Crj C700

Front 1

Max Tire Speed

Back 1

182Kts

Front 2

Max takeoff weight

Back 2

75,000

Front 3

Max taxi weight

Back 3

75,250

Front 4

Max Zero Fuel Weight

Back 4

42,000

Front 5

Min Flight Weight

Back 5

39,835

Front 6

Maxium altitude for takeoff and landing

Back 6

8000

Front 7

Maximum operating altitude is

Back 7

41000

Front 8

Maximum and minimum temperature for takeoff and landing

Back 8

ISA +35, -40c

Front 9

Cowl anti-ice system must be on when the ambient temperature is below

Back 9

OAT 10C or below

Front 10

Engine cowl anti ice system must be on when (2 conditions)

Back 10

1) in icing conditions
2) ICE is annunciated by the detections system.

Front 11

Wing Anti-Ice System
When must wing anti-ice must be on for takeoff and landing

Back 11

OAT 5C or Below
2) Visable moisture and Vis is < 1 Mile
3) Contanimated Runway
4) TypeII, TypeIV anti-ice fluids applied
5) Must be selected on just prior to takeoff

Front 12

What are the engine types are on the CRJ700

Back 12

GE CF34-8C5B1

Front 13

Maximum and minimum Limitations for the following indications
N1)
N2)
ITT C
OilTemp C
Oil Press psi

Back 13

N1) 99.4-Limit 99.5
N2) 99.3-Limit 99.4
ITT) Vatiable
Oil Temp) 164, 156-163, -40 to 155
Oil Temp) 0-24 (red)

Front 14

Use of Engine High PWR Sched switchlight is....

Back 14

Prohibited!

Front 15

Engine Warm up
The engine must remain idle until...
During all starts, do not exceed**** percent N1 for ***minutes or untill all operatins indications are in the normal range

Back 15

1) 75%
2) 2minutes

Front 16

Airplane cold Soak
Before the first flight of the day, when the plane is soaked for -30C or below for more the 8hrs what must be accomplished?
1)
2)

Back 16

1) the engines must be motored for 60 sec and the fan rotations must be verified before engine start is intinated
2) thrust reversers must be actuated until the deploy and stowed cycles are 2 sec. or less.

Front 17

Continuous engine ignitions must be used during the following
1)
2)
3)
4)

Back 17

1) Takeoff and landings on contanimated ryws
2) Flight through moderate or intense rain
3) flight through moderate or heave intense turbulance
4) flight in vicinity of thrunderstorms

Front 18

Starter Cranking Limits
the starter must not be indicated in N2 rpm exceeds 45%
At initiations of thrust lever movement from Shut Off to idle:
1), 2)

Back 18

1)ITT must be 120C or less for all ground starts
2) ITT must be 90C or Less for all air starts

Front 19

Engine Relight Limits
1) Windmilling a)

Back 19

Altitude from 21,000 to 10,000 ft:
Speed
Speed 290 KIAS to Vmo, 7.2% N2 minimum

Front 20

Engine Relight Limits
1) Windmilling b)

Back 20

Altitude from 10,000 feet to sea level:
speed 250 KIAS to Vmo and 7.2%N2 minimum

Front 21

Engine Relight Limits
Starter Assisted

Back 21

Altitude from 21,00 ft to sea lvl
Speed from Vref up to Vmo and from 0 to 45% N2

Front 22

Engine Relight Limits
All Engine-Out Rapid Relight

Back 22

Altitude from 10,000 ft. to sea lvl:
FADEC rapid relight capabilty has been demonstrated at 200 KIAS for up to 15-sec fuel interruptions.

Front 23

Wing tank capacities

Back 23

7,492 lbs
7,290 lbs Gravity Refueling

Front 24

Center Tank

Back 24

4610 lbs

Front 25

total tank capacities

Back 25

19,594lbs, 14,580 refueling

Front 26

Fuel Temp limits for Jet A
1) Bulk Fuel Takeoff Limit
2) Bulk Fuel Freezing Point

Back 26

1) -30C
2) -40C

Front 27

Takeoff with engine fuel temp indications below**** is prohibited

Back 27

5C

Front 28

takeoff with bulk fuel temp indications below****** ***** is prohibited

Back 28

limits stated

Front 29

Takeoff with a fuel load in excess of ****** in the center tank is not permitted unless unless the wing tank is ******lbs

Back 29

1) 500lbs
2) 4,400

Front 30

The Minimum fuel quantity for go around per tank

Back 30

600lbs per wing with max 10 degree nose up.

Front 31

During flight, bulk fuel temps must remain above....

Back 31

applicable bulk fuel freezin point.

Front 32

Maximum permissible fuel imbalance between wing tanks are given

Back 32

1) 300 lbs during takeoff
2) 800 all other phases of flight

Front 33

Oil Consumptions
What is the maxumim oil consumption on each engine

Back 33

6.4 us ounces per hour

Front 34

What types of oil go into the engine

Back 34

Castrol 4000

Front 35

What are the Oil using components on the plane

Back 35

Engines, Air turbine Starter, Integrated Drive Generator, Aux Power Unit

Front 36

Engine Oil Level
What is the Max durations for checking the oil without servicing

Back 36

36 hours

Front 37

In excess of 36 hrs without checking the oil, what are the new checking limits?

Back 37

oil level must be checked within 3 mins to 1 hour after every shutdown.

Front 38

For Oil Replenishment System
Maximum oil refill allowable without dry motoring

Back 38

2US quarts

Front 39

What must be done if the oil system as been replenished to maximum capacity and the replenish period has been exceeded

Back 39

The engine must be dry motoring

Front 40

Mixing of the oils is permitted, T or F

Back 40

F

Front 41

What Brand of APU is there on the CRJ too?

Back 41

Allied Signal RE 220 RJ

Front 42

What is the Ambient temp limit for starting a cold soaked APU on the ground

Back 42

-40C

Front 43

Maxumim EGT ( dependant upon altitude and temps) are?

Back 43

for 0-100 %RPM 692C to 1038C

Front 44

The APU is limited to how many started cycles on one hour?

Back 44

3 starter cycles attemtps in one hour.

Front 45

How long is the delay for cooling the starter between cranking?

Back 45

two minute delay

Front 46

Operating Range
MAx RPM

Back 46

Max RPM 106

Front 47

Max EGT

Back 47

1038

Front 48

What is the Maximum APU starting Altitude

Back 48

37,000

Front 49

What is the Max operating altitude.

Back 49

41,000

Front 50

ECS Operations
What is the Max altitude to extract bleed air.

Back 50

25,000 and below

Front 51

If the use of the oil replenishment system is required, how long do you have to replinish the oil after shutdown

Back 51

15 minutes to 1 hour after engine shutdown

Front 52

What is required if the oil system has to be replenished to a maximum capacity and the replenished period has been exceeded?

Back 52

the engine must be dry motored

Front 53

Is Mixing oil types allowed

Back 53

It is prohibited to mix oil types

Front 54

APU Bleed Ait Limits
What is the limit for Using Bleed air to start the Main engine (In Flight)

Back 54

Starter assisted main engine start(MES) using APU bleed air is limited to 21,000 ft or below(not an APU bleed limitations but an in-flight MES altitude limitation)

Front 55

What are the Limitations for a APU Bleed Air Main Engine start (on Ground)

Back 55

No Limitations

Front 56

What is the Bleed Air Limit for ECS operations

Back 56

APU Bleed air extraction is not permitted above 25,000

Front 57

Memory Items for Rejected Takeoff (3 Items)

Back 57

Thrust Levers....Idle
Wheel Brakes.....Maximum untill safe stop
Thrust reversers...Maximum (consistant with directional control)

Front 58

Flight Compt. Smoke Removal Proceedures
(2 items)

Back 58

1) Oxygen mask/Smoke Goggles...don & 100%
Crew
2)Communications...Establish

Front 59

Air Condition Smoke
(2 Items)

Back 59

1) Oxygen mask/Smoke...Don 100%
2) Crew communication....Establish

Front 60

Electrical Smoke of Fire
(2 Items)

Back 60

1) Oxygen mask/Smoke goggles DON & 100%
2) Crew Communications...Establish

Front 61

Cabin Alt Msg or Emerg Descent Procedure
(2 items)

Back 61

1) Oxygen Mask....don 100%
2) Crew Communication...Establish

Front 62

Rudder System Jammed
(2 items)

Back 62

1)Yaw Damper Disc...Select
2)Rudder pedals...overpower

Front 63

Stablilzer Trim Runaway
(2 Items)

Back 63

1)Conrol Wheel...Assume Manual COntrol and Override Runaway
2)Stab Trim...Disconnect

Front 64

During Landing Execessive Asymmerty or Loss of Braking
(3 Items)

Back 64

1) Wheel brakes..Release momentarily
2)Anti Skid...Off
3)Wheel Brake...Re-Apply As Required

Front 65

Configurations Warning
(one Items)

Back 65

Takeoff...Discontinue Immediately

Front 66

Aileron System Jammed
(4 items)

Back 66

1)Autopilot...Disengage
2)Aileron controls (both) release pressure
3) Roll disc...Pull, Turn and Lock
4) Airplane control...transfer to pilot with operative aileron

Front 67

Elevator System Jammed
(4 items)

Back 67

1) AutoPilot...Disengage
2) Elevator controls(both)...Release Pressure
3) Pitch Disc...Pull, Turn and Lock
4) Airplane control...Transfer to pilot with operative elevator

Front 68

List the 4 required equipment systems for RVSM

Back 68

1) Autopilot (1)
2) Altitude Alerter System
3) Altitude Reporting transponder (2)
4) Air Data Computers (2)

Front 69

Cargo Flight reqirements
Fligth with Cargo must be within .....Minutes from a suitable airport, if installed in .....compartment

Back 69

1) 60 minutes
2) either compartment

Front 70

Maximum runway slopes approved for takeoff and landing

Back 70

+/- 2 degrees

Front 71

What are the center tank fuel capacities

Back 71

4610

Front 72

What is Max Speed of the Aircraft

Back 72

Mach .85

Front 73

What is the Maximum operating speed in RVSM Airspace?

Back 73

Mach .83

Front 74

Max altitude for Starting the APU for ECS purposes

Back 74

25,000 ft.

Front 75

Flap speed for the following flap Settings
1) Flaps 1
2) Flaps 8
3) Flaps 20
4) Flaps 30
5) Flaps 45

Back 75

1) 230
2) 230
3) 230
4) 185
5) 170

Front 76

Gear Positions Speeds
1)Extention
2)Down and Locked
3)Retractions

Back 76

1) 220 KIAS
2) 220 KIAS
3) 200 KIAS

Front 77

Max APU EGT
Green Limit
Red Limit

Back 77

Green 806 C
Red 807 C

Front 78

Max APU RPM
Green Limt
Red Limit

Back 78

Green Limit 0-106%
Red Limit 107%

Front 79

If APU Door is indicated open or unsure what are the Proceedures?

Back 79

1) the Max speed is 220 KIAS
2) The APU must remain in Operations

Front 80

Maximum permissable electrcal load on the APU

Back 80

40 KVA

Front 81

Max Speed for the ADG
(Air Driven Generator)

Back 81

VMO/MMO

Front 82

What is the Maximum speed one may fly through turbulance

Back 82

280KIAS or Mach .75 which ever is lower.

Front 83

Minumum operating speed

Back 83

Nothing lower that Stick spaker and even not that close without purpose for flight testing purposes.

Front 84

Max Windshield wiper operating speeds

Back 84

250 KIAS in the Parked position. If not in use but not parked, Max speed 250 KIAS

Front 85

What are the maneuvering Limit Load Factors for operation
1) Flaps Retracted
2) Flaps Extended

Back 85

1) -1.0 to 2.5 G
2) 0.0 to 2.0 G

Front 86

Minimum altitude for Auto pilot engagement after takeoff?

Back 86

600 Ft.

Front 87

Minimum alt. for auto pilot engagement on a non-precisions approach

Back 87

400ft

Front 88

Min. Alt for autopilot engagement on a percision approach< 3.5 degrees

Back 88

80 ft

Front 89

Min alt. for autopilot engagement for a precision approach <3.5 degrees with an airport alt <4000ft.

Back 89

120ft

Front 90

Flight spoilers must be retracted below what altitude

Back 90

300ft. and also not within 10KIAS of approach speed

Front 91

Flight slats and Flaps may not be extended above what altitude?

Back 91

15,000

Front 92

What are the 4 requirements for PRNAV

Back 92

1) flight Management Computer (2)
2) FMS control Display (2)
3) VHF NAV(2) DME(2)
4) GPS (2)

Front 93

Max Oil Pres

Back 93

Green/ Variable
Amber/ Variable
Red/ 0 to 24psi

Front 94

What is the Max Oil Temperature

Back 94

Green/ -40 to 155
Amber/ 156-163
Red/ 164

Front 95

ITT temd during Ground starts

Back 95

815 Deg C

Front 96

Max N1 and Idle Percent

Back 96

99.5/ 20-25%

Front 97

Max Windmill start temp

Back 97

927 Deg.

Front 98

Expexted N2 during
1) Ground Start
2) Assissted Start
3) Idle
4) Max Continuous
5) Max

Back 98

1) 45%
2) 45%
3 55-65
4) 98%
5) 99.4%

Front 99

Max Oil Press on Ground Start, Assisted Start, Windmill, idle, Max Cont, Normal T/O

Back 99

182psi -95
182 psi -95
182psi- 95
25-60/psi
45-95psi
45-95 psi

Front 100

Max oil temp is..

Back 100

155Deg

Front 101

Under what conditions is Flex Power not usable

Back 101

Flex Power is not to be used for the followin conditions
1) Wing and Cowl anti Ice
2) Runway is contanimated
3) Warning or forecast of windshear or downdrafts
4) Antiskid system is inperative.

Front 102

What are the icing conditions in flight considered

Back 102

Icing conditions are considered a TAT of 10 deg C or below and visable moisture in anyform is encountered.

Front 103

What are the amounts of ice and frost permissable for takeoff on the underside of the wings surfaces, associated with the fuel tanks

Back 103

max 1/8 in layer of frost
max 1/16 in layer of ice

Front 104

What is the max airport pressure altitude for takeoff.

Back 104

8000ft is the max press altiude.

Front 105

When must wing anti-ice system be on for takeoff with the OAT is below 5 deg C and below

Back 105

1) visible moisture with 1 mile visible moisture
2) Contaminated runways
3) When Anti Icing fluids have been applied.

Front 106

What is the Maximum continuous ITT

Back 106

960 deg C

Front 107

What is the Max continuous N2

Back 107

98%

Front 108

What is the Max continuous N1

Back 108

99.5%

Front 109

What is the oil pressure limits for Ground, Starter assisted and Windmill start

Back 109

182 to 95 psi after 10 minutes. Values make peak above 182 psi to 95psi

Front 110

What is the oil pressure during idle

Back 110

25-60 psi / 25-95 for oil temp greater than 60 deg C

Front 111

Minimum oil level for flight during ground start

Back 111

Ground start min oil level for flight is 40% with the affected engine not started.