Limitations CRJ-550/700.

CRJ Max MMO/VMO

* .85 mach * 315 KIAS

Maximum APU EGT.

* 1038°C.

During landing, maximum reverse thrust is prohibited below _________ , and reverse idle should be achieved by __________?

* 75 KIAS. * 60 KIAS.

Continuous engine ignition must be used during the following

* T/O and LDG on contaminated runways * flight through moderate or heavier intensity rain * flight through moderate or heavier intensity turbulence * flight in the vicinity of thunderstorms

Maximum slope for Takeoff and Landing.

+ 2 % uphill - 2 % downhill

With engines running and bleeds configured for T/O, target N1 values must correspond to thrust setting charts _____

+ or - 1 %

Maximum negative differential pressure is

-0.5 PSI

Before the first flight of the day when the airplane has been cold-soaked at an ambient temperature of ______ or below for more than ____

-30°C for 8 hours. * Engine must be motored for 60 seconds and fan rotation verified before an engine start is initiated. * Thrust reversers must be actuated until deploy and stow cycles are 2 seconds or less.

T/O with bulk fuel temperature indications below ______ or _______ depending on fuel type is prohibited.

-30°C. -40°C.

Minimum ambient air temperature for T/O

-40°C

Maximum ambient temperature for starting a cold soaked APU on the ground is _____

-40°C.

Engine Operating Limit OIL TEMP @ Ground Start

-48°C minimum.

Maximum cruise Mach number for CRJ 550/700 in RVSM.

.83 Mach

Engine Operating Limit N2 @ Assisted Air Start

0 - 45%

Engine Operating Limit N2 @ Ground Start

0-45%

During taxi, T/O and LDG the maximum pressure differential is

0.1 PSI

Maximum tailwind component

10 knots

APR power 1 eng is limited to __________?

10 minutes for 1 engine APR power.

Taxi lights must be switched off whenever the airplane is stationary in excess of _____

10 minutes for taxi lights.

Engine Operating Limit ITT @ APR (max power)

1006°C (2min) 990°C (5min)

APU Maximum RPM

106 %

Maximum permissible continuous load on the TRUs is

120 amps

ITT must be below ______ before attempting to ground start engine

120°C.

Flight with Slats/Flaps extended at altitudes above ______ is prohibited

15,000 feet

The use of the EMERG DEPRESS switch above _______ is prohibited

15,000 feet

Engine Operating Limit OIL TEMP @ Max Continuous

155°C.

Maximum oil pressure is limited to _____ when oil temperature transient is less than _____

156 psi 60 C

Engine Operating Limit OIL TEMP @ Normal T/O

163°C (15min)

Engine Operating Limit OIL TEMP @ APR

163°C. (15min)

The CRJ 550/700 Maximum Tire Limit Speed is_________.

182 Knots ground speed

Engine Operating Limit OIL PRESS @ Assisted Air Start

182 psi / 95 psi (after 10min)

Engine Operating Limit OIL PRESS @ Windmill

182 psi / 95 psi (after 10min)

Engine Operating Limit OIL PRESS @ Ground Start

182 psi / 95psi (after 10min)

The APU must observe _____ cool down between start attempts

2 minutes for cool down.

Engine Operating Limit N1 @ IDLE

20-25%,

CRJ 550/700 All Engine Out Rapid Relight 10000-sea level FADEC rapid relight capability has been demonstrated at _______ for up to ______ fuel interruptions

200 KIAS 15 sec.

Engine Operating Limit OIL PRESS @ IDLE

25 - 60 psi / 25 - 95 psi ( oil temp <60.C)

APU bleed extraction is not permitted above ______

25,000 feet

Oil pressures above IDLE between _______ require oil temperature monitoring

25-45 PSI

Maximum airspeed for windshield wiper operation is ______

250 KIAS

CRJ 550/700 Engine Relight Windmilling 25,000 ft to sea level:

250 KIAS - VMO and 7.2 % N2 minimum

For ground operations, the left and right fuel tanks should Never have a difference greater than.?

2500 lbs.

Maximum airspeed for turbulence penetration is _____

280 KIAS or .75 mach whichever is lower.

The APU starter motor duty cycle is not limited to not more than _________

3 start attempts in 1 hour with 2 min cool down in between.

Maximum permissible fuel imbalance between the contents of the left/right wing tank: During T/O __________ All other phases of flight ________

300 LBS 800 LBS

Flight spoilers must not be extended in flight below an altitude of

300 feet AGL

The maximum altitude for single pack operation for the CRJ 550/700 is.

31,000 feet.

Maximum duration without engine oil servicing is ___ operation hours

36 hours

Airplane operations in excess of _____ operation hours the engine oil level must be checked within _______ after every engine shutdown

36 hours 3 min to 2 hours

APU may not be started above ________

37,000 feet

Minimum Operating Empty Weight for CRJ 700.

39,835 lbs

Engine Operating Limit OIL LEVEL for flight

40 % minimum with affected engine not started

Maximum generating loading

40 KVA

Maximum permissible load on the APU generator

40 KVA

APU generator may be use up to ________

41,000 feet

Maximum operating altitude

41,000 feet

Minimum Flight Weight for CRJ 700

42,000 lbs

Minimum Flight Weight for CRJ 550.

42,000 lbs.

The starter must not be used if indicated N2 RPM exceeds

45 % RPM

Engine Operating Limit OIL PRESS @ APR

45 - 95 psi

Engine Operating Limit OIL PRESS @ Normal T/O

45 - 95 psi

Engine Operating Limit OIL PRESS @ Max Continuous

45 - 95 psi

Normal T/O and maximum power 2 eng is limited to ________?

5 minutes for 2 engine at Maximum power.

The maximum permissible time for ground operations with DC power is__________ to protect the CRT displays.

5 minutes to protect CRT displays.

T/O with a fuel load in excess of _____ in the center tank is not permitted unless: * each main wink tank is above _____

500 lbs 4,400 lbs

Engine Operating Limit N2 @ IDLE

55 - 65%

Maximum Zero Fuel Weight for CRJ 550.

59,000 lbs.

T/O with engine fuel temperature indications below ______ is prohibited.

5°C.

Flights must be within ___ of a suitable airport if cargo is carried in either cargo compartment

60 minutes

Minimum fuel quanity for go-around is _____ per tank assuming a maximum climb attitude of ____

600 lbs 10 degrees nose up

Maximum Landing Weight for CRJ 550

61,000 lbs.

Maximum Zero Fuel Weight for CRJ 700

62,300 lbs

Maximum Takeoff Weight for CRJ 550.

65,000 lbs.

Maximum Taxi and Ramp Weight for CRJ 550.

66,000 lbs.

Maximum Landing Weight for CRJ 700

67,000 lbs

During all starts do not exceed ______ for ______ after start, or until all operating indications or in the normal range, whichever is longer

75 % N1 2 mins

Maximum Takeoff Weight for CRJ 700

75,000 lbs

Maximum Ramp Weight for CRJ 700

75,250 lbs

Maximum Airport Pressure Altitude for takeoff and Landing

8,000 feet

Maximum relief differential pressure is

8.7 PSI

Engine Operating Limit ITT @ Assisted Air Start

815°C.

Engine Operating Limit ITT @ Ground Start

815°C.

ITT must be below ______ before attempting to air start engine

90°C.

Engine Operating Limit ITT @ Windmill Start

927°C.

Oil Pressure may be greater than ____ for a maximum of ______

95 PSI 10 minutes

Engine Operating Limit ITT @ Max Continuous

960°C.

Engine Operating Limit ITT @ Normal T/O

964°C (2min) 948°C (5min)

Engine Operating Limit N2 @ Max Continuous

98.0%

Engine Operating Limit N2 @ Normal T/O

99.4%

Engine Operating Limit N2 @ APR (max power)

99.4%

Engine Operating Limit N1 @ APR (max power)

99.5%

Engine Operating Limit N1 @ Max Continuous

99.5%

Engine Operating Limit N1 @ Normal T/O

99.5%

The CRJ-700 Auxilary Power Unit

Allied Signal RE 220 RJ

What is the Maximum Crosswind component during Takeoff for the CRJ-550/700?

CRJ-550/700 max cross wind takeoff is 28 knots.

What is the Maximum demonstrated Crosswind during landing for the CRJ-550/700?

CRJ-550/700 the max crosswind is 30 knots.

Flying in supercooled large droplet icing

Continued operation in SLD icing conditions is prohibited. The wing and cowl icing systems must be on. Leave icing conditions imediately when side window icing occurs

For initial thrust lever movement from SHUT-OFF to IDLE for engine starts on the ground and in-flight. The ITT must be?

Engine Starts on the ground ITT must be less than 120°C. Engine Starts in-flight the ITT must be less than 90°C.

Maximum Landing Gear Operating Speeds

Extension 220 KIAS Down and Locked 220 KIAS Retraction 200 KIAS

Maximum Flap Extended Speeds for CRJ 550/700.

Flap Position VFE Flaps 1 - 230 KIAS Flaps 8 - 230 KIAS Flaps 20 - 230 KIAS Flaps 30 - 185 KIAS Flaps 45 - 170 KIAS

The Maximum G. Loading for the CRJ 550/700.

Flaps Retracted -1.0 to 2.5 G Flaps Extended 0.0 to 2.0 G

In cold weather operations, Take off is Prohibited when?

Frost , Ice, Snow, or Slush is adhering to any of the Critical areas. ( Wings, Upper Fuselage, Horizontal Stabilizer, Vertical Stabilizer, Control Surfaces, and Engine Inlets).

The CRJ-550/700 uses two ____________ engines

GE CF34-8C5B1

APU Indications Green

Green APU EGT - 0 to 806 C APU RPM - 0 to 106%

Maximum ambient air temperature for T/O or LDG

ISA +35 C

Engine must remain at ______ until oil pressure reaches ___________

Idle. normal operating range.

The CRJ-550/700 Fuel Tank quantities for Gravity Fueling.

Left & Right Wing- Gravity 7,290 lbs. Total - Gravity 14,580 lbs.

The CRJ 550/700 Fuel Tank quantities for Pressure Fueling.

Left & Right Wing- Pressure 7,492 lbs. Center Tank - Pressure 4,610 lbs. Total - Pressure 19,594 lbs.

Engine Operation Limits Due to Wind Direction Within 30 degrees on either directon of airplane nose or >30 degrees in either direction of the airplane nose; >5 knots windspeed

No limitation -TOGA thrust may be applied before brake release, but must be set by 60 KIAS.

Powered crossflow and gravity crossflow must be ____ for Takeoff.

OFF

Both stall protection system switches must remain ____ for _________

On. all phases of flight.

Enroute use of Slats/Flaps is?

Prohibited enroute.

Thrust reversers are approved for ground use only, activation of the thrust reversers in flight is?

Prohibited in-flight.

Backing up with thrust reversers is

Prohibited to back up with thrust reverser's.

Takeoff with any thrust reverser icons or EICAS warning and/or caution messages displayed is _________?

Prohibited with messages displayed.

The use of the Engine High-Power Schedule Switchlight is ___________?

Prohibited.

APU Indications Red

RED APU EGT 807 C APU RPM 107%

Engine Start or Motoring in Flight

START MAXIMUM TIME ON FOLLOWED BY Start 1 / 120 sec / 10 secs cool down Starts 2-5 / 60 sec / 5 min cool down

Engine Motoring on the Ground

START MAXIMUM TIME ON FOLLOWED BY Start1 / 90 sec / 5 min cool down Starts2-5 / 30 sec / 5 min cool down

Engine Start on the Ground

START MAXIMUM TIME ON FOLLOWED BY Starts 1&2 / 90 secs / 10 sec cool down Starts 3-5 / 90 secs / 5 min cool down

CRJ 550/700 Engine Relight Starter Assisted. 21,000 to sea level:

Speed VREF - VMO and 0% to 45% N2.

Minimum height use of the autopilot for the CRJ 550/700.

Takeoff - 600 feet AGL NonPrecision Approach - 400 feet AGL Precision apporach - 80 feet AGL with Glide slope <3.5 Or 120 feet AGL with Glide slope >3.5 to 4.0.

Do not attempt a go-around after deployment of the_________?

Thrust reversers

The maximum speed for ADG operations is _____

VMO/MMO

Cowl anti-ice system must be on, in flight when the TAT.

is 10°C or below, except when the SAT is -40°C or below: * in icing conditions * Ice is annunciated by the ice detection system.

Wing anti-ice sytem must be on, in flight when TAT.

is 10°C or below, except when the SAT is -40°C or below: * in icing conditions below 230 KIAS * ice is annunciated by the ice detection system. NOTE: * Do not hold in icing conditions with Slats/Flaps extended.

Cowl anti-ice system must be on, on the ground when the OAT

is 10°C or below: * when visible moisture is present * operating on contaminated taxiways and runways

Wing anti-ice system must be on, on the ground when OAT.

is 5°C or below: * when visible moisture is present * operating on contaminated runways When TYPE II or IV anti-icing fluids have been applied *wing anti-ice turned on just prior to T/O

With the thrust levers set for T/O target and actual N1 values should ________

match

To ensure adequate maneuver margins, flight spoilers must not be extended in-flight airspeeds below the recommended approach speed _____

plus 10 Knots

Oil Pressures should show a ______ value during start and may peak beyond _____ and are displayed as ______

positive 182 PSI amber dashes

The Maximum Weight capacity for the CRJ 550/700 cargo bins are?

~ Forward cargo is 1,000 lbs. ~ Aft cargo is 3,740 lbs.

T/O is permitted with frost adhering to:

•The upper surface of the fuselage if it is possible to distinguish surface features. •Maximum 1/8 inch layer of frost on underside of wing that is caused by cold soaked fuel.

The use of Reduced/Flex thrust for takeoff is NOT authorized when:

•Wing and cowl anti-ice bleeds are in use. •Warnings or forecasts of wind shear or downdrafts exist. Including LLWAS. •Runway is contaminated with standing water, slush, snow or ice. •Antiskid system is inoperative. •The engine cannot achieve full rated thrust.

Engine Operation Limits Due to Wind Direction >30 degrees in either direction of the airplane nose; >30 knots windspeed

Apply maximum of idle/taxi thrust before brakes released, then TOGA thrust by 60 KIAS.

Engine Operation Limits Due to Wind Direction >30 degrees in either direction of the airplane nose; between 5 and 30 knots windspeed

Apply up to a maximum of 75% N1 before brakes released, then TOGA thrust by 60 KIAS.

RVSM Required Equipment List

Autopilot Must be operational Altitude Alerting System Must be operational Altitude Reporting Transponder(2) One must be operational Air Data Computer(2) Two must be operational