CRJ Limitations 700/900 Flashcards
Max Ramp Wt. ________lbs.(CRJ700)
75,250
Max Ramp Wt. ________lbs.(CRJ900)
85,000
Max T/O Wt. ________lbs.(CRJ700)
75,000
Min. Flight Wt. _______lbs.(CRJ900)
45,000
Wing span(CRJ900)
81ft 4in
Max T/O & Lnd Altitude_______ft.
9,600
Crosswind Limitation: Landing(CRJ900)
32 kt (SW)
MB______M
0.75
WET SNOW Takeoff/Landing
0.59 in./0.88 in.
APU Max Alt Bleed use_______ft.
25,000
Min Bulk Fuel Temp for T/O______°C
-30
Max OIL PRESSURE after cold start:_______
Engine must remain at idle until oil psi returns to normal range. Must be in normal range within 10 min.
Max T/O Wt. ________lbs.(CRJ900)
84,500
Max Lnd Wt.______lbs.(CRJ700)
67,000
Max Lnd Wt.______lbs.(CRJ900)
75,100
Max Zero Fuel Wt. _______lbs.(CRJ700)
62,300
Max Zero Fuel Wt. _______lbs.(CRJ900)
70,750
Min. Flight Wt. _______lbs.(CRJ700)
42,000
Wing Span(CRJ700)
76ft 3in
Aircraft Length(CRJ700)
106ft 8in
Aircraft Length(CRJ900)
119ft 4in
Tail Height(CRJ700)
24ft 10in
Tail Height(CRJ900)
24ft 7in
Max Ops Alt_______ft.
37,000(SW)
Max Temp T/O & Lnd_______°C
ISA+35
AE Max Temp T/O & Lnd_______°C
ISA+40
Min Temp T/O_______°C
-40
Max Tailwind T/O & Lnd____kts.
10
Crosswind Limitation: Takeoff(CRJ700)
28 kt (SW)
Crosswind Limitation: Takeoff(CRJ900)
35 kt (SW)
Crosswind Limitation: Landing(CRJ 700)
30 kt (SW)
Crosswind Limitation: Takeoff or Landing with RCC 1 or 2 or Poor BA, >1/8” Standing Water, > 1/8” Slush, Ice
10kt (SW)
Crosswind Limitation: Takeoff or Landing with Wet ice, Slush over Ice, Water over Compact Snow, Dry Snow over Ice, Wet Snow over Ice
Prohibited
Prohibited
VMO_____KIAS
335
MMO______M(CRJ700)
0.85 (0.83 RVSM)
MMO______M(CRJ900)
0.84 (0.82 RVSM)
VLO EXT______KIAS
220
VLO RET______KIAS
200
VLE_____KIAS
220
VTire______kts. (CRJ 700)
182 (GS)
VTire______kts. (CRJ 900)
195 (GS)
V ADG DEPLOY MAX
VMO/MMO
VB______KIAS
280
V WIPER OPS Max______KIAS
250
Flap 1____KIAS
230
VFE 8 ____KIAS
230
VFE 20 ____KIAS(CRJ700)
230
VFE20____KIAS(CRJ900)
220
VFE 30____KIAS
185
VFE 45____KIAS
170
Max Flaps Alt______ft.
15,000
Use of flaps is_______ for enroute ops.
prohibited
Min spoiler speed
Appr. speed + 10
(Appr. speed is current flaps maneuvering or straight-in speed)
Min Alt. Spoilers
1,000ft HAT
Spoilers use with flaps at____prohibited.
45°
Minimum Runway Width____ft.
100
Minimum Taxiway Width____ft.
35 (SW)
STANDING WATER Takeoff/Landing
0.50 in./0.75 in.
SLUSH Takeoff/Landing
0.59 in./ 0.88 in.
DRY SNOW Takeoff/Landing
3.00 in./3.75 in.
When operating on runways contaminated with ice, dispatch with one thrust reverser is_____.
prohibited
The taxi lights must be switched OFF whenever______.
the airplane is stationary in excess of
10 minutes
Ozone Concentration. Operations are prohibited on routes where ozone concentration exceed limits in ________________________.
Quick Reference Handbook (QRH) Volume 1
APU Min Temp Start______°C
-40
APU Max Ops Alt_______ft.
37,000 (SW)
APU Max Start Alt_______ft.
37,000
APU Max Alt Eng Start_______ft.
21,000
Max Door Open with APU not operating_____KIAS
220
APU Starter Duty Cycle
No more than three starts/start attempts in one hour. A two minute delay must be observed between cranking attempts.
Autopilot must be engaged above_______ unless otherwise permitted by the MEL.
FL200
IAS MODE is ______ during approach
prohibited
DES MODE (F/D or A/P coupled) is ______ during approach
prohibited
APPR MODE is _____ for ___ approaches
prohibited
VOR
ADC SOURCE coupled to active autopilot must be _______ to ATC transponder during flight in RVSM airspace.
the same as that coupled
Ground Ops DC ONLY
5 min
Max continuous DC TRU
120A
APU generator
to FL410-40kVA
CARGO FIREX-Flight time to suitable airport
60 min
Total - Pressure Refueling______lbs.
19,594
Total - Gravity Refueling_______lbs.(CRJ700)
14,580
Total - Gravity Refueling_______lbs.(CRJ900)
14,810
Max Imbalance for T/O____lbs.
300
Min for GA per wing______lbs. (CRJ700)
(700 Assumes a maximum airplane climb attitude of 10° nose up)
Min for GA per wing______lbs. (CRJ900)
(Assumes a maximum airplane climb attitude of 10° nose up) 750
Min Bulk Fuel Temp in flight______°C
-40
Takeoff with fuel in excess of ____ lbs. in the center tank is not permitted unless: Each main wing tank is above ______lb., or Each main wing tank is above ______lb., and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lb., and the allowable center of gravity (CG) in this configuration is verified to be within allowable CG envelope.
500
4,400
2,000
Powered crossflow and gravity crossflow must be ______ for takeoff.
off
Do not exercise the _______ _______ through the detent positions before _______ _______ with the battery master ON.
thrust levers, engine start
Max wind milling/starter-assisted cross-bleed relight altitude:______
FL210
Until oil pressure reaches green band:______
Do not exceed idle
Do not exceed 75% N1 until:______or_________
2 minutes, All operating indications in green band, whichever is longer
During 2nd engine APU bleed start:_____
Operating engine <70% N2
Engines must not be shutdown until:______
2 minutes at idle/near idle thrust. Note -Taxi time counts towards this limitation.
SkyWest prohibits the use of thrust reversers__________
during taxi operations
With the engines running and bleeds configured for takeoff, the crew must verify the target _____ values correspond with ACARS or TLR data _______. When the thrust levers are set for takeoff, target and N1 values must match.
N1
±1.0%
Single Pack Ops to FL______
310
CPAM Pax O2_______ft.
≥14,000
Use of the EMER DEPRESS switch above ______ft. is prohibited.
15,000
Limit climb to less than _____FPM above FL ____
1500
300
Memory Items
