Limitations & Emergency Procedures Flashcards
CR2 memory items for Double Engine failure
Ignition, CONT - ON
Airspeed - Not less than 240 kts
When should you use continuous ignition?
TO & LNDs on contaminated runway Crosswind >10kts CRJ200 Mod or greater Turbulence Mod or greater Rain Vicinity of thunderstorm
With OAT <=-20C, thrust lever at idle N2 should be _______
> 57%
If N2 is <=57% with OAT -20C or greater do not advance thrust lever above idle Contact Maintenance
Spoiler usage with _______ are __________ .
Flaps 45
Prohibited
CR7/9 memory items for Double Engine Failure?
Igntion, CONT - ON
If engines continue to run-down (N2<40%)
Thrust Levers (Both) - SHUT OFF
ADG Manual Deploy Handle - PULL
When ADG power is established:
Stab Trim, CH2 - CONFIRM ENGAGED
Target airspeed - Establish
Above F340 - 0.7 MACH
Below F340 - 240 kts
Maintain airspeed until ready to restart engines
CR7 Vfe 45
170
CR2 Engine start times
60 seconds ON / 10 seconds OFF
60 seconds ON / 10 seconds OFF
60 seconds ON / 5 minutes OFF
60 seconds ON / 5 minutes OFF
CR7 Max ramp weight
75,250
CR7/9 Max continuous DC TRU
120 A
CR2 Mmo
0.85
Ground Idle N2 split
2%
CR9 Vmo
335
CR2 APU Max Ops Alt
37,000ft
CR9 APU Max Alt Eng Start
21,000ft
CR7 Pressure refueling / gravity
19,594 / 14,580
CR9 Vlo RET
200
CR2 Max landing weight
47,000
CR7 Max door open with APU not operating
220 kts
What altitude the AFCS must be turn on by?
F200
CR9 Max Operating Altitude
37,000 ft (Skywest limit)
CR9 Mb
0.75
CR9 Vwiper ops max
250
CR9 Max zero fuel weight
70,750
CR2 Min fuel for GA per wing
450lb
Assumes max pitch up of 10 degrees
CR2 Vmo
335
When should taxi lights must be switched OFF when in a stationary period?
10 minutes
What is consider a contaminated runway?
More than 25% of runway has 1/8 inch of standing water, slush, wet or dry snow or slush
CR2 memory items for stabilizer trim runaway?
Control Wheel - Assume manual control and override runaway
Both Stab Trim Disc - Press, Hold, and Release
Airplane control - Transfer to Pilot (LH) side
Stab CH 1 and CH 2 HSTCU
Circuit breakers (2F5 and 4A1) - OPEN
CR7 APU Max Start Alt
37,000ft
CR7 APU Max Alt Eng Start
21,000ft
Crosswind Limitation. Takeoff or landing with wet ice, slush over ice, water over compacted snow, dry snow over ice, wet snow over ice
Prohibited
What is the min spoilers altitude?
1,000 ft HAT (SW)
CR2 Cargo FIREX time to suitable airport
45 min
CR7 Mb
0.75
CR2 Vadg deploy Max
250 (Wet)
Vmo/Mmo (Dry)
CR9 Vfe 45
170
Max Ground Ops with DC only
5 minutes
What it’s the CRJ200 memory items for No Light OFF?
Affected Thrust Lever - Shutoff
Ignition - OFF
Dry Motor - Until starter time limit
Affected Engine - STOP
CR2 Vfe 20
215
CR7/9 APU generator
To FL410
40kVA
CR2 Max door open with APU not operating
300 kts
CR2 Vfe 8
215
CR7/9 Max fuel imbalance for T/O
300lb
CR2 AFCS min altitude use TO / Non-precision / Precision
TO - 600ft
NP - 400ft
P - 80ft
CR7/9 memory items for stabilizer trim runaway?
Control Wheel - Assume manual control and override runaway
Stab trim disc - Select
CR7 Max zero fuel weight
62,300
CPAM PAX O2
14,000 +/-500ft
IAS Mode is _______ during approach
Prohibited
CR2 Maximum runway contaminant depth
Takeoff / Landing Standing water 0.5 / 0.75 Slush 0.50 / 0.88 Wet snow 1.00 / 1.50 Dry snow 3.00 / 3.75
CR2 APU Max Alt Eng Start
13,000ft
Crosswind limitation CRJ700 Takeoff
28kt(SW)
DES Mode F/D or A/P coupled is ________
During approach
Prohibited
CR2 Max T/O and Landing Altitude
10,000ft (Skywest limit)
Crosswind Limitation CRJ900 landing
32kts (SW)
CR2 Vwiper Ops Max
220
Until oil pressure reaches the green band. _______. Do not exceed 75% N1 until ______ or ________, whichever is longer.
Do not exceed idle
2 minutes OR
All Indications in the green
CR2 Max Temperature for T/O and Landing
ISA + 35C
CR2 Pressure refueling / gravity
14,518 / 13,906
CR2 APU Max Start Alt
30,000ft
CR7 Vadg deploy max
Vmo/Mmo
Crowing limitation. CRJ200 takeoff or landing
27kt (SW)
What is approached speed considered?
Approach speeds is current flaps
Maneuvering or straight-in
CR7 Vfe 30
185
EMERGENCY DEPRESS switch ______ is prohibited
Above 15,000ft
CR9 Vadg deploy max
Vmo/Mmo
CR2 Max fuel imbalance for T/O
800 lb
CR9 Vb
280
CR9 AFCS Min altitude use TO / Non-precision / Precision
TO - 600ft
NP - 400ft
P - Glide <=3.5 degrees - 80ft
P - Single engine - 110ft Airport Elevation >4,000ft Prohibited
Single engine Cat 2 - DH set to published DH or 110ft whichever is
Higher
CR9 Total pressure refueling / gravity
19,594 / 14,810
CR7/9 Operation in windy conditions.
> 30 either direction of nose & >30 knots wind speed
Apply Max of idle/taxi thrust before brakes released, then TOGA thrust. RLNG Takeoff procedure
CR2 Vfo 20
200
CR7/9 Limit climb to less than _______ above ______.
1,500 FPM
above F300
CR2 Vfe 45
170
CR7 Max T/O weight DL/AS
74,999
CR2 Max ramp weight
53,250
CR9 Vfe 8
230
When operating on runways contaminated with ice, dispatch with one thrust reverser is
Prohibited
CR2 Dry Motor limits
90 seconds ON - 5 minutes OFF
30 seconds ON - 5 minutes OFF
Powered cross flow and gravity cross flow must be _________ for takeoff
Off
CR7 Max Operating Altitude
37,000 ft (Skywest limit)
Max Flaps operating
15,000
CR2 Automatic performance reserve must be used when takeoff performance is predicated upon use of
APR
CR2 APU Starter Duty Cycle
Start 1 - 30 seconds - 2 minute delay
Start 2 - 30 seconds - 20 minutes off
Start 3 - 30 seconds - 2 minute delay
Start 4 - 30 seconds - 40 minutes off
CR2 Max zero fuel weight
44,000
CR2 Min spoiler speed
Appr speed + 20
CR7 Max Temperature for T/O and Landing
ISA + 35C
ISA + 40C (AE)
CR2 APU Max Alt Bleed Use
15,000ft
APPR mode is ______ for ______ approaches
Prohibited
VOR approaches
CR7 Vtire
182 (GS)
CR7/9 Min fuel for GA per wing
600 lb
CR9 APU Max Alt Bleed Use
25,000ft
CR7 Mmo
0.85 (0.83 RVSM)
CR7/9 Operation in windy conditions.
> 30 either direction of nose & 5 to 30 knots wind speed
Apply Max of 75% N1 before brakes released, then TOGA thrust
NML Takeoff procedure
During 2nd engine start with the APU the operating engine _____
<70%
Where can you find the maximum crosswind performance for takeoff, landing and contamination criteria? Is this data considered a pilot limitation?
See Company manuals > Weather section
Yes, All crosswind data provided is considered a pilot limitation
CR9 Vle
220
CR2 Min Temperature for T/O
-40C
CR7/9 Single Pack Ops Alt limit
F310
CR7 Vmo
335
CRJ200 Wing Span
69ft 8in
CR9 Mmo
0.84 (0.82 RVSM)
CR7/9 Cargo FIREX time to suitable airport
60 min
Min reduced thrust
3A1 - 85%
3B1 - 83.5%
CR7 Max landing weight
67,000
CR2 When fuel over than Jet A is to be used, consult ______ for limitations.
QRH Vol 1
What is the CRJ200 memory items for hot start, interrupted start, N2 stagnation?
Affected thrust lever - Shutoff
Ignition - OFF
Dry motor - Until ITT less than 120C respecting starter time limits
Affected Engine - STOP
CR9 Vfe 20
220 **
Oil pressure should be in the normal range after cold start within
10 minutes
CR7 Vfe 20
230
CR7/9 Engine start times
90 seconds ON / 10 seconds OFF 90 seconds ON / 10 seconds OFF 90 seconds ON / 5 minutes OFF 90 seconds ON / 5 minutes OFF 90 seconds ON / 5 minutes OFF
CR2 APU generator
To FL370
30kVA
CR9 Min spoiler speed
APPR speed + 10
Crosswind Limitation CRJ700 landing
30kts (SW)
CR9 APU Max Ops Alt
39,000ft (SW)
CRJ200 Aircraft Length
87ft 10in
CR9 APU Max Start Alt
37,000ft (SW)
CR9 Max T/O weight
84,500
CR2 Mb
0.75
CR2 Single pack Ops Alt limit
F250
CR2 Min flight weight
30,000
CR2/7/9 Max Tailwind for TO & LND
10 kts
CR9 Max door open with APU not operating
220 kts
CR9 Vfe 30
185
CR9 Max Temperature for T/O and Landing
ISA + 35C
CR7 Max T/O weight
75,000
CR2 Min reduced thrust for 3A1
85.0
CR7 Min spoiler speed
APPR speed + 10
CR7/9 Dry Motor limits
90 seconds ON / 5 minutes OFF 30 seconds ON / 5 minutes OFF 30 seconds ON / 5 minutes OFF 30 seconds ON / 5 minutes OFF 30 seconds ON / 5 minutes OFF
CR7 Vwiper Ops max
250
CR2 Max continuous DC TRU
100 A
CR2 Vfe 30
185
CRJ memory items for excessive asymmetry or loss of braking during landing?
Wheel brakes - Release Momentarily
Anti-skid - OFF
Wheel brakes - Re-apply, as required
CR7 Min flight weight
42,000
CR2 Vle
220
CR7 APU Max Ops Alt
39,000ft (SW)
CR2 APU Min start temperature
-40C
CR9 Min flight weight
45,000
CR2 Vlo RET
200
When must the APR system be selected off?
When APR caution message exists
When temp is -18C and below and pressure altitude less than 1,000 (3A1 engines only)
Min bulk fuel temp for T/O and in flight
T/O: -30C
In flight: -40C
CR2 Vtire
182 (GS)
CR7 Vfe 8
230
CR2 Vb
280
CR2 Vfo 8
200
CR7 Vlo RET
200
Enroute slats / flaps / spoilers are ____________ .
Prohibited
CR9 Max landing weight
75,100
Engine Cool down
2 minutes near idle thrust
CR9 Min Temperature for T/O
-40C
ADC source coupled to active autopilot must be ______ to the ATC transponders during flight in RVSM airspace.
The same as coupled
CR9 Vtire
195 (GS)
Operations are prohibited on routes with ozone concentrations exceed limits in
QRH vol 1
Crosswind Limitation. Takeoff or landing with RCC 1 or 2 or Poor BA with >1/8in standing water, slush, ice
10kt SW
Min runway width
100ft
CR7 APU Min start temp
-40C
CR7/9 Maximum runway contaminant depth
Takeoff / Landing Standing water 0.5 / 0.75 Slush 0.59 / 0.88 Wet snow 0.59 / 0.88 Dry snow 3.00 / 3.75
When operating on runways contaminated with ice, dispatch with one thrust reverser is ____________.
Prohibited
When is flex not allowed
W-Windshear warnings reported or forecasted W-Wing or Cowl A/I ON A-Anti-skid INOP T-Tailwind > 5 kts C-Contaminated Runway H-Heavy takeoff behind Flaps 8 TO CRJ200
CR9 APU Min start temp
-40C
CR7/9 Operation in windy conditions.
30 either direction from nose & No wind speed limit
OR
>30 either direction from nose & <5kts wind speed
No limitations
TOGA thrust may be applied before brakes released
CR7 Vlo EXT
220 (220)
CR9 Max T/O and Landing Altitude
9,600 (Skywest limit)
CR9 Max ramp weight
85,000
CR7 Vle
220
CRJ200 Tail height
20ft 8in
Crosswind limitations CRJ900 Takeoff
35kts (SW)
CR2 Max Operating Altitude
37,000 ft (Skywest limit)
CR2 Max windmilling starter assisted cross bleed relight altitude ?
F210
CR7 Vb
280
CR7 AFCS Min altitude use TO / Non-precision / Precision
TO - 600ft NP - 400ft P - Glide <=3.5 degrees - 80ft P - Glide >3.5 to <=4.0 - 120ft Airport Elevation >4000ft Prohibited P - Glide >4.0 - Prohibited
CR7 APU Max Alt Bleed Use
25,000ft
CR7 Max T/O and Landing Altitude
9,600 (Skywest limit)
CR2 Max T/O weight
53,000
CR9 Vlo EXT
220 (SW)
Takeoff with fuel > 500 in center tank is prohibited unless the main tank is above _______ or _________
4,400 OR
2,000 and allowable saw is reduced by weight of fuel in center tank in excess of AND
CG is within limits
CE7/9 APU Starter Duty Cycle
No more than three starts/start attempts in 1 hour
A two minute delay must be observed between cranking attempts
What is the CR7/9 memory items for Start abort message, Hot start?
Affected thrust lever - Shutoff
Dry Motor - Untill ITT deuces below 120C, respecting starter time limit
Affected Engine - Stop
CR7 Min Temperature for T/O
-40C
CR2 Min reduced thrust for 3B1
83.5
CR2 Vlo EXT
220 (SW)
