CRJ 200 Limitations Flashcards
MAX RAMP
53,250LB
MAX T/O
53,000LB
MAX LND
47,000LB
MAX ZFW
44,000LB
MIN FLT WT.
30,000LB
WING SPAN
69’8”
AIRCRAFT LENGTH
87’10”
TAIL HEIGHT
20’8”
MAX OPS ALT
41,000’
MAX T/O & LND ALT
10,000’
MAX TEMP T/O & LND
ISA +35C
MIN TEMP T/0
-40C
MAX TAILWIND T/O & LND
10KTS
VMO
335KTS
MMO
MACH .85
VLO EXT
250KTS
VLO RET
200KTS
VLE
250KTS
VTIRE
182KTS (GS)
VADG DEPLOY MAX
250KTS(WET) VMO/MMO(DRY)
VB
280KTS
MB
MACH .75
VWIPER OPS MAX
22OKTS
VFO 8
200KTS
VFO 20
200KTS
VFE 8
215KTS
VFE 20
215KTS
VFE 30
185KTS
VFE 45
170KTS
MAX ALT SLATS/FLAPS
15,000’
FLAPS/SLATS ENROUTE
PROHIBITED
MIN SPOILER SPEED (stuck)
Approach speed Vref (flaps 45) +17kts
MIN ALT SPOILER
800’ AGL
SPOILERS WITH FLAPS 45
PROHIBITED
MIN RUNWAY WIDTH
75’
STANDING WATER T/0
.5 INCH
STANDING WATER LND
.75 INCH
SLUSH T/O
.5 INCH
SLUSH LND
.88 INCH
WET SNOW T/O
1 INCH
WET SNOW LND
1.5 INCH
DRY SNOW T/O
3 INCH
DRY SNOW LND
3.75 INCH
APU MIN TEMP START
-40C
MAX APU OPS ALT
37,000’
MAX APU START ALT
30,000’
MAX APU ALT BLEED USE
15,000’
MAX ALT APU ENG START
13,000’
MAX DOOR OPEN SPEED APU NOT IN USE
300KIAS
APU BAT START 1
30 SECONDS ON 2 MINUTES OFF
APU BAT START 2
30 SECONDS ON 20 MINUTES OFF
APU BAT START 3
30 SECONDS ON 2 MINUTES OFF
APU BAT START 4
30 SECONDS ON 40 MINUTES OFF
AUTO PILOT MUST BE ENGAGED IN
RVSM Airspace
AUTO PILOT IAS MODE
PROHIBITED DURING APP
AUTO PILOT DES MODE
PROHIBITED DURING APP
AUTO PILOT APPR MODE
PROHIBITED DURING VOR APPROACH
MAX TIME DC ONLY
5 MINUTES
MAX CONTINUOUS DC TRU
100A
TOTAL FUEL (PRESSURE REFUELING)
14,518LB
TOTAL FUEL(GRAVITY REFUELING)
13,906LB
MAX FUEL IMBALANCE FOR T/O
800 LB
MIN FUEL FOR GO-AROUND PER WING
459 LB
MIN BULK FUEL TEMP FOR T/O
-30C
MIN BULK FUEL TEMP IN FLIGHT
-40C
MIN REDUCED THRUST 3A1
85%
MIN REDUCED THRUST 3B1
83.5%
ENG START ON GND 1
60 SECONDS ON 10 SECONDS OFF
ENG START ON GND 2
60 SECONDS ON 10 SECONDS OFF
ENG START ON GND 3
60 SECONDS ON 5 MINUTES OFF
ENG START ON GND 4
60 SECONDS ON 5 MINUTES OFF
WHEN BOTH ENGINES ARE TO BE STARTED USING THE APU THE OPERATING ENGINE MUST NOT EXCEED
70% N2
DRY MOTORING 1
90 SECONDS ON 5 MINUTES OFF
DRY MOTORING 2
30 SECONDS ON 5 MINUTES OFF
MAX WINDMILLING/STARTER ASSISTED CROSS BLEED RELIGHT ALT
FL210
DO NOT EXCEED 75% N1 UNTIL:
2 MINUTES OR ALL OPERATING INDICATIONS ARE IN THE GREEN BAND, WHICHEVER IS LONGER.
MAX GROUND IDLE SPLIT N2
LESS THAN OR EQUAL TO 2%
WITH OAT -20C THRST LEVERS AT IDLE N2
GREATER THAN 57%
IF N2 IS NOT GREATER THAN 57% AT IDLE WITH -20C
DO NOT ADVANCE THRUST LEVER, CONTACT MX
ENGINE COOL DOWN
2 MINUTES AT IDLE/NEAR IDLE THRUST
THRUST REVERSER USE DURING TAXI
PROHIBITED
OIL PRESSURE: STEADY STATE IDLE
25 psi minimum
SINGLE PACK OPS
FL250
CPAM PAX O2
14,000’ +/- 500’
BEFORE THE FIRST FLIGHT OF THE DAY WHEN THE AIRPLANE IS COLD SOAKED THE ENGINES MUST BE
MOTORED FOR 60 SECONDS AND FAN ROTATION VERIFIED BEFORE ENGINE START IS INITIATED
AFTER BEING COLD SOAKED THE THRUST REVERSERS MUST BE ACTUATED UNTIL:
THE DEPLOY AND STOW CYCLES ARE LESS THAN 5 SECONDS
HOT START, INTERRUPTED START N2 STAGNATION “QRC MEMORY ITEM”
AFFECTED THRUST LEVER……SHUTOFF
IGNITION….OFF
DRY MOTOR…..UNTIL ITT REDUCED BELOW 12O DEGREES, RESPECTING THE STARTER TIME LIMIT
AFFECTED ENGINE…STOP
NO LIGHT OFF “QRC MEMORY ITEM”
AFFECTED THRUST LEVER…SHUTOFF
IGNITION…OFF
DRY MOTOR…UNTIL STARTER LIMIT
AFFECTED ENGINE…STOP
At what crosswind component is continuous ignition required for takeoff
Greater than 10 kts
When is reduced thrust prohibited?
- Wings/Cowls anti-icing bleeds are in use
- Contaminated RWY
- Warnings of windshear or downdrafts are forecast
For an unpressurized landing, the pressurization is set to what altitude before takeoff?
3000’ above field elevation
What conditions/indications would direct a decision to abort the takeoff?
- Engine Failures
- Fire
- Loss of Directional Control
- Windshear
- Unable to Fly
The autopilot must be engaged above
RVSM Airspace - FL290
The autopilot can be engaged at
600’
What is the climb speed schedule below 10,000
250
What is the climb speed schedule above 10,000
290/.74
What bank deviation requires a PM call out
In excess of 30 Degrees
What Speed deviation requires a PM call out
+10/-5 KIAS or .02M
What heading from bugged or course deflection require PM call out
+/- 10 degrees
Course from established 1/4 deflection
What are the PM callouts
SPEED BANK HEADING COURSE PITCH VERTICAL SPEED
On the Speed Cards VMD speed line, what do the dashed lines indicate?
Does not provide adequate bank protection for turns in excess of 15 degrees. Bank angles in excess of 15 degrees and holding are prohibited at these altitudes and weights
Double Engine Failure Memory Item
IGNITION CONTINOUS
NO LESS THAN 240KIAS
When should you arrive at traffic pattern altitude and flap 0 maneuving speed?
12 miles out straight-in approach, or
8 miles out abeam approach
For VMC circle-to-land the aircraft must be aligned with the runway by?
500ft HAT
Arming the APPR too early may result in a?
False localizer capture
What are the STABILIZER TRIM RUNAWAY memory items?
- Control Wheel…….Assume Manual Control and Override runaway
- Both Stab Trim Disc…..Press,Hold,and Release
- Airplane Control…….Transfer to Pilot (LH) side
- Circuit Breakers (2F5 and 4A1)…..OPEN
Maximum rate of descent for an overweight landing
360fpm
What are the EXCESSIVE ASYMMETRY OR LOSS OF BRAKING memory items?
- Wheel Brakes……..Release Momentarily
- Anti-Skid……….OFF
- Wheel Brakes……Re-Apply, as required
What is the allowance for delamination along the edge of the windshield or window
2 inches from the edge of the window around the entire periphery
What is the allowance for delamination along the corner of the windshield or window
4 inches of penetration is allowable in the corners
When is a cold weather preflight required
- OAT Less than 5
- Wing Fuel Temp is 0 or less
- Atmospheric conditions have been conducive to frost formation
What is a Holdover Time (HOT)
Is an estimate of the time the deicing/anti-icing fluid is effective in preventing the formation of frost, ice, or the accumulation of snow on a treated surface.
What is the clean wing concept
Aircraft must not take off when frost, ice, or snow is adhering to the wings, control surfaces, engine inlets, and other critical surfaces of the aircraft.
What Altitude does RVSM start?
FL290
MIN FUEL
1,550 lb
EMER FUEL
1,050 lb
Max X-Wind TO/LND CRJ 200
27 Kts
Max X-Wind TO/LND RCC 1 or 2
> 1/8” Standing Water
> 1/8” Slush
Ice
10 Kts
TO/LND Wet Ice Slush Over Ice Water over Compact snow Dry Snow over ice Wet snow over ice
Prohibited
Max Number of PAX on Door
4 PAX or 1,000 pounds
Flaps AD for Landing
Flaps should not be extended out of 0° unless:
* Prec. app vis. is above the vis. associated with the landing min and expected to remain so.
* Non. prec. same as prec. app but ceilings must also remain above requirments
* An emergency requires landing at nearest airport
* Fuel remaining is sufficient to conduct app, go missed, divert with flaps extended in landing config., conduct app, and land with 1,000lbs of fuel remianing.
Min. Oil Pressure Idle
Min. 25psi
Min. Oil Pressure for Takeoff
Min. 45psi
Max Oil Continious Temp.
+155° C
Max. Oil Permissable Temp.
+163° C
APU Max EGT
743° C
Never Go Below What Mach Speed in a Climb
.70M
Holding Speeds
200 KIAS = Below 6001’
230 KIAS = 6001 - 14,000’
265 KIAS = Above 14,000’
RVSM Required Equipment
- Two independent altitude measuring systems
- An altitude alerting system
- An automatic altitude control system
- A seconday survellance radar transponder with altitude reporting system that can be connected to the altitude measuring system in use for altitude keeping
Max Rotation Rate
3° per second
Kinds of Operations
IFR, VFR, Known Icing
MIN OIL PRESSURE: TAKEOFF THRUST
45 psi minimum
OIL PRESSURE: MAXIMUM CONTINUOUS
115 psi maximum
OIL PRESSURE: MAXIMUM TRANSIENT AFTER COLD START
156 psi maximum
(130 psi at idle. 10 min max)
COWL A/I MUST BE ON? (GROUND)
OAT 10° C or below AND =
* Visible moisture is present
* When operating on any contaminated runway
* Anytime the wing A/I system is on
WITH COWL A/I ON, CAUTION MESSAGE SHOULD DISAPPEAR BY
78% N2 or must call maintenance
COWL A/I MUST BE ON? (FLIGHT)
- In icing conditions
- When “ICE” is annunciated by the ice detection system
WING A/I ON WHEN (GROUND)
- During final taxi prior to takeoff if the OAT is 5° C or less (Unless type II, III, or IV have been applied)
- On for Takeoff when OAT is 5° C or less and
- Visible moisture in any form below 400’ AGL
- contaminated runway
- Presence of any precipitation
WING A/I ON WHEN (FLIGHT)
- “ICE” is annuciated by the ice detection system
- In icing conditions and airspeed less than 230 KIAS
WHEN DO YOU TURN ON WING A/I IF TYPE II, III, OR IV HAVE BEEN APPLIED
JUST BEFORE TAKEOFF THRUST IS APPLIED
CRITICAL AIRCRAFT SURFACES
- Wings
- Upper fuselage
- Horizontal stabilizers
- Vertical stabilizers
- Control surfaces
- Engine inlets
MAX RUNWAY SLOPE FOR T/O
- 2% uphill
- -2% downhill
MINIMUM FLIGHT CREW
One pilot and one copilot
MAXIMUM CABIN DIFFERENTIAL PRESSURE
8.7 psi
MAX NEGATIVE PRESSURE DIFFERNTIAL
-0.5 psi
MAX DIFFERENTIAL PRESSURE DURING GROUND MANEUVERING
0.1 psi
MAX DIFFERENTIAL PRESSURE AT TOUCHDOWN
1.0 psi
MIN ALT FOR AUTOPILOT ENGAGEMENT ON NON-PREC APP
400’ AGL but no lower than 50’ below the DDA, whichever is higher
MIN ALT FOR AUTOPILOT ENGAGEMENT ON PREC APP
50’ below the DA or 80’, whichever is higher
CIRCUT BREAKER RESET LIMITATION
Unless in the AFM, no reset unless safety of flight
TAXI LIGHT USE LIMIT
Must be off if aircraft is stationary for more than 10 min
COLD SOAKED AIRCRAFT DEFINITION
Ambient temperature of -30° C or less for more than 8 hours
MIN FUEL TEMP FOR TAKEOFF
5° C
MAX OIL CONSUPTION PER HOUR
6.4 ounces per hour (0.05 gallons / 0.2 qts)
MAX HOURS WITHOUT OIL SERVICING
16 Hours
MAX OIL REFILL ALLOWED
2 qts without dry motoring
MAX TURBULENT PENETRATION SPEED
280 kias / 0.75M
MAX LOAD FACTOR
- Flaps up: -1.0G to 2.5G
- Flaps down: 0.0G to 2.0G
VFO 30
185kts
VFO 45
170kts
