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229 Cards in this Set
- Front
- Back
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What is Vmo? |
Maximum Operating Speed 340 K.C.A.S. |
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What is maximum Mmo? |
Maximum Mach Operating speed .88 Mt |
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What is Va? |
Maneuvering speed Va-170 K.C.A.S. Airplane 1000-1213 Va-206 K.C.A.S Airplane 1000-1213 with A.S.C. 190 or 1214 |
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What is turbulent penetration speed? |
270 K.C.A.S. / .75 Mt |
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What is maximum ramp weight? |
73,600 LBS for Airplane 1000-1213 75,000 LBS for Airplane 1214 & subsequent |
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What is Maximum takeoff weight? |
73,200 LBS for Airplane 1000-1213 74,600 LBS for Airplane 1000-1213 with ASC 190 < !214 & subsequent |
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What is Maximum landing weight? |
58,500 LBS for airplane 1000-1213 66,000 LBS for airplane 1000-1213 with ASC 190 , airplane 1214 & SUb |
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What is maximum zero fuel weight ? |
46,500 airplane 1000-1213 49,000 airplane 1000-1213 with ASC 190, Airplane 1214 & sub |
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What is the maximum approved altitude for takeoff & landing ? |
15,000 feet |
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What is Maximum approved slope for takeoff & landing? |
+_ 2% |
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What is the maximum tailwind for takeoff & landing? |
10 knots |
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What is the maximum approved altitude? |
45,000 feet |
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What is VMC? |
Vmca 104 air Vmco 111 ground |
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What limitations is there on the use of landing lights ? |
Ground operation is limited to 5 minutes |
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Other than the Airplane Flight Manuel what 2 publications are required to be immediately available to the flight crew? |
The HONEYWELL SPZ-8000 or SPZ 8400 - Digital Automatic Flight Control System pilots Manuel Honeywell Flight Management System pilots Manuel |
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What is the minimum altitude for AUTOPILOT engagement? |
200 feet AGL |
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What is the minimum altitude for AUTOPILOT operation on approach? |
50 feet AGL OR Unless VNAV is used then min altitude for autopilot coupled with IFR VNAV operations is 300 ft AGL OR 50 feet below min descent altitude whichever is HIGHER |
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What is the minimum altitude for autothrottle operations on approach? |
50 feet AGL |
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When is the autothrottle not authorized for use during takeoff or go around? |
When WING ANTI-ICE is used |
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What is the engine starter duty cycle? |
30 sec ON/3 min OFF 30 sec ON/3 min OFF 30 sec ON/15 min OFF |
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What is the duty cycle for AIRSTART ignition? |
30 sec ON/30 sec OFF or 5 min ON/ 30 min OFF for Airplane 1000-1249 FOR AIRPLANE 1000-1249 with ASC 304 & airplane 1250 & sub IGNITION CAN OPERATE CONTINUOUSLY
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What is the maximum engine fuel temperature? |
90*C Indefinitely or 120*C for 15 minutes |
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What is the minimum engine fuel temperature ? |
-40 C/F |
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What is the maximum oil temperature? |
105 C - indefinitely or 120 C for 15 minutes |
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What is the minimum oil temperature for starting ? |
-40 C/F |
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What is the minimum oil temperature for opening the power lever? |
-30*C |
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What is the limitation regarding the engine synchronizer system? |
The engine synchronizer MUST BE OFF for takeoff & landing |
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When do we need to cancel reverse thrust during landing? |
Initiate cancellation of reverse thrust @ 70 KCAS to achieve idle reverse thrust by normal taxi speed |
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What is the maximum APU EGT? |
RUNNING -732*C WITH BLEED AIR SELECTED-680*C STARTING-988*C |
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What is the maximum APU RPM? |
110.0% |
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What are the APU starts duty limits if starting on the airplane batteries? |
3 /30 second attempts /20 min OFF Followed by 3 more 30 second attempts / 1hour OFF |
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What are the APU starter duty limits if starting on external power unit? |
2 / 15 second attempts/ 20 min OFF 2/ 15 second attempts / 1hr off |
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What is the APU starter duty cycle if the starts are successful? |
SUCCESSFUL consecutive starts are LIMITED to 6 STARTS with 10 minute intervals between starts then 1 hour OFF |
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What is the APU starting envelope? |
From sea level to 15000 ft @ airspeeds BELOW 250 knots the start is GUARANTEED FROM 15,000 feet to 20,000 feet the start is possible |
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What limitations must be considered if the APU is operated ABOVE 30,000 feet? |
An inspection is REQUIRED if the APU is operating ABOVE 30,000 feet for more than 1 hour OR MORE THAN 5 TIMES |
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What is the allowable electrical load on the APU airborne? |
THE APU alternator can deliver 100% power from SEA LEVEL TO 22,000 feet. FROM 22,000 feet to 30,000 feet the limit decreases linearly to 50 % power AIRPLANE 1000-1155 without ASC 96 |
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What limitations apply to the standby electrical system? |
MIn HP RPM 67% Speed breaks slow 5 sec for full range NO ground spoilers or thrust reversers on LANDING |
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What limitation must be observed before pulling the flight power shutoff handle? |
The speed brakes must be retracted |
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What is VLE? |
Maximum speed you can fly with the gear extended. 250 KCAS |
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What is VLo? |
Airspeed at which the landing gear can be safely operated NORMAL-225 KCAS ALTERNATE-175 KCAS |
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What is the maximum tire speed? |
Non-SP- 182 knots SP- 195 knots |
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What is the maximum altitude with the landing gear extended? |
20,000 feet |
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When are speed brakes not authorized? |
When flaps are @39. Landing gear is extended |
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If a takeoff is made with the ground spoilers inoperative what configuration must be used? |
Anti-skid operative 20 of Flaps Rated thrust must be used NO COWL OR WING ANTI-ICE |
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If a takeoff is made with anti-skid inoperative what configuration must be used? |
Ground spoilers must be operational 20 Flaps Rated thrust must be used Cowl & Wing anti-ice NOT USED |
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What break messages must be cleared prior to takeoff? |
Brake Pedal (break by wire only) Brake Fail |
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What are the VFe speeds? |
Flaps 10 - 250 KCAS Flaps 20 - 220 KCAS Flaps 39 - 170 KCAS FLAPS 39-180 KCAS for airplane 1000-1213 with ASC 190, or airplane 1214 & subs |
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What is maximum speed with both MACH TRIM compensators inoperative or electric trim inoperative? |
.75 Mt |
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What speed consideration must be observed if the yaw damper fails in flight? |
220 KCAS above FL180 Below FL180 see AFM for minimum speeds |
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What limitation apply if both Mach trims compensators and the yaw damper are inoperative ? |
MAXIMUM Altitude 41,000 feet Speed limits apply |
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Are the Mach Trim compensators required to be on during flight? |
YES |
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Are the stall barrier computers required to be on during flight? |
YES |
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What is the maximum altitude that the you can operate the flaps 39? |
20,000 Feet |
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What limitation applies if a takeoff is made with the yaw damper inoperative? |
Maximum Fuel Load is 9,000 LBS |
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What bleed consideration must be observed above 41,000 FEET? |
DO NOT OPERATE ABOVE 41,000 without Both engine bleeds ON Each engine being bleed by either the Air conditioning system or engine cowl anti ice |
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What is maximum cabin differential? |
9.8 PSI |
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What is the maximum cabin differential permitted during taxi, takeoff, & landing? |
.3 PSI |
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What is the maximum windshield wiper speed? |
200 KCAS |
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When is the cowl anti ice required on the ground? |
WHEN static air temperature (SAT) below 8 C Visible moisture, precipitation, wet runway |
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When is wing anti ice required? |
When icing conditions are imminent Immediately detection of ice formation on wings, winglet, or windshield |
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What condition must be met to turn off 1 boast pump at cruise? |
Fuel contains anti-icing additive Fuel tank temperature is above 0 C |
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What is a total useable fuel? |
29,500 LBS |
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What is the maximum fuel imbalance? |
2,000 lbs @ 60,500 400 lbs @ max gross |
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If thrust reverser deploys accidentally what happens to engine thrust? |
Reduced to idle A cable automatically retards the respective power lever |
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What E.V.M. Indications are considered normal in icing conditions and otherwise? |
In Icing -1.25 Not in icing - .60 |
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When checking engine oil what precaution must be observed when reading the sight gauge? |
There are 2 tapes on on either side of the sight gauge One for the left One for the right |
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What 3 indications should be observed before prior to opening the HP FUEL cock during engine start? |
15 % HP Illumination of the IGN light Positive rotation of the LP spool Start valve open light, Oil pressure |
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What hydraulic systems power the thrust reversers? |
Left powered by the combined system Right powered by the flight system |
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During the preflight what should you look for on the thrust reversers? |
General Condition, doors fully stowed, & hydraulic leaks |
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If a flameout occurred & you are unable to close the HP cock What would you suspect has happened? |
Shaft separation |
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Where do we tap customer bleed? |
7th & 12th stages |
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Will the oil flitter bypass? |
YES |
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Will the fuel filter bypass? |
NO |
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What is the minimum engine idle on the ground, airborne with flaps less then 22? Airborne with flaps @ 22 plus? |
46.6% HP 46.6% HP 67.0% HP |
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What are the colors on the engine instruments indicate? |
RED-Maximum and or Min Amber- Takeoff & Caution White- Normal |
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When do standby engine instruments come on? |
IN AUTO-if a primary engine instrument fails IN MANUAL-Full time |
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What engine parameters are displayed on the standby engine instruments? |
The primary engine instruments Left side of the DU #3 |
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What would you suspect if the APU master switch is turned ON & the low level oil pressure light did not come on? |
The APU inlet door did not open |
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What is the APU used for on the ground? In the Air? |
Ground- Air & Electricity Air - Electricity |
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When shutting down the APU by using the over speed/test switch when should you turn off the Master Switch? |
After the RPM reaches 10% |
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If an automatic shutdown of the APU occurs where would you look to determine what caused the shutdown? |
On the APU fault indicator panel in the tail compartment |
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If a flag is in view on the APU fault panel what should be down before starting the APU? |
Actuate the reset switch & make note of which flag was in view |
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Where does the APU receive its fuel? |
From the left fuel ejector line |
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IF the APU is started & for some reason it shuts down What must be down with the APU cockpit controls prior to restart? |
The APU masters switch must be turned off then back ON |
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Once the APU is operating how long should we wait before placing electrical loads on the APU Pueumanic? |
Electricity is available immediately APU should be operated for 2 minutes before AIR is extracted |
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What is the correct configuration for APU shutdown? |
Alternator-OFF AIR unchanged |
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When we shutdown the APU we press the overspeed/test switch What does this actually do? |
It simulates an overspeed of 11.4% which causes the ECU to close the APU fuel valve |
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After the APU is operating how would you turn on the ALTERNATOR? |
By selecting AUX power ON |
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If the APU is operating & AUX power switch is ON when both engine drive alternators are operating will the APU off light be on? |
NO |
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What occurs automatically in the pneumatic system when we turn on the APU Air? |
The isolation valve OPENS |
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If 2 Boast pumps fail on the same side how would you keep the fuel balanced? |
By opening the intertank & using sideslip |
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After start we check the fuel & oil temperatures. What are we checking & why? |
We should check to see that the temperatures are similar To verify that the fuel/oil heat exchanger is working |
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How would you read the fuel tank temperature? |
On the fuel page |
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Explain the fuel quantity test? |
Place the toggle switch to D See all 8 lights Place the toggle switch to T left & Right fuel quantity with the indicate 7000 lbs, total will indicate 14000 lbs EICAS display will turn AMBER , The FUEL LEVEL LOW message will show |
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What is the indication of low fuel light? |
Low fuel lights on Standby fuel quantity flashes for 30 seconds Then remain on steady Fuel quantity on the EICAS will turn amber FUEL LEVEL LOW message will appear |
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What is the intertank valve used for? |
To MOVE the fuel from ONE hopper to the other using sideslip, and defueling |
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What is the crossflow valve used for? |
To move fuel from one hopper to the opposite engine by using a boost pump it through the valve |
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What is indicated if a L or R MAIN or ALt fuel pressure low message (AMBER) is on the EICAS & the CB in the switch is illuminated? |
The CIRCUIT BREAKER on the power distribution box has opened |
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What 2 devices serve to keep the hopper full? |
Flapper valve & fuel ejector |
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What items are powered from the battery tie bus? |
The APU starter & The AUXILIARY Hydraulic. Pump |
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How many alternators are installed in the airplane? |
4 |
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Where do the the battery charges receive power? |
The respective MAIN AC buses |
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In normal operations how many EPMP switches must be in AUTO? |
6 |
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What does the E inverter feed? |
The Essential AC BUs (Phase A) E Inverter=Ess Ac (phase A) |
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What does the Standby Electrical power system supply power to? |
The Essential Busses ABEX STBY=The Essential BUSES |
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How should you turn on the Standby Electric Power System? |
Standby Electric Switch ON E Inverter TRU SET |
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IF the Standby Electric system is in the use & it comes off line how should you reinstate it? |
By turning the Standby Electric switch Off then Back ON |
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How would you read the power on the Essential Busses? |
By selecting Essential on the volt/freq meter switch (top row of switches) and read the outputs |
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How would you read the load on the LEFT convertor output? |
By reading the % of load on the AC & DC loadmeters |
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How would you read the load on the Left converter? |
By reading the % of load on the AC & DC loadmeter |
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What is the power source priority for the main buses? |
Respective, Auxiliary, Opposite |
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What is the power source priority for the Essential buses? |
Left, Right, Battery, or E Inverter |
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What drives the ABEX ALT (generator)? |
The combined hydraulic system |
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What type of fluid is used in the hydraulic system? |
Type IV (sky drop) -red |
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What is normal pressure for the hydraulic system? |
3,000 PSI |
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What is the proper pre charge pressure on the hydraulic accumulators? |
1,000 PSI |
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What components can the Auxilary Hydraulic system operate that are useful prior to and during landing? |
Flaps & Brakes (with anti-skid) |
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Where does the utility system receive its fluid? |
From the combined system RESERVIOR |
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What drives the utility system pump? |
Flight system pressure |
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Where does the Auxiliary system receive its fluid? |
From a dedicated chamber with the combined system reservior |
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What drives the Auxiliary system pump? |
An electric motor |
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How many hydraulic filters are equipped with the differential pressure indicators? |
10 Combined Manifold 5 Flight manifold 3 Right main gear wall 1 /2 Left main gear wall |
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How is the hydraulic fluid cooled? |
By the heat exchanger in each hopper Left - -combined Right— Flight |
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What is the normal Flight system quantity? |
Full |
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What is normal combined system quantity? |
Full is the gear down. About 1/2 way between add & full is gear up. |
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If the Utility pump is armed when will it come up? |
If Flight system pressure is Normal . Flight system fluid is not overheated and combined system pressure is low. |
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When will the Auxiliary pump come on? |
AUX pump On/OFF switch. Inside door switch. Brake application. (Assuming an absence of combined/Utility pressure. Outside door switch. Ground service valve. |
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What is the purpose of the nutcracker system? |
To provide an air/ground signal to various systems within the airplane |
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If the nutcrackers fail their test with while airborne. What precaution should be observed? |
DO NOT ARM the Ground Spoilers |
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If we press the nutcracker test switch and both lights come on what does that indicate? |
That both main gear nutcrackers are in the airborne mode |
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If one main gear nutcracker is in flight & the other is on the ground where do the systems that rely on this information think they are? |
Airborne |
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What does pulling the emergency gear handle (T Handle ) do? |
Pulling the T Handle positions the dump valves ( to port fluid to return if there is any) and supplies N2 to the landing gear to extend |
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What does pulling the handle (D Ring) adjacent to the copilots right leg do? |
Resets the dump valves in the landing gear system so that it can operate normally |
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What does the RED light in the landing gear landing indicate? |
If the handle is UP-one or more landing gear doors are not closed If the handle is DOWN-it indicates that one or more landing gear are not down & locked |
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If we do an emergency extension & all 3 landing gear come down & locked what will be the indication on the gear handle? |
3 Green lights will be on & the red light in the handle will be off |
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What precautions should be observed before towing the airplane? |
The nose scissors should be disconnected The landing gear pins should be installed IF cabin door is open it must be supported with a jury cable |
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What 2 methods can we use to steer the nose wheel? |
The handwheel & the rudder pedals |
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There is a guarded toggle switch in front of the handwheel. What does it do? |
Turns off steering @ the rudders & the handwheel |
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On some airplanes there is a switch aft of the handwheel labeled “Normal and Handwheel only” If it is in the “Handwheel Only” position what has been done? |
The rudder pedal steering has been turned off |
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If you move the landing gear control handle you reposition the landing gear control valve. Is this done electrically or mechanically? |
Mechanically |
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What is the proper brake accumulator pre charge pressure? |
1200 PSI |
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If we land the airplane with 1,200 PSI on the brake system pressure gauge & normal brakes fail will the emergency brakes (through the parking brake ) be available ? |
NO the accumulator has to be charged with hydraulic fluid |
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How do we set the parking brake? |
Full the handle fully up & rotate 1/4 turn Pressurize the brake system to 3,000 PSI using Auxiliary Hydraulic Pump. |
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If we use the parking brake to stop the airplane during landing will we have anti-skid? |
NO |
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Are brakes automatically applied during retraction? |
YES |
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ON SPZ 8000 airplanes that are equipped with B.T.M.S. If we move the brake temperature monitor system selector switch to the “ALL” position what temperature is being displayed? |
The hottest brake |
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How do we determine the hottest brake on the SPZ-8400 system? |
Pull up the brake page & the hottest brake is displayed at the bottom of the page. |
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When we do a brake B.I.T.E. Check we generate 4 messages (BBW system) or 3 messages (HHAB)the brake ECU does the B.I.T.E. Check what is the indication of a successful check? |
All of the messages go away |
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What flight controls have trim tabs? |
Both elevators Left aileron |
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What is the maximum speed for the operation of the speedbrakes? |
Vmo/MMO |
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What does the Emergency flap handle do? |
IF mechanically repositions the flap selector valve which will move the flaps if hydraulic pressure is available to the valve |
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What feature of the airplane reduces control forces during flap movement? |
Automatic repositioning of the horizontal stabilizer |
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What precaution should be observed prior to engaging the gust lock? |
Make sure all hydraulic pressure has been bleed from the system |
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How is the rudder trimmed? |
By repositioning the rudder itself |
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If we are in flight with speedbrake retracted & apply left aileron which spoilers will come up? |
The outboard 2 on the left wing |
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Assuming both computers are working normally how many stall barriers computers are required to give us a stick shaker? Pusher |
Shaker - 1 Pusher - 2 |
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What is the rudder limiter for? |
To trim the amount of rudder deflection available based on airspeed |
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What does the rudder limit message mean? |
That further application of the rudder pedal will not displace the rudder |
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What does the “No Ground Spoiler” message mean? |
The primary control valve has opened & the ground spoilers did not deploy |
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What does the “Ground Spoiler” message mean? |
The primary control valve has opened & the ground spoilers did not deploy |
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What is bleed air used for? |
Engine Start Wing anti-ice, cowl anti ice Pressurization Door seals TAT Probe
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What is the purpose of the isolation valve? |
To separate the Left & Right sides of the bleed air manifold |
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Name 3 ways to open the isolation valve? |
1) Isolation Switch 2) Turning on APU bleed Air 3) By selecting the start master or crank master switch (ground Only) |
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How are the outflow valves controller? |
The normal outflow valve is normally operated by an AC motor, although a DC motor will reposition the valve is manual pressurization is selected. The safety outflow is normally closed however it will begin to open if pressure differential reaches 9.8 PSI |
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What function does the FLIGHT?LANDING switch serve ? |
In FLIGHT position is gives control to the flight tape on the pressurization controller (unless the field elevation is higher) In LANDING position it gives control to the landing tape on the pressurization controller. |
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What prevents us from using the APU to pressurize the airplane airborne? |
The nutcracker system closes the APU bleed valve when airborne |
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What is the minimum pressure that cowl anti-ice is effective? |
4 PSI |
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What does the wing warm light mean? |
That the wing is warm enough to prevent ice from forming |
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What does a wing hot message mean? |
That the wing is too HOT |
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What would happen if one wing anti-ice valve failed closed when we selected wing anti-ice on? |
Both wings would be heated by the other valve & crossover duct |
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Where is the cowl anti-ice air exhausted? |
Into the engine air inlet |
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What respect to ice and rain protection what precaution should be observed if the MAIN AC bus loses power momentarily? |
The windshield heat switches should be cycled off. Wait 2 seconds the BACK ON to prevent windshield heat controller from running away |
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What prevents the fan nose cone from icing? |
The nose cone has a rubber tip on it. If ice forms it will tend to vibrate thereby shedding the ice. |
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What is the proper pre charge pressure for the fire bottle? |
600-625 PSI |
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Which buses powers the engine & APU fire extinguishing systems? |
Essential DC |
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What would happen if one wing anti-ice valve failed closed when we selected wing anti-ice on? |
Both wings would be heated by the other valve & crossover duct |
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Where is the cowl anti-ice air exhausted? |
Into the engine air inlet |
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What respect to ice and rain protection what precaution should be observed if the MAIN AC bus loses power momentarily? |
The windshield heat switches should be cycled off. Wait 2 seconds the BACK ON to prevent windshield heat controller from running away |
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What prevents the fan nose cone from icing? |
The nose cone has a rubber tip on it. If ice forms it will tend to vibrate thereby shedding the ice. |
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Which buses powers the engine & APU fire extinguishing systems? |
Essential DC |
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What takes place if the fire handle is pulled? |
FUEL shutoff valve closes HYDRAULIC shutoff valve closes TRUST reverser is disabled THE alternator is tripped BOTH FIRE BOTTLES are armed to discharge in the respective engine |
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Will a fire warming automatically bring up a checklist? |
YES |
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How many fire bottles are installed? |
3 |
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How many engine fire bottles are installed? |
2 |
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Normally how many fire loops are necessary to tigger an engine fire loop? |
2 |
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If a fire loop has a fault can the engine its installed on still have fire warning? |
Yes when the fault occurs the “Eng Ft loop alert” message will appear. By pressing lighted button the fire warning for that engine is configured to produce a warning if only 1 loop registers the fire |
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If there is no fire warning what must be done in order to pull the fire handle? |
Press the button below the handle |
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If the oxygen mask flow selector is set to normal what will be delivered to the mask? |
Diluted oxygen in a decreasing ratio to about 35,000 feet. Above 35,000 +_ foot you will receive 100% oxygen. |
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If the passenger oxygen control is set to automatic the passenger Oxygen mask should deploy if cabin altitude gets high enough. What should be done if this does not happen? |
Place the passenger Oxygen control to Manuel |
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How do we shut off the Oxygen flow to crew Oxygen masks after it is no longer needed? |
Push the reset/test bar forward |
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When using the crew oxygen mask what 2 ways are there to receive oxygen under positive pressure? |
1) Rotating the selector know to emergency 2) Automatically between 36,000 feet and 45,000 feet |
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There are 2 Oxygen pressure gages on the Oxygen control panel. If both of those gages indicate an adequate supply of Oxygen can we expect to receive oxygen if needed? |
Not necessarily the gages will indicate bottle pressure even if the supply switches are off |
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If the crew masks are needed how would we verify that we are receiving oxygen? |
By observing the flow indicator in the forward right corner of the stowage box, ( Yellow & black +- ) |
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What communication equipment will be available if the emergency batteries are the only source of power? |
The #1 VHF communication radio |
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What communication equipment will be available if the standby system is used? |
The #1 VHF communication radio |
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ON the audio panel what does the “Mask” button do? |
It enables the oxygen mask microphone |
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On the audio panel what does the “HMIC” button do? |
If both crewmembers select HMIC they may communicate without using the inter phone key. |
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On the audio panel what does the “Page” button on? |
It enables the cockpit crew member to speak to all passenger in the cabin through the cabin speaker |
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What is the priority for messages of different color? |
Red, Amber, Blue |
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If a red message in flashing how can it be stopped? |
By pressing either MASTER WARNING LIGHT |
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If a blue message is flashing how can it be stopped? |
It stops on its own after 5 seconds |
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In which axes does the autopilot have authority? |
ROLL & PITCH |
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What does the BC button do on the flight guidance panel? |
It enables the Flight Director to track a back course |
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If the yaw damper fails will the autopilot work? |
NO |
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What takes place when TOGA is selected in flight? |
Autopilot disconnects If autothrottles are engaged they will go to GO AROUND power Flight Director issues a pitch command of +12 (or speed command in SPZ 8400 Flight Director rolls wings level Missed Approach is displayed (IF the FMS is properly sequenced) |
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What practical conditions must be meet to engage autothrottles on the ground? |
Arm button must be on Takeoff mode must be on the flight director (TOGA) EPR must be @ least 1.17 Isolation valve must be CLOSED |
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Where are the shoulder harness locks? |
On the inbound side of each pilots seat toward the bottom end aft |
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How do you open the overwing emergency exits? |
Pull the handle UP & PULL window inboard |
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There is a ring on the upper surface of the wing approximately 10-12 feet from the fuselage about mid-chord. What is it for? |
So that a rope can be attached from the emergency exit to the ring. Then the rope can be used as a hand rail. |
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Where are the crew life jackets stowed? |
In a pouch at the back of the seat toward the bottom |
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When doing the cabin preflight what should we check for in the hand held fire extinguisher? |
Pressure gage in the green arc Current inspection |
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What does the X over the CAS display signify? |
Failure of the FAULT WARNING COMPUTER |
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Which exterior lights are powered from the emergency batteries? |
The lights below each emergency exit. ONE on the leading edge of the wing ONE underwing light |
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What is the power source for the cabin emergency lights? |
A self contained battery pack using batteries that are approximately the same as D cell flashlight batteries |
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How would you turn all the cockpit lights to full bright? |
By turning on the floodlight override switch |
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If the passenger oxygen shutoff valve is opened what cabin sign will come on automatically? |
THE “NO SMOKING SIGN” |
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The taxi lights are located on the nose strut. If the nosewheel streering is turned will the taxi lights also turn? |
YES |
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If the taxi lights are on when the landing gear is retracted will the lights go on? |
S/N 1000-1155 -NO S/N 1000-1155 with a ASC 131 or 1156 & subs - YES |
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What are the pulse lights? |
Turning on the pulse lights causes the landing lights to illuminate alternatively making the airplane easier to see |
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The utility lights are contained in the tail compartment. Can these lights be turned on in flight? |
Yes there is a switch labeled tail compartment lights on the right hand side of the baggage compartment that controls the lights |
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What is the difference between a Display Unit going blank accompanied by an amber CHECK DU X message, A display unit going blank with a RED X displayed? |
If the Display unit blank has failed if red X appears on a blank screen the symbol generator supplying it has failed |
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If all of the right engine instruments show amber dashes what would you suspect is the problem & how would you correct it? |
DAU #2 Channel B has failed GO TO the sensor page Select DAU #2 Channel A |
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The DBDI’s have 3 lights in the upper right hand corner, ONE is green (AHDG), amber (STBY), what does they mean? |
If GREEN LIGHT comes on:is using the alternate IRS for heading information. IF AMBER LIGHT comes on it indicate that the IRS input has failed & DBDI is using information from the flux valve. IF RED LIGHT comes on the flux valve input has failed |
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Why do we not use the RUNWAY position feature? |
If the runway update feature is used it will realign the IRS position. However, the GPS. Will correct this entry the next time the GPS update is done |
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How do you create a place/bearing/distance waypoint? |
By the line selecting a waypoint into the scratch pad. Typing in the desired bearing then typing in the distance. When this is done line select this information into the flight plane whenever you want it |
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What is the priority for navigation sensor use by the FMS? |
GPS DME/DME. VOR/DME. LRN blending |
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If NDB approach is made we must identify the Navi’s prior to starting the approach However, it is not necessary to monitor it continuously during the approach. WHY? |
Because if the signal from the NDB is LOST the bearing pointer will DISAPPEAR |
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How many autopilots are in the airplane? |
2 |
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On audio panel what does “cabin” button do? |
It enables cockpit crew member to speak directly to a cabin attendant at a specific location usually in the galley |
