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Skywest ERJ 175 Limitations Test With Complete Solution., Exams of Law

Skywest ERJ 175 Limitations Test With Complete Solution.

Typology: Exams

2024/2025

Available from 07/05/2025

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Skywest ERJ 175 Limitations Test
With Complete Solution
Max Ramp Weight LR, LL - ANSWER LR 85,870 lb, LL 85450
Max T/O Weight LR,LL - ANSWER LR 85,517 lb, LL 85098
Max LND Weight LR, LL - ANSWER LR 74,957 lb, LL 74957
Max ZERO Fuel Weight LR, LL - ANSWER LR 69,886 lb, LL 69467
Min RWY Width - ANSWER 100' (8 stripes)
Wing span - ANSWER 93' 11"
Aircraft length - ANSWER 103' 11"
Tail height - ANSWER 32' 4"
Max Ops Alt - ANSWER 41,000 ft
Max ALT T/O & LND - ANSWER 10,000 ft
Max Temp TO/LND - ANSWER ISA + 35*C (52*C)
Min Temp TO/LND - ANSWER -40*C
RWY Slope - ANSWER +/- 2%
Max Tailwind - ANSWER 15
Max 1 Pack Opperations - ANSWER 31,000 ft
Vmo (SL-8000) - ANSWER 300
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Skywest ERJ 1 75 Limitations Test

With Complete Solution

Max Ramp Weight LR, LL - ANSWER LR 85,870 lb, LL 85450 Max T/O Weight LR,LL - ANSWER LR 85,517 lb, LL 85098 Max LND Weight LR, LL - ANSWER LR 74,957 lb, LL 74957 Max ZERO Fuel Weight LR, LL - ANSWER LR 69,886 lb, LL 69467 Min RWY Width - ANSWER 100' (8 stripes) Wing span - ANSWER 93' 11" Aircraft length - ANSWER 103' 11" Tail height - ANSWER 32' 4" Max Ops Alt - ANSWER 41,000 ft Max ALT T/O & LND - ANSWER 10,000 ft Max Temp TO/LND - ANSWER ISA + 35C (52C) Min Temp TO/LND - ANSWER -40*C RWY Slope - ANSWER +/- 2% Max Tailwind - ANSWER 15 Max 1 Pack Opperations - ANSWER 31,000 ft Vmo (SL-8000) - ANSWER 300

V RAT Deploy MAX - ANSWER Vmo/MMO

  • Vmo (10,000- Mach Trans) - ANSWER
  • MMO - ANSWER.
  • Va - ANSWER
  • Vlo EXT - ANSWER
  • Vle RET - ANSWER
  • Vle - ANSWER
  • V tire - ANSWER
  • (To Provide Electrical Power) - ANSWER Vmin
  • Vb (below 10,000ft) - ANSWER
  • V wiper ops MAX - ANSWER Vb (above 10,000ft) - ANSWER 270 / .76M (lowest)
  • V window - ANSWER
  • Vfe 1 - ANSWER
  • Vfe 2 - ANSWER
  • Vfe 3 - ANSWER
  • Vfe 4 - ANSWER
  • Vfe 5 - ANSWER
  • Vfe FULL - ANSWER

Engine Start 3 - 5 Crank Limits (FLT) - ANSWER 120 sec ON / 5 min OFF Dry Motoring Duty Cycle Limits #1 - ANSWER 90 sec ON / 5 min OFF Dry Motoring Duty Cycle Limits #2 - 5 - ANSWER 30 sec ON / 5 min OFF Dry Motoring Duty Cycle Limits after 5 - ANSWER 15 min cool down limit When necessary to perform an engine start with tailwind, monitor _ - ANSWER N1 / verify N1 increase before starter cutoff (50% N2). If no N indication engine must be manually aborted T/O with Automatic Takeoff Thrust Control System (ATTCS) OFF is ___. - ANSWER Not Authorized.

Max Fuel Capacity - ANSWER 20,935 lbs

Max Imbalance - ANSWER 794 lbs

Min Fuel Tank Temp - ANSWER -37c

What is max Fuel imbalance before landing - ANSWER 794 lbs

Fuel XFeed must be selected __ during T/O and LND - ANSWER OFF

Wait __ after EICAS is energized to start the APU - ANSWER 30 sec

Do not leave the A/C unattended more than __ with APU running - ANSWER 5 minutes

Simultaneous use of __ is prohibited. - ANSWER APU bleed and HP cart

APU starter Duty cycle starter attempt 1 & 2 - ANSWER 60 sec OFF

APU Starter Duty Cycle Starter Attempt 3 - ANSWER 5 min OFF

APU Start Temp - ANSWER -54*C - ISA +

APU Start Alt - ANSWER 30,

Apu engine start - ANSWER 21,

APU Cont Opp Temp - ANSWER -54C - ISA +35 (52C)

APU Cont Opp Alt - ANSWER 33,000 ft

After selecting reverse thrust , do not move thrust levers into the forward range until the __ - ANSWER REV icon on the EICAS is shown in Amber or green.

The use of thrust reversers during normal taxi operations and power back operations is__ - ANSWER Prohibited

There is __ temp limit for anti-icing system automatic operation. - ANSWER No

ADS probes on when - ANSWER 0 degrees c & visible moisture, contaminated probes, faults or indications

Icing conditions may exist whenever OAT on the GND or before TO or Total Air Temp (TAT) in flight, is__. Icing conditions may also exist when OAT on the GND and for TO is __. - ANSWER 10*C or bellow and visible moisture in any form

&

10*C or bellow when operating on ramps, taxiways, runways where surface

snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles, or engine sensor probes

Min engaged AP alt - ANSWER 400 ft

Min use AP ALT - ANSWER 50 ft

Min use AP alt NP-APP - ANSWER MDA

TAS, TAT and SAT info are only valid above - ANSWER 60 kts

While transmitting in VHF 1, ____. - ANSWER STBY MAG Compass is Not valid

Baro ALT MINS must be used for all __ APP. - ANSWER CAT l

Navigation is not to be predicated on the use of - ANSWER Terrain Awareness System

The use of predictive EGPWS function should be manually inhibited when __.

  • ANSWER landing at an airport that is not in the database to avoid unwanted alerts