9E CRJ- 200 limitations

53,250


CFM 3-14

• 53,000
• May be further limited due to performance considerations.

CFM 3-14

• 47,000
• May be further limited due to performance considerations.

CFM 3-14

44,000


CFM 3-14

30,000


CFM 3-14

Both 200 knots

This limitation complies with AD 2009-06-12

CFM 3-22

185 knots

This limitation complies with AD 2009-06-12

CFM 3-22

170 knots

This limitation complies with AD 2009-06-12

CFM 3-22

230 knots

This limitation complies with AD 2006-12-21

CFM 3-22

185 knots

This limitation complies with AD 2006-12-21

CFM 3-22

170 knots

This limitation complies with AD 2006-12-21

CFM 3-22

Must be switched off whenever the aircraft is stationary in excess of 10 minutes


CFM 3-48

• 1. T/O & landing on contaminated runway
• 2. T/O X-wind in excess of 10 knots
• 3. Flight thru mod/heavy rain
• 4. Flight thru mod/heavy turbulence
• 5. flight in vicinity of thunderstorms
• 6. Flight at/near shaker/pusher settings is predicated on an operable auto-ignition system
• CFM 3-31

• ITT must be 120 C or less for grnd start
• ITT must be 90 C or less for air start

CFM 3-32

Carry out an engine motoring cycle immediately to reduce ITT.

CFM 3-31

• 800 LBS
• fuel reamaning in tanks when indicating 0, is unusable

CFM3-34

TO with a fuel load in excess of 500 lbs. in center tank is not permitted unless each wing tank is above 4,400 lbs.

CFM 3-34

• 450 lbs. per wing with airplane level.
• This assumes a maximum airplane climb attitude of 10° nose up.

CFM 3-35

• Use of DES submode (FD or AP coupled) during approach is not permitted.
• AP prohibited below 600 ft. AGL. except:
• visual and/or non precision  then 400 ft. agl
• Precision approaches 80ft. agl.
• ADC source coupled to the active AP must be the same as that coupled to the ATC transponder during flight in RVSM airspace.
• CFM 3-48

• start                               time                      followed by
• 1                                      1 min                     10 sec off
• 2                                      1 min                     10 sec off
• 3 & more                          1 min                      5 min off
• CFM 3-32

• Attempt                     time                   followed
• 1                                  90 sec                  5 min off
• 2                                  30 sec                  5 min off
•                     Thrust levers at shutoff may be
•                            used on grnd & air
• CFM 3-32

The dry motoring cycle (with thrust levers at shut off) may be used for engine grnd starts and engine airstarts. comply with dry motoring cycle limits

CFM 3-32

• T.O. with EICAS messages/or lights prohibited
•     1. Thrust reverser UNLK light
•     2. REV icon N1 gauge
•     3. L or R rev unlocked caution message (unless MEL)
• Reduced to idle below 60 knots. (idle not above 30% N1
• Grnd use only full stop landings. Do not attempt a GA after deployment. For preflight check TR limited to idle.
• CFM 3-47

@ 10,000 ft. or SAT less then 0 C. Ailerons must be manually operated every 5,000 ft. until TOC.

• Must not extend below 1000 ft. agl. Must not extened at speed below approach or maneuvering speeds +17 knots. For turns upto 40 degrees + 10 added to above. VA or VMM +17+10
• Spoilers prohibited with flaps greater then 30 degrees.

Flaps not extended beyond 0 degrees unless: Percission approach VIS or RVR is at or above mins. & forecast in main body of TAF after landing to remain. Nonpercision, both VIS & RVR

En-route use of flaps prohibited. Prohibited above 15,000 ft.

• Observe limits between landing or rejected T.O. & subsequent takeoff to comply with cooling limits in Ch. 8 CFM
•               P. 8-83 performance.

With APU door open EICAS message door_ _ _ . Then speed less then equal to 300 knots OR APU must remain in operation.

Fog with less then equal to 1 mile vis. Or clouds, rain, snow, sleet, ice crystals.

• START             MAX ON            FOLLOWED BY
• 1                      15 sec                   2 min off
• 2                      15 sec                   20 min off
• 3                      15 sec                   2 min off
• 4                      15 sec                   40 min off

• START               MAX ON         FOLLOWED BY
• 1                        30 sec            2 min off
• 2                        30 sec            20 min off
• 3                        30 sec            2 min off
• 4                        30 sec            40 min off

-40 c.

• 1. If T.O. N1 speed less than 85%
• 2. With an engine that cannot achieve full rated
•     thrust
• 3. If wing and/or cowl ice in use
• 4. Windshear downdrafts
• 5. Contaminated runway
• 6. Dept. procedure requires full thrust
• 7. Anti-skid inop
•     May be used on wet runway with wet data

• Engine must be running at least 2 min. prior to T.O. & idle for same before shut-down.
•      N2 equal to less then 80%

If N2 rpm exceeds 55%, do not use starter

• 1. N2 22% to 25% rpm
• 2. ITT 450 c to 600 c
• 3. N2 56.5% to 68% rpm (N2 ^{match within 2%})
• 4. Fuel flow approx. 350 PPH
• 5. Oil pressure greater then 25 PSI

• 1. Motor engines for 60 sec. Verify fan rotation
• 2. Deploy & stow reverse thruster until cycle
•     less then 5 sec.

• Connected to co-pilot (R) aileron & left elevator only.
•    Aileron trim is electronically operated

Power from pump 3B which is powered by the ADG

• Wing & cowl anti-ice.
• Thrust reversers
• Wing isol valve for X-bleeding

• Enviro air, pressurization
• Engine starting,may be cross-bleed through ISOL valve
• May be supplied from engine, APU, external air.

• When the SIC has less then 100 hrs. and
• 1. Vis at/below 3/4 mile or RVR at/below 4000
• 2. Contaminated or wet runway
• 3. Breaking action less then good
• 4. X-wind greater then 15 knots
• 5. Windshear
• 6. LASHO ops, or any other time PIC deems so.

• 1. Affected thrust lever.......Shutoff
• 2. Ignition.........................Off
•    Dry motor until ITT less then 120 c. or starter time limit of 60 sec. then Stop button

• 1. Affected eng stop light...........Push
• 2. Engine & bleed air source.......Shutdown
•    If starter remains engaged..10^th stage bleed air source.....shutdown

• Red....Max/Min limits
• Amber...Caution range
• Green...Normal range

• 1. L & R bleed air SOV's open (if closed)
• 2. Isol valve opens
• 3. Start valve on assoc. engine opens
• 4. Igniter energized
• 5. Ignition lgt. illuminated
• 6. Manually add fuel @ 20% N2
• 7. @55% starter cut-off--start lgt extinguishes
• 8. Start valve closes
• 9. Igniter de-energized

Powered & gravity cross-flow must be off for T.O.

• D.I.G.S.         & ECU powered
• D..door open message (inlet door)
• I..in bite test runs
• G..gauges for APU appear
• S.. sov fuel feed opens

Speed reduction below stick shaker operation is prohibited unless authorized for testing/training

-30 c

• Above FL 310. use long range cruise speed (LRC).
• At/below FL 310. 2 engine holding speed Vmo. reference buffet margin. Hold 8-110 LRC P. 8-104 to 8-106 performance

• Above 10,000 ft. not less then 250 knots/ .70 mach unless...
• 1.Mountainous terrain in dept. path then VX or Vref flaps +10 k. until clear.
• 2. Asked by ATC, climb at VY except in icing above 15,000 ft.
• 3. Restricted by MEL but not slower the VX.
• If unable to maintain 300 fpm climb at 250/.7 mach, then stop climb

OAT is 10c or less & visible moisture in any form present. And/or on contaminated or standing water on taxi or runways.

• Icing cond. on ground & OAT is 5c or less and visible moisture in any form below 400 agl. Runway wet or contaminated. Or any precip.
• If wing ice on for T.O. then cowl ice must be on also.
•  Must be on during final taxi before T.O. if OAT less then /equal 5c. unless type II, III, IV fluids used.
•  Must be turned on after both engines running & no later then the BTO check.
• 1. During taxi L/R wing A/ice caution may be posted but must be out & wing A/ice on posted prior to T.O.. If not required for T.O. turn off
• 2. After type II, III, IV fluids wing A/ice only on just prior to T.O. only if needed.
•   Can't use indicated SAT or TAT on ground.

• When TAT 10c or less in visible moisture below speed of 230 K. or if ICE is annunciation by the detection system.
• Warning: delaying wing anti-ice can change stall speed, margin characteristics

In visible moisture at TAT of 10 c or less except when SAT is -40c or below in icing cond. And/or enunciated by ice detection system