do not hold in icing condition with flaps/slats extended.
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Cold Weather Operations
Take-off is prohibited with frost, ice, snow or slush adhering to any critical surface (wings, upper fuselage, horizontal stabilizer, vertical stabilizer,control surfaces and engine inlets).
NOTE
Take-off is permitted with frost adhering to:
- the upper surface of the fuselage; and/or
- the underside of the wing, that is caused by cold soaked fuel
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Landing Gear
Wheel Brake Cooling
A minimum brake cooling time of...
15 minutes must be observed between a landing stop or a rejected takeoff and the subsequent takeoff.
BTMS brake temperatures must be in the green range before takeoff.
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Miscellaneous
Taxi Lights
The taxi lights must be switched OFF whenever the aircraft is stationary in excess of ________.
10 minutes.
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Structural Weights
Structural Weight Limitations
Maximum Ramp
MRAMP - 75,250 lbs.
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Structural Weights
Structural Weight Limitations
Maximum Takeoff
MTOW - 75,000 lbs.
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Structural Weights
Structural Weight Limitations
Maximum Landing
MLW - 67,000 lbs.
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Structural Weights
Structural Weight Limitations
Maximum Zero Fuel
MZFW - 62,300 lbs.
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Structural Weights
Structural Weight Limitations
Minimum Flight Weight
42,000 lbs.
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Structural Weights
Structural Weight Limitations
Minimum Operating Empty Weight
39,835 lbs.
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