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E175 Study Guide > Limitations > Flashcards

Limitations Flashcards

1
Q

Aircraft dimensions

  • Length
  • Width
  • Height
A

Aircraft dimensions

  • Length = 103’ 11” (104’)
  • Width = 93’ 11” (94’)
  • Height = 32’ 4” (33’)
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2
Q

Cabin Loading

- Max PAX

A

Cabin Loading
- Max PAX = 76
(12 First / 64 Coach)

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3
Q

Cargo compartments
*max weight limits
FWD =
AFT =

A

Cargo Compartments
*max weight limits
FWD = 3,306 lbs.
AFT = 2,535 lbs.

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4
Q 
Aircraft Weights
MRW -
MTOW-
MLW-
MZFW-
A 
Aircraft Weights
MRW - 85,800 lbs. 
MTOW- 85,500 lbs. 
MLW- 74,900 lbs. 
MZFW- 69,800 lbs.
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5
Q

Minimum Crew

A

Left seat Pilot & right seat Pilot (i.e. Captain & First Officer)

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6
Q

Aircraft operations

A
  • Day & Night
  • VFR & IFR
  • Icing Conditions
  • CAT I & CAT II
  • RVSM
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7
Q

Air
- Max Cabin Differential Overpressure:

  • Max Cabin Diff. Pressure (Above FL370):
  • Max Cabin Diff. for Takeoff & Landing:
  • Max Cabin Diff. Negative Pressure:

Note: Max Altitude Depressurized -

A

Air

  • Max Cabin Differential Overpressure:
    8. 8 psi
  • Max Cabin Diff. Pressure (Above FL370): 8.4 psi
  • Max Cabin Diff. for Takeoff & Landing: 0.2 psi
  • Max Cabin Diff. Negative Pressure: -0.5 psi

Note: Max Altitude Depressurized - 10,000’ or MEA whichever is Higher

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8
Q

Airspeeds

Mmo (Above FL280) -

Vmo (Above 10,000’ to FL280) -

Vmo (Below 10,000’) -

Va -

A

Airspeeds

Mmo (Above FL280) - 0.82

Vmo (Above 10,000’ to FL280) - 320 KIAS

Vmo (Below 10,000’) - 250 KIAS*
*FAA reg. Speed / structural speed limit is 300 KIAS

Va - 240 KIAS

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9
Q

Airspeeds

Vle - 
Vlo - 
Vlr - 
Vfe1 -
Vfe2 -
Vfe3 -
Vfe4 -
Vfe5 -
VfeFull -
A

Airspeeds

Vle - 250 KIAS
Vlo - 250 KIAS
Vlr -  250 KIAS
Vfe1 - 230 KIAS
Vfe2 - 215 KIAS
Vfe3 - 200 KIAS
Vfe4 - 180 KIAS
Vfe5 - 180 KIAS
VfeFull - 165 KIAS
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10
Q

Airspeeds

Max turbulent airspeed (below 10,000’):
Max turbulent airspeed (10,000’ and above):
Max crosswind for takeoff (Dry) - | (Wet) -
Max tailwind -
Max DV window operation -
Max tire speed -
Max windshield wiper speed -

A

Airspeeds

Max turbulent airspeed (below 10,000’): 250 KIAS
Max turbulent airspeed (10,000’ and above): 270 KIAS or .76 Mach
Max crosswind for takeoff (Dry) - 35 kts| (Wet) - 30 kts
Max tailwind - 10 kts
Max DV window operation - 160 kts
Max tire speed - 195 KIAS
Max windshield wiper speed - 250 KIAS

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11
Q

Airspeeds

Max crosswind for landing

6 Dry - 
5 Good -
4 Good to Medium -
3 Medium -
2 Medium to Poor -
1 Poor -
A

Airspeeds

Max crosswind for landing

6 Dry - 38 kts
5 Good - 31 kts
4 Good to Medium - 20 kts
3 Medium - 15 kts
2 Medium to Poor -  12 kts
1 Poor - 8 kts
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12
Q

Altitudes and Temperatures

Max operating:

Max Altitude with flaps extended:

Max Takeoff & Landing:

Min Takeoff & Landing:

Min | Max Takeoff & Landing Temperature (SAT):

Max altitude display difference in flight for RVSM:

Note: in the event of a landing below -40 C,

A

Altitudes and Temperatures

Max operating: 41,000’

Max Altitude with flaps extended: 20,000’

Max Takeoff & Landing: 10,000’

Min Takeoff & Landing: -1’000’

Min | Max Takeoff & Landing Temperature (SAT): -40 C | 52 C

Max altitude display difference in flight for RVSM: 180 ft.

Note: in the event of a landing below -40 C, the airplane may not takeoff without further maintenance inspection.

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13
Q

APU

Type - 
First & second start attempts -
Third start attempt -
Min operation temp:
Max operation temp:
EGT (start) -
EGT (Continuous) -

Note: no time limit in amber on the ground /inflight from ____C to _____ C

Max operation Alt. (Electrical) -
Max start altitude -
Max operation altitude (eng. start assist) -
Max operation altitude (ECS Bleed) - 
Max Rotor Speed -
A

APU

Type - Sundstrand APS 2300
First & second start attempts - START/ON then 60 sec. OFF
Third start attempt - START/ON then 5 min. OFF
Min operation temp: -54 C
Max operation temp: ISA +35 C
EGT (start) - 1032 C
EGT (Continuous) - 717 C

Note: no time limit in amber on the ground /inflight from 662 C to 717 C

Max operation Alt. (Electrical) - 33,000’
Max start altitude - 30’000’
Max operation altitude (eng. start assist) - 21,000’
Max operation altitude (ECS Bleed) - 15,000’
Max Rotor Speed - 108%

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14
Q

Autopilot

Minimum engagement altitude -

Minimum engaged altitude -

A

Autopilot

Minimum engagement altitude - above 400’

Minimum engaged altitude - above 50’

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15
Q

Engine

Type -
N1 RPM Max -
N2 RPM Max -
Max start ITT -

A

Engine

Type - GE CF34-8E5
N1 RPM Max - 99.5%
N2 RPM Max - 99.4%
Max start ITT - 815 C

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16
Q

Engine

Max Start ITT -

Max Normal T/O ITT -

Max T/O & G/A ITT -

Max Continuous ITT -

A

Engine

Max Start ITT - 815 C

Max Normal T/O ITT - 965 C (2min)
                                      949 C (3min) [Total - 5 min]
Max T/O & G/A ITT - 1006 C (2 min)
                                    990 C (3 min) [total - 5 min]

Max Continuous ITT - 960 C

17
Q

Engine

Min/Max Oil Pressure -

Continuous Oil Temperature -

Transient Oil Temperature -

A

Engine

Min/Max Oil Pressure - 25 psi / 95 psi

Continuous Oil Temperature - 155 C

Transient Oil Temperature - 163 C ( 15 min. Limit)

18
Q

Engine Thrust

T/O-1 =_________ / OEI ATTCS =_________

T/O-2 =_________ / OEI ATTCS =_________

A

Engine Thrust

T/O-1 = 13,000 lbs. / OEI ATTCS = 14,200 lbs.

T/O-2 = 11,800 lbs. / OEI ATTCS = 13,000 lbs.

19
Q

Fuel

Brazilian -
ASTM -
American -

Minimum Fuel Tank Temp:

Crossfeed Operation -

A

Fuel

Brazilian - QAV1
ASTM - Jet A or A1
American - JP8

Minimum Fuel Tank Temp: -37 C

Crossfeed Operation - Crossfeed knob must be OFF for Takeoff and Landing

20
Q

Fuel

Maximum fuel capacity -

Maximum usable quantity -

Unusable quantity -

Maximum fuel imbalance -

Note: Weights listed above have been determined for an adopted Fuel density of 6.767 lbs./US Gal.

A

Fuel

Maximum fuel capacity - 20,934 lbs. (10,467 lbs. per tank)

Maximum usable quantity - 20,784 lbs. (10,392 lbs. per tank)

Unusable quantity - 150 lbs. (75 lbs. per tank)

Maximum fuel imbalance - 794 lbs.

Note: Weights listed above have been determined for an adopted Fuel density of 6.767 lbs./US Gal.

21
Q

Starter

1st Dry Motor -

2nd to 5th Dry Motor -

Note: After 5 sequential dry motors, the cycle may be repeated following a 15 min. cool-down period.

1st & 2nd Start -

3rd to 5th Start -

A

Starter

1st Dry Motor - Max 90 sec. followed by 5 min. Cool down

2nd to 5th Dry Motor - Max 30 sec. followed by 5 min. Cool down

Note: After 5 sequential dry motors, the cycle may be repeated following a 15 min. cool-down period.

1st & 2nd Start - 90 sec. (Grd)/120 sec. (Flt) with 10 sec. cool down

3rd to 5th Start - 90 sec. (Grd)/120 sec. (Flt) with 5 min. cool down

E175 Study Guide (23 decks)

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