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175 E > Limitations > Flashcards

Limitations Flashcards

1
Q

Weights LR/LL

A

MRW 85,870 / 85,450
MTOW 85,517 / 85,098
MLW 74,957 / 74,957
MZFW 69,886 / 69,467

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2
Q

MIN FLIGHT CREW

A

2 = pilot and copilot

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3
Q

max runway slope
runway surface type
max altitude for flaps extended
max operating altitude
max T&O & landing altitude
min T&O & landing altitude

A

+/- 2%
paved
20,000

41,000*
10,000
-1000

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4
Q

Max speed to open direct vision window

A

160

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5
Q

max latitude for stationary alignment

A

78.25N-78.25S

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6
Q

min ambient temp approved for T&O
max ambient air temp for takeoff and landing

A

-54c

52c

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7
Q

VLO RET, VLO EXT, VLE speeds (gear)

A

250

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8
Q

Flap speeds

A

flap 1 230
flap 2 215
flap 3 200
flap 4 & 5 180
flap Full 165

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9
Q

aircraft max operating speed

A

VMO/MMO

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10
Q

max operating mach

A

.82

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11
Q

max airspeed for RAT operation

A

VMO/MMO

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12
Q

turbulent air below 10,000
turbulent air above 10,000

A

250
270 or 0.76 whichever is lower

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13
Q

max tire limit ground speed
max windshield wiper speed

A

195
253

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14
Q

max operating speed up to 8,000
8,000 - 10,000
10,000 - FL290
FL290-FL410

A

300

300-320
320
.82

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15
Q

Max recommended xwind for landing

A

Max recommended xwind for landing

Dry 28
wet 28
compacted snow 20
standing water/slush/wet snow/dry snow 18
ice 12

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16
Q

max static takeoff crosswind

A

25 kts

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17
Q

cargo loading weights

A

FWD 3306
AFT 2535

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18
Q

icing conditions may exist

A

icing conditions may exist whenever the Outside Air Temperature (OAT) on the
ground or for Takeoff, or Total Air Temperature (TAT) in-flight, is 10°C or below
and visible moisture in any form is present (such as clouds, fog with visibility of
one mile or less, rain, snow, sleet and ice crystals)

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19
Q

APU min start temp (outside temp)

APU max alt to start

APU max operating alt

APU max electrical generation

A

-54C

30,000

33,000

33,000

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20
Q

APU bleed altitude

A

15,000

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21
Q

Altitude for APU to assist engine start

A

21,000

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22
Q

APU max rotor speed %

A

108%

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23
Q

APU amber range (no time limit)

A

662 - 717C

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24
Q

APU EGT start temp

A

1032

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25
Q

APU EGT continuous TEMP

A

717

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26
Q

APU start limits times

A

1 & 2 1 min on/1 min off

3 1 min on/5 mins off

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27
Q

CAT II flaps position

A

flaps 5

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28
Q

CAT II demonstrated wind components (not considered limiting)

A

headwind 25
tailwind 10
crosswind 12

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29
Q

CAT II required equipment

A

2 Air Data System (ADS).
2 Flight Director Systems.
2 Inertial Reference Systems.
2 Primary Flight Displays (PFD).
2 VOR/ILS NAV System.
Autopilot System Channel.
Cat II Engagement Logic.
EGPWS.
Radio Altimeter.
Rudder in Normal Mode.
SPOILER FAULT message not presented.
VHF/COMM System.
Windshield Wipers.

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30
Q

max fuel capacity total

max fuel capacity per tank

unusable fuel per tank

A

20935 lbs

10392.5 lbs

75 lbs

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31
Q

min fuel tank temp

max fuel imbalance

A

-37C in left tank

794 lbs

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32
Q

max differential pressure

Maximum differential overpressure

Maximum differential negative pressure

Maximum differential pressure for Takeoff and Landing

A

8.4 psi

8.8 psi

-.5 psi

.2 psi

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33
Q

Single PACK operations limit

A

FL 310

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34
Q

Thrust reversers conditions

A

Upon Landing, if thrust reversers have been used, reverser should be set to MIN REV at 60 KIAS, and be closed by 30 KIAS.
A Go-Around Maneuver should not be attempted after Thrust Reversers have been deployed

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35
Q

autopilot use

A

min engagement height in AFM - 400
min engagement height in CFM - 1,000’*
min use height - 50’

36
Q

CF 34-8E5 engines with takeoff thrust time limited to ____ minutes OR POSTMOD SB170-73-0002

A

10 minutes

37
Q

N1 max percentage

N2 min - max percentage

A

99.5%

58.5% - 99.4%

38
Q

TT max Start

A

815

39
Q

ITT max take off and go around temp and time limits

A

ITT max take off and go around temp and time limits

990C

  1. Time limited to 5 min with all engines operative. This limit is extended to 10 min with one engine inoperative for airplanes Post- Mod SB 170-73-0002 or equipped with an equivalent modification factory incorporated.
  2. Can be exceeded up to 1006°C during the first 2 minutes.
40
Q

ITT max continuous temp

A

960

41
Q

oil pressure PSI min- max

A

25-95psi

42
Q

oil temp continuous

A

155

43
Q

oil temp transient

A

163 (Transient operation above 155°C limited to 15 minutes.)

44
Q

Engine starter limits attempts

A

Engine starter limits attempts

1 and 2 - 90 Seconds on/ 10 Seconds off

3 , 4 and 5 - 90 Seconds On/5 Minutes off

120 seconds on In-flight

45
Q

Engine dry motor starter limits attempts

A

Engine dry motor starter limits attempts

1 - 90 Seconds on/ 5 Minutes off

2 through 5 - 30 Seconds on/5 Minutes off

After five sequential motorings, cycle may be repeated following a 15 minute cool down period.

46
Q

for FLEX - The total thrust reduction must not exceed ____ of the full Takeoff thrust.

FLEX is prohibited on ____ runways

A

25%

contaminated

47
Q

TAS, TAT and SAT information are only valid above____ KIAS

A

60

48
Q

While transmitting in ____ the standby magnetic compass indication is not valid.

A

VHF1

49
Q

Baro altimeter minimums must be used for all ____Approaches.

A

CAT I

50
Q

Pilots are authorized to deviate from their current Air Traffic Control (ATC) clearance to the extent necessary to comply with an

A

EGPWS warning.

51
Q

Localiser Back course Approaches using _____ are prohibited.

A

IESS

52
Q

RSVM required equipment list

A

RSVM required equipment list

(2) Air Data Computers (ADC) (Two must be operational)

(2) Altitude Reporting Transponders (One must be operational)

(1) Altitude Alerting System (Must be operational)

(1) Autopilot

53
Q

RVSM tolerances

A

RVSM tolerances

Total Vertical Error +/- 300 ft.

Altimetry System Error +/- 245 ft.

Assigned Altitude Deviation +/- 300 ft.

54
Q

Use of Temperature compensation

A

Use of Temperature compensation

The use of temperature compensation feature must be coordinated with ATC if Baro-VNAV operation is intended.

The use of temperature compensation feature is required if Baro-VNAV operation outside the temperature limits published on Approach
procedure chart is intended.

55
Q

APU max start temp (outside temp)

A

52C

56
Q

In the event of a Landing below ___, the airplane may not Takeoff without further maintenance inspection.

A

-40C

57
Q

Flaps load factor

A

Flaps Up -1.00g to 2.5 g

Flaps Down 0g to 2 .00g

58
Q

Fuel Specification

A

JP8

59
Q

Crossfeed Operation

A

Crossfeed Selector Knob must be set OFF during Takeoff and Landing

60
Q

The maximum N1 percentage with brakes applied is

A

60%

61
Q

For Flex - reduction must not exceed

A

The total thrust reduction must not exceed 25% of the full Takeoff thrust.

62
Q

Flex is prohibited on

A

Flex is prohibited on

Use of reduced Takeoff thrust procedures is not allowed on runways contaminated with standing water, slush, snow or ice and are not allowed on wet runways
unless suitable performance accountability is made for the increased stopping distance on the wet surface.

63
Q

The TO DATASET MENU on the MCDU must be set to ENG in the following cases when OAT is

A

The TO DATASET MENU on the MCDU must be set to ENG in the following cases when OAT is

between 5°C and 10°C and:
1. If there is any possibility of encountering visible moisture up to 1,700 ft AFE, or
2. When operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.

64
Q

The TO DATASET MENU on the MCDU must be set to ALL in the following cases when

A

The TO DATASET MENU on the MCDU must be set to ALL in the following cases when

OAT is below 5°C and:
1. If there is any possibility of encountering visible moisture up to 1,700 ft AFE, or
2. When operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.

65
Q

Steering degrees for steering handle and rudder

A

Steering degrees for steering handle and rudder

0 - 10kts 76 degrees
11 - 26kts 20 degrees
27 - 100kts 7 degrees (rudder)

66
Q

TOGA pitch bar range in degrees

A

TOGA pitch bar range in degrees
8 - 18 degrees

67
Q

Fuel low level warning occurs in each tank at what lbs?

A

Fuel low level warning occurs in each tank at what lbs?

660lbs

68
Q

turn radius for 180 degrees

A

turn radius for 180 degrees

59’ 2”

69
Q

aircraft dimensions

A

aircraft dimensions

height 32’ 4”
wing span 93’ 11”
length 103’ 11”

70
Q

IESS alignment time

A

90 sec

71
Q

GE CF34-8E5 max thrust

A

GE CF34-8E5 max thrust

13,000 - 14,200

72
Q

hydraulic temp limits

A

hydraulic temp limits

100C HYD HI TEMP EICAS
125C auto shutoff
145C HYD OVERHEAT EICAS

73
Q

Taxi speeds

A

Taxi speeds

straight/Dry 20
Turns/dry 10
straight/wet or contaminated 10
turns/wet or contaminated 5

74
Q

two engine out speed

A

two engine out speed

pitch for 250kts MINIMUM

75
Q

single engine drift down speed

A

single engine drift down speed

green dot

76
Q

green dot represents

A

green dot represents
1.3G over stick shaker speed

77
Q

Pitch angles for flap positions

A

Pitch angles for flap positions

Flaps 1 11 degrees
Flaps 2 10 degrees
Flaps 4 12 degrees

78
Q

radar altimeter comes alive at

A

radar altimeter comes alive at

2,500 AGL

79
Q

percent of recirculation air

52% fresh

A

percent of recirculation air

52% fresh
48% rec

80
Q

The APU oil capacity is

A

The APU oil capacity is
4.12 qt

81
Q

BATT 1 (2) OVERTEMP EICAS message will appear at what temp?

A

BATT 1 (2) OVERTEMP EICAS message will appear at what temp?
A
70C for 2 seconds

82
Q

Manuals and Documents (15 items)

A
  1. Jumpseat Briefing Card.
  2. Passenger Briefing Safety Information Cards.
  3. Passenger Count Card.
  4. TOLD Cards.
  5. 2 CAT II INFORMATION and CALLOUTS Cards.
  6. 2 ECS Off Takeoff checklist, Engine Battery Start checklists.
  7. 2 EPCs.
  8. 2 Icing Conditions, Cold Weather and Cold Soak Operations.
  9. 2 Lightning Strike, Turbulent Air Penetration, Hot Weather.
  10. 2 Normal Operations Checklist(s).
  11. Airworthiness Certificate and Registration.
  12. AML
  13. QRH
  14. Radio Station Certificate.
  15. W&B Manifest.
    3
83
Q

E-175 aircraft are Group ___ aircraft and require a minimum _____ ft of runway at
Sea Level.

A

E-175 aircraft are Group ___ aircraft and require a minimum _____ ft of runway at
Sea Level.

7
6,000

84
Q

emergency equipment (7)

A

Crash Axe (1)
Escape Ropes (2)
Fire Extinguisher (1)
Flashlights (2)
Life Vests (3)
Oxygen Masks (3)
PBE (1)

85
Q

Flight Kit items (12)

A

Airman Certificate

Extra Pair of Corrective Lenses* Only required if wearing corrective lenses

FCC Restricted Radio
Telephone Operating Permit

Flashlight

Jeppesen Inflight Pubs (EFB or Paper)

Log book

Medical Certificate

Mesa Airlines, Inc. ID Card

Passport

Pen

Required Manuals (EFB or Paper)

Training Folder Only required if in training

86
Q

considered stable approach

A

Stabilized Approach Criteria
1. Flights will be stabilized by 1,000 feet AFE.
2. An approach is considered to be stable when all of the following conditions are met:
a. All appropriate briefings and checklists have been accomplished.
b. The aircraft is in the planned landing configuration.
NOTE
The planned landing configuration is gear down and locked, final landing flaps, and flight spoilers are retracted.
c. The aircraft is on the correct track.
NOTE
The correct track includes normal maneuvering required to align with the final approach course. In VMC conditions this may include turns below 1,000 feet (AFE) but must be aligned by 500 feet (AFE). However, all of the criteria for stabilized approach must be met by 1,000 feet (AFE).
d. The aircraft is not more than the planned approach speed +10 KIAS, while correcting to the proper speed, and not less than VREF.
NOTE
Adjustments may be made for ground speed when applicable. Momentary excursions (deviations which last only a few seconds with every indication that it will return to a stabilized criteria) are acceptable.
e. The power setting is appropriate for the aircraft configuration.
NOTE
At no point except for rollout and flare should the thrust levers be reduced to idle below 1,000 feet AGL. If this occurs then a goaround is mandatory.
f. The rate of descent is no greater than 1,000 fpm.
NOTE
If an expected rate of descent greater than 1,000 fpm. is planned, a special approach briefing should be performed.
NOTE
If an unexpected sustained rate of descent greater than 1,000 fpm. is encountered during the approach, a missed approach or goaround should be performed.

g. After glidepath intercept, or after the FAF, the pilot flying (PF) requires no more than normal corrections to maintain the correct track and desired profile to landing within the touchdown zone.
NOTE
Normal bracketing corrections relate to bank angle of not more than 30°, rate of descent ±300 fpm. deviation from target, and power management in the range required to maintain a constant rate of descent and speed. Normal bracketing corrections occasionally involve momentary overshoots made necessary by atmospheric conditions. Such overshoots are acceptable. Frequent or sustained overshoots caused by poor pilot technique are not normal bracketing corrections.
–

175 E (21 decks)

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