Max 90deg crosswind for takeoff and landing

27 knots

Max 90deg crosswind for landing from cat 2 approach

15 knots

Max headwind for landing from cat 2 approach

16 knots

Max direct tailwind for takeoff and landing

10 knots

Max runway slope approved for takeoff and landing

-2% (downhill)/ +2% (uphill)

Max operating alt. 700 and 900

41,000

Max pressure alt takeoff and landing

8,000 feet

Max ambient temp for takeoff and landing

ISA +35C

Min ambient temp approved for takeoff

-40C

Maneuvering limit load factors
flaps retracted

-1 to +2.5 G

Maneuvering limit load factors
flaps extended

0 to +2.0 G

Max taxi and ramp weight
700

75,250 lbs

Max taxi and ramp weight
900

85,000 lbs

Max takeoff weight
700

75,000 lbs

Max takeoff weight
900

84,500 lbs

Max landing weight
700

67,000 lbs

Max landing weight
900

75,100 lbs

Max zero fuel weight
700

62,300 lbs

Max zero fuel weight
900

70,750 lbs

Vb

280 KIAS/.75M
whichever is lower

Max gear extension speed

220 KIAS

Max gear extended speed

220 KIAS

Max gear retraction speed

200 KIAS

Max airspeed for windshield wiper operation

250 KIAS

Max airspeed for windshield wiper operation
FAILED IN NON PARKED POS.
700 & 900

250 KIAS

Max cruise Mach
RVSM airspace

.82M

Tire limit ground speed
700

182 Knots

Tire limit ground speed
900

195 Knots

Vfe
Flap 1

230 KIAS

Vfe
Flaps 8

230

Vfe
Flaps 20

220 KIAS

Vfe
Flaps 30

185 KIAS

Vfe
Flaps 45

170 Kias

Vfe and Vfo speeds are equal
True or False

True

Define
Ground contamination

Runways, ramps or taxiways with
surface snow, ice, slush or standing water.

Define
visible moisture

1. visible moisture or precip in any form ie..(fog with visibility of 1mi or less, mist,rain, snow, sleet and ice Crystal's or clouds in flight.

A. If visible moisture is present below 400ft AGL with OAT 10c or below activate cowl anti-ice for takeoff

B. If OAT 5C or below activate both cowl and wing anti-icefor takeoff

Anti-Ice operation
TAXI

Condition:Ground contamination. or Vis. moisture
Temp.:          OAT 10C or below      
IAS:                        N/A
Anti-ice:         Cowl
                        

Anti-ice operation
in flight less than 230 KIAS

Condition:   Vis. moisture
Temp.:          From TAT 10C to SAT -39C    
IAS:      less than 230 KIAS
Anti-ice: WING AND COWL

Anti-ice operation
in flight greater or equal to 230KIAS

Condition:     Vis. moisture
Temp.:       From TAT 10C to SAT -39C
IAS:       Greater or equal to 230 KIAS
Anti-ice:    Cowl

Anti-ice operation
Ice annunciated inflight

Condition:  ON
Temp.:       N/A   
IAS:                        N/A
Anti-ice:  Wing and cowl

Anti-ice operation
Takeoff
OAT 10C or below

Condition:  Ground contamination. or Vis. moisture
Temp.:          OAT 10C or below      
IAS:                        N/A
Anti-ice:  Cowl

Anti-ice operation
Takeoff
OAT 5C or below

Condition:  Ground contamination. or Vis. moisture
Temp.:          OAT 5C or below      
IAS:                        N/A
Anti-ice:  Cowl and wing

Engine indication
RED

Maximum or minimum limitations

Engine indication
AMBER

Caution range

Engine indication
GREEN

Normal operating range

Operate engines at or near idle for how long prior to shutdown?

2 Minutes

During all starts, do not exceed __________%N1 for ____ minutes after start, or until all operating indications are in the normal range.

75% N1, 2 minutes whichever is longer

ITT must be below _____°C before attempting  to ground start engine.

120°C

ITT must be below ____°C before attempting to air start engine

90°C

Engine oil psi
Steady-state idle

25 psi min.

Engine oil psi
Takeoff power

45 psi min.

Continuous engine ignition must be used
during.

1. Takeoff and landing on contaminated runways
2. Takeoff with high crosswind components  (15Kts or greater)
3. Flight through moderate or heavier intensity rain.
4. Flight through moderate or heavier intensity turbulance.
5. Flight in the vicinity of thunderstorms.

Engine operating limits due to wind direction:
within 30° on either direction of the airplane nose
no wind speed limit
OR
>30° in either direction of the airplane nose
< 5 Kts windspeed

No limitation- TOGA thrust may be
applied before brakes released.

operating limits due to wind direction:
>30° on either direction of the airplane nose
between 5 and 30 Kts windspeed

Apply max of 75% N1 before brake release,
then TOGA thrust

operating limits due to wind direction:
>30° on either direction of the airplane nose
>30 Kts windspeed

Apply max of idle/taxi thrust before
brakes release, then TOGA thrust

Engine starter cranking limits
GROUND

1. 90 sec on 10 sec off
2. 90 sec on 10 sec off
3+. 90 sec on 5 min off

Engine starter cranking limits
FLIGHT

1. 2 Min on 10 sec off
2+. 1 Min on 5 Min off

Starter must not be engaged if indicated N2 RPM exceeds ____%
(inflight or on the ground)

45%

A dry motoring cycle (thrust levers at shutoff) may be used for
engine ground starts and engine air starts

1. 90 sec on 5 min off
2+. 30 sec on 5 min off

Oil pressure
Steady-state idle

25 psi Min.

Oil pressure
Takeoff power

45 psi Min.

Oil pressure
Max continuous

95 psi Max

Oil pressure
Max transient

156 psi when oil temp <60°C

Oil pressure
Max transient after cold start
(10 Min Max)

182 psi or amber dashes

After cold start, engine must remain at _____ until
oil psi returns to ______ range.

Idle, Normal

Max fuel imbalance
700
Takeoff
All other phases of flight

Takeoff -- 300 lbs.
All other phases of flight -- 800 lbs.

Powered crossflow and gravity crossflow must be ____ for takeoff

OFF

Takeoff with a fuel load in excess of ___ lbs. in the center tank is not permitted
unless each wing tank is above ______lbs.

500 lbs, 4400 lbs.

The APU starter duty cycle is limited to not more than ____ starts/star attempts in _______
with _____ min. delay between attempts.

3, 1hr., 2 min

Bleed air extraction from APU is NOT permitted above:

25,000 ft.

Each engine may be started using the APU as a bleed air source for:

Engine start during ground operations.

Apu door not closed or door position unknown
Airplane is limited to:

220 KIAS
Or APU must remain in operation

use of SPEED MODE (DES, IAS), flight director or autopilot coupled
is not permitted when

During approach

Use of VNAV, flight director or autopilot coupled
is not permitted when?

During climb
and
approachs only  permitted  when  using  LPV  or  LNAV/VNAV minimums.

Operation of the autopilot engagedis prohibited below 600 ft AGL
EXCEPT

1. For visual and non-precision approaches,  the min height for autopilot is 400 ft AGL.

2.For precision approaches  (PAR, ILS), min height for autopilot use is 80 ft AGL unless
A. the glide path angle is >3.5° and >,= to 4.0° and the airport elevation
is less than or equal to 4000 ft the min height for a/p is 120 ft AGL
B. ILS approaches with a glide path angle of greater than 4.0° is prohibited

3. (900) For precision  approaches (PAR, ILS) or approach procedures with vertical guidance,
the minimum height for autopilot use with 1 engine operating is 110 ft AGL

Cat 2 approaches ______ be flown with autopilot ________.

Must, engaged

The ___ source coupled to the active ___ must be the same as the coupled to the __ 
___________ during flight in RVSM

ADC, FCC, ATC transponder

In flight,______ to entering RVSM airspace all _____ ________ for operation in RVSM
airspace _______ be operational.

prior, required equipment, must.

Max cruise speed in RVSM

.82 Mach

RVSM required equipment

Autopilot with altitude hold
Altitude alerting system
Altitude reporting transponder (at least 1)
Air data computers (2 must be operational)

To protect flight compartment CRT displays, the Max permissible
time for ground operations with DC power only is ?

5 minutes

Enroute use of slats/flaps is _________!

prohibited

Maximum flap and or slats extended altitude is ?

15,000 ft.

Minimum altitude for flight spoiler deployment is ?

1000 ft. AGL

To ensure adequate maneuvering margins, flight spoiler must not be extended inflight
at airspeeds below the recommended __________

REF speed + 10 KIAS

During landing, Max reverse thrust is prohibited below ______, and reverse idle
should be achieved by _________.

75 KIAS, 60 KIAS

Taxi lights must be switched off

whenever the airplane is stationary in excess of 10 minutes.

Minimum brake cooling time is ______ , and all _____ ________ must
be _______ and are not increasing.

15 minutes, BTMS indicators, green.

IAI
BRAKING LOSS/ ASYMMETRY

IAI
CABIN ALT MSG
EMERGENCY DESCENT PROCEDURE

IAI
SMOKE/ FIRE/ FUMES

IAI
STAB TRIM RUNAWAY

The  AFCS  controls  and  supplies  information  to:

• Dual  independent  flight  directors
• Two axis  autopilot
• Automatic  pitch  trim
• Yaw  damping function

The  AFCS  consists  of  the  following  system components:

• Flight  control  panel  (FCP)
• Two  flight  control  computers  (FCCs)
• Two  autopilot  servomotors
• Two  independent  yaw  dampers

The  integrated  avionics  processing system (IAPS)  provides

interface  between  the  various  avionics systems

Half bank mode is automatically selected when climbing through

31,600 ft
or if the airplane is above the 1/2 bank transition altitude when the FD is turned on.

Maximum altitude  for  single  pack  operation:

31,000

Minimum temperature  for  cold-soaked APU  starting  on  the  ground:

-40°C

Starter  assisted  main  engine  start  (MES)  using  APU  bleed  is  limited  to:
____ft

21,000 ft

Maximum APU Starting Altitude

37,000

Maximum APU Operating Altitude

41,000

Load  Limitation
Main  Generator  (each),  APU  Generator

40 Kva

Inflight
Maximum continuous  load  on  each  TRU

120 amps

Takeoff  with  engine  fuel  temperature  indications  below  ____ is prohibited.

5°C

The  minimum  fuel  quantity  for  go-around  per  wing  tank

600 lbs

Icing  conditions  exist  in  flight  at  a  ____________  or  below,  and  visible  moisture  in  any  form  is encountered  (such  as  clouds,  rain,  snow,  sleet,  or  ice-crystals),  except  when  the  _____________________.

TAT of 10°C,  SAT is -40°C or below.

Do not  hold  in  icing  conditions  with

slats  and/or  flaps  extended

Category  II  approaches  are  prohibited  when  the  braking  action  is  reported  as  less  than

"less than" Medium

The  difference  between  the  published  field  elevation  and  the  altimeter  display  should  not  exceed

75 ft

minimum  of  two  primary altimeters  should  agree  with  a  maximum  difference  of?

200 ft or less.

If  Static/Standing  takeoff  data  is  generated  and  wind  limits  prevent  a  Static/Standing  takeoff:

A.)  If  Auto  Wind  using  METAR  is  unavailable,  winds  must  be  entered  in ACARS.- 
OR
B.)  For  aircraft  with  both  ACARS  inoperative  and  cFDP COMM:  NO,  Dispatch  must  manually a          insert  winds  into TLR  data.

Except  in  an  emergency,  takeoff  or  landing  will  not  be  attempted  whenever  peak  wind  value  exceeds

50Knts

TOT FUEL
pressure fueling

19,594

Tot. Fuel
700
Gravity fuel

14580

Tot. fuel
900
gravity fueling

14,810

how many hydraulic systems? What are their nominal psi?

3, 3000 psi

hyd sys. 1, 2 and 3  pumps are run by what?

Main 1 and 2 pumps are engine driven pumps (EDP)
1 and 2 backup pumps are AC motor driven(ACMP)
sys 3 both pumps are ACMPS
Pump 3A runs continuously when sw on.
3B runs when ADG is deployed

2 ways to close the hydraulic  SOVs

L/R HYD SOV switch or ENG FIRE PUSH sw.

HYD SYS 1 and 2 are cooled how?

hyd fluid is cooled through a single air/oil heat exchanger
air from a ram air scoop (in air)
cooling fan (on the ground)

HYD SYS 3 is cooled how.?

by natural convection.

HYD SYS PRESS (GREEN)

1800-3200psi

HYD SYS PRESS (AMBER)

1800 psi or less
amber dashes = invalid data

O2 min psi?

3 crewmembers = 1110
2 crewmembers = 960

The  following  limitations  apply  to  reduced  thrust  takeoff:

1. Anti-skid  must  be  operative
2. PROHIBITED on contaminated  runways
3. PROHIBITED if  the  airplane  has  been  de-iced
4. PROHIBITED if  wing  and/or  cowl  anti-icing  bleeds  are  in  use
5. PROHIBITED if  warnings  of  windshear  or  downdrafts  have  been  forecast
6. PROHIBITED with  an  engine  that  cannot  achieve  full-rated  thrust
7. PROHIBITED when  a  special  departure  procedure  specifies  full  thrust  for  takeoff

Live animals shall NOT be carried in which cargo compart?

forward compartment.

Non normal methodology

1. PF  -  Maintain Aircraft  Control
2. Identify  the  Non-normal  (Either  pilot  cancels  the  warning)
3. Accomplish  Memory  Items  (if  applicable)
4. Check  the  QRC  for  Immediate Action  Items
5. Captain  Assigns  PF
6. Complete  the  QRH  Procedures
7. Develop  and  Communicate  a  Plan

Average bag weights

STDs. check bag = 34lbs
plane side bag  = 22lbs
heavy check bag = 59lbs
Bag 100lb or heavier =  Actual

Average pax weights

Summer    pax    198lbs
Summer child        85lbs

Winter     Pax      203lbs
Winter      child       90lbs

Crew weights

Pilot                   229lbs
Flt Att                 181lbs
Acm+bag           253lbs
Crew roll bag        34lbs

Crj 700 dimensions

Wingspan      76.27ft
Length           106.67

Crj 900
Dimensions

Wingspan 81ft 6in
Length     118ft 10.7in

Brief   N.E.W.D.A.T.E.S

N... names
E... emergency procedures
W... weather
D... door entry procedures
A... aircraft specific information MELS
T... turbulence
E... estimated flight time
S... special considerations

Holding speed

Psa

Flaps 0+30 kts

Holding speed
FAA
MHA-6000

200 kias

Holding speed
FAA
6001-14000

230 kias

Holding speed
FAA
14001 and up

265 kias

Min reserve fuel
CR7

2100lbs

Min reserve fuel
CR9

2200lbs

Minimum contingency fuel
CR7

937

Minimum contingency fuel
CR9

1082

Minimum tanker fuel

330

Allowable fuel variance

+/- 500lbs
Never less than takeoff + taxi!!!

Approx fuel burn/hr

3000lbs

5 items required for the release

Airports of dept and arrv.
min fuel
Statement of operation (IFR)
TRIP #
F
REG#

Fuel  to  the Alternate  is  calculated  via  direct,  using  the  Long  Range  Cruise  table.

— 0-50 miles  at  10,000  ft.
— 51-100 miles  at  15,000  ft.
— 101-150 miles  at  20,000  ft.
— 151 miles or  greater  at  25,000  ft.

Taxi fuel is calculated at _____lbs/min

19lbs/min

How much dry ice does PSA carry?

275 lbs tot.
5.5 lbs per pax
50 lbs for medical shipments
Do Not carry if both packs deferred
50 lbs with 1 pack

How is RAMP fuel determined?

T/O FUEL + TANKER FUEL + TAXI FUEL

How is TAKEOFF fuel determined?

BURN + RESERVE + ALT + CONTINGY

How is TANKER fuel determined?

Added fuel for APU burn + Unusual ground delays

What do you add up to figure how long you can hold

BURN+ALT+RSV+MISSED

How is RSV FUEL CALCULATED

45 min at LR CRUISE AT FL250

What is CONTIGY fuel for

Anything involving delays into the airport.
traffic, holding, missed, .etc.....

Cabin max cabin psi.

8.6 psi +/- .1
or
8.7 depending the source

Cabin neg psi

-.5

Selection of EMER DEPRESS prohibited at

15000 ft and above.

What engines do the CRJ 701/900 use?

CRJ 701 use CF34-8C5B1

CRJ 900 use CF34-8C5

How many psi controllers are there?
How many motors for outflow valve?

two cpcs but there is a manual mode.
3 motors can control the outflow valve.
2 cpcs
1 manual

Single engine taxi conditions.

non operating boost pump off
do not exceed _____80_____%N2
exercise caution jet blast can harm personnel and equipment
prohibited when ramps or taxiways are contaminated with snow,slush or ice
prohibited when snow or other freezing/frozen precip present
sgl eng taxi with apu off, cabin  temp permitting.

What are the classes of NEF?
how long do they last?

Class 1 nef = 10 days
Class 2 nef = 30 days
CA nef = 90 days

Approach requirements can be found where?

QRH CH17

5 Items you must confirm before changing in an emergancy?

Thrust levers
engine fire switchlights
generator switches
fuel boost pump switchlights
All other guarded switches.

When do TAFS come out, how long are they good for?

Midnight 0600 1200 1800
6 hrs

Max Psi during ground manuvering?

0.1 psi

Max differential psi at touchdown?

1.0 psi

Max continuous  oil temp?

+155 °c

max permisable oil temp?

+163°c (15 min. max)

when do sigmets come out?
how long are they good for?

come out every 55min.
good for 2hrs.

pressurization modes
how many?

8 modes

Ground
pre-presurization
takeoff abort
climb
flight abort
descent
landing
touch and go

Aft cargo weights?

fwd and aft cargo weights vary by aircraft #  go check FRED!

Req CAT II rvr?

1200, 600, 300
mid not req
no rollout than no less than 1400 rvr
in ops spec c60

APU ALT FAIL message means?

APU operation is limited to 17000 feet or less.
failure of surge valve....

what distributes all the AC power in the aircraft?

ACPC   aircraft power center

What distributes DC power in the aircraft?

2 DC power centers

Bulk fuel takeoff limit temp?

-30°c

Tactile check required of wing when?

OAT is 10°c or less, or

the bulk fuel is 0°c or less, or

the conditions have been conducive for frost formation.

max frost of 1/8in under wing is ok (caused by cold soaked fuel)

When is mach trim active?

When at .4 mach or higher when hand flying.
adjust trim levels to compensate for mach tuck.

Standard T/O minimums (C056)

1sm or 5000 RVR

Changes to ______ in the departure and ________   ___________ procedures are _____!

altitudes,  missed approach,  PROHIBITED

descent angles above _______ at high altitude may result
in unintended acceleration beyond permitted speeds.

>4.5 °

Flights must be within _____ of a suitable airport, if cargo is
carried in either cargo compartment.

60 minutes

Weather minimus for airports without prescribed takeoff minimums.

800ft and 2sm
900ft and 1 1/2sm
1000ft and 1sm

Holding leg times?

sl to 14000 = 1min
above 14000 = 1min 30sec

Missed approach fuel
cr7
cr9

cr7=170
cr9=222
is part of contingency fuel.

Oil consumption

.05 gal/hr