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CRJ 900 > Shaded Box Limitations > Flashcards

Shaded Box Limitations Flashcards

1
Q

Emergency Checklist Items

A
  1. Engine Fire or Severe Engine Damage
    (In Flight)
  2. APU Fire
  3. Engine Fire or Severe Engine Damage
    (On Ground)
  4. In Flight Engine Shutdown
  5. Double Engine Failure
  6. Smoke or Fumes Removal Procedure
  7. SMOKE AFT (FWD) CARGO

** BACK **

  1. MLG BAY OVHT
  2. BRAKE OVHT
  3. Passenger Evacuation
  4. CABIN ALT or
    Emergency Descent
  5. Uncommanded Yaw Motion
  6. Ditching or Forced Landing Imminent
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2
Q

Length:
Wingspan:
Height

A

Length: 118 ft. 11 in.
Wingspan: 81 ft. 6 in.
Height: 24 ft. 1 in.

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3
Q

Structural Weight Limitations:

MRW:
MTOW:
MLW:
MZFW:
MFW:
A 
MRW: 85,000 (75,250)
MTOW: 84,500 (75,000)
MLW: 75,100 (67,000)
MZFW: 70,750 (62,300)
MFW: 45,000
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4
Q

Cargo Limitations:

A

Aft: 3,650 lbs.
(Company)

Fwd: 1,700 lbs.

(700: 1,000 lbs.)

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5
Q

Engine and Thrust

A

GE CF34-8C5

Normal: 13,600 lbs. thrust

APR: 14,510 lbs. thrust

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6
Q

Max Mach RVSM:

A
  1. 82 in RVSM

700: 0.83

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7
Q 
Flap Speeds:
1:
8:
20:
30:
45:
A

1: 230 KIAS
8: 230 KIAS
20: 220 KIAS
30: 185 KIAS
45: 170 KIAS

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8
Q

Landing Gear Speeds:

Extension:
Retraction:
Extended and locked:

A

Extension: 220 KIAS
Retraction: 200 KIAS
Extended and locked: 220 KIAS

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9
Q

Max airspeed for:

windshield wiper operation

OR

failed in a non-parked position

A

250 KIAS

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10
Q

Max tire speed

A

195 Knots Groundspeed

700: 182 Knots

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11
Q

Max speed for ADG operation

A

Vmo/Mmo

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12
Q

Wind Components

Max tailwind:
Max x-wind t/o dry:
Max x-wind ldg dry:
Max x-wind wet:
Max x-wind b.a. FAIR:
Max x-wind b.a. POOR:
Max x-wind dry high mins CA/FO:
A 
Max tailwind: 10 KIAS
Max x-wind t/o dry: 35 KIAS (28 KIAS)
Max x-wind ldg dry: 32 KIAS (30 KIAS)
Max x-wind wet: 27 KIAS
Max x-wind b.a. FAIR: 20 KIAS
Max x-wind b.a. POOR: 15 KIAS
Max x-wind dry high mins CA/FO: 25/15 KIAS
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13
Q

Max pressure altitude

for t/o and ldg

A

8,000 feet

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14
Q

Max and min temp. for t/o

A

Max: ISA + 35C

Min: -40C

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15
Q

LAHSO min. distance

A

SL - 999 ‘ MSL:
7,000 ft. (700: 6,000 ft.)

1000-1999’ MSL:
7,100 ft. (700: 6,100 ft.)

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16
Q

Flights must be within __ min.

of a suitable airport with cargo

A

60 minutes

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17
Q

Max diff press:

Max neg. diff press:

During taxi, t/o and ldg
max diff press:

Max altitude single pack:

Max altitude EMER DEPRESS use:

A

Max diff press: 8.7 psi

Max neg. diff press: -0.5 psi

During taxi, t/o and ldg
max diff press: 0.1 psi

Max altitude single pack: 25,000 ft.

Max altitude EMER DEPRESS use: 15,000 ft.

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18
Q

Minimum AP use height:

Visual and NPA:
ILS:
ILS Single Engine:

Max ILS glidepath angle:

A

Minimum AP use height:

Visual and NPA: 400’ AGL
ILS: 80’ AGL
ILS Single Engine: 110’ AGL

Max ILS glidepath angle: 3.5 deg

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19
Q

kVA Load Limitation

Main generator (each):

APU generator:

A

kVA Load Limitation

Main generator (each):
40 kVA (0-41,000 ft)
APU generator:
40 kVa (0-41,000 ft)
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20
Q

Max permissible continuous

load on each TRU

A

120 amps

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21
Q

Cowl Anti-Ice ON

(GROUND and
TAKEOFF)

A

OAT 10C or below

AND

visible moisture

OAT 10C or below

AND

taxiing over SWISS
(standing water, ice, snow, slush)

22
Q

Cowl Anti-Ice ON

FLIGHT

A

ICING CONDITIONS:

(TAT of 10C or below
AND
visible moisture,
unless SAT -40C or below)

ICE annunciated

23
Q

Wing Anti-Ice ON

Takeoff

A

OAT 5C or below

AND

visible moisture

OAT 5C or below

AND

SWISS

NOTE: ON prior to thrust increase
if type 2-4 applied

24
Q

Wing Anti-Ice ON

Flight

A

Icing conditions <230 KIAS

or

ICE annunciated

25
Q

With APU as bleed source

in manual mode:

A

Wing and/or cowl anti-ice

PROHIBITED

26
Q

Max fuel imbalance during:

Takeoff:

All other phases of flight:

A

Max fuel imbalance during:

Takeoff: 300 lbs.

All other phases of flight: 800 lbs.

27
Q

When can you takeoff with
more than 500 lbs.
in center tank?

A

When each wing tank
is above 4,400 lbs.

OR

When each wing tank
is above 2,000 lbs. AND
ZFW reduced by
weight of fuel in excess of 500 lb.

28
Q

Min. fuel for go-around

A

600 lbs. per wing

Max 10 deg. nose up

29
Q

Minimum fuel temperature

Engine fuel for takeoff:

Bulk fuel for takeoff:

A

Engine fuel for takeoff: 5C

Bulk fuel for takeoff: -30C

30
Q

Minimum temperature starting

cold soaked APU

31
Q

APU starter motor duty cycle

A

3 starts/start attempts in 1 hr

32
Q

How long must you wait between

APU start attempts

33
Q

APU altitude limits

Ground starting:
Bleed extraction:
Air starting:
Generator loading:

A

APU altitude limits

Ground starting: 15,000 ft.
Bleed extraction: 25,000 ft.
Air starting: 37,000 ft.
Generator loading: 41,000 ft.

34
Q

When can you exceed 75% N1

after engine start?

A

2 minutes after start

35
Q

Before FFOD when a/c
cold soaked
-30C
for more than 8 hrs…

A
  1. Motor engines 1 min. and
    verify N1 rotation
  2. Thrust reverser actuated
    until deploy/stow cycles
    2 seconds or less
36
Q

Continuous Ignition Req’d

A
  1. T/O and ldg contam. RWY
  2. Flight in mod. or heavier rain
  3. Flight in mod. or heavier turb.
  4. Flight in vicinity of TS
37
Q

Order if both cowl anti-ice and

continuous ignition req’d

A
  1. Cowl anti-ice

2. Continuous ignition

38
Q

Cannot FLEX when CAWI

A
  1. Contaminated runway
  2. Anti-skid INOP
  3. Windshear forecast
  4. Wing and/or cowl a/ice in use
39
Q

Max N2 with starter

40
Q

Engine Start Cycles

GROUND

A

Start 1 and 2:
1 min. 30 sec. ON, 10 sec. OFF

Start 3,4,5:
1 min. 30 sec. ON, 5 min. OFF

41
Q

Engine Start or
Motoring Cycles

(FLIGHT)

A

Start 1:
2 min. ON, 10 sec. OFF

Start 2,3.4,5:
1 min. ON, 5 min. OFF

42
Q

Motoring Cycles

GROUND

A

Motor 1:
1 min. 30 sec. ON, 5 min. OFF

Motor 2,3.4,5:
30 sec. ON, 5 min. OFF

43
Q

ITT temp for thrust lever

SHUT OFF to IDLE

A

Ground: < 120C

Flight: < 90C

44
Q

Thrust Reverser Usage

Max reverse thrust
PROHIBITED below:

Idle reverse thrust
achieved by:

A

Max reverse thrust
PROHIBITED below: 75 KIAS

Idle reverse thrust
achieved by: 60 KIAS

45
Q

Engine Operating Procedure
Due To Wind:

Less than 5 knots

OR

Within 30 deg. of nose:

A

Rolling, Normal, Standing T/O

46
Q

Engine Operating Procedure
Due To Wind:

5-30 knots

MORE than
30 deg. off nose

A

Rolling or Normal Takeoff

(Normal = Max 75% N1
before brake release)

47
Q

Engine Operating Procedure
Due To Wind:

More than 30 knots

MORE than
30 deg. off nose

A

Rolling Takeoff

Idle thrust before brake release

48
Q

Flight Spoiler Usage

Min. altitude:

Min. speed:

A

Min. altitude: 1,000’ AGL

Min. speed: Vref + 10

49
Q

What is min climb speed above

FL 330?

50
Q

EICAS Messages
At Various Altitudes

8,500 ft:

10,000 ft:

14,000 +/- 300 ft:

14,500 +/- 500 ft:

A

8,500 ft:
CABIN ALT caution msg

10,000 ft:
- CABIN ALT warning msg
- NO SMKG and SEAT BELTS
Signs Automatically On

14,000 +/- 300 ft:
Oxygen masks drop

14,500 +/- 500 ft:
Altitude limiter of outflow valve

51
Q

What will not work when
CPCP fails?

(Cabin Pressure Control Panel)

A
  1. NO SMKG and SEAT BELTS
    signs will not automatically turn on
    at 10,000 ft.
  2. Oxygen masks will not
    drop at 14,000 +/- 300 ft.

CRJ 900 (7 decks)

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