POH Chapter 3 Flashcards
Minimum flight crew
One Captain and one First Officer
Maximum 90 degree crosswind for takeoff and landing
27 knots
Maximum 90 degree crosswind for landing from a Category II Approach
15 knots
Maximum headwind for landing from a Category II Approach
16 knots
Maximum direct tailwind for takeoff and landing
10 knots including gusts
Maximum runway slope approved for takeoff and landing
+2.0% (uphill) -2.0% (downhill)
Maximum operating altitude
41,000 ft
Maximum pressure altitude for takeoff and landing
8,000 ft
Maximum ambient temperature for takeoff and landing
ISA +35°C
Minimum ambient temperature approved for takeoff
-40°C
Maneuvering Limit Load Factors Flaps Retracted
-1.0 to +2.5G
Maneuvering Limit Load Factors Flaps Extended
0.0 to +2.0G
Except in an emergency, takeoff or landing will not be attempted whenever peak wind value ______.
exceeds 50 knots
Maximum Taxi and Ramp Weight
700: 75,250 lbs 900: 85,000 lbs
Maximum Takeoff Weight
700: 75,000 lbs 900: 84,500 lbs
Maximum Landing Weight
700: 67,000 lbs 900: 75,100 lbs
Maximum Zero Fuel Weight
700: 62,300 lbs 900: 70,750 lbs
Flight must be within ______ of a suitable airport, if cargo is carried in either cargo compartment.
60 minutes
Turbulence Penetration Speed
280 KIAS/.75M whichever is lower
Maximum gear extension speed
220 KIAS
Maximum gear extended speed
220 KIAS
Maximum gear retraction speed
200 KIAS
Maximum airspeed for windshield wiper operation
220 KIAS
Maximum airspeed for windshield wiper operation failed in the non-parked position
250 KIAS
Maximum Cruise Mach in RVSM Airspace
0.82M
Tire limit ground speed 700
182 knots
Tire limit ground speed 900
195 knots
Vfo/Vfe Flaps 1
Flaps 1 – 230 KIAS
The VFE and VFO speeds are ______.
equal
The Wing and Cowl Anti-Ice System(s) shall be operated in accordance with the following conditions:
Ground contamination definition
Runways, ramps or taxiways with surface snow, ice, slush or standing water
Visibile moisture definition
- Visible moisture or precipitation in any form (such as fog with visibility of 1 mile or less, mist, rain, snow, sleet and ice crystals or clouds in flight)
- If visible moisture is present below 400 feet AGL with OAT of 10°C or below activate cowl anti-ice for takeoff. If OAT 5°C or below activate both cowl and wing anti-ice for takeoff
Engine Indications (Red, Amber, Green)
- Maximum and minimum limitations
- Caution range
- Normal operating range
During all starts, do not _______________________________________________.
exceed 75% N 1 for 2 minutes after start, or until all operating indications are in the normal range, whichever is longer.
Prior to shutdown _________________________.
Operate engines at or near idle for 2 minutes
ITT limitations for ground start and airstart
Below 120°C before attempting to ground start and below 90°C before attempting to airstart
Steady-state idle minimum oil pressure
25 psi
Takeoff power minimum oil pressure
45 psi
Continuous engine ignition must be used during the following:
- Takeoff and landing on contaminated runways
- Takeoff with high crosswind components (15 knots or greater)
- Flight through moderate or heavier intensity rain
- Flight through moderate or heavier intensity turbulence
- Flight in the vicinity of thunderstorms
Engine operating limits due to wind direction
Engine Starter Cranking Limits (701 Ground only) (900 Ground Only)
Engine Starter Cranking Limits (701 Flight only) (900 Flight Only)
The starter must not be engaged if ________________.
indicated N2 RPM exceeds 45% (inflight or on the ground)
At initiation of thrust lever movement from SHUT OFF to IDLE:
- ITT must be 120°C or less for all ground starts
- ITT must be 90°C or less for all air starts
A dry-motoring cycle (with thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts. Limitations:
Oil pressure limitations
Maximum permissible fuel imbalance between left and right tank
- Takeoff: 300 lbs
- All other phases of flight: 800 lbs
Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is _________.
not usable
Fuel quantities are based on _______.
6.75 lbs / per U.S. gallon
Takeoff with a fuel load in excess of ______ in __________ is not permitted unless ___________________. __________________ must be OFF for takeoff.
500 lbs. in the center tank is not permitted unless each wing tank is above 4,400 lbs. Powered crossflow and gravity crossflow must be OFF for takeoff.
The APU starter motor duty cycle is limited to not more than _____ starts/start attemps in ______ hour with a ______ minute delay between cranking attemps
3 starts/start attempts in 1 hour with a 2 minute delay between cranking attempts
APU Bleed Air Limitations
With the APU door not closed or the door position is unknown:
- The airplane must be limited to: 220 KIAS
- Or the APU must remain in operation
Use of ______________ during approach is not permitted.
SPEED MODE (DES or IAS), flight director or autopilot coupled
Use of ______________ during the climb and approach phases of flight is not permitted.
VNAV, flight director or autopilot coupled
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 ft. AGL
- For precision approaches (PAR/ILS), the minimum height for autopilot use is 80 ft. AGL unless:
- The glide path angle is greater than 3.5° and less than or equal to 4.0° and the Airport elevation is less than or equal to 4000 feet the minimum height for autopilot use is 120 ft. AGL
- ILS approaches with a glide path angle of greater than 4.0° is prohibited
- For precision approaches (PAR/ILS) or approach procedures with vertical guidance, the minimum height for autopilot use with one engine operating is 110 ft. AGL
- Category II Approach must be flown with the autopilot engaged.
- The ADC source coupled to the active FCC must be _________
- In flight, prior to entering RVSM airspace __________
- Maximum cruise speed in RVSM airspace is ________
- the same as that coupled to the ATC transponder during flight in RVSM airspace.
- all required equipment for operation in RVSM airspace must be operational.
- 0.82M
RVSM Required Equipment List
To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DC power only is _______.
5 minutes
- Enroute use of slats/flaps is _________
- Maximum slats and/or flaps extended altitude:
- prohibited
- 15,000 ft
Minimum altitude for flight spoiler deployment:
1,000 ft AGL
To ensure adequate maneuver margins, flight spoilers must not ____________________.
be extended inflight at airspeeds below the recommended reference speed plus 17 KIAS
During landing, maximum reverse thrust is ________________________________.
prohibited below 75 KIAS, and reverse idle should be achieved by 60 KIAS
The taxi lights must be switched OFF whenever _____________________________.
the airplane is stationary in excess of 10 minutes
Minimum brake cooling time is __________, and all _____________ must be _________________________.
15 minutes; BTMS indicators must be green and are not increasing
Maximum altitude for single pack operation
31,000 feet
Vfo/Vfe Flaps 8
Flaps 8 – 230 KIAS
Vfo/Vfe Flaps 20
Flaps 20 – 220 KIAS
Vfo/Vfe Flaps 30
Flaps 30 – 185 KIAS
Vfo/Vfe Flaps 45
Flaps 45 – 170 KIAS
Maximum starting altitude for the APU
37,000 feet
Maximum altitude for APU Bleed Air for Air Conditioning
25,000 feet
Maximum time at TOGA power on 2 engines
5 minutes
After cold start, engine must remain at ____ until oil pressure returns to normal range
idle
If Static/Standing takeoff data is generated and wind limits prevent a Static/Standing takeoff Winds must be entered in ____ OR for aircraft with ACARS inoperative, Dispatch must _______ winds into TLR data
ACARS
manually insert
Maximum fuel quantity for pressure refueling (total)
19,594 lbs
Maximum fuel quantity for gravity refueling (total)
700 - 14,580 lbs
900 - 14,810 lbs
Minimum fuel quantity for go-around per wing tank (with airplane level) and assuming a maximum airplane climb attitude of 10° nose up ____ lbs
600 lbs (CRJ700 & 900)
Icing conditions in flight exist when visible moisture is present, and the TAT ____ except when the SAT is _____ or below
10°C or below, except when the SAT is -40*C or below
Exterior Inspection to determine that the wing is free from forst, ice, snow, or slush when:
- The OAT is ___ or less, or
- The bulk fuel temperature is ____ or less or
- __________________
- Ice and frost may continue to adhere to wing surfaces for some time even at outside air temperatures above _____
- 10*C
- 0°C
- The atmospheric conditions have been conducive to frost formation
- 10°C
Do not hold in icing conditions with ______ extended
slats and/or flaps
Category II approaches are prohibited when the braking action is reported as less than _____.
Medium
Cabin Alt/Emergency Descent
Oxygen masks……………..DON and 100%
Crew communication……………..ESTABLISH
Captain Assumes PF Duties
Smoke/Fire/Fumes
Oxygen masks (if required)……………DON and 100%
Crew communication…………….ESTABLISH
Stabilizer Trim Runaway
Control wheel…………………ASSUME manual control and OVERRIDE runaway
STAB TRIM DISC…………………….Push, hold and release
Braking Loss/Asymmetry
Wheel brakes………….Release momentarily
PM will select ANTI-SKID to OFF
Wheel brakes………….Re-apply as required
Reverse Thrust………..Apply maximum until stopping assured
