Term
| 1.) What category is the Saab 340 Certified? 2-1 |
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Definition
| Transport category… FAR part 25 |
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Term
| 2.) What is the max taxi weight of the Saab 340B? 2-3 |
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Definition
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Term
| 3.) What is the max takeoff weight of the Saab 340B? 2-3 |
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Definition
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Term
| 4.) What is the max landing weight of the Saab 340B? 2-3 |
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Definition
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Term
| 5.) What is the max zero fuel weight of the Saab 340B? 2-3 |
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Definition
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Term
| 6.) What is the max Cargo Weight for C1? 2-4 |
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Definition
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Term
| 7.) What is the max Cargo Weight for C2? 2-4 |
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Definition
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Term
| 8.) What is the Max Combined Cargo Weight? 2-4 |
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Definition
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Term
| 9.) What is the max torque for takeoff with APR or Go Around Power? 2-5 |
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Definition
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Term
| 10.) What is the max torque for takeoff? 2-5 |
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Definition
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Term
| 11.) What is max continuous power (torque) with one engine inop? 2-5 |
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Definition
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Term
| 12.) What is the max transient torque for 12 seconds? 2-5 |
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Definition
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Term
| 13.) What is the max ITT for takeoff with APR or Go Around Power? 2-5 |
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Definition
| 950°C for 2 minutes followed by 940°C for 3 additional minutes (5min total) |
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Term
| 14.) What is the max ITT for takeoff? 2-5 |
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Definition
| 927°C for 2 minutes followed by 917°C for 3 additional minutes (5min total) |
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Term
| 15.) What is the max continuous power (ITT) with one engine inop? 2-5 |
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Definition
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Term
| 16.) What is the max transient ITT for 12 seconds? 2-5 |
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Definition
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Term
| 17.) What is the max ITT during engine starting? 2-5 |
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Definition
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Term
| 18.) What is the max Engine RPM for takeoff with APR or Go Around Power? 2-5 |
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Definition
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Term
| 19.) What is the max Engine RPM for takeoff? 2-5 |
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Definition
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Term
| 20.) What is the max continuous Engine RPM with one engine inop? 2-5 |
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Definition
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Term
| 21.) What is the max transient Engine RPM for 12 seconds? 2-5 |
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Definition
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Term
| 22.) What is the max prop RPM for Takeoff / Takeoff + APR / Go Around / Max continuous power? 2-5 |
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Definition
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Term
| 23.) What is the max transient prop RPM for 12 seconds? 2-5 |
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Definition
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Term
| 24.) What is the MINIMUM prop RPM between ground idle and flight idle with the propeller unfeathered? 2-5 |
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Definition
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Term
| 25.) What is the normal operating range for engine oil pressure? 2-5 |
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Definition
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Term
| 26.) What is the engine oil pressure range when between ground idle and flight idle with the propeller unfeathered? 2-5 |
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Definition
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Term
| 27.) What is the max engine oil pressure at starting an initial ground idle operation with extremely cold oil? 2-5 |
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Definition
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Term
| 28.) What is the normal operating range for engine oil temperature? 2-5 |
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Definition
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Term
| 29.) What is the max engine oil temp allowed for 15 minutes? 2-5 |
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Definition
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Term
| 30.) What is the normal operating range for prop oil pressure? 2-5 |
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Definition
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Term
| 31.) What is the minimum prop oil pressure with prop unfeathered? 2-5 |
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Definition
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Term
| 32.) Can you conduct ground operations with prop oil pressure in the yellow arc while unfeathered (5-25 psi and 140-225 psi)? 2-6 |
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Definition
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Term
| 33.) What is the operating range for prop oil pressure with the prop feathered? 2-6 |
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Definition
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Term
| 34.) What is the normal operating range for prop oil temperature? 2-5 |
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Definition
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Term
| 35.) What is the max propeller temperature between ground idle and flight idle with the propeller unfeathered? 2-5 |
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Definition
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Term
| 36.) What is the max propeller oil temperature for 15 minutes? 2-6 |
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Definition
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Term
| 37.) What is the Minimum oil temp for engine starting? 2-7 |
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Definition
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Term
| 38.) How many start attempts can you make before the 25 minute cooling period? 2-6 |
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Definition
| 2 (Start, 3 minute cool, start, 25 minute cool) |
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Term
| 39.) How many motor attempts can you make before the 60 minute cooling period? 2-6 |
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Definition
| 3-30 second motors (Motor, 3 minute cool, motor, 3 minute cool, motor, 60 minute cool) |
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Term
| 40.) What is the max time to light off (from initial Ng rotation to ITT rise) during a direct start? 2-6 |
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Definition
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Term
| 41.) What is the max time a starter/generator can be engaged? 2-6 |
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Definition
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Term
| 42.) What is the max time a starter can be used for motoring? 2-6 |
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Definition
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Term
| 43.) What is the minimum battery temp for a battery start? 2-6 |
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Definition
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Term
| 44.) What is the minimum battery voltage for a battery start? 2-6 |
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Definition
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Term
| 45.) After a successful engine start, how long do you wait before you start the other engine? 2-6 |
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Definition
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Term
| 46.) Can the FUEL TEMP LOW light be on for takeoff? 2-8 |
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Definition
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Term
| 47.) The XFEED and CONN VALVE switches shall be _____ and _____ during takeoff and landing in normal operation. 2-8 |
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Definition
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Term
| 48.) What three de-ice boot modes must be working before dispatch into know icing conditions? 2-9 |
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Definition
| One Cycle, Continuous, Manual |
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Term
| 49.) What is the definition of icing conditions for Engine anti-ice operation? 2-9 |
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Definition
| +10°C or colder AND visible moisture OR standing water, slush, or snow on the ground |
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Term
| 50.) After exiting icing conditions, how long must the engine anti-icing equipment (intake) be left on? 2-9 |
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Definition
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Term
| 51.) A runway with how much water / slush / wet snow is acceptable? 2-10 |
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Definition
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Term
| 52.) A runway with how much dry snow is acceptable? 2-10 |
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Definition
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Term
| 53.) When do you turn the propeller deice system to norm? 2-10 |
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Definition
| -5°C or colder and there is any ice accretion on any part of the aircraft |
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Term
| 54.) When do you turn the propeller deice system to max? 2-10 |
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Definition
| -13°C or colder unless vibrations occur at warmer temperatures |
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Term
| 55.) Can you turn the propeller heat to max if the temperature is between -10°C to -12°C? 2-11 |
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Definition
| Yes, if unacceptable propeller vibration occurs, use caution for runback ice |
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Term
| 56.) What is the definition of icing conditions for operation of wing and stabilizer deicing boots and for adherence to minimum airspeed and AP/FD limitations for icing conditions? 2-11 |
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Definition
| +5°C or colder AND any visible moisture, OR any ice is on the aircraft, OR it is not certain there is no ice on the aircraft |
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Term
| 57.) When should the deice boots be used? 2-11 |
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Definition
+5c w/vis moisture or ice on AC Until 400’ AFE, only at the first sign of ice accretion anywhere on the aircraft If SAT is below -40°C only if ice is accumulating on aircraft |
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Term
| 59.) What is the max flap speed for flaps 7 or 15? 2-13 |
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Definition
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Term
| 60.) What is the max flap speed for flaps 20? 2-13 |
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Definition
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Term
| 61.) What is the max flap speed for flaps 35? 2-13 |
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Definition
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Term
| 62.) What is gear retraction speed (Vlor)? 2-13 |
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Definition
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Term
| 63.) What is gear extension speed (Vloe)? 2-13 |
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Definition
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Term
| 64.) What is Emergency extension speed (Vloee)? 2-13 |
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Definition
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Term
| 65.) What is max extended speed (Vle)? 2-13 |
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Definition
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Term
| 66.) What is the Vmo up to 16,000’? 2-14 |
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Definition
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Term
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Definition
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Term
| 68.) What is Vmm at flaps 0? 2-15 |
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Definition
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Term
| 69.) What is rough air penetration speed (Vra) up to 21,000’? 2-15 |
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Definition
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Term
| 70.) What is Vra above 21,000’? 2-15 |
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Definition
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Term
| 71.) What is the minimum enroute speed with ice while level, holding, or in a descent? 2-16 |
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Definition
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Term
| 72.) What is Vmm at flaps 0 with ice (below MSA)? 2-16 |
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Definition
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Term
| 73.) What speed is used for enroute climb with icing (below MSA)? 2-13 |
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Definition
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Term
| 74.) What is the minimum climb speed below MSA with ice while NOT maneuvering? 2-17 |
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Definition
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Term
| 75.) What is the minimum climb speed below MSA with ice while maneuvering? 2-17 |
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Definition
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Term
| 76.) What are the minimum flap speeds above MSA (climb, cruise, descent, hold, APPR)? 2-16 |
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Definition
| Flap 0° = 160 KIAS, Flap 7° = 150 KIAS, Flap 15° = 145 KIAS, Flap 20° = 140 KIAS, Flap 35° = 130 KIAS |
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Term
| 77.) What is the minimum final approach speed while maneuvering with ice? 2-17 |
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Definition
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Term
| 78.) What is the minimum final approach speed while NOT maneuvering with ice? 2-17 |
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Definition
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Term
| 79.) What is minimum speed for missed approach/go around below MSA with ice? 2-17 |
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Definition
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Term
| 80.) With all systems operating what types of flight is the Saab approved for? 2-19 |
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Definition
| Day and night VFR, IFR, Atmospheric icing conditions |
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Term
| 81.) What are the airport pressure altitude limits? 2-19 |
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Definition
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Term
| 82.) What is the max tailwind component for TO and Landing? 2-19 |
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Definition
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Term
| 83.) What is the max operating altitude for the Saab? 2-19 |
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Definition
| 25,000’ pressure altitude |
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Term
| 84.) What is the minimum main battery temp for takeoff? 2-20 |
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Definition
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Term
| 85.) What is the maximum cabin differential pressure? 2-20 |
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Definition
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Term
| 86.) What is the maximum cabin differential pressure while operating in auto mode? 2-20 |
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Definition
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Term
| 87.) When is the flight director not authorized for use during a takeoff? 2-25 |
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Definition
| When below 500’ AGL or acceleration altitude, whichever is higher |
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Term
| 88.) When is the use of Autopilot not authorized during takeoff? 2-25 |
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Definition
| Below 500’ AGL or acceleration altitude, whichever is higher |
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Term
| 89.) When is the use of Autopilot not authorized during a precision approach? 2-25 |
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Definition
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Term
| 90.) When is the use of Autopilot not authorized on a non-precision app? 2-25 |
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Definition
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Term
| 91.) When is the use of Autopilot not authorized during a visual approach? 2-25 |
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Definition
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Term
| 92.) When is the use of Autopilot not authorized during a Go-around? 2-25 |
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Definition
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Term
| 93.) During Icing conditions with Autopilot and/or FD engaged which vertical mode must be used? 2-25 |
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Definition
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Term
| 94.) When is the Yaw Damper not authorized for use? 2-25 |
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Definition
| Takeoff, Go around, and Landing |
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Term
| 95.) When is it prohibited to have flaps extended in flight? 2-26 |
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Definition
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Term
| 96.) When must final aircraft configuration be completed in IMC? 2-26 |
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Definition
| Prior to FAF (except for circling approaches, OEI, or ATC restrictions) |
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Term
| 97.) When must final aircraft configuration be completed in VMC? 2-26 |
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Definition
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Term
| 98.) How long is the cargo fire protection for an aircraft with 1 or 2 bottles? 2-27 |
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Definition
| 1 bottle = 35 minutes 2 bottles = 60 minutes |
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Term
| 99.) Can the aircraft be moved on the ground while the AHRS is initializing? 2-27 |
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Definition
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Term
| 100.) What is the maximum difference between the 2 EADIs and the Standby Attitude indicator allowed for takeoff? 2-27 |
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Definition
| Less than 3 degree bank and pitch |
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Term
| 101.) Can you take off if the heading on the compass card is slewing away from the aircraft heading? 2-27 |
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Definition
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Term
| 102.) If a reduced power takeoff is performed with APR armed which speeds are used? 2-27 |
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Definition
| Speeds for the assumed temperature (far right column) |
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Term
| 103.) What is the maximum airspeed for windshield wiper use in low mode? 2-29 |
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Definition
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Term
| 104.) What is the maximum airspeed for windshield wiper use in high mode? 2-29 |
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Definition
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Term
| 105.) What is the maximum crosswind allowed for takeoff and landing? 2-29 |
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Definition
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Term
| 106.) When is HP bleed air operation not authorized for cabin conditioning? 2-29 |
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Definition
| When OAT is at or between 0ºC and 20ºC |
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Term
| 107.) What is the maximum load for a DC generator? 2-29 |
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Definition
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Term
| 108.) What is the nominal load for a DC generator? 2-29 |
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Definition
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Term
| 109.) At what battery temperature is a battery start not allowed? 2-30 |
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Definition
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Term
| 110.) At what battery temperature is a cross generator start not allowed? 2-30 |
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Definition
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Term
| 111.) What is the max battery temperature for takeoff? 2-30 |
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Definition
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Term
| 112.) At what battery temperature is takeoff not allowed? 2-30 |
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Definition
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Term
| 113.) At what battery temperature does the BAT HOT LIGHT illuminate? 2-30 |
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Definition
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Term
| 114.) What is the maximum voltage allowed for external power usage? 2-30 |
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Definition
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Term
| 115.) What are the minimum and maximum external power currents during engine start? 2-30 |
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Definition
| Min 1200 Amps Max 1600 Amps |
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Term
| 116.) What is the minimum O2 pressure for 2 or 3 crew members for a flight planned at or below 10,000’ MSL? 2-30 |
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Definition
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Term
| 117.) What is the minimum O2 pressure for 2 crew members for a flight with a planned cruise altitude above 10,000’ MSL? 2-30 |
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Definition
| 1250 psi at a maximum temperature of 40ºC |
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Term
| 118.) What is the minimum O2 pressure for 3 crew members for a flight with a planned cruise altitude above 10,000’ MSL? 2-30 |
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Definition
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Term
| 119.) Are reverse taxi operations or power-backs STRICTLY PROHIBITED? 2-30 |
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Definition
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Term
| 120.) Where do you set Ng to conduct the auto-ignition test during engine shutdown? 2-32 |
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Definition
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Term
| 121.) Verify the IGN lights in the Flight Status Panel (FSP) illuminate momentarily while Ng is above _____ during shutdown. 2-32 |
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Definition
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Term
| 1.) Up to how many passengers can the Saab 340s at Colgan carry? (1-1) |
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Definition
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Term
| 2.) How many navigation lights are on the Saab? 1-22 |
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Definition
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Term
| 3.) How many flashing beacons are on the Saab 340? 1-23 |
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Definition
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Term
| 4.) How many landing lights are installed on the Saab 340? 1-25 |
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Definition
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Term
| 5.) How many taxi lights are installed on the Saab 340? 1-25 |
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Definition
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Term
| 6.) When does the taxi light automatically extinguish? 1-25 |
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Definition
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Term
| 7.) What is the wingspan of the Saab 340B? 1-35 |
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Definition
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Term
| 8.) What is the length of the Saab 340? 1-35 |
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Definition
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Term
| 9.) What is the width between the two main landing gear on the Saab 340? 1-35 |
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Definition
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Term
| 10.) What is the prop diameter of the on the Saab 340? 1-35 |
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Definition
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Term
| 11.) What is the prop blade clearance from the ground? 1-35 |
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Definition
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Term
| 12.) How many tires are installed on the Saab 340? 1-35 |
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Definition
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Term
| 13.) What is the turning radius on the ground of the Saab 340? 1-36 |
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Definition
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Term
| 14.) What is the wingtip sweep for a minimum radius ground turn for the Saab 340B? 1-36 |
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Definition
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Term
| What is the Maximum combined fuel on the Saab 340? |
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Definition
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Term
| What is the Maximum fuel per wing? |
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Definition
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Term
| Does the Saab 340 have negative G fuel capabilities? |
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Definition
| Yes, through the negative g canister in the hopper tank |
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Term
| What does an illuminated LOW LEVEL indicate? |
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Definition
| Less than 300 lbs ± 70 lbs in the respective tank |
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Term
| Does the Fuel quantity indicator show usable or total fuel? |
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Definition
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Term
| How many ways are there to check fuel quantity and what are they? |
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Definition
| 3: Fuel quantity indicators, Magnetic sticks, Fuel panel gauges |
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Term
| At what quantity do the magnetic fuel quantity indicators become useful? |
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Definition
| When fuel levels are below 1100 lbs |
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Term
| Where are the Standby pressure pumps located? |
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Definition
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Term
| What does an illuminated MAIN PUMP light indicate? |
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Definition
| A failure of the main pump |
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Term
| When is the STBY PUMP activated? |
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Definition
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Term
| What does an illuminated green STBY PRESS light indicate? |
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Definition
| Standby pressure is detected at a main pump inlet |
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Term
| Can the right pump supply fuel to the left engine? |
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Definition
| Yes, through the cross feed valve |
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Term
| What powers the Standby pressure pumps? |
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Definition
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Term
| What powers the Main Pumps? |
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Definition
| Engine accessory gear box |
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Term
| What supplies fuel to the engine during engine start? |
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Definition
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Term
| When does the automatic activation of the STBY PRESS pump not occur with a decrease in Main pump pressure? |
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Definition
| With the condition lever in fuel off |
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Term
| How many fuel pumps are on the Saab? |
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Definition
| 6, 2 main pumps, 2 standby pumps and 2 high pressure pumps in the HMU |
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Term
| What lights on the overhead panel do not trigger a CWP FUEL light? |
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Definition
| X FEED ON, CONN VLV, STBY PRESS |
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Term
| How is the Fuel Shut Off valve closed? |
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Definition
| Pulling of the Fire Handle |
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Term
| What is indicated by an illuminated VALVE CLOSED light? |
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Definition
| Fuel shut off valve is closed |
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Term
| What is indicated by an illuminated XFEED ON light? |
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Definition
| The cross feed valve is open |
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Term
| What is indicated by an illuminated CONN VALVE light? |
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Definition
| The fuel connect valve is open |
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Term
| What is the purpose of the fuel connect valve? |
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Definition
| To balance fuel by gravity transfer |
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Term
| What is indicated by an illuminated FUEL FILTER light? |
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Definition
| An impending bypass of the Fuel filter (>18 psid) |
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Term
| What is the maximum pressure for single point refueling? |
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Definition
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Term
| What does an illuminated FUELING light indicate? |
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Definition
| The fuel panel switch is selected ON, THE defueling valve is open |
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Term
| Where does the fueling panel get power from? |
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Definition
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Term
| If an automatic level control circuit fails and causes an overfill, what happens? |
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Definition
| An overfill sensor in each outboard tank closes the related valve and illuminates the OVERFULL light to come on |
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Term
| To achieve maximum capacity what fueling procedure is used? |
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Definition
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Term
| How is defueling accomplished? |
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Definition
| Pressure defueling uses Standby pumps to pump fuel from the aircraft, Suction is used from the fuel truck. |
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Term
| 1.) The hydraulic system supplies pressure for the operation of what? 10-1 |
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Definition
| Flaps, Landing gear, Brakes, and Nose wheel steering |
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Term
| 2.) Are Hydraulic lines routed to their respective systems inside the aircraft? 10-1 |
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Definition
| No, they are routed externally in “hydraulic tunnels” |
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Term
| 3.) What pressurizes the main hydraulic reservoir? 10-2 |
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Definition
| Emergency accumulator circuit |
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Term
| 4.) What is the back up to the emergency accumulator for pressurizing the reservoir? 10-2 |
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Definition
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Term
| 5.) What would cause a HYDR CWP light to illuminate with all gauges normal? 10-2 |
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Definition
| High temperature has been noted in the main reservoir (116ºC) |
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Term
| 6.) What supplies hydraulic fluid to the Hand Pump reservoir? 10-2 |
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Definition
| Overflow fluid from the main reservoir |
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Term
| 7.) What does the Hand Pump reservoir supply fluid to? 10-2 |
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Definition
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Term
| 8.) What does the main reservoir supply fluid to? 10-2 |
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Definition
| Overflows to the Hand Pump Reservoir, Electric hydraulic pump |
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Term
| 9.) What is the normal source of pressure for the hydraulic system? 10-2 |
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Definition
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Term
| 10.) What electrical bus supplies power to the electric pump in AUTO? 10-2 |
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Definition
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Term
| 11.) What electrical bus supplies power to the electrical pump in OVRD? 10-2 |
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Definition
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Term
| 12.) Why is it important to verify the BUS TIE CONN light illuminates during left engine shutdown while taxiing? 10-2 |
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Definition
| Hydraulic pump is powered from the left main bus |
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Term
| 13.) With a failure of the electric hydraulic pump can the main accumulator be pressurized? 10-2&3 |
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Definition
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Term
| 14.) What does the Main Accumulator supply pressure to? 10-3 |
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Definition
| Nose wheel steering, Flap actuation, Gear retraction and extension, To pressurize the brake accumulators |
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Term
| 15.) At what pressure does the Pressure relief valve vent pressure? 10-3 |
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Definition
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|
Term
| 16.) Is there protection for an overpressure of the hydraulic system? 10-3 |
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Definition
| Yes the pressure relief valve |
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Term
| 17.) Where does the Pressure relief valve return fluid to? 10-3 |
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Definition
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Term
| 18.) Where does the Fluid from the hand pump get returned to after use? 10-3 |
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Definition
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Term
| 19.) What is the most likely problem if a HYDR CWP light is illuminated and hydraulic quantity, main accumulator and inboard accumulator pressure all indicate low? 10-3 |
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Definition
| A leak in the inboard brake |
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Term
| 20.) What is the normal operating pressure in AUTO mode? 10-4 |
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Definition
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Term
| 21.) What is the operating pressure when the pump is in OVRD? 10-4 |
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Definition
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Term
| 22.) What causes the electric pump to automatically activate? 10-4 |
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Definition
| Pressure in the main accumulator decreases below 2100 psi, Landing gear is extended or retracted |
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Term
| 23.) What can the Hand Pump pressurize? 10-4 |
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Definition
| All accumulators except the Emergency accumulator |
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Term
| 24.) The selector valve facilitates pressure of what? 10-4 |
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Definition
| Main, Inboard brake, and Outboard brake accumulators |
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Term
| 25.) Can the landing gear be hand pumped down with a total electrical failure? 10-4 |
|
Definition
| No, the gear requires left battery bus power to operate the selector valve |
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Term
| 26.) Can the flaps be hand pumped with a total electrical failure? 10-4 |
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Definition
| No, flap operation requires left battery bus to be powered |
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Term
| 27.) With an outboard brake accumulator leak, can the main accumulator be pressurized by the Hand Pump? 10-3&5 |
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Definition
| No, the Main accumulator will equalize to the leaking brake accumulator |
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Term
| 28.) Which accumulators have check valves? 10-5 |
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Definition
| Emergency, Inboard and Outboard brake accumulators |
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|
Term
| 29.) What is the pressure of the nitrogen pre-charge in the accumulators? 10-5 |
|
Definition
|
|
Term
| 30.) What pressure is read on the gauges if hydraulic qty in the accumulator decreases to zero, leaving just the nitrogen pre-charge pressure? 10-5 |
|
Definition
| Zero psi on the gauges in the flight deck. The actual accumulators should read 1650psi in the nose well |
|
|
Term
| 31.) What is the purpose of the Nitrogen charged accumulators? 10-5 |
|
Definition
| To absorb pump pulsations and surges caused by large fluid demands |
|
|
Term
| 32.) What pressure triggers a HYDR↓ CWP light to illuminate? 10-2&5 |
|
Definition
| Pressure less than 1850 psi, or High Temp |
|
|
Term
| 33.) Which accumulators will trigger the HYDR CWP light to illuminate with pressure below 1850 psi? 10-5 |
|
Definition
| Main and Emergency accumulators |
|
|
Term
| 34.) What is the Purpose of the Emergency accumulator? 10-2&5 |
|
Definition
| Emergency extension for up lock release, To pressurize the Main reservoir |
|
|
Term
| 35.) What is the indication for a hydraulic filter that is clogged and bypassed? 10-5 |
|
Definition
| Clog indicator button pops up on the filter housing |
|
|
Term
| 36.) What is being pressurized by the Hand Pump when the selector is in the FLAPS LDG GR position? 10-5 |
|
Definition
|
|
Term
| 37.) How many hydraulic accumulators are on the Saab 340? 10-5 |
|
Definition
|
|
Term
| 38.) Why do the brakes have 2 accumulators? 10-5 |
|
Definition
| One for inboard and one for outboard brake systems in case of a leak in one system brakes are still available |
|
|
Term
| 39.) What does the Emergency landing gear extension use hydraulic pressure for? 10-5 |
|
Definition
| To release the up locks and allow the gear to free fall |
|
|
Term
| 40.) Can the flaps be extended AND retracted with only the Hand Pump? 10-5 |
|
Definition
| Yes, by pressurizing the main accumulator |
|
|
Term
| 41.) Where can the 1650 psi Nitrogen pressure be checked? 10-6 |
|
Definition
| Nose wheel well, right side of the aircraft |
|
|
Term
| 42.) Where are the hydraulic filter bypass pins located? 10-6 |
|
Definition
| Nose wheel well on the left side of the aircraft |
|
|
Term
| 43.) What does an illuminated HYDR PCW light indicate? 10-7 |
|
Definition
| Pressure in the main or emergency accumulators less than 1850 psi, High temp in the main reservoir (116ºC) |
|
|
Term
| 44.) Does the HYDR CWP light illuminate for low quantity? 10-7 |
|
Definition
|
|
Term
| 45.) Does the HYDR CWP light illuminate for high pressure? 10-7 |
|
Definition
|
|
Term
| 46.) Where is the Hand Pump handle stored? 10-8 |
|
Definition
| Behind the First Officer seat on the bulkhead |
|
|
Term
| 47.) Is the electric hydraulic pump protected by a resettable circuit breaker? |
|
Definition
|
|
Term
| 1.) What is required for the SAAB to be dispatched into know icing conditions? 11-1 |
|
Definition
| All ice protection systems must be operable |
|
|
Term
| 2.) Can the SAAB be dispatched into icing conditions with side windshield INOP? 11-1 |
|
Definition
| Yes, if only one side window heat is INOP there is MEL relief. |
|
|
Term
| 3.) Which electrical ice protection system is NOT powered by the AC Generator? 11-2 |
|
Definition
|
|
Term
| 4.) What powers the Standby Pitot heat? 11-2 |
|
Definition
|
|
Term
| 5.) How long does it take for the standby pitot to reach full operating temperature? 11-2 |
|
Definition
|
|
Term
| 6.) What is powered automatically when the 1st AC GEN comes online? 11-3 |
|
Definition
| Main Pitot tubes, temp probe, AOA vanes |
|
|
Term
| 7.) What is the power source for the OAT probe? 11-5 |
|
Definition
|
|
Term
| 8.) Is there a pilot controlled switch for the OAT Probe heating? 11-5 |
|
Definition
|
|
Term
| 9.) When is the OAT probe heated? 11-5 |
|
Definition
| From the time the gear is retracted till landing |
|
|
Term
| 10.) When is power supplied to the AOA vanes for heating? 11-6 |
|
Definition
| As soon as an AC Generator is online |
|
|
Term
| 11.) What is the power source for the windshield heat? 11-7 |
|
Definition
| 115 Volt “wild” frequency bus |
|
|
Term
| 12.) What powers the 115 Volt “wild” frequency bus? 11-7 |
|
Definition
|
|
Term
| 13.) What is the time limit for side windshield heating? 11-8 |
|
Definition
| Operate in NORM for 7 minutes before selecting HIGH |
|
|
Term
| 14.) What is indicated by an illuminated L/R SIDE or L/R FRONT lights? 11-8 |
|
Definition
| Either an overheated windshield or a controller fault |
|
|
Term
| 15.) If power is interrupted to a windshield causing a FRONT/SIDE light to illuminate, will the light extinguish when power is restored? 11-8 |
|
Definition
| No, the switch must be turned off and then back on again to reset the system |
|
|
Term
| 16.) What does the AIR SUPPLY switch control? 11-10 |
|
Definition
| Controls a shut off valve to allow bleed air to the boot system |
|
|
Term
| 17.) What stage does the bleed air for engine anti-ice come from? 11-10 |
|
Definition
|
|
Term
| 18.) When deflated what holds the boots “down” tight to the wing? 11-10 |
|
Definition
|
|
Term
| 19.) What items use Bleed Air for Ice protection? 11-10&13 |
|
Definition
| Boot De-Icing, Engine split lip, engine guide vanes |
|
|
Term
| 20.) What order are the boots cycled in one cycle? 11-10 |
|
Definition
| Stab, outboard wing, inboard wing, stab |
|
|
Term
| 21.) Will the deice boots inflate with both bleed valves closed? 11-10 |
|
Definition
|
|
Term
| 22.) Will boots inflate with H/P valves closed? 11-10 |
|
Definition
|
|
Term
| 23.) Can boot inflation be monitored? 11-10 |
|
Definition
| Yes, by watching the boot indicator lights |
|
|
Term
| 24.) How often are the boots cycled when operating in “CONT”? 11-10 |
|
Definition
|
|
Term
| 25.) Does the CWP ICE PROT light illuminate with all the Icing systems? |
|
Definition
|
|
Term
| 26.) What is indicated by an illuminated DE-ICE OV TEMP light? 11-10 |
|
Definition
| An over temperature has been noted in the boot system (>150ºC) |
|
|
Term
| 27.) What is indicated by an illuminated TIMER light? 11-11 |
|
Definition
| The de-ice timer valves are malfunctioning |
|
|
Term
| 28.) Can the pilot manually de-ice just the wings? 11-11 |
|
Definition
|
|
Term
| 29.) Can the pilot manually de-ice just the stabilizer? 11-11 |
|
Definition
|
|
Term
| 30.) How can the pilot de-ice just the outboard wing section? 11-11 |
|
Definition
| By pressing and holding the outboard push button for 6 seconds |
|
|
Term
| 31.) Why are HP valves kept in AUTO during flight in icing conditions? 11-11 |
|
Definition
| To insure proper boot inflation at low power settings |
|
|
Term
| 32.) What is indicated by an illuminated blue ENG ANTI-ICE light on the status panel? 11-13 |
|
Definition
| The associated Engine Intake switch is on |
|
|
Term
| 33.) Does the blue ENG ANTI-ICE status panel light extinguish with a failure of the Intake heat? 11-13 |
|
Definition
|
|
Term
| 34.) Which light on the status panel does NOT indicate system working properly? 11-13 |
|
Definition
|
|
Term
| 35.) Which ice protection system can not be transferred to the opposite side AC GEN? 11-13 |
|
Definition
|
|
Term
| 36.) How is the inlet lip heated? 11-13 |
|
Definition
|
|
Term
| 37.) How are the inlet frame vanes heated? 11-13 |
|
Definition
|
|
Term
| 38.) How is the splitter lip and guide vanes heated? 11-13 |
|
Definition
|
|
Term
| 39.) What controls bleed air to the splitter lip and guide vanes? 11-13 |
|
Definition
| Anti-Ice start bleed valve (AISBV) |
|
|
Term
| 40.) What is indicated by an illuminated L AIR VALVE light? 11-14 |
|
Definition
| Associated Air valve is not positioned properly |
|
|
Term
| 41.) What is indicated by an illuminated INTAKE light? 11-14 |
|
Definition
| Intake heat has failed or lost one or more phases |
|
|
Term
| 42.) Is prop ice protection used as a de-ice or anti-ice system? 11-15 |
|
Definition
|
|
Term
| 43.) When is Prop De-Ice turned on? 11-16 |
|
Definition
| When ice accretion is observed and SAT is -5ºC or colder |
|
|
Term
| 44.) What temperatures is NORM used for prop de-ice? 11-16 |
|
Definition
|
|
Term
| 45.) At what temperature does prop de-ice switch to MAX? 11-16 |
|
Definition
| Colder than 12ºC with ice accretion |
|
|
Term
| 46.) Why is it important to operate the props only after ice accretion? 11-16 |
|
Definition
|
|
Term
| 47.) What is “run back” ice? 11-16 |
|
Definition
| Ice that melt and refreezes on the unheated section |
|
|
Term
| 48.) How much thrust is lost with “run back” ice on the props? 11-16 |
|
Definition
| Up to 30 percent of thrust |
|
|
Term
| 49.) Can the MAX mode be used between temperatures of -5ºC and -12ºC? 11-16 |
|
Definition
| Yes if propeller vibrations occur MAX can be used up to -10ºC until vibrations dissipate |
|
|
Term
| 50.) What is the procedure for switching from NORM to MAX on prop heat? 11-16 |
|
Definition
| Turn switch off before switching to MAX to avoid nuisance cautions |
|
|
Term
| 51.) Which Ice protection systems have a Flight Status panel light? 11-16 |
|
Definition
| Prop De-Ice, and Engine Intake |
|
|
Term
| 52.) What does an illuminated blue PROP DE-ICE light on the status panel indicate? |
|
Definition
| Prop De-ice is working properly |
|
|
Term
| 53.) What is the difference between the Engine and Prop status panel lights? 11-13&16 |
|
Definition
| Engine is switch only and the prop is system status |
|
|
Term
| 54.) What is indicated by an illuminated L AC GEN light? |
|
Definition
| Left AC GEN not supplying power |
|
|
Term
| 55.) What is indicated if a PROP DE-ICE status light is extinguished? 11-16 |
|
Definition
| Either the switch is turned off or the system malfunctioned |
|
|
Term
| 56.) What are the cycle times in NORM for Prop De-Ice? 11-16 |
|
Definition
| 11 seconds on 79 seconds off |
|
|
Term
| 57.) What are the cycle times in MAX for Prop De-Ice? 11-16 |
|
Definition
| 90 seconds on 90 seconds off |
|
|
Term
| 58.) What is indicated with an illuminated PROP light on the overhead panel? 11-16 |
|
Definition
| Associated prop de-ice system is malfunctioning |
|
|
Term
| What is indicated by an illuminated STBY PITOT light? |
|
Definition
| Standby Pitot is not powered. |
|
|
Term
| 60.) What is the purpose of the Park system on the windshield wiper? 11-22 |
|
Definition
| To return the wiper to the stowed position |
|
|
Term
| 1.) How many gear doors are there on each main gear? 12-1 |
|
Definition
|
|
Term
| 2.) How are the main gear doors attached to the gear? 12-1 |
|
Definition
| 2 doors mechanically linked and a 3rd door that is rigidly attached |
|
|
Term
| 3.) How is the gear door opened during preflight for inspection? 12-1 |
|
Definition
|
|
Term
| 4.) Does the gear swing forward or aft during retraction? 12-1 |
|
Definition
|
|
Term
| 5.) What is used for normal Gear extension and retraction? 12-1 |
|
Definition
|
|
Term
| 6.) What centers the nose wheel for retraction? 12-2 |
|
Definition
| Centering cams within the strut |
|
|
Term
| 7.) What is used to lock the gear in the down position? 12-3 |
|
Definition
| Over center extension and Hydraulic pressure |
|
|
Term
| 8.) What locks the gear up? 12-4 |
|
Definition
|
|
Term
| 9.) What is used to open the up lock during normal gear extension? 12-4 |
|
Definition
|
|
Term
| 10.) How many weight on wheel switches per main gear? 12-4 |
|
Definition
|
|
Term
| 11.) How many weight on wheels on the nose gear? 12-4 |
|
Definition
|
|
Term
| 12.) How is the gear retracted if a weight on wheel switch fails? 12-4 |
|
Definition
| By pressing the down lock release pushbutton |
|
|
Term
| 13.) What lights illuminate while pressing the gear test button? 12-4 |
|
Definition
| Left, Nose, Right main gear lights and an Amber gear lever light |
|
|
Term
| 14.) Which gear must be locked down for the Amber light to extinguish? 12-4 |
|
Definition
| All gear must be down and locked |
|
|
Term
| 15.) When is a CONFIG warning given for an unsafe Landing Gear condition? 12-4 |
|
Definition
| Any gear is not down and locked AND RA <500’AGL, or 1 or both power levers are below the 64º angle |
|
|
Term
| 16.) What altitude does the EGPWS provide “to low gear”? 12-4 |
|
Definition
|
|
Term
| 17.) At what flap angle with gear not down and locked is a CONFIG WARNING alert given? 12-4 |
|
Definition
|
|
Term
| 18.) Which CWP light will illuminate if the gear is not locked down by 500’ RA? 12-4 |
|
Definition
|
|
Term
| 19.) What prevents gear retraction on the ground? 12-5 |
|
Definition
| A spring loaded latch pin |
|
|
Term
| 20.) What does pushing the Down lock release button do? 12-5 |
|
Definition
| Mechanically releases the latch pin |
|
|
Term
| 21.) What is used for emergency extension? 12-7 |
|
Definition
| Gravity, airflow, and assisted by springs |
|
|
Term
| 22.) Does the gear handle have to be in the down position for emergency EXTENSION? 12-7 |
|
Definition
|
|
Term
| 23.) What’s lost if Emergency extension is used and the gear handle is not down? 12-17 |
|
Definition
|
|
Term
| 24.) After Emergency extension will the gear doors be open or closed? 12-7 |
|
Definition
|
|
Term
| 25.) During Emergency Extension what separates the gear doors from the actuating linkages? 12-7 |
|
Definition
|
|
Term
| 26.) How are the brake pads preflight checked? 12-9 |
|
Definition
| By observing the wear pins |
|
|
Term
| 27.) What determines if the brake pad wear indicators are within limits? 12-9 |
|
Definition
| If the indicators extend above the circular casing |
|
|
Term
| 28.) How are the brakes operated? 12-9 |
|
Definition
|
|
Term
| 29.) How many brake systems on the aircraft? 12-9 |
|
Definition
| 2, Inboard and outboard brakes |
|
|
Term
| 30.) At what speed does the Anti-skid cut out? 12-10 |
|
Definition
|
|
Term
| 31.) What protects the tire from over pressure due to brake temperatures? 12-10 |
|
Definition
| Pressure relief blow out plugs |
|
|
Term
| 32.) What is the purpose of the Anti-skid system? 12-10 |
|
Definition
| To limit brake pressure and avoid locked wheels |
|
|
Term
| 33.) How does the Anti-skid determine if a wheel is “skidding”? 12-10 |
|
Definition
| Compares inboard and outboard wheel speed |
|
|
Term
| 34.) What is required for Anti-skid operation? 12-11 |
|
Definition
Anti-skid switch ON and landing gear handle down: PL below flight idle +3 sec. Or WOW switch activated +3 sec. Or Average Wheel Speed above 50kts |
|
|
Term
| 35.) What is touchdown brake protection? 12-12 |
|
Definition
| Prevents brake application for 3 seconds after main gear compression or wheel speed exceeds 50Kts |
|
|
Term
| 36.) Can the brakes be set without getting a CWP light? 12-12 |
|
Definition
|
|
Term
| 37.) Can the brakes be set without the PARK BRK ON CWP light illuminated? 12-12 |
|
Definition
| Yes, (1500psi sets the brake, 1700psi required for light to illuminate) |
|
|
Term
| 38.) At what psi does the PARK BRK ON light extinguish? 12-12 |
|
Definition
|
|
Term
| 39.) What psi is required for the PARK BRK ON light to illuminate? 12-12 |
|
Definition
|
|
Term
| 40.) How is the parking brake set? 12-12 |
|
Definition
| Pulling the handle up, rotating 30º clockwise, and pushing the brake pedals |
|
|
Term
| 41.) What does the lockout switch do to the nose wheel steering system? 12-13 |
|
Definition
| When activated, inhibits tiller function to prevent NWS activation during ground handling ops |
|
|
Term
| 42.) When must the nose gear pin be installed? 12-13 |
|
Definition
| During pushback or towing |
|
|
Term
| 43.) How many degrees of steering does the NWS provide? 12-13 |
|
Definition
| 60º either side of center |
|
|
Term
| 44.) What does pushing the tiller down do electrically? 12-13 |
|
Definition
| Electrically opens the steering shutoff valve |
|
|
Term
| 45.) What does pushing the tiller down do mechanically? 12-13 |
|
Definition
| Mechanically engages the tiller wheel |
|
|
Term
| 46.) What is the purpose of the C-Clip (gear pin)? 12-13 |
|
Definition
| Deactivates the steering system for ground handling |
|
|
Term
| 47.) What is the max steering deflection for operations? 12-13 |
|
Definition
| 120º or 90º (depending on MOD) |
|
|
Term
| 48.) Can the nose wheel rotate all the way around? 12-13 |
|
Definition
|
|
Term
| 49.) What is indicated by an illuminated Anti-skid CWP light? 12-20 |
|
Definition
| A system fault or gear is down with Anti-skid off |
|
|
Term
| 1) What are the power sources for the DC electrical system? |
|
Definition
| Batteries, External power, Generators |
|
|
Term
| 2) How many Ni-Cad batteries does the Saab 340 have? |
|
Definition
| Seven - 2 main, 5 emergency lighting under cabin floor |
|
|
Term
| 3) What type of main batteries does the Saab 340 have? |
|
Definition
| 24 volt 43 Amp hour Ni-Cad batteries |
|
|
Term
| 4) Where are the main batteries located? |
|
Definition
| In the respective wing-fuselage fairing |
|
|
Term
| 5) How are the batteries ventilated for cooling? |
|
Definition
| By ram air in flight, and fans on the ground |
|
|
Term
| 6) What are the 4 separate parts of the electrical system? |
|
Definition
| 28V DC, 115/26V AC, Emergency DC power, “wild” frequency 115V AC |
|
|
Term
| 7) What is the power source for the 115/26V AC system? |
|
Definition
| Two - 115/26V AC inverters powered by the DC system |
|
|
Term
| 8) What is the power source for the emergency power system? |
|
Definition
| Powered from the 28V DC system or the emergency battery |
|
|
Term
| 9) What is the power source for the “wild” frequency 115V AC system? |
|
Definition
| Two engine driven AC generators |
|
|
Term
| 10)What is the “wild” frequency 115V AC power used for? |
|
Definition
|
|
Term
| 11)What makes up the 28V DC electrical system? |
|
Definition
| One generator and one battery for each side |
|
|
Term
| 12)Where is the “wild” frequency generator located? |
|
Definition
|
|
Term
| 13)What cools the DC generator? |
|
Definition
| Ram air in flight and fans on the ground |
|
|
Term
| 14)An illuminated GEN OV TEMP light on the overhead panel indicates what? |
|
Definition
| Generator is overheated (150ºC) |
|
|
Term
| 15)What is indicated by an illuminated L/R MAIN BUS light? |
|
Definition
| The associated main bus is unpowered |
|
|
Term
| 16)What is indicated by an illuminated NO BAT START light? |
|
Definition
| One or both battery temps has reached 57ºC |
|
|
Term
| 17)What is indicated by an illuminated EMER PWR light? |
|
Definition
| Either the emergency bus is not supplied power or the battery had decreased below 24V |
|
|
Term
| 18)What is indicated by an illuminated L/R GEN light? |
|
Definition
| The respective Gen relay is open, “gen off line” |
|
|
Term
| 19) The starter/generators are rated at what voltage? |
|
Definition
|
|
Term
| 20)When will the external power magnetic switch release automatically? |
|
Definition
| GPU voltage drops below 10V or exceeds 31V or During an engine start if the GPU voltage drops below 7V |
|
|
Term
| 21)What is the voltage limit during a start with the start switch held to start? |
|
Definition
| Voltage may drop to 7 volts |
|
|
Term
| 22)What is the amperage of the 28V GPU? |
|
Definition
|
|
Term
| 23)What does the blue EXT PWR AVAIL light indicate? |
|
Definition
| GPU is connected to the aircraft and supplying at least 4 volts |
|
|
Term
| 24)How many alternators are installed on each engine? |
|
Definition
| One Engine driven alt to provide electrical power to the engine only |
|
|
Term
| 25)How many generators on each engine? |
|
Definition
| Two, one starter generator and one AC generator |
|
|
Term
| 26)What is the starter/generator amp limits? |
|
Definition
| 600 amps for 5 minutes then 400 amps |
|
|
Term
| 27) The starter/generators are rated at how many amps? |
|
Definition
|
|
Term
| 28)With the GPU powering the aircraft what lights illuminate on the DC ELEC panel? |
|
Definition
| White EXT PWR, L/R GEN, L/R BAT |
|
|
Term
| 29)With the aircraft on battery power alone what lights illuminate on the DC ELEC panel? |
|
Definition
| L/R GEN, L/R MAIN BUS, Bus Tie Conn |
|
|
Term
| 30)What is the voltage required for a GPU to be used? |
|
Definition
|
|
Term
| 31)What type of Battery is used for the Emergency battery? |
|
Definition
| 24 volt 5 amp hour lead acid battery |
|
|
Term
| 32)When is the starter/generator acting as a starter? |
|
Definition
| During engine start. When engine Ng is between 0-55% |
|
|
Term
| 33)What is the purpose of the Series/Parallel relay? |
|
Definition
| During a battery start of the first engine the batteries are connected in series to produce 48 volts. |
|
|
Term
| 34)Are batteries being used for a cross generator start? |
|
Definition
| Yes, the batteries assist the generator to achieve a faster, cooler start |
|
|
Term
| 35)When is the GEN relay automatically opened? |
|
Definition
| GCU detects a malfunction, “except overheating”, External power is used, Fire handle has been pulled |
|
|
Term
| 36)When is the Gen relay light expected to be on? |
|
Definition
| When the respective Gen switch is off, on GPU, Fire handle pulled, Ng <55%, Gen failure. |
|
|
Term
| 37)What minimum Ng is required to connect the starter/generator to the GEN BUS? |
|
Definition
|
|
Term
| 38)What is indicated by an illuminated L/R ESS BUS light? |
|
Definition
| Associated bus is not powered |
|
|
Term
| 39)What is indicated by an illuminated L/R BAT HOT light? |
|
Definition
| Associated battery temp has exceeded 71ºC |
|
|
Term
| 40)What other light(s) would be on when a BAT HOT light is illuminated? |
|
Definition
| NO BAT START, L/R BATT, Elec on CWP |
|
|
Term
| 41)What protection occurs when a battery temp reaches 71oC |
|
Definition
|
|
Term
| 42) Can the battery be connected to supply power to the GEN bus with a BAT HOT? |
|
Definition
| Yes, in an emergency the BAT switch can be set to OVRD |
|
|
Term
| 43)What is the purpose of the Bus Tie relay? |
|
Definition
| To connect the left and right busses to run off one power source |
|
|
Term
| 44)What is indicated by an illuminated BUS TIE CONN light? |
|
Definition
| The bus tie relay is closed |
|
|
Term
| 45)What are three reasons the Bus Tie relay closes? |
|
Definition
| To supply L and R GEN BUS when EXT PWR is on, To enable power supply to both L & R Gen Bus from only one GEN, To connect the two main batteries |
|
|
Term
| 46)What is the purpose of the bus tie over-current relay? |
|
Definition
| To protect the Main Distribution system in case of a short |
|
|
Term
| 47) Bus Tie relay opens if the over-current exceeds how many amps? |
|
Definition
|
|
Term
| 48) Can the Bus Tie over-current be reset manually? |
|
Definition
| Yes, through the K-1 reset button located on the captains circuit breaker panel. |
|
|
Term
| 49) Can the Generators be online with EXT PWR on? |
|
Definition
| No, the relay automatically opens |
|
|
Term
| 50)What 7 items can be powered by the Emergency battery? |
|
Definition
| Master Warning, bus tie conn, Audio back-up, fire detection, tailpipe hot det., emergency voltage indication, Stby Instr. Emer. Lighting |
|
|
Term
| 51)What is required to close the Utility Bus relay (RCCB)? |
|
Definition
| EXT PWR on or both generators on |
|
|
Term
| 52)What three conditions must be met for the GEN relay to close? |
|
Definition
| EXT PWR must be off, engine start complete, Gen field reset |
|
|
Term
| 53) The left battery is connected to which bus? |
|
Definition
|
|
Term
| 54)What bus is used for battery charging? |
|
Definition
| Respective GEN bus with at least one generator online |
|
|
Term
| 55)Which bus is the right battery connected to? |
|
Definition
|
|
Term
| 56)What powers the Emergency Bus? |
|
Definition
| The L BATT BUS (batteries must be ON/OVRD) or the Emergency Battery |
|
|
Term
| 57)When does the Emergency battery begin to power the EMER BUS? |
|
Definition
| When the L Battery drops below 24 volts |
|
|
Term
| 58)What powers the Emergency Avionics Bus? |
|
Definition
| The Emergency Bus, when the ESS AVION switch is on |
|
|
Term
| 59)What items are on the EMER AVIONCS BUS? |
|
Definition
| VHF COMM 1 and Standby Horizon |
|
|
Term
| 60)What does an illuminated AC GEN light indicate? |
|
Definition
| Respective AC GEN not supplying power |
|
|
Term
| 61)What is the minimum prop RPM for an AC GEN to supply power? |
|
Definition
|
|
Term
| 62) If prop RPM drops below 1000 RPM, how is the AC GEN reset? |
|
Definition
| Automatically resets when prop RPM increases above 1000 RPM |
|
|
Term
| 63)What three conditions must be met for a battery relay to close? |
|
Definition
| BAT switch on, GPU off, Batt temp below 71C |
|
|
Term
| 64)What is indicated by an illuminated INVERTER light? |
|
Definition
| Inverter switch is set to OFF or associated Inverter has failed |
|
|
Term
| 65)With a failure of the 26V output of the inverter what warnings or cautions are given? |
|
Definition
| No CWP warnings or cautions, but an RMI failure and VOR CDI failure will occur |
|
|
Term
| 66)What limitation must be observed when a battery temp has reached 57ºC? |
|
Definition
|
|
Term
| 67)What limitation must be observed when a battery temp has reached 61ºC? |
|
Definition
| No cross generator start allowed |
|
|
Term
| 68)What limitation must be observed when a battery temp has reached 64ºC? |
|
Definition
|
|
Term
| 69)What is the minimum battery temperature for takeoff? |
|
Definition
|
|
Term
| 70)Why is the AC GEN called the “wild” frequency? |
|
Definition
| Frequency varies with prop RPM, 460Hz to 640Hz |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| General Electric CT7-9B turboprop |
|
|
Term
| Take-off Power + APR or go-around power Tq |
|
Definition
|
|
Term
|
Definition
| (max. 5 min) & (max. 2 min) 100% |
|
|
Term
|
Definition
|
|
Term
| Transient except Take-off (max 12 sec) Tq |
|
Definition
|
|
Term
| Take-off Power + APR or go-around power ITT |
|
Definition
| Max 5 min (940) Max 2 min (950) |
|
|
Term
|
Definition
| (max. 5 min) 917 (max. 2 min) 927 |
|
|
Term
|
Definition
|
|
Term
| Transient except Take-off (max 12 sec) ITT |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| Two start attempts with 3 minutes cooling between, then 25 minutes cooling before subsequent starts. |
|
|
Term
|
Definition
| Three 30-second ventilations with 3 minutes cooling between each, then a one-hour cooling period before subsequent starts or motoring. |
|
|
Term
| Maximum time with engaged starter |
|
Definition
| 70 seconds of which max 30 seconds plain motoring |
|
|
Term
| BAT start is not allowed if the battery temperature is below |
|
Definition
|
|
Term
| Minimum voltage for any battery start |
|
Definition
|
|
Term
| Minimum time between engine starts when starting subsequent engine. |
|
Definition
|
|
Term
| Continuous operation of the propeller on the ground |
|
Definition
|
|
Term
| FUEL TEMP LOW light must be |
|
Definition
|
|
Term
| XFEED and CONN VALVE switches shall be |
|
Definition
| OFF and CLOSED during takeoff and landing in normal operation |
|
|
Term
| Definition of Icing Conditions for Engine Anti- Icing |
|
Definition
| Whenever OAT or SAT is +10c or colder and visible moisture or when on ground standing water, slush, or snow on AOA. |
|
|
Term
| Engine Anti-Icing Operation |
|
Definition
| Engine anti-icing must be ON when in icing conditions, and maintained on for at least 5 min after exiting icing. |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Maximum Rough Air Penetration Speed, VRA |
|
Definition
| 190 KIAS up to 21 000 ft. ISA. Above this altitude, reduce the speed as indicated by the VMO pointer minus 30 kts. |
|
|
Term
| Minimum speed enroute with ice |
|
Definition
|
|
Term
| Minimum Airspeed for Icing Climb (no maneuvering) |
|
Definition
|
|
Term
| Minimum Airspeed for Icing Climb (maneuvering) below (MSA) |
|
Definition
|
|
Term
| Minimum Airspeed for Icing Climb above MSA, cruise, descent, holding and approach (Flaps 0) |
|
Definition
|
|
Term
| Minimum Airspeed for Icing Corrected VREF |
|
Definition
|
|
Term
| Minimum Airspeed for Icing Final Approach (maneuvering |
|
Definition
|
|
Term
| Minimum Airspeed for Icing Missed approach/go-around below MSA |
|
Definition
|
|
Term
| Airport Pressure Altitude |
|
Definition
|
|
Term
| Maximum Takeoff and Landing Tailwind Component |
|
Definition
|
|
Term
| Maximum Operating Altitude |
|
Definition
| 25,000 ft. pressure altitude |
|
|
Term
| Windshield Wipers Low Mode |
|
Definition
|
|
Term
| Windshield Wipers High Mode |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Battery Temperatures No Cross Gen Start Max for Takeoff |
|
Definition
|
|
Term
| Characteristics of a pressure transducer failure on PGB |
|
Definition
| the oil pressure indication will rapidly go to zero or to the upper limit of the gauge. |
|
|
Term
| PGB oil is also used for fuel heating what? |
|
Definition
| prevent icing in the fuel filter, lubrication, use in the propeller pitch control system |
|
|
Term
| PGB differential oil pressure transducer does what? |
|
Definition
| transducer provides signals to the flight deck indicator and low power (PL < FLT IDLE) oil pressure warning. |
|
|
Term
| PGB differential oil pressure switch provides? |
|
Definition
| The pressure switch provides signals to the high power (PL > FLT IDLE) oil pressure warning. |
|
|
Term
| PGB L/R ENG OIL PRESS CWP light. Same as engine, comes on when? |
|
Definition
| The warning comes below 25 psi (PL > FLT IDLE) and below 7 psi (PL < FLT IDLE). |
|
|
Term
|
Definition
| Wing and Stab boots, and propeller. |
|
|
Term
|
Definition
| Windshields, Engine ( Inlet, Main frame, IGVs & Spliter lip) Probes ( Pitot, OAT, & AOA) |
|
|
Term
| Which ice protection systems are electric? |
|
Definition
| Engine inlet, Propeller, Windshields, Pitot, OAT, and AOA. |
|
|
Term
| Which ice protection systems are Pneumatic? |
|
Definition
| Boots, Splitter lip and Inlet guide vanes. |
|
|
Term
| Which ice protection systems are hot oil systems? |
|
Definition
|
|
Term
| With failure of AC Gen what ice protection system will not auto transfer? |
|
Definition
|
|
Term
| With an AC Gen Bus failure, does the load transfer automatically? |
|
Definition
|
|
Term
| How do you transfer Ice protection with a AC Gen Bus failure? |
|
Definition
| Move L/R AC Gen switch to Load XFR. |
|
|
Term
| What are the three ways to inflate De-ice boots? |
|
Definition
| 1. Continuous 2. One-cycle 3> Manual. |
|
|
Term
| How long for a complete ice boot cycle? |
|
Definition
| 24 sec. 6 sec, for each boot. (Stab,outboard,inboard,stab) |
|
|
Term
| If cycling boots manually why inflate the Stabs twice? |
|
Definition
| Because the tail surfaces pick up ice faster than the wings. |
|
|
Term
| Which engine ice protection uses one phase? |
|
Definition
| Pitots, AOA, OAT, Side windshields. |
|
|
Term
| Which engine ice protection uses two phases? |
|
Definition
|
|
Term
| Which engine ice protection uses three phases? |
|
Definition
| Prop de-ice and engine intake. |
|
|
Term
| Reasons for getting L/R INTAKE light? |
|
Definition
| System failure, loss of DC control power, total or partial loss of AC power, over/under temps detected. |
|
|
Term
|
Definition
| Anti-Ice Start Blled Valve. Controlled by HMU. |
|
|
Term
|
Definition
| Regulates 5th stage air to the Splitter lip and Inlet guide vanes. Also At low Ng sends air to IPSD to help in FOD removal. |
|
|
Term
| AISBV discrepencies trigger what light? |
|
Definition
|
|
Term
| What does an amber L/R AIR VALVE light indicate? |
|
Definition
| Valve position not agreeing with selected position. |
|
|
Term
| How can you tell if the engine anti-ice is working in flight? |
|
Definition
| Torque will drop, ITT should rise. |
|
|
Term
| What does Amber L/R PROP light indicate? |
|
Definition
Loss of AC/DC power Timer failure Improper heating current
Blue prop deice lights extinguish Master caution, flashing amber ICE PROT on CWP |
|
|
Term
| How do you tell if you have a windshield anti-ice controller or DC power failure? |
|
Definition
| Loss of opposite windshield/side window anti-ice |
|
|
Term
| How do you tell if your windshield AC bus or Gen fails? |
|
Definition
| Loss of same side windshield/side window anti-ice. |
|
|
Term
| PPPWhat does the DE-ICE OV TEMP light indicate? |
|
Definition
| Illminates when bleed air suppl from either source becomes overheated. (>150c) |
|
|
Term
| AUTOCOARS LOW light illuminates when? |
|
Definition
| PLA <64 deg., Ng >55% on bith engines, Starter/Gen rpm >60% on both engines |
|
|
Term
| AUTOCOARS HIGH light illuminates when? |
|
Definition
| On both engines PLA >64deg. , P3 air >120psi, TRQ 50%. |
|
|
Term
| The synchrophaser system has authority to adjust propeller rpm to within? |
|
Definition
| Plus 10 PRPM of the governor setting. |
|
|
Term
| Where is the PROP SYNC switch located? |
|
Definition
| To the right of the flap handle. |
|
|
Term
| When does ENGINE OV TEMP illuminate? |
|
Definition
|
|
Term
| How is an oil leak usually charecterized on the gauge? |
|
Definition
| fluctuating oil pressure followed by pressure decreasing to approximately 20 psi. |
|
|
Term
| 1) What engines are on the Saab 340B? |
|
Definition
|
|
Term
| 2) How much power do the CT7-9B engines produce? |
|
Definition
| 1750 SHP at 35ºC at seal level |
|
|
Term
| 3) What controls the inlet variable guide vanes? |
|
Definition
| Hydromechanical unit, “HMU” |
|
|
Term
| 4) What is used to prevent bird ingestion into the engine? |
|
Definition
| Inlet protection device (inertial separator) |
|
|
Term
| 5) Where are large objects directed after being caught in the Inlet protection device? |
|
Definition
| Overboard through a duct on the underside of the nacelle |
|
|
Term
| 6) Where do small items such as sand and hail exit after being separated from airflow? |
|
Definition
| Through the separator duct and out the tailpipe |
|
|
Term
| 7) How many fuel pumps are installed on each engine? |
|
Definition
|
|
Term
| 8) What prevents power levers from being retarded below flight idle in flight? |
|
Definition
| Automatic Flight Idle Stop |
|
|
Term
| 9) The Flight Idle Stop automatically opens at touchdown with inputs from the what? |
|
Definition
| Both main gear downlock switches, Anti-skid computer (for wheel speed monitoring), Both weight-on-wheel systems |
|
|
Term
| 10)How is the FI Stop opened with a WOW failure? |
|
Definition
| By pulling the FI STOP OVRD knob |
|
|
Term
| 11)When is the FI Stop Automatically opened? |
|
Definition
| When either main gear is downlocked AND: Any wheel speed exceeds 25kts OR either WOW detects the Aircraft on the ground |
|
|
Term
| 12) If the gear is not retracted when does the FI stop automatically close? |
|
Definition
| Both WOW systems detect the A/C is airborne And All wheel speeds decrease below 9kts. |
|
|
Term
| 13)What indication is given if while on the ground with the FI STOP OVRD knob pulled, the left engine is started? |
|
Definition
| A red CONFIG Master warning |
|
|
Term
| 14) Can the config warning be cancelled for a FI STOP OVRD knob pulled while starting the left engine? |
|
Definition
| No. the condition lever must be returned to FUEL OFF |
|
|
Term
| 15)What is the placarded operating range for condition levers? |
|
Definition
| FUEL OFF, FEATHER, START, UNF, MIN-MAX, T/M |
|
|
Term
| 16)What is the placarded operating range for the power levers? |
|
Definition
|
|
Term
| 17)What position on the power lever is identified by a detent? |
|
Definition
|
|
Term
| 18) The engine driven alternator supplies AC power to what 3 engine systems? |
|
Definition
| Ignition exciter power supply, DECU power supply, ENG (Ng) indication (RPM of the AC Generator) |
|
|
Term
| 19)Are there any controls or indications for the Engine Electrical System? |
|
Definition
|
|
Term
| 20)What are the three modes of the ignition system? |
|
Definition
| Start ignition, Auto ignition, Continuous ignition |
|
|
Term
| 21)When is Start Ignition available? |
|
Definition
| When the switch is in NORM, ignition is activated when the start relay closes and terminates when the start relay opens at the end of a start cycle |
|
|
Term
| 22)Auto Ignition occurs when the DECU detects what? |
|
Definition
| Engine flameout, or Np overspeed |
|
|
Term
| 23)How long is Auto ignition activated for? |
|
Definition
|
|
Term
| 24)When is Continuous Ignition active? |
|
Definition
| When the switch is selected to CONT or when power is lost from the respective battery bus |
|
|
Term
| 25)When will the respective IGN light illuminate on the status panel? |
|
Definition
| Anytime the switch is selected to CONT or when NORM is selected and any of the following occur: Engine start cycle, Auto relight is activated, Control power is lost, The power turbine overspeeds. |
|
|
Term
| 26)What is used to prevent fuel filter icing? |
|
Definition
|
|
Term
| 27)What is the heat source for the fuel heater? |
|
Definition
|
|
Term
| 28) Can the engine operate without a working main pump? |
|
Definition
| Yes, standby pressure is sufficient |
|
|
Term
| 29) Can the engine operate without a HP pump from the HMU? |
|
Definition
|
|
Term
| What functions does the HMU provide? |
|
Definition
| Fuel scheduling through the metering valve for Ng governing, Controls actuation of the inlet guide vanes and anti-ice start bleed valve, Protects the gas generator spool from overspeeding, Accomplishes engine shutdown by means of the fuel shutoff valve. |
|
|
Term
| 31)How does the HMU protect the gas generator from overspeeding? |
|
Definition
| By automatically shutting fuel off at 110% Ng |
|
|
Term
| The DECU accomplishes what functions? |
|
Definition
| Np overspeed protection, Auto ignition, Bottom Governing, Engine gauge indications |
|
|
Term
| 33)At what speed does the DECU shut off fuel to protect the Np for overspeeding? |
|
Definition
| (25000 power turbine RPM) or 1572 PRPM |
|
|
Term
| 34)When will the fuel shut off valve be reopened due to a prop overspeed? |
|
Definition
| When prop RPM decreases below 1572 or (power turbine RPM decreases below 25000 ) |
|
|
Term
| 35)What prop RPM does bottom governing maintain? |
|
Definition
|
|
Term
| 36)During maximum reversing prop RPM increases to what RPM? |
|
Definition
|
|
Term
| 37)Where must the condition lever be in order to obtain bottom governing? |
|
Definition
|
|
Term
| 38)What controls CTOT and APR operation? |
|
Definition
| The DECU through the HMU torque motor |
|
|
Term
| 39) If a flameout should occurs with the CTOT on, what torque increase does the CTOT provide? |
|
Definition
| 7% increase in torque to the operating engine |
|
|
Term
| 40)What procedure is done to correct a DECU failure that is causing over-temp, over-torque, or prop overspeed? |
|
Definition
|
|
Term
| 41)While in T/M range where is fuel vented to? |
|
Definition
| Fuel is vented overboard so it is important not to stay in the T/M range |
|
|
Term
| 42)Does T/M lockout affect propeller governing? |
|
Definition
|
|
Term
| 43)What “normal” functions will be lost if while operating in T/M lockout? |
|
Definition
| Bottom governing, CTOT, and APR functions |
|
|
Term
| 44) Before selecting The CTOT switch to ON or APR power lever should be set to? |
|
Definition
| Within 10-15% of target torque |
|
|
Term
| 45)What temperature will the CTOT limit the engine to? |
|
Definition
|
|
Term
| 46)Does the CTOT provide torque and temperature protection during T/O and GA? |
|
Definition
| Yes, it will increase to selected torque value or 955ºC whichever is higher |
|
|
Term
| 47)Does the Autocoarsen switch have to be on to achieve APR function? |
|
Definition
|
|
Term
| 48)How is scavenge oil cooled? |
|
Definition
| By an oil-to–fuel heat exchanger and then directed to the inlet frame vanes to aid in inlet anti-icing which further cools the oil |
|
|
Term
| 49)On the Dowty props what is used to drive the engine to the feathered position? |
|
Definition
|
|
Term
| 50)With a loss of Prop oil press will the prop feather when the CL is placed in fuel off? |
|
Definition
|
|
Term
| 51)How is the Prop feathered after a loss of Prop oil pressure? |
|
Definition
| Using the MAN FEATHER pump |
|
|
Term
| 52)What is the quantity of oil in the prop gear box? |
|
Definition
|
|
Term
| 53)Of the 5 quarts in the prop gear box reservoir how much is kept for a reserve for emergency feathering? |
|
Definition
|
|
Term
| 54)With the PL above FLT IDLE what psi triggers an OIL PRESS cwp for the prop? |
|
Definition
|
|
Term
| 55)With the PL below FLT IDLE what psi triggers an OIL PRESS cwp for the prop? |
|
Definition
|
|
Term
| 56)What is the governor speed control range? |
|
Definition
|
|
Term
| 57)What are the 2 different modes for the Autocoarsen system? |
|
Definition
|
|
Term
| 63)What is used to keep both props at the same RPM? |
|
Definition
|
|
Term
| 64)Which prop is considered the Master prop in the Synchrophasing system? |
|
Definition
| The left prop is the master and controls the right prop (slave) |
|
|
Term
| 66) If an engine temperature of 1050ºC occurred what indication would be indicated on the gauge? |
|
Definition
|
|
Term
| 67)What is indicated by an illuminated AUTOCOARS cwp light? |
|
Definition
| Autocoarsen computer has failed |
|
|
Term
| 68)What is indicated by an illuminated ENG OIL PRESS light on the cwp? |
|
Definition
| The associated prop gear box OR engine oil pressure is low |
|
|
Term
| 69) Engine light off must occur within how many seconds of rotation? |
|
Definition
| 20 seconds “direct start only” |
|
|
Term
| 70)What is the time limit for ITT rise after fuel introduction? |
|
Definition
|
|
Term
| 71)What is the function of Bottom governing? |
|
Definition
| To maintain a minimum prop RPM during taxi and reverse operations |
|
|
Term
| 72) Is takeoff permitted with a FUEL LOW TEMP light illuminated? |
|
Definition
|
|
Term
| 73)What temperature will trigger a FUEL LOW TEMP light to illuminate? |
|
Definition
|
|
Term
| The amber CHIP DETECT light illuminates why? |
|
Definition
| Metal debris was detected in the returning scavenge oil. |
|
|
Term
| The amber OIL BYPASS indicates what? |
|
Definition
| Engine oilfilter is blocked, oil will bypass filter as needed. |
|
|
Term
| The red ENGINE OIL PRESS light illuminates why? |
|
Definition
| low differential oil pressure (<30 psi) is detected, for the Prop The warning comes below 25 psi (PL > FLT IDLE) and below 7 psi (PL < FLT idle) |
|
|
Term
| What fuel pumps are installed on each engine? 14-2 |
|
Definition
| HMU HP pump, Main fuel pump |
|
|
Term
| The Flight Idle Stop automatically opens at touchdown with what inputs? 14-4 |
|
Definition
| Both main gear down lock switches, Anti-skid computer (for wheel speed monitoring), Both weight-on-wheel systems |
|
|
Term
| If the gear is not retracted when does the FI stop automatically close? 14-5 |
|
Definition
| Both WOW systems detect the A/C is airborne, All wheel speeds decrease below 9kt |
|
|
Term
| What is indicated by an oil pressure gauge reading zero without a CWP light on? |
|
Definition
| Failure of the oil pressure gauge |
|
|
Term
| How many emergency exits are on the Saab 340? 13-1 |
|
Definition
|
|
Term
| Which side is recommended for emergency exit through the cockpit escape hatch? |
|
Definition
| Left side due to the strap length |
|
|
Term
| Where is the crash axe located? 13-5 |
|
Definition
| Behind the captains seat on the bulkhead |
|
|
Term
| How long is a PBE’s air supply useful? 13-6 |
|
Definition
|
|
Term
| How is the PBE activated? 13-6 |
|
Definition
| By pulling the straps on each side of the hood forward, then rearward to secure |
|
|
Term
| Why must the PBE hood not be removed in the presence of fire? 13-6 |
|
Definition
| Due to the oxygen concentrations in the hood |
|
|
Term
| What does a flashing red light on the Cabin Flashlight indicate? 13-7 |
|
Definition
| Batteries are serviceable |
|
|
Term
| How many O2 mask in the cockpit? 13-9 |
|
Definition
|
|
Term
| How many smoke goggles in the cockpit? 13-9 |
|
Definition
|
|
Term
| How many life vests are in the cockpit? 13-9 |
|
Definition
|
|
Term
| What type of Fire Extinguisher is located in the cockpit? 13-9 |
|
Definition
|
|
Term
| Where is the water extinguisher stored? 13-9 |
|
Definition
| Forward Entry storage area |
|
|
Term
| How is the water extinguisher activated? 13-9 |
|
Definition
| Turn the handle fully clockwise to puncture the CO2 cartridge in the handle |
|
|
Term
| What type of fires would the water extinguisher be used on? 13-9 |
|
Definition
|
|
Term
| What type of fire would the water extinguisher not be used on? 13-9 |
|
Definition
| Liquid fire, metal fire and anytime electricity is involved |
|
|
Term
| Where is the Automatic Defibrillator located? 13-10 |
|
Definition
| In the right hand overhead storage bin |
|
|
Term
| What is stored in the last right hand overhead storage bin? 13-10 |
|
Definition
| Grab-n-go kit (if available), AED unit, Enhanced Medical kit |
|
|
Term
| What is stored under seat 12D ? 13-10 |
|
Definition
| First Aid Kit, pbe, halon extinguisher |
|
|
Term
| When must the Emergency Lights be armed? 13-13 |
|
Definition
| Anytime the Aircraft is moving under its own power |
|
|
Term
| Where are the Emergency light batteries located? 13-13 |
|
Definition
|
|
Term
| How long do the Emergency Light Batteries last? 13-13 |
|
Definition
|
|
Term
| When do the Emergency lights automatically activate? 13-13 |
|
Definition
| Anytime power is lost is lost on the right main bus with the switch in ARMED |
|
|
Term
| How can the Emergency lights be turned off if activated automatically? 13-13 |
|
Definition
| The switch to off as long as there is right essential power available |
|
|
Term
| What is the main O2 system normally charged to? 13-16 |
|
Definition
|
|
Term
| What protects the O2 system from overpressure? 13-17 |
|
Definition
| A pressure relief valve vent |
|
|
Term
| What indicates a thermal discharge of the O2 system? 13-17 |
|
Definition
| The green blow out plugs are missing |
|
|
Term
| What does an illuminated OXYGEN CWP light indicate? 13-17 |
|
Definition
| O2 pressure is less than 800 ±35psi |
|
|
Term
| Does the main O2 knob have to be pulled to get PAX O2 to the outlets? 13-17 |
|
Definition
| Yes, both the main and the PAX O2 valve lever must be open |
|
|
Term
| What is the minimum psi for the portable O2 bottle? 13-24 |
|
Definition
|
|
Term
| How long will the portable O2 bottle last? 13-24 |
|
Definition
| Will flow for a minimum of 60 minutes |
|
|
Term
| What is the first aid bottle psi? 13-24 |
|
Definition
| GREEN ARC (minimum 1800 psi) |
|
|
Term
| How long will the first aid bottle last? 13-24 |
|
Definition
| Varies from 20 minutes to 30 minutes |
|
|
Term
| Who is authorized to use the medical kit? 13-27 |
|
Definition
|
|
Term
| L/R ENG FIRE Cwp indicates |
|
Definition
| Fire is detected in the associate engine compartment. (fire bell) |
|
|
Term
| AVIONIC SMOKE Cwp indicates |
|
Definition
| Smoke is detected in the avionics rack area |
|
|
Term
|
Definition
| Smoke is detected in the lavatory |
|
|
Term
| L/R ENG OIL PRESS Cwp indicates |
|
Definition
| The associated propeller gearbox (<25 Psi w/related PL above FLT IDLE, <7Psi w/PL below FLT IDLE) or ENGINE oil pressure is <30 Psi |
|
|
Term
| CARGO SMOKE Cwp indicates |
|
Definition
| Smoke is detected in the cargo area |
|
|
Term
| CABIN PRESS↓ Cwp indicates |
|
Definition
| Cabin pressure has exceeded 7.5 psid, or cabin altitude is above 10,000 ft. |
|
|
Term
| L/R TAIL P HOT Cwp indicates |
|
Definition
| Excessive temperature is detected in the associated tailpipe area |
|
|
Term
|
Definition
| Automatic trim has failed |
|
|
Term
|
Definition
| The airplane is not in proper configuration for takeoff or landing or starting left engine with AFIS override pulled |
|
|
Term
|
Definition
| The auto coarsen computer has failed |
|
|
Term
|
Definition
| The pitch trim synchronizer has failed |
|
|
Term
| RUDDER LIMIT Cwp indicates |
|
Definition
| The rudder limiter system has failed |
|
|
Term
| L/R FIRE DET FAIL Cwp indicates |
|
Definition
| The associated fire detection system has failed |
|
|
Term
|
Definition
| An annunciator has illuminated on the overhead fuel panel |
|
|
Term
|
Definition
| An annunciator has illuminated on the overhead electrical panel |
|
|
Term
|
Definition
| An annunciator has illuminated on the overhead ice protection panel |
|
|
Term
|
Definition
| An annunciator has illuminated on the overhead ENGINE panel |
|
|
Term
|
Definition
| An electrical malfunction in the flap system occurred |
|
|
Term
|
Definition
| An annunciator has illuminated on the overhead AIR COND panel |
|
|
Term
| PARK BRK ON Cwp indicates |
|
Definition
| The parking brake valve has trapped proper pressure |
|
|
Term
|
Definition
| Hydraulic pressure in the main or emergency accumulator is low (<1850 psi), or main reservoir fluid is hot (>116°C) |
|
|
Term
| EMER LTS UNARMED Cwp indicates |
|
Definition
| The flight deck EMER LIGHT switch is off |
|
|
Term
|
Definition
| Oxygen pressure is low (<800 psi) |
|
|
Term
| A-SKID INOP↓ Cwp indicates |
|
Definition
| Gear is down, and the antiskid system has failed or is turned off. |
|
|
Term
|
Definition
| Indication warns of avionics comparator malfunction |
|
|
Term
| AVIONICS VENT Cwp indicates |
|
Definition
|
|
Term
|
Definition
| An annunciator has illuminated on the overhead DOORS panel |
|
|
Term
| L/R STALL FAIL Cwp indicates |
|
Definition
| The associated stall warning system has failed |
|
|
Term
|
Definition
| Rudder gust lock did not disengage when released |
|
|
Term
| PUSHER SYSTEM Cwp indicates |
|
Definition
| The stick pusher system has failed |
|
|
Term
| STBY PITOT ICE PROTECTION Panel light indicates |
|
Definition
| The standby pitot mast heating is inoperative |
|
|
Term
| L/R ALPHA ICE PROTECTION Panel light indicates |
|
Definition
| The associated alpha probe heating is inoperative |
|
|
Term
| OAT ICE PROTECTION Panel light indicates |
|
Definition
| The outside air temp probe heating is inoperative |
|
|
Term
| L/R SIDE ICE PROTECTION Panel light indicates |
|
Definition
| Associated side window heating is inoperative or is being controlled by the overheat sensor |
|
|
Term
| L/R FRONT ICE PROTECTION Panel light indicates |
|
Definition
| Associated front window heating inoperative or is being controlled by the overheat sensor |
|
|
Term
| L/R PROP ICE PROTECTION Panel light indicates |
|
Definition
| Associated propeller heating is inoperative |
|
|
Term
| L/R INTAKE ICE PROTECTION Panel light indicates |
|
Definition
| Associated engine intake heating is inoperative |
|
|
Term
| L/R AIR VALVE ICE PROTECTION Panel light indicates |
|
Definition
| The associated generator is not on line |
|
|
Term
| DEICE OV TEMP ICE PROTECTION Panel light indicates |
|
Definition
| Deicer bleed air temperature is excessive |
|
|
Term
| TIMER ICE PROTECTION Panel light indicates |
|
Definition
| The deice timer or valves are malfunctioning |
|
|
Term
| L/R AC GEN ICE PROTECTION panel light indicates |
|
Definition
| Associated AC generator is off-line |
|
|
Term
| L/R VALVE CLOSED FUEL Panel light indicates |
|
Definition
| The associated valve is closed |
|
|
Term
| FUEL FILTER FUEL Panel light indicates |
|
Definition
| Bypass of the associated fuel filter is impending |
|
|
Term
| L/R MAIN PUMP FUEL Panel light indicates |
|
Definition
| The associated pump is not developing pressure |
|
|
Term
| X FEED ON FUEL Panel light indicates |
|
Definition
| The fuel crossfeed valve is open |
|
|
Term
| L/R LOW LEVEL FUEL Panel light indicates |
|
Definition
| The associated fuel level is 300 lb. +70, or less |
|
|
Term
| STBY PRESS FUEL Panel light indicates |
|
Definition
| Positive pressure is detected on the main pump inlet |
|
|
Term
| CONN VLV OPEN FUEL Panel light indicates |
|
Definition
| The fuel connect valve is open |
|
|
Term
| L/R OIL BYPASS ENGINE panel light indicates |
|
Definition
| Bypass of the oil filter is impending |
|
|
Term
| L/R CHIP DETECT ENGINE panel light indicates |
|
Definition
| Metal chips are detected in the associated engine oil system |
|
|
Term
| FUEL LOW TEMP ENGINE panel light indicates |
|
Definition
| Fuel temperature is low (<2°C) |
|
|
Term
| NO BAT START ENGINE panel light indicates |
|
Definition
| Battery temperature exceeds >57°C |
|
|
Term
| INVERTER AC ELEC panel light indicates |
|
Definition
| The selected inverter has failed or is switched OFF |
|
|
Term
| L/R ESS BUS DC ELEC panel light indicates |
|
Definition
| Power is lost on the associated essential bus |
|
|
Term
| L/R BAT HOT DC ELEC panel light indicates |
|
Definition
| The associated battery is hot (>71°C) |
|
|
Term
| L/R BAT DC ELEC panel light indicates |
|
Definition
| The associated battery relay is open |
|
|
Term
| EMER PWR DC ELEC panel light indicates |
|
Definition
| Emergency Bus voltage is less than 24 volts |
|
|
Term
| BUS TIE CONN DC ELEC panel light indicates |
|
Definition
| The bus tie relay is closed |
|
|
Term
| L/R MAIN BUS DC ELEC panel light indicates |
|
Definition
| Power is lost on the associated main bus |
|
|
Term
| L/R GEN OV TEMP DC ELEC panel light indicates |
|
Definition
| The associated generator is hot (>150°C) |
|
|
Term
| L/R GEN DC ELEC panel light indicates |
|
Definition
| The associated generator relay is open |
|
|
Term
| EXT PWR ON DC ELEC panel light indicates |
|
Definition
| The external power switch is ON |
|
|
Term
| L/R DUCT OV TEMP AIR COND panel light indicates |
|
Definition
| The associated air conditioning duct is hot (>82°C); or ACM DISCHARGE IS HOT (>225C) |
|
|
Term
| L/R BLD AIR LEAK AIR COND panel light indicates |
|
Definition
| The associated bleed air line is leaking |
|
|
Term
| L/R BLD FAULT AIR COND panel light indicates |
|
Definition
| Bleed air temp is excessive (>288°C); or bleed pressure is high (>43psi); or bleed valve did not close after receiving a close signal |
|
|
Term
| X VALVE OPEN AIR COND panel light indicates |
|
Definition
| The pneumatic cross valve is open |
|
|
Term
| L/R BLD CLOSED AIR COND panel light indicates |
|
Definition
| The associated engine bleed air valve is closed |
|
|
Term
| L/R HP HIGH AIR COND panel light indicates |
|
Definition
| The associated high pressure bleed air valve is open after receiving CLOSE SIGNAL |
|
|
Term
| EMER CABIN SIGNS panel light indicates |
|
Definition
| Emergency switch is activated at flight attendant or flight deck interphone |
|
|
Term
| CALL CABIN SIGNS panel light indicates |
|
Definition
| The flight attendant has pressed the CALL button on the cabin interphone |
|
|
Term
| CARGO DOOR DOORS panel light indicates |
|
Definition
| The cargo door is not locked |
|
|
Term
| MAIN DOOR DOORS panel light indicates |
|
Definition
| The main door is not closed |
|
|
Term
| MAIN DOOR HANDLE DOORS panel light indicates |
|
Definition
| The main door handle is not locked |
|
|
Term
| CREW HATCH DOORS panel light indicates |
|
Definition
|
|
Term
| FUELING STATUS panel light indicates |
|
Definition
| The fueling panel power switch is in ON, or the defueling valve is not closed |
|
|
Term
| EXT PWR AVAIL STATUS panel light indicates |
|
Definition
| The external power is plugged in and available |
|
|
Term
| GROUND CREW LIGHT (Blank white no label) light indicates |
|
Definition
| ground crew headset is connected in the nosewheel well. |
|
|
Term
| Bottom governing is canceled below what prop rpm? |
|
Definition
|
|
Term
| With CL in Min or above bottom governing becomes available at what PRPM? |
|
Definition
|
|
Term
| At what Ng is autoignition canceled to prevent relight? |
|
Definition
|
|
Term
| Engine test fire indication? |
|
Definition
Both fire handles Both engine fire lights Fire bell Master warning light |
|
|
Term
| Tailpipe hot fire test indications |
|
Definition
Both tailpipe hot lights Triple chime Master caution |
|
|
Term
| Tailpipe hot light illuminates at what temp? |
|
Definition
|
|
Term
| How many check valves in the hydraulic system. |
|
Definition
4 check valves for accumulators 3 check valves for hand pump 2 check valves for reservoir |
|
|
Term
| Gear actuation Control/Operation |
|
Definition
Normal = electric/electric Alternate = electric/hand pump Emergency = Hydraulic/gravity |
|
|
Term
| How close must usable alternate be to operate |
|
Definition
|
|
Term
| What is the height of the tail of the Saab 340 B+? |
|
Definition
|
|
Term
| What is the BITE light and what is indicated if it is illuminated? |
|
Definition
Unlabeled round white light on Test 1 panel. Malfunction in a WEU alert channel Indicates loss of reliability of redundant channels |
|
|
Term
| 5 things that happen when pulling firewall fuel valve? |
|
Definition
Fuel shutoff valve closes Gen relays open Lp/HP bleed closed Squibs armed Master warning reset Fire bell silenced |
|
|
Term
Items on the emergency bus 6 |
|
Definition
Audio system back-up Bus tie relay CONN function L/R engine fire detect L/R tail pipe hot detect Warning system backup Emergency voltage indication |
|
|
Term
|
Definition
L engine fire extinguisher L fire handle control L battery control Ahrs1 L batt voltage indication Cargo extinguisher 1 Dome, entrance, cargo lights |
|
|
Term
|
Definition
R engine fire extinguisher R fire handle R battery control AHRS 2 R batt voltage indication Cargo extinguisher 2 Fuel panel Clock |
|
|
Term
Ice protection level 1 For all flight ops Includes? |
|
Definition
STBY Pitot - on L/R front windshield - as necessary for defog L/R side windshield - as necessary |
|
|
Term
Ice protection level 2 +10c with vis. moisture |
|
Definition
Level one items plus: L/R engine anti-ice and wing and stab boots |
|
|
Term
Ice protection level 3 -5c with vis. Moisture |
|
Definition
Level 2 items plus: Prop deice NORM |
|
|
Term
Ice protection level 4 -13c or colder w/vis. Moisture |
|
Definition
Level 3 items plus: Prop deice MAX |
|
|
Term
|
Definition
| 106 Kias (Flaps 20 and 35) |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Fire switch on test one triggers what indications? |
|
Definition
Master warning For fire detection: Both red ENG FIRE lights Both red FIRE HANDLES FIRE BELL activation For tailpipe hot: Both red TAILPIPE HOT TRIPLE CHIME |
|
|
Term
| What discrepancies cause timer light? |
|
Definition
Manual inflation button pushed during auto cycle The timer fails or controller power is lost PSI discrepancy detected between distributor control signals and the line PSI downstream from the valve |
|
|
Term
| What is the max tire speed? |
|
Definition
|
|
Term
|
Definition
|
|
Term
What must you do after a high energy abort?
80Kias+ |
|
Definition
| contact MX for brake inspection wait alloted time. |
|
|
Term
| How long for brake cooling when aborting under 80 Kias? |
|
Definition
|
|
Term
| When is reduced power takeoff prohibited? |
|
Definition
Anti-Skid inop
Tailwind
windshear
CTOT inop
Runway contaminated
deice/anti ice fluids on aircraft |
|
|
Term
| Circuit breakers you must never pull! |
|
Definition
|
|
Term
| At what altitudes are trends done? |
|
Definition
Between 10,000-20,000'
15,000' is optimal
Max cruise set 1270 PRPM
Eng. Anti-ice off
5 Min. Stabilized cruise
DC Gen load normal
Hydr pump not running
ECS-on
Ng>85% |
|
|
Term
At what Knot windshear for company? |
|
Definition
|
|
Term
| Required Navigational Performance |
|
Definition
Oceanic=4 Nm
Enroute=2 Nm
Terminal=1 Nm
Approach=0.3 Nm |
|
|
Term
| 5 Items when the Fire Handle is pulled? |
|
Definition
Fire bell cancelled
Master Warning reset
Fuel valve closed
Bleeds HP/LP closed
Gen Relays opened |
|
|
Term
| Hydr. Indicator Bus powered by? |
|
Definition
|
|
Term
Gear activation:
Control-Operation
Normal
Alternate
Emergency |
|
Definition
Electric-Hydraulic
Electric-Hand pump
Hydraulic-Gravity
|
|
|
Term
| Parking brake disengages at what PSI? |
|
Definition
|
|
Term
| 6 items that will cause a L/R INTAKE light? |
|
Definition
Loss of Temp sensors
Loss of AC/DC power
Overtemp/Undertemp
Failure of a heating element
Loss of 1 or more AC phases |
|
|
Term
Ice protection switches powered by?
|
|
Definition
|
|
Term
EVACUATION
emergency action items |
|
Definition
Captain:Parking brake--Set
Condition levers--Fuel off
Engine fire handle--Pull
Fire EXT. switches--On
Evacuation--Order
After all radio comunication complete:
Batt switches--Off
First officer:Emer light switch--On
Press Dump--On
ELT--As Reqd.
ATC/Ground crew--Notify |
|
|
Term
Aborted Engine Start:
Emergency action items |
|
Definition
Condition lever (affected engine)--Fuel off
IGnition--Off
Starter Switch--L/R:
Motor Engine ITT to below 175c or for a minimum of 10 Sec.
|
|
|
Term
Loss of Braking
Emergency action items |
|
Definition
|
|
Term
Split Flaps
emergency action items |
|
Definition
| Flap Selector--Select previous setting |
|
|
Term
Avionic smoke warning light illuminated or Electric smoke or fire:
Emergency action items |
|
Definition
Oxygen masks-- Don/100%
Smoke Goggles--On
Mic Switch--Mask
Communication--Established |
|
|
Term
Air Conditioning Smoke
Emergency action items |
|
Definition
Oxygen masks--Don/100%
Smoke Goggles-- On
Mic switch--Mask
Communications--Established |
|
|
Term
Rapid depressurization/Emergency descent
Emergency action items |
|
Definition
Oxygen Masks--Don/100% O2
Mic Switch-- Mask
Communications-- Established |
|
|
Term
|
Definition
Prop overspeed gov.
PGB oil pump
Prop control unit
AC Generator |
|
|
Term
| 5 Items on Accessory gear box |
|
Definition
Main fuel pump
HMU
Oil/Scavenge pumps
Starter/Generators
Engine Alternator |
|
|
Term
GCU provides what protection?
4 |
|
Definition
Overexitation
Over current
Over vortage
Reverse Current |
|
|
Term
What do power levers do on the ground?
In the air? |
|
Definition
Control prop blade angles using the PCU when <flt idle.
Controls fuel to engine through HMU. |
|
|
Term
| What 3 engine gauges are supplied information from the DECU? |
|
Definition
|
|
Term
When selected to Auto or Norm when will you see an auto ignition FSP light?
4 |
|
Definition
Engine start cycle
Auto relight is activated
control power is lost
Power turbine overspeed |
|
|
Term
| Min fuel temp for takeoff is? |
|
Definition
|
|
Term
| STBY Attitude indicator is powered buy what bus? |
|
Definition
Emergency Avionics bus.
Also powers Comm 1 |
|
|
Term
| Where does the rudder limiter get its information from? |
|
Definition
|
|
Term
|
Definition
115Vac either from GPU or Gen.
Must also have one engine running(oil PSI relay from either engine) |
|
|
Term
| DFDR light illuminated indicates? |
|
Definition
Failure of system or not powered.
One Gen must be online. |
|
|
Term
CVR is powered by the Batt Bus,
turned on with what switch? |
|
Definition
Essential avionics switch
CVR will die during engine start due to loss of essential bus!!!!! |
|
|
Term
| 5 ways to disconnect Autopilot |
|
Definition
Stall warning activation
AP switch off
press go around button
AP Disc switches
Activate main/STBY pitch trims |
|
|
Term
| When do you never use 1/2 bank? |
|
Definition
| In terminal area, or while holding. |
|
|
Term
| Blade angle for max reverse? |
|
Definition
|
|
Term
| Blade angle for Grnd Idle? |
|
Definition
|
|
Term
| Blade angle for flight Idle (Ground only)? |
|
Definition
|
|
Term
| What Prop angle turns on the BETA light? |
|
Definition
|
|
Term
| What blade angle for bottom Governing? |
|
Definition
|
|
Term
| What 3 times will you get a CONFIG CWP? |
|
Definition
When not properly configured for:
Takeoff
In flight
During Engine Start |
|
|