SkyWest SV Questions with correct Answers

SkyWest SV Questions with correct Answers wing span 69 feet 8 inches length from nose to tail 87 feet 1 inch top of vert stab to ground 20 feet 8 inches danger area in front of engines at max thrust 25 feet max landing weight 47000 max zero fuel weight 44000 4 mx security seals (silver) TRU panels and aft equipment bay L 10th DUCT flashing master warning, triple chime, and voice advisory What caution messages warrant RTO REV UNLOCK SMOKE TOILET AC 1 AUTOXFER caution message accompanied by flashing amber master caution light and single chime ECP buttons used to box caution and status messages cas and stat EICAS (ED1) fails, how do you display synoptic pages on EICAS (ED2) SSP on lower pedestal must be used. point SSP knob to operative display then use ECP as required QRH calls for ECS page display for cross bleed start. How do you display status page and ecs page at the same time select ecs on ED2 then select DRP to EICAS ECP microprocessor fails, what 4 buttons remain active? PRI, CAS, STAT, STEP What ECP button moves between multiple pages of caution messages? CAS DC SERVICE switch is on, what is available? navs, lavs, limited flight deck and cabin lighting green AVAIL on AC external switchlight means proper phase, frequency, and voltage Amber IDG 1 caution message indicates HOTLOP IDG 1 or IDG 2 caution message is displayed does the IDG still generate power? yes pressing the AC ESS BUS does what? change power source of AC ESS BUS after pressing AUTO XFER, AUTOXFER OFF status message appears. what does it mean AC ESS BUS - AC BUS 2. power priority is inhibited AC power priority on side, apu, off side, external DC bus tie that is never automatic 3. ESS tie constant speed drive portion of IDG provides means of converting variable engine speed to constant generator speed the 15 KVA ADG supplies AC power to Hyd pump 3B and Ac essential bus AC BUS 2 shorts and AC 2 AUTOXFER message appears. What mus tbe done to re-establish power to AC BUS 2? Can't if the system automatically transfers If AC 2 AUTOXFER appears what are the total AC and DC busses unpowered? 6, AC UTIL 1,2 AC SERVICE, AC BUS 2, DC UTIL BUS 1,2 criteria for auto ADG deploy loss of all AC, last internal AC source, WOW, parking brake off why does EMER PWR ONLY checklist direct pilot to pull ADG handle power is lost when ADG spools down if handle isn't pulled so reverses won't deploy. AFTER TAKEOFF CHECK following bleeds closed departure, sequence for changing bleed source R 10, ISOL, L 10, APU LCV cooling for pack heat exchangers is supplied by ram air pushing pressurization control switch light once = manual mode twice = switches to opposite CPC Manual pressurization, readouts are displayed on what pages EICAS - pri, stat, ecs "Cabin Pressure" aural warning heard cabin altitude greater than 10,000 What valves automatically close with L (R) PACK HI PRESS caution message with engine supplying bleed air? ISOL, pack valve, association 10th stage bleed BLEED MISCONFIG occurs when wing and/or cowl anti-ice on and engines supplying 10th stage bleed air with gear and/or flaps extended outflow valves supplied with pneumatic energy from 10th stage air during engine starts, what two valves automatically close L and R pack PRSOVs if hydro switches in AUTO and ON, when to ACMP 1B and 2B turn on? flaps selected out of 0 with associated IDG's online which ACMP can be directly powered by adg 3B normal hydro pump switch position 1B, 2B, 3B all in AUTO and 3A on IF AUTO function of a hyd B pump is deferred crew must turn it on for TO and LDG how are hydro 1 and 2 cooled? ram air what would you do if HYD 1 LO PRESS and HYD 2 LO PRESS cautions displayed at the same time? combined procedure