Term
| What category is the Saab 340 certified? |
|
Definition
| Transport category ..... FAR part 25 |
|
|
Term
| Where are Master Warning/Caution annunciator lights located? |
|
Definition
| CWP (Central Warning Panel) and glareshield panel |
|
|
Term
| "OXYGEN" light on the CWP indicates __? |
|
Definition
| Oxygen system pressure is below 800 psi (+/-35) |
|
|
Term
| Oxygen(O2) gauge in cockpit indicates __? |
|
Definition
| Fixed oxygen bottle pressure |
|
|
Term
| How is OXYGEN made available to the passenger? |
|
Definition
| Pull O2 ON/OFF handle & lift pax O2 valve lever |
|
|
Term
| Normal charging pressure in O2 bottle? |
|
Definition
|
|
Term
| What is normal O2 pressure reduced to? |
|
Definition
| 70 psi in pressure regulator |
|
|
Term
| The crew escape hatch may be opened at __ knots max? |
|
Definition
|
|
Term
| Reason to open crew hatch in flight? |
|
Definition
|
|
Term
| Which aircraft doors are connected to door warning system? (3) |
|
Definition
Crew escape hatch;
Main entrance;
Cargo door. |
|
|
Term
| Emergency exits may be opened from interior or exterior T/F. |
|
Definition
|
|
Term
| Can cargo door be operated from inside the aircraft? |
|
Definition
|
|
Term
| What supplies the pneumatic system? |
|
Definition
| High & Low pressure engine bld air, ALTERNATELY |
|
|
Term
| Pneumatic air operates which systems? (3) |
|
Definition
Air conditioning;
Pressurization;
Boot de-icing. |
|
|
Term
| LP bld air is NORMAL source for pneumatics T/F. |
|
Definition
|
|
Term
| When is the ONLY time HP bld air is AUTOMATICALLY supplied? |
|
Definition
| If LP bld air is insufficient (Ng below approx. 80%) |
|
|
Term
| When will the high pressure (HP) bld valve close? (5) |
|
Definition
Bld air temp (after precooler) > 288° C;
HP valve switch OFF;
Fire handle pulled;
Loss of elec. pwr.;
N g > 80% (approx.) |
|
|
Term
| How do you reopen HP bld valve after air temp drops below 288° C? |
|
Definition
| HP valve switch to RESET and then to AUTO |
|
|
Term
| What does an overhead "L HP HIGH" light indicate? |
|
Definition
| Left HP bld valve failed to close after a close signal |
|
|
Term
| Overhead "L/R HP HIGH" light illuminates with which other light? |
|
Definition
| "AIR COND" light on the Central Warning Panel (CWP) |
|
|
Term
| Low & High pressure bld valves are electrically actuated T/F. |
|
Definition
|
|
Term
| Bld valve switch on NC panel placed in AUTO means __? |
|
Definition
| Valve automatically regulates air to manifold as function of altitude |
|
|
Term
| When will the Bld Valve close? (6) |
|
Definition
Bld air temp>288° C;
Bld valve switch OFF;
Fire handle pulled;
Regulated pressure > 43.5 psi;
Pack discharge temp > 225° C;
Duct temp > 82° C. |
|
|
Term
| What indicates Bld Valve failed to close after close signal? |
|
Definition
| Overhead "BLD FAULT" light (plus "AIR COND" light on CWP) |
|
|
Term
| What indicates a closed Bld Valve? |
|
Definition
| Overhead "BLD CLOSED" light (plus "AIR COND" light on CWP) |
|
|
Term
| "BLD FAULT" light illuminated may indicate __? (3) |
|
Definition
Bld air temp too high;
Regulated pressure exceeds limits;
Valve failed to close. |
|
|
Term
| When will the "BLD FAULT" light extinguish? |
|
Definition
| When temp or pressure is below limits, after valve has closed |
|
|
Term
| Main use of the air precooler __? |
|
Definition
| Lowers HP bld air temp and cools air to the boots |
|
|
Term
| If elec pwr to Bld Valve fails, it fails in the __ position? |
|
Definition
| Open (HP valve fails to CLOSED position) |
|
|
Term
| How is it possible to interconnect the 2 bleed systems? |
|
Definition
| A Cross Valve (X valve) in the manifold |
|
|
Term
| The X valve may be opened below 10,000 feet T/F. |
|
Definition
| False (open only on the ground) |
|
|
Term
| What is required to open the bleed air X valve? |
|
Definition
| X valve switch to OPEN & one bld valve closed |
|
|
Term
| What indicates a hot bleed air leak? |
|
Definition
| Overhead "BLD AIR LEAK" light (plus "AIR COND" Lt. on CWP) |
|
|
Term
| Where is the hot air leak detection loop installed? |
|
Definition
| Between the engine nacelles and the X valve |
|
|
Term
| An overhead "L/R DUCT OV TEMP" light indicates __? |
|
Definition
Pack compressor outlet temp > 225° C
or duct temp> 82° C |
|
|
Term
| When will the "AIR COND" light on the CWP illuminate? (4) |
|
Definition
Bld air leak;
Bld air temp too high;
Bld valve closed;
LP/HP valve not closed after a close signal |
|
|
Term
| Will a bld leak close the LP Bleed Valve? |
|
Definition
|
|
Term
| "Recirc Fan" light illuminated indicates __? |
|
Definition
| Fan operating less than 80% |
|
|
Term
| Will the Recirc Fan light extinguish when switch is turned ON? |
|
Definition
| Not until the fan is above 80%, so not immediately. |
|
|
Term
| What cools the Recirc Fan? |
|
Definition
|
|
Term
| When can the Recirc Fan operate without bld air? |
|
Definition
| During takeoff, up to acceleration altitude |
|
|
Term
| What is indicated by illumination of "AVIONICS VENT" light? |
|
Definition
|
|
Term
| X valve can be used in flight to power both A/C packs T/F. |
|
Definition
| False (only allowed to open on the ground) |
|
|
Term
| What is indicated by the "CABIN PRESS" light on the CWP ? |
|
Definition
Cabin altitude above 10,000 ft. or
Cabin pressure > 7.5 psi |
|
|
Term
| What controls the outflow valves? |
|
Definition
|
|
Term
| The avionics rack ventilation fan draws air from the ___? |
|
Definition
|
|
Term
| A/C temp select switch in AUTO provides what temp range? |
|
Definition
|
|
Term
| "FAULT" light on the overhead cabin pressure control panel indicates? |
|
Definition
| A system failure or ON for 3 seconds during system self test |
|
|
Term
| "AIR COND" light on CWP comes on with any caution light, except __? |
|
Definition
|
|
Term
| "AUTO TRIM" light on CWP indicates __? Red or Amber? |
|
Definition
AP detects a failure in AP or FD auto trim.
Red Warning! |
|
|
Term
| Will the autopilot operate if the flight director fails? |
|
Definition
|
|
Term
| Will the AP operate if the FD indicators are turned OFF? |
|
Definition
|
|
Term
| Yaw Damper can be engaged with or without the AP T/F. |
|
Definition
|
|
Term
| Go-Around displays a pitch command of __ degrees on the ____? |
|
Definition
|
|
Term
| When is 1/2 Bank mode inhibited? |
|
Definition
| During Approach mode (after APPR LOC/VOR capture) |
|
|
Term
| What are the 1/2 Bank limits? |
|
Definition
| Reduces bank from 27° to 13.5° in HDG & NAV mode |
|
|
Term
| Is 1/2 Bank annunciated in left or right corner on EADI ? |
|
Definition
| Neither (no annunciator for 1/2 Bank) |
|
|
Term
| Will the APPR mode track a VOR? |
|
Definition
| Yes, but it will be twice as sensitive |
|
|
Term
| What are the Climb mode speeds? |
|
Definition
Low - 140 kts
Medium - 160 kts
High - 182 kts |
|
|
Term
| Which modes on MSP should NOT be selected in icing cond's? |
|
Definition
|
|
Term
| Does the GA mode disconnect the AP? |
|
Definition
|
|
Term
| Does the GA mode disconnect the YD? |
|
Definition
|
|
Term
| Does the GA mode disconnect the FD? |
|
Definition
|
|
Term
| Which mode on MSP is approved in icing conditions? |
|
Definition
|
|
Term
| Flight Director PTCH mode operates as part of which mode? |
|
Definition
| Only operates in GA mode (A reversing of the GA mode) |
|
|
Term
| What turns the AP off? (4) |
|
Definition
AP disconnect on control wheel;
AP/YD switches to OFF;
Selecting GA on power levers;
Operating Pitch Trim switches. |
|
|
Term
| What turns the YD off? (3) |
|
Definition
AP disconnect on control wheel;
AP/YD switches to OFF;
Selecting GA on power levers. |
|
|
Term
|
Definition
| It doesn't turn off, only turns off FD indications (V Bars) |
|
|
Term
| A flashing Red box w/FD letters displayed on EFIS indicates ____? |
|
Definition
| Failure of the flight director (V-bars also disappear) |
|
|
Term
|
Definition
Not authorized below 200 AGL on T/O or GA;
Speeds below 1.3 X stall speed in HDG mode;
Above Vmo/Mmo |
|
|
Term
| What AUTOMATICALLY disengages the AP/YD ? |
|
Definition
| Stall warning computer or AP/YD failure detected |
|
|
Term
| The FD has 8 vertical, 2 lateral and 2 combined modes T/F. |
|
Definition
|
|
Term
| How is the PTCH mode engaged ? |
|
Definition
| VERT SYNC button pressed & released in the GA mode |
|
|
Term
| VERT SYNC works with which lateral modes? |
|
Definition
| None (This is NOT a trick question) |
|
|
Term
| VERT SYNC works with which vertical modes? |
|
Definition
|
|
Term
| AP will disconnect if VERT SYNC is pressed in IAS mode T/F. |
|
Definition
|
|
Term
| Two ways to manually move HDG bug? |
|
Definition
| HDG knob on Course Hdg Panel (CHP) or TURN knob on the APP |
|
|
Term
| Basic FD modes that are displayed at power up? (2) |
|
Definition
|
|
Term
| The FD's NAV mode includes VOR, LOC, ILS, & BC tracking T/F. |
|
Definition
| False (Not ILS: GS is inhibited in NAV mode) |
|
|
Term
| Armed (selected) FD modes are annunciated on EADI in ___? |
|
Definition
|
|
Term
| Captured (active) FD modes are annunciated on EADI in ____? |
|
Definition
|
|
Term
| All lateral FD modes, when selected, annunciate on EADI T/F. |
|
Definition
| False (1/2 Bank is not shown) |
|
|
Term
| Pressing the APPR mode button prior to the approach,immediately will suppress the 1/2 Bank mode. T/F. |
|
Definition
| False (not suppressed until LOC/VOR capture) |
|
|
Term
| APPR mode functions are the same as NAV mode functions, except ___? |
|
Definition
| APPR captures & tracks a vertical ILS GS if available |
|
|
Term
| Radio altimeter is utilized by FD's APPR mode during ILS T/F. |
|
Definition
| True (Uses RA information for increased precision) |
|
|
Term
| Can you use the HDG bug after pressing APPR or NAV on MSP? |
|
Definition
| Yes. Until LOC or VOR shows "CAP" (captured) in green. |
|
|
Term
| What indicates the FD is set for a BC (back course) approach? |
|
Definition
| Yellow B/C light comes on replacing the GS pointer & scale on the EADI and EHSI |
|
|
Term
| VOR approach has tighter gains in APPR mode than NAV mode T/F. |
|
Definition
|
|
Term
| In APPR mode, BC has slightly less gains than in LOC mode T/F. |
|
Definition
|
|
Term
| GA clears previously selected FD vertical modes ONLY T/F. |
|
Definition
| False (clears both vertical & lateral) |
|
|
Term
| Selecting GA disengages the AP ,FD & YD. T/F. |
|
Definition
|
|
Term
| When is Diagnostic Mode available using EFIS Test Panel #2 ? |
|
Definition
| Only on the ground with AP & YD off AND before power shutdown. |
|
|
Term
| How do you clear NAV mode? |
|
Definition
|
|
Term
| What is the ONLY button on MSP used as both ON & OFF? |
|
Definition
|
|
Term
| Purpose of the "NAVS L/R" button light on the glareshield? Red, Green or Amber? |
|
Definition
| Used to couple L or R navigation source to AP/FD. Green Lt. |
|
|
Term
| A green box w/letters AP on upper left of EFIS turns Red & flashes, indicating __? |
|
Definition
|
|
Term
| What is indicated by a yellow EL, AIL or RUD on left lower corner of EFIS? |
|
Definition
| Elevator, Aileron or Rudder mistrim detected, indicating difficulties in trimming out control forces |
|
|
Term
| Lower left side of EFIS, a flashing yellow FD indicates ___? |
|
Definition
| FD comparator caution (Difference of more than 5°) |
|
|
Term
| How is the FD comparator caution reset? |
|
Definition
| Pressing Master Caution button |
|
|
Term
| Purpose for emergency switch on the audio panel? |
|
Definition
| Direct connect to COM (bypass REU if audio system fails) |
|
|
Term
| Communications are recorded by CVR, including PTT signals T/F. |
|
Definition
| False (PTT signals for the COM's are recorded by FDR) |
|
|
Term
| What bus powers the L & R Audio Control Panels (ACP)? |
|
Definition
|
|
Term
| GPWS & PA chime audio levels are adjusted on the ACP T/F. |
|
Definition
| False (fixed audio levels) |
|
|
Term
| Engine oil press controls 1 of 2 PA fixed audio levels T/F. |
|
Definition
| True (increased for engine/prop noice compensation) |
|
|
Term
| What indicates a ground crew headset is connected in nose? |
|
Definition
| Plain "White" light on the overhead Ground Status Panel. |
|
|
Term
| VHF#1 is powered by __ bus? |
|
Definition
|
|
Term
| VHF#2 is powered by __ bus? |
|
Definition
|
|
Term
| Red "EMER" light on overhead Cabin Sign Panel, indicates ____? |
|
Definition
| Flight Attendant Emergency Call (comes on flashing red) |
|
|
Term
| What indicates the Flt. Attendant has called the cockpit? |
|
Definition
| Hi-low chime & amber light on overhead cabin signal panel |
|
|
Term
| Name the four separate parts of the electrical power system. |
|
Definition
28V DC;
l15/26V AC;
Emergency DC power;
"Wild" freq. 115V AC |
|
|
Term
| 28V DC system's power source? |
|
Definition
| Two engine generators, two batteries or external power source |
|
|
Term
| Frequency controlled 115/26V AC system's power source? |
|
Definition
| Two 115/26V AC inverters powered by the DC system |
|
|
Term
| Emergency power system's power source? |
|
Definition
| Pwr'd from ordinary DC system or an emergency power battery |
|
|
Term
| "Wild" frequency 115V AC system's power source? |
|
Definition
| Powered from two engine driven AC generators |
|
|
Term
| The 28V DC system is split into a L/R system, each with one generator and one battery T/F. |
|
Definition
|
|
Term
| "Wild" frequency 115V AC is primarily used for __? |
|
Definition
| Ice protection (Only used for Ice Prot. on some aircraft) |
|
|
Term
| What drives the Wild frequency AC generators? |
|
Definition
| Driven by respective propeller gearbox |
|
|
Term
| How are the DC generators cooled? |
|
Definition
| Fan on the ground and ram air when airborne |
|
|
Term
| An overhead "GEN OV TEMP" light indicates ___? |
|
Definition
| Generator is overheated (150° C ) |
|
|
Term
| What is indicated by illumination of "L/R MAIN BUS" light? |
|
Definition
| Associated bus is not powered |
|
|
Term
| What AC power is lost when the "L MAIN BUS" is not powered? |
|
Definition
| Loss of the #1 or Main 115/26V inverter |
|
|
Term
| When will you see a "L/R MAIN BUS" light? |
|
Definition
| During engine start when L/R Gen Busses are battery powered or when Main Bus relay has tripped due to a tripped generator |
|
|
Term
| What is indicated by illumination of "L/R GEN" light? |
|
Definition
| Gen relay open disconnecting Gen from Gen Bus (Gen offline) |
|
|
Term
| The 2 starter/generators are rated at __ volts each? |
|
Definition
|
|
Term
| How many alternators on each engine? (Not a trick question) |
|
Definition
| One (provides ENGINE electrical power ONLY) |
|
|
Term
| How many generators on each engine? |
|
Definition
| Two (starter/generator & "wild" frequency AC gen) |
|
|
Term
| What does the GCU provide for the starter/generator? (3) |
|
Definition
Excites field;
Voltage reg. for control & protection of DC system against faults;
Controls engine start cycle. |
|
|
Term
| How does the GCU control & protect the DC system? |
|
Definition
| If generator parameter is not correct or if fire handle is pulled, the GCU cuts out generator by opening field relay & disconnects generator from GEN BUS by opening generator relay |
|
|
Term
| The starter/generators are rated at ___ amps each? |
|
Definition
|
|
Term
| Max starter/generator amp limits ___? |
|
Definition
| 600 amps for 5 minutes, then 400 amps |
|
|
Term
| How is GEN field relay reset? |
|
Definition
| Respective GEN switch to reset |
|
|
Term
| To connect generator to GEN BUS, Ng must be above ___? |
|
Definition
|
|
Term
| What is indicated by illumination of "L/R ESS BUS" light? |
|
Definition
| Associated bus is not powered |
|
|
Term
| What is indicated by illumination of "L/R BAT" light? |
|
Definition
| Associated battery relay is open (battery disconnected) |
|
|
Term
| What is indicated by illumination of "L/R BAT HOT" light? |
|
Definition
| Associated battery temp is excessive, over 71° C |
|
|
Term
| Takeoff is prohibited with "L/R BAT HOT" light ON T/F. |
|
Definition
|
|
Term
| Takeoffis prohibited when battery temp is 67° C and the "L/R BAT HOT" light is NOT on T/F. |
|
Definition
| True (T.O. is prohibited if batt temp>64° C) |
|
|
Term
| What is indicated by illumination of "NO BAT START" light? |
|
Definition
| L or R battery temp exceeds 57° C |
|
|
Term
| Takeoff is prohibited with "NO BAT START" light on T/F. |
|
Definition
| False (unless battery temp exceeds 64° C) |
|
|
Term
| A battery temp > 71° C, AUTOMATICALLY disconnects battery T/F. |
|
Definition
|
|
Term
| To read external power, the Ext Pwr switch must be ON T/F. |
|
Definition
|
|
Term
"EXT PWR AVAIL" light on gnd status panel indicates __ ?
Blue,White or Red light? |
|
Definition
| External power connected & available. Blue light |
|
|
Term
"EXT PWR ON" light on DC Elec Panel indicates ___?
Blue, White, or Red light? |
|
Definition
| Ext. pwr. switched on & left battery bus powered. White Lt. |
|
|
Term
| "EMER PWR" light on DC Elec Panel indicates ___? |
|
Definition
| Emergency power less than 24 volts. Emergency bus not powered |
|
|
Term
| Can the 71° C (Bat Hot) thermal switch be overridden? |
|
Definition
| In Emer situation: BAT switch to OVRD assures pwr to GEN BUS |
|
|
Term
| "INVERTER" light on AC Elec Panel indicates __ ? |
|
Definition
| Selected inverter failed or inverter switch in OFF position |
|
|
Term
| "L/R AC GEN" light on Engine Anti-Ice Panel indicates __ ? |
|
Definition
| AC generator not supplying power |
|
|
Term
| Will the CWP "ELEC" Lt. come ON with a L/R AC GEN light? |
|
Definition
| No (The "ICE PROT" light does) |
|
|
Term
| How many 24V batteries on the aircraft ? |
|
Definition
| Three including emergency battery |
|
|
Term
| Will the battery automatically disconnect with "BAT HOT" light? |
|
Definition
|
|
Term
| What is indicated by illumination of "BUS TIE CONN" light? |
|
Definition
| Bus tie connected closed. (L & R GEN BUS connected) |
|
|
Term
| Three reasons the bus tie relay closes? |
|
Definition
To supply L & R GEN BUS when ext pwr is on;
To enable power supply to both L & R GEN BUS from only one generator;
To connect the two main batteries. |
|
|
Term
| Purpose of the bus tie over-current relay ___? |
|
Definition
| Protects the Main Distribution system in case of a short |
|
|
Term
| Bus tie relay OPENS if the over-current exceeds ___? |
|
Definition
|
|
Term
| Can the bus tie over-current be reset manually? |
|
Definition
| Yes, by pressing K-l on the Captain's C.B. panel |
|
|
Term
| Is there any time the 800 amp over-current relay can be EXCEEDED? |
|
Definition
| Yes. Over-current PROTECTION occurs during engine start |
|
|
Term
| Generators automatically disconnect with Ext Pwr ON T/F . |
|
Definition
|
|
Term
| What can be powered by the emergency battery? (5) |
|
Definition
Master warning;
Bus tie relay CONN;
Fire detection;
Tailpipe Hot detection;
Emergency voltage indication. |
|
|
Term
| During preflight, all exterior lighting may be checked while using battery power T/F. |
|
Definition
|
|
Term
| What is required to close the Utility Bus relay (RCCB)? |
|
Definition
| External power ON or both generators ON |
|
|
Term
| Is Ext Pwr connected to R GEN BUS through the Bus Tie Relay? |
|
Definition
|
|
Term
| How is battery compartment ventilated? |
|
Definition
| Fan on the ground. Ram air in flight |
|
|
Term
| Will Ext Pwr de-energize the battery relays? |
|
Definition
| Yes, unless the battery switches are in OVRD |
|
|
Term
| R Hot Battery Bus can be de-energized from the cockpit T/F . |
|
Definition
|
|
Term
| When a generator relay closes, which bus is powered? |
|
Definition
|
|
Term
| Three conditions to be met for generator relay to close __? |
|
Definition
Ext Pwr relay open;
Engine start complete;
Gen field reset. |
|
|
Term
| Below ____ volts, ext pwr drops off line & switch moves to OFF? |
|
Definition
|
|
Term
| What is the lowest ext pwr voltage during engine start ? |
|
Definition
|
|
Term
| During engine start, if ext pwr drops off line will start continue? |
|
Definition
| Yes, it will continue on batteries |
|
|
Term
| Left battery is connected to the __ bus? |
|
Definition
|
|
Term
| What bus charges batteries? |
|
Definition
| Respective GEN BUS with at least ONE generator on line |
|
|
Term
| Right battery is connected to the __ bus? |
|
Definition
|
|
Term
| What powers the EMERGENCY BUS? |
|
Definition
| L BATT BUS (batteries MUST be ON/OVRD) or Emergency battery |
|
|
Term
| When does emergency battery begin to power EMERGENCY BUS? |
|
Definition
| When the L BAT BUS drops below 24 volts |
|
|
Term
| What powers the EMER AVIONlCS BUS? |
|
Definition
| EMERGENCY BUS, when the ESS A VION switch is ON |
|
|
Term
| What items are on the EMER AVIONIC BUS? |
|
Definition
|
|
Term
| Minimum Prop RPM to keep "Wild" freq. AC Generator on line ____? |
|
Definition
|
|
Term
| Why is it called a "Wild" frequency AC system? |
|
Definition
| Frequency varies, 460 to 640 Hz due to prop rpm variations |
|
|
Term
| Taxiing out, one reason you might see a L/R AC GEN light? |
|
Definition
|
|
Term
| How do you RESET an AC Generator if prop rpm drops below 1000? |
|
Definition
| It is automatic & light goes out when prop rpm goes above 1000 |
|
|
Term
| What items are powered by the 115V AC GEN BUSSES? (6) |
|
Definition
Prop de-ice;
Windshield heat;
Pilot heat;
AOA sensor heat;
OAT probe heat (R Bus);
Gallery jug heating on some aircraft
(L Bus) |
|
|
Term
| Is engine intake anti-ice powered by 115V AC L/R Generator? |
|
Definition
| Yes. Powered directly from Generators, NOT from GEN BUS |
|
|
Term
| Three conditions to be met for battery relay to close? |
|
Definition
| Batt switches ON, Ext pwr OFF, Battery temp below 71° C |
|
|
Term
"AVIONIC SMOKE" light on CWP indicates __?
Red or Amber? |
|
Definition
| Smoke is detected in avionics area. RED Master Warning. |
|
|
Term
| "LAV SMOKE" light on CWP indicates __? Red or Amber? |
|
Definition
| Smoke is detected in lavatory area. RED Master Warning. |
|
|
Term
| "CARGO SMOKE" light on CWP indicates __? Red or Amber? |
|
Definition
| Smoke is detected in cargo area. RED Master Warning. |
|
|
Term
| How long will the Avionic, Lav or Cargo Smoke lts. stay on ? |
|
Definition
| As long as the smoke condition exists |
|
|
Term
| How long will the "L/R ENG FIRE" light remain illuminated? |
|
Definition
| As long as the fire exists |
|
|
Term
| "L/R FIRE DET FAIL" light on CWP indicates __? |
|
Definition
| Short circuited engine fire detection loop. |
|
|
Term
| How long will the "L/R FIRE DET FAIL" light remain on ? |
|
Definition
| Until the loop is replaced |
|
|
Term
| "L/R TAIL P HOT" light on CWP indicates __? Red or Amber? |
|
Definition
| Associated tail pipe overtemp. Red Master Warning. |
|
|
Term
| Actions required to discharge either engine fire bottle __? |
|
Definition
| Pull L/R Fire T-handle & engage respective FIRE EXTG switch |
|
|
Term
| Pressing "LAV SMOKE" lt. discharges overhead fire extg T/F. |
|
Definition
|
|
Term
| Overhead "CARGO EXTG" light indicates __? Red, White or Amber light |
|
Definition
| Pressure has dropped below 310-260 in inner bottle. White Lt |
|
|
Term
| MINIMUM time between firing cargo extinguisher #1 & #2? |
|
Definition
|
|
Term
| Normal wait time before firing cargo extinguisher #2 ? |
|
Definition
|
|
Term
| When Cargo Extg is activated, will "CARGO EXTG" light come ON? |
|
Definition
| Not immediately. May take up to 15 minutes. |
|
|
Term
| What results when the fire handle is pulled? (6) |
|
Definition
Bleed valves closed;
Gen relay open (offline);
WEU reset;
Fuel valve closed;
Squibs armed;
Fire bell cancelled. |
|
|
Term
| R Engine fire bottle can be discharged into LEFT nacelle T/F. |
|
Definition
|
|
Term
| What does the right pitot tube supply? |
|
Definition
| The co-pilot's instruments |
|
|
Term
| Maximum radio altimeter altitude indication is ____? |
|
Definition
|
|
Term
| Altitude alert sounds a 2 second C-cord & Amber light at _? |
|
Definition
| 1000 & 200 feet from set altitude |
|
|
Term
| AHRS initialization requires approx. __ seconds? |
|
Definition
|
|
Term
| Best time for AHRS initialization is during taxi to RWY T/F . |
|
Definition
| False (aircraft MUST NOT be moved during initialization) |
|
|
Term
| Disagreement of more than __ degrees between the EADls & the Standby Attitude Indicator is a grounding item. |
|
Definition
|
|
Term
| Does the Air Data Computer operate L & R flight instruments? |
|
Definition
|
|
Term
| Is the auto pilot lost if ADC fails? |
|
Definition
|
|
Term
| Four AHRS initialization conditions to be met prior to T/O? |
|
Definition
Background visible & correct;
No warning flags;
Attitude within 30 on all indicators;
Heading on compass card not slewing away from aircraft heading. |
|
|
Term
| What is indicated by illumination of "STBY PITOT" light? |
|
Definition
| Pitot heat is inoperative |
|
|
Term
| If the overhead STBY PITOT light comes on, you MAY also get a "RUDDER LIMITER" and/or "CABIN PRESS" light on the CWP T/F. |
|
Definition
|
|
Term
| Warning flag on the left ASI indicates __? Red or Amber? |
|
Definition
Test button pressed, IAS indicator failed or Loss of airspeed data from ADC.
Red flag |
|
|
Term
| What do red dashes indicate on upper left corner of EHSI? |
|
Definition
| ADC speed information has failed |
|
|
Term
| Cockpit Voice Recorder can be erased provided __ & __? |
|
Definition
| Aircraft on the ground & gust lock set |
|
|
Term
| CVR records continuously after _ & __ switches are ON? |
|
Definition
| Left Battery & Ess Avionics switches |
|
|
Term
| What should be done if EADI fails (tube is blank)? |
|
Definition
|
|
Term
| Which flight instruments operate if primary electric fails? |
|
Definition
| Standby attitude indicator, #1 VHF and standby altimeter |
|
|
Term
| What is seen if right DPU fails with EFIS switches in NORM ? |
|
Definition
| Right EHSI and EADI will be blank |
|
|
Term
| What should the pilot do if right DPU fails? |
|
Definition
| Select DRIVE XFR on right overhead EFIS panel |
|
|
Term
| What indicates a left AHRS failure? |
|
Definition
| HOG flag on left EHSI and ATT flag on left EADI |
|
|
Term
| What should the pilot do if left AHRS fails? |
|
Definition
| Select XSIDE DATA on left overhead EFIS panel |
|
|
Term
| EADIs, EHSIs & MFD will go blank when DC volts drop below ___? |
|
Definition
|
|
Term
| How can maintenance diagnose EFIS problems after a flight? |
|
Definition
| EFIS has a MEMORY as long as power is maintained |
|
|
Term
| How can elec power remain established to keep EFIS MEMORY? |
|
Definition
| Prior to engine shut down have gnd pwr established & ON, leave avionics switches ON and hydraulic pump OFF |
|
|
Term
| Pulling pitch or roll disconnect handle illuminates CWP T/F. |
|
Definition
|
|
Term
| Tail strikes (T/O or Ldg.) may occur at __ pitch angles? |
|
Definition
|
|
Term
| How many trim tabs are controlled mechanically from cockpit? |
|
Definition
|
|
Term
| With gust lock engaged, how is takeoff inhibited ? |
|
Definition
| Power level movement is restricted |
|
|
Term
| A gust lock system failure will fail in the __ position? |
|
Definition
|
|
Term
| When will the Red "CONFIG" Lt. on CWP illuminate for takeoff? (3) |
|
Definition
| With PWR advanced and flaps beyond 15° or Pitch trim out of normal T/0 range or Condition levers not set for max rpm |
|
|
Term
| "PITCH TRIM" light on CWP indicates __? Red, Amber or White? |
|
Definition
| Pitch trim synchronization is deactivated. Amber Caution |
|
|
Term
"FLAPS" light on CWP indicates __?
Red, Amber or White? |
|
Definition
Electrical malfunction in flap system.
Amber Caution |
|
|
Term
| "GUST LOCK" light on CWP indicates __? Red, Amber or White? |
|
Definition
| Gust lock handle OFF, but rudder lock still engaged. Amber. |
|
|
Term
"RUDDER LIMITER" lt. on CWP indicates __?
Red, Amber or White? |
|
Definition
Rudder limiting system has failed.
Amber Caution |
|
|
Term
| Can rudder limiter be overriden in case of system failure? |
|
Definition
|
|
Term
| What is the procedure for MAXIMUM fuel tank fill capacity ? |
|
Definition
|
|
Term
| How many fuel pumps on aircraft & how are they powered? |
|
Definition
Four:
2 engine driven main pumps & 2 elec driven stby pumps |
|
|
Term
| What controls the electric standby pumps? |
|
Definition
| Overhead switches & automatic switches in condition levers |
|
|
Term
| Can fuel temp be checked? |
|
Definition
|
|
Term
| How many ways can fuel quantity be checked? |
|
Definition
| 3 (Magnetic dipsticks, refuel panel gauges, normal gauges) |
|
|
Term
| What electric bus powers the refueling panel? |
|
Definition
|
|
Term
| Fuel temps at or below 0° C require anti-ice additives T/F . |
|
Definition
|
|
Term
| What is indicated by illumination of "L/R STBY PRESS" light? |
|
Definition
| Standby pump pressure is available |
|
|
Term
| What is indicated by illumination of "L/R MAIN PUMP" light? |
|
Definition
| Respective main pump differential pressure less than 6 PSID |
|
|
Term
| What happens if the right main pump fails or low pressure? |
|
Definition
| R Stby Pump actuated, provided R STBY PUMP switch in AUTO |
|
|
Term
| What supplies fuel to the engine during engine start ? |
|
Definition
|
|
Term
| In case of engine shutdown, a condition lever actuated switch will inhibit the standby pump's auto starting feature T/F. |
|
Definition
|
|
Term
| What is indicated by illumination of blue "FUELING" light? |
|
Definition
| Fueling power switch is ON or the defueling valve is open |
|
|
Term
| Fuel gauges are calibrated to show actual fuel remaining T/F. |
|
Definition
| False (shows usable quantity remaining) |
|
|
Term
| Internal bypassing of the fuel filter occurs at __? |
|
Definition
|
|
Term
| What is indicated by illumination of "L/R FUEL FILTER" light? |
|
Definition
| Associated fuel filter is experiencing an impending clog |
|
|
Term
| "L/R FUEL FILTER" light illuminates at approx. __? |
|
Definition
| 9 psid (bypasses at 18 psid) |
|
|
Term
| "L/R VALVE CLOSED" light on Fuel Panel indicates __? |
|
Definition
| Associated fuel shutoff valve is closed |
|
|
Term
| How many ways to close the L/R Fuel Shutoff Valve? |
|
Definition
| Only one; the fire handle. |
|
|
Term
| "L/R LOW LEVEL" light on Fuel Panel indicates __? |
|
Definition
| Fuel tank is below 300 lb (+/- 70 lb) |
|
|
Term
| "FUEL" lt. on CWP comes on with all Fuel Panel lts. except ___? |
|
Definition
| Only one; the fire handle |
|
|
Term
| Useable fuel capacity is __ pounds? |
|
Definition
|
|
Term
| Where are the standby fuel pumps located? |
|
Definition
| One in each tank (hopper tank) |
|
|
Term
| Fuel vent also serves as an overflow system T/F. |
|
Definition
|
|
Term
| Where is the single point refueling control panel located? |
|
Definition
|
|
Term
| The fuel "XFEED" lt. indicates a valve or switch position? |
|
Definition
|
|
Term
| Can one Stby Pump supply enough fuel to operate BOTH engines? |
|
Definition
|
|
Term
| Fuel test switch will cause what indications? |
|
Definition
| Fuel flow 1000lb (+/- 50 lb) & Fuel quantity 760 lb (+/- 35 lb) |
|
|
Term
| Firewall shutoff valves must be open to transfer fuel from wing to wing T/F. |
|
Definition
|
|
Term
| How is fuel transferred from wing to wing? |
|
Definition
| By gravity through the interconnect line |
|
|
Term
| Does green "STBY PRESS" lt. indicate the standby pump is ON? |
|
Definition
| Actually NO (Positive pressure at inlet side of pump) |
|
|
Term
| When will the CWP ''HYDR'' light illuminate? |
|
Definition
| Main Hyd reservoir temp above 116° C or Main/Emergency accumulators below 1850 psi |
|
|
Term
| Which aircraft systems use Hydraulic Power? (5) |
|
Definition
| Flaps, Ldg gear, Brakes, NWS, Prop Brake (if installed) |
|
|
Term
| Hydraulic pump is electrically driven T/F |
|
Definition
|
|
Term
| What subsystems can be operated with the Hyd hand pump? |
|
Definition
| Flaps, Brakes and Ldg Gear |
|
|
Term
| When is main hydraulic pump automatically activated? |
|
Definition
| Main accumulator pressure drops below 2100 psi and Ldg. gear extension/retraction selected. (Pump switch in AUTO) |
|
|
Term
| Number of hydraulic accumulators? |
|
Definition
|
|
Term
| Why do the brakes have two hydraulic accumulators? |
|
Definition
| One for outboard brakes & one for inboard brakes |
|
|
Term
| Emer accumulator ONLY supplies ldg gear uplock release TIF . |
|
Definition
| False (also pressurizes main reservoir) |
|
|
Term
| How does emergency landing gear extension use hydraulics? |
|
Definition
| Hyd press disengages the uplocks, allowing gear to free fall |
|
|
Term
| Power supply (bus) for the hydraulic pump __? |
|
Definition
|
|
Term
| Location of the hydraulic pump circuit breaker (CB) ? |
|
Definition
| No CB; protected by a 200 amp fuse in the L PDU |
|
|
Term
| Main hydraulic reservoir is pressurized by __? |
|
Definition
| Spring & emergency accumulator hydraulic pressure |
|
|
Term
| "HYDR" light on CWP indicates low hyd quantity T/F. |
|
Definition
|
|
Term
| "HYDR" light on CWP indicates hyd pressure is too high T/F. |
|
Definition
|
|
Term
| Can Main hyd accumulator be pressurized by the hand pump? |
|
Definition
|
|
Term
| Can Emer hyd accumulator be pressurized by the hand pump ? |
|
Definition
|
|
Term
| Can the flaps be extended AND retracted by the hand pump? |
|
Definition
|
|
Term
| Where can the nitrogen pre-charge be checked? |
|
Definition
| L H side of nose wheel well |
|
|
Term
| Nitrogen pre-charge pressure is? |
|
Definition
|
|
Term
| Hand pump uses MAIN reservoir fluid thru a stand pipe T/F . |
|
Definition
| False (uses hand pump reservoir fluid) |
|
|
Term
| Is elec hyd pump protected by a resettable circuit breaker? |
|
Definition
| No (more like a current limiter) |
|
|
Term
| Hyd's are pressurized up to __ psi in the OVRD position? |
|
Definition
|
|
Term
| Systems supplied with hyd press from emergency accumulator? |
|
Definition
| Ldg gear emer uplock release & main reservoir pressurized |
|
|
Term
| How is filter element clogging indicated? |
|
Definition
| Pin protruding from head offilter in nose wheel well |
|
|
Term
| Hyd quantity indicator is electric T/F. |
|
Definition
|
|
Term
| A relief valve protects system if pressure exceeds __ psi? |
|
Definition
| 3750 psi (3600 psi on "A" models) |
|
|
Term
| Fluid pumped with hand pump returns to main reservoir T/F. |
|
Definition
|
|
Term
| What items use bld air in the ice protection system? (3) |
|
Definition
Boot de-icing;
Engine split lip;
Inlet guide vanes. |
|
|
Term
| What is pwr'd automatically when the first AC GEN comes on line? (3) |
|
Definition
Main pitot tubes;
Temp probe;
Angle of attack sensors. |
|
|
Term
| CWP "ICE PROT" lt. comes on with all icing system lights TIF |
|
Definition
|
|
Term
| Will the CWP "ICE PROT" lt. come on with any overhead lights not on the Ice Protection Panel ? |
|
Definition
| Yes, will come on with a "L/R AC GEN" light |
|
|
Term
| What is indicated by "DE-ICE OV TEMP" lt. on Ice Prot. Panel? |
|
Definition
| An overheat of the boot de-ice bld air (>150°C) |
|
|
Term
| What is indicated by "TIMER" lt. on Ice Protection Panel? |
|
Definition
| The de-ice timer or valves are malfunctioning |
|
|
Term
| What order are Boots inflated when ONE CYCLE is selected? |
|
Definition
| Stabilizer, outboard wing, inboard wing, stabilizer again |
|
|
Term
| Can boot inflation be monitored? |
|
Definition
| Yes, by following green indicator lts. (BOOT IND switch ON) |
|
|
Term
| If CONT is selected, inflation cycles repeat __? |
|
Definition
|
|
Term
| Can the pilot manually de-ice wings ONLY? |
|
Definition
|
|
Term
| Will boots inflate if both LP & HP bld valves are closed? |
|
Definition
|
|
Term
| "L/R AIR VALVE" lt. on the Engine Anti-ice Panel indicates ___? |
|
Definition
| Associated air valve is not properly positioned |
|
|
Term
| Which ice protection items have a light on Flt Status Panel? |
|
Definition
| Blue "L/R PROP DE-ICE" and "L/R ENG ANTI-ICE" |
|
|
Term
| What is indicated by illumination of "L/R AC GEN" light? |
|
Definition
| AC Generator not supplying power |
|
|
Term
| Right AC GEN can power left electrical inlet duct heat T/F. |
|
Definition
|
|
Term
| Blue "L/R PROP DE-ICE" lt. on Flt. Status Panel will GO OUT in case of system failure T/F. |
|
Definition
|
|
Term
| What are the prop de-icing ON & OFF times, in NORM and MAX? |
|
Definition
NORM - ON 11 sec / OFF 79 sec.
MAX - ON 90 sec / OFF 90 sec. |
|
|
Term
| Blue "L/R ENG ANTI-ICE" lt. on Flt Status Panel will GO OUT in case of system failure T/F . |
|
Definition
| False (illuminated as long as switch is on) |
|
|
Term
| "L/R PROP" lt. on prop/windshield De-ice Panel indicates ___? |
|
Definition
| Fault is detected in active system (prop heat inop.) |
|
|
Term
| Side windshield heat time limitations? |
|
Definition
| Operate in NORM for 7 minutes before selecting HIGH |
|
|
Term
| What is indicated by "L/R SIDE" & "L/R FRONT" lights? |
|
Definition
| Overheat or controller fault has occured |
|
|
Term
| Windshield heat is powered by __? |
|
Definition
| 115V AC wild frequency BUS |
|
|
Term
| "ICE PROT" annunciator is part of Master Warning System T/F. |
|
Definition
| False (part of Master Caution System) |
|
|
Term
| What is indicated by illumination of "R INTAKE" light? |
|
Definition
| Respective engine intake heat lost one or more phases |
|
|
Term
| All Gear retracts foward except nose wheel T/F. |
|
Definition
| False (all retract forward) |
|
|
Term
| Each Gear is equipped with dual wheels, except nose gear T/F. |
|
Definition
|
|
Term
| Normal Gear operation is Hyd T/F. |
|
Definition
|
|
Term
| Emer Gear extension is by free fall or use of hand pump T/F. |
|
Definition
|
|
Term
| Anti-skid requirements to operate? |
|
Definition
| Anti-skid switch ON & Ldg gear handle ON & PL's below flight idle OR WOW switch activated |
|
|
Term
| What is the touchdown brake protection feature? |
|
Definition
| Prevents brake application until 3 seconds after main gear compression OR wheel speed exceeds 50 knots |
|
|
Term
| Anti-skid system cuts out at approximately __ knots ') |
|
Definition
|
|
Term
| "A-SKID INOP" light on CWP indicates __? |
|
Definition
| A system fault or gear is down with anti-skid switch OFF |
|
|
Term
| Which CWP light comes on if gear NOT down below RA 500 ft? |
|
Definition
|
|
Term
| Anti-skid is NOT available using emergency braking T/F. |
|
Definition
| False (anti-skid is available) |
|
|
Term
| "PARK BRK ON" light on CWP indicates __? |
|
Definition
| Brake handle is pulled & brake press > 1700 psi |
|
|
Term
| What is indicated if the CWP "PARK BRK ON" light goes OUT? |
|
Definition
| Brake handle pushed dn and/or press dropped <900 psi |
|
|
Term
| It's possible to set brakes without triggering CWP light T/F. |
|
Definition
|
|
Term
| Can you name ALL systems associated with WOW switches? |
|
Definition
| Just say YES. (If you can, you don't need this book) |
|
|
Term
| Where is the Anti-skid switch located? Don't cheat |
|
Definition
|
|
Term
| Emer gear extension & NWS are pwr'd off which electric bus? |
|
Definition
|
|
Term
| NWS is __ actuated & __ operated? |
|
Definition
| Electrically Hydraulically |
|
|
Term
| During emer extension of gear, an explosive device seperates gear doors from actuating linkage T/F. |
|
Definition
|
|
Term
| Which CWP lt. comes on with flaps > 15 and gear NOT down? |
|
Definition
|
|
Term
"AUTOCOARS" light on CWP indicates __?
Red or Amber? |
|
Definition
The autocoarsen computer has failed.
Amber Master Caution |
|
|
Term
| "L/R ENG OIL PRESS" light on CWP indicates __? |
|
Definition
| Associated propeller gear box OR engine oil pressure is low |
|
|
Term
| What indicates an Autocoarsen activation? (2) |
|
Definition
| Status panel light goes out & Prop oil pressure is LOW |
|
|
Term
| Autocoarsen system operates in 2 distinct modes __ & __? |
|
Definition
| Low power & High power modes |
|
|
Term
| What INDICATIONS feather the prop in Auto Coars High mode? |
|
Definition
Failed engine torque < 50%;
P3 < 120 psi;
Torque split>25% (between engines) when Torque > 50% on Operating engine |
|
|
Term
| What happens if autocoarsen switch is turned OFF after an AUTOCOARSEN has feathered the prop? |
|
Definition
|
|
Term
| Which power plant gauges operate in both analog & digital? |
|
Definition
|
|
Term
| An ITT split during taxi as high as 150° C may indicate what? |
|
Definition
| A HP bleed valve is open. |
|
|
Term
| Engine Lt. Off must occur within __ of initial Ng rotation? |
|
Definition
|
|
Term
| Maximum starter engagement time is limited to __ seconds? |
|
Definition
|
|
Term
| What supplies electrical power to each engine? |
|
Definition
| Engine driven AC Alternator |
|
|
Term
| During start, the starter assists Ng rotation until __? |
|
Definition
| Ng is approximately 55% (CT7-9B) |
|
|
Term
| HMU provides high pressure metered fuel for combustion T/F |
|
Definition
|
|
Term
| If HMU torque motor is cut out after a malfunction, what primarily controls fuel flow? |
|
Definition
| Position of the power lever. |
|
|
Term
| What is powered from the Engine AC Alternator? (3) |
|
Definition
| DECU, Ng, Ignition system |
|
|
Term
| Propeller gear box uses oil from the engine oil system T/F. |
|
Definition
|
|
Term
| Function of the bottom governor is to __? |
|
Definition
| Increase RPM in reverse range |
|
|
Term
| What prevents ice formation on the engine scroll vanes? |
|
Definition
|
|
Term
| Fuel heater, used to prevent icing, uses __ oil? |
|
Definition
|
|
Term
| Is takeoff permitted with "FUEL LOW TEMP" light on ? |
|
Definition
|
|
Term
| What are the indications of a 55% speed sensor failure? |
|
Definition
| CWP & overhead lights remain dark (no starter cut out at 55%) |
|
|
Term
| When will "FUEL LOW TEMP" light come on? |
|
Definition
|
|
Term
| Minimum oil temp for engine start (type II oil)? |
|
Definition
|
|
Term
| Max engine RPM for takeoff __? (CT7-9) |
|
Definition
|
|
Term
| Max engine operating limits for takeoff __? (CT7-9) |
|
Definition
| 917 ITT for 5mins.(lOO% torque) or 927 ITT for 2 min. |
|
|
Term
| Max Continuous Power ? (CT7-9) |
|
Definition
| 940 ITT or 100% torque, whichever is reached first |
|
|
Term
| Starter duty cycle limits during engine start __? |
|
Definition
| Wait 3 min. after 1 st start cycle, then 25 min. after 2nd |
|
|
Term
| Motoring limits __? (CT7-9) |
|
Definition
| Three 30 second ventilations with a 3 min cooling after first and second, and 1 hour cooling after the third |
|
|
Term
| Max allowable ITT during engine start __? |
|
Definition
|
|
Term
| Procedure to lock out the torque motor __? |
|
Definition
| Push CL to Max, lift up & push hard into T/M, then pull back to approx. half between Max-Min, then set desired PRPM |
|
|
Term
| A single stroke chime indicates __? |
|
Definition
| The Master Caution System has activated |
|
|
Term
| How is the T/O Inhibit function reset? |
|
Definition
| Press "T/O INT", Press "GND OP" or when Ldg gear retracts |
|
|
Term
| A double stroke chime indicates a Master Warning cond T/F. |
|
Definition
|
|
Term
| Inoperative Radio Altimeter has what effect on the GPWS? |
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Definition
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Term
| Overspeed warning will sound at approximately __? |
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Definition
| Vmo + 1.5 KIAS (Vmo + 6 kts. on FO's side) |
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Term
| Name 3 different warnings provided by the Stall System? |
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Definition
| Shaker, Clacker, Lights (pusher is not a Warning) |
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Term
| White "BITE" light indicates __? |
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Definition
| Loss of redundancy (back-up) in Warning Annunciator system |
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Term
| Which WARNINGS are inhibited by the "T/O INT" buttonlight ? |
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Definition
| NONE, except the "AUTO TRIM" annunciator |
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Term
| How long will the glareshield Master Warning light stay on? |
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Definition
| Until reset by pressing either Master Warning buttonlight |
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Term
| How long will a CWP Master Warning light stay on? |
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Definition
| Until the fault is corrected |
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Term
| Which CWP lights are recorded by the FDR? |
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Definition
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Term
| During engine start, GND OP mode reverts to T/O INH mode T/F . |
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Definition
| True (then reverts back to GND OP mode after start) |
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Term
| Purpose of GND OP mode __ ? |
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Definition
| Minimizes the nuisance of caution alerts on ground |
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Term
| GND OP mode will come ON automatically after landing T/F. |
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Definition
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Term
| GND OP mode inhibits ALL aural cautions T/F. |
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Definition
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Term
| Purpose of the T/O INH mode __? |
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Definition
| Inhibits non-essential warnings during takeoff phase |
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Term
| When will T/O inhibited warnings, if any, appear on CWP? |
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Definition
| After T/O INH mode is reset (gear retracted) |
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Term
| Aural alerts are repeated every 5 seconds, except for __? |
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Definition
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Term
| Initially, Warning & Caution lights illuminate BRIGHT, regardless of the Bright/Dim switch position T/F. |
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Definition
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Term
| What does the UPR lamp test activate? |
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Definition
| All overhead annunciator lights and a single chime |
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Term
| What does the LWR lamp test activate? |
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Definition
| All annun. lts. on glareshield & instr. panel w/ triple chime |
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Term
| Which lights are not effected by the Lamp Test Switch? |
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Definition
| Drive XFR, Gear in transit, Pressurization "Fault" light |
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Term
| How many bulbs are in each CWP light? |
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Definition
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Term
| Why do the CWP bulbs alternate during Lamp Test? |
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Definition
| To verify each bulb illuminates |
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Term
| When is the Stall Warning System inhibited? |
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Definition
| On the ground and until 7 seconds after T/O (WOW) |
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Term
| Which disengages the AP, the stick Pusher or stick Shaker? |
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Definition
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Term
| One stall warning computer will activate Stick Pusher T/F |
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Definition
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Term
| What information are stall warnings based on? |
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Definition
| Wing de-ice system, Flap position, Angle of attack (ADA) |
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Term
| What indicates the loss of heating circuit to AOA sensor? |
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Definition
| Overhead Amber "L/R ALPHA" light |
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Term
| PUSHER forces elevator down ____ ° at ___ lbs of force. |
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Definition
| 4 degrees at 80 lbs of force |
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Term
| Stick pusher actuator has a __ stop switch? |
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Definition
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Term
| How can a pilot disarm stick pusher? |
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Definition
| Press "PUSHER DISARM" buttonlight |
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Term
| How is stick pusher reset after it has been disarmed? |
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Definition
| Cannot be reset while airborne |
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Term
| Name 3 systems not announced OR reset thru the Master Warning system? |
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Definition
| AP disconnect, Stall warning, Overspeed warning |
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Term
| Minimum environmental temp for Takeotf __? |
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Definition
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|
Term
| What is the max operating altitude __? |
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Definition
| 31,000 ft. (25,000 ft. press. altitude; most airlines) |
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Term
| What is the Vmcl speed __ ? |
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Definition
| 106 KIAS (Flaps 20° or 35°) |
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Term
| Max flaps extension speed (Vfe) for 7° or 15° ___? |
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Definition
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Term
| Max flaps 20° extension speed __? |
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Definition
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Term
| Max flaps 30° extension speed ___? |
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Definition
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Term
| Minimum altitude to select ldg flaps __? |
|
Definition
| Select before 300 ft. radio height during norrnal ldg. |
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Term
|
Definition
| LOW - 130 knots HIGH - 160 knots |
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Term
| Max tire speed (most models) __? |
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Definition
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Term
| Max landing gear retraction speed (Vlor) __? |
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Definition
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Term
| Max landing gear extension speed (Vloe) __? |
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Definition
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Term
| Max Emergency ldg gear extension speed (Vloee) ___? |
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Definition
| 150 knots (because of gear doors) |
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Term
| Max operating speed w/ gear extended (VLe) __? |
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Definition
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Term
| Max rough air penetration speed (Vra) __? |
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Definition
| 190 KIAS up to 21,000 ft. MSL, then Vmo pointer minus 30 kts. |
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Term
|
Definition
| 250 KIAS to 16,000 ft ., decreasing to 210 KIAS by 25,000 ft . |
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Term
| Maneuvering load acceleration limits, flaps retracted __? |
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Definition
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Term
| Maneuvering load acceleration limits, flaps extended __? |
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Definition
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|
Term
| Airport pressure altitude limits __? |
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Definition
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|
Term
| Runway slope limits, landing __? |
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Definition
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Term
| Runway slope limits, takeoff __? |
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Definition
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Term
| Max tailwind component for Takeoff __? |
|
Definition
| Consult the Perfonnance, Brake Energy Limits |
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Term
| Max tailwind component for Landing __? |
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Definition
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|
Term
| Max number of missing vortex generators on vertical tail __? |
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Definition
| Fin - 1 per side, Rudder - 2 per side but not two adjacent |
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Term
| Limits if more than 1 Vortex Gen is missing from stabilizer? |
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Definition
| Flaps restricted to 20 max (right bottom stabilizer) |
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Term
| Minimum main battery temp for takeoff __? |
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Definition
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|
Term
| Minimum emergency lighting battery temp __? |
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Definition
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|
Term
| Max differential pressure __? |
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Definition
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|
Term
| Max, Auto Mode, differential pressure __? |
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Definition
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|
Term
| Max negative differential pressure __? |
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Definition
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|
Term
| Max differential pressure landing __? |
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Definition
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|
Term
| Flight Director limitations __? |
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Definition
| FD in GA mode during takeoff is prohibited |
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Term
| Yaw Damper limitations __? |
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Definition
| OFF during takeoff, go around, landing |
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Term
| Max maneuvering speed (Va) __? |
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Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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|
Term
| Fuel temp limitations __ ? |
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Definition
| Exceeding +43° C or below -35° C, do NOT operate aircraft |
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Term
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Definition
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