Term
| Autopilot and Flight Director approaches are approved for glideslope angle of ___ through ___. Glide slope angles greater then ___ are approved for approach flap ___ only. |
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Definition
| Autopilot and Flight Director approaches are approved for glideslope angle of 2.5 through 4. Glide slope angles greater then 3 are approved for approach flap 15 only. |
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| The AFCS is approved for __________ Operations only |
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Definition
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| During autopilot operation the flying pilot must: |
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Definition
| be seated at the controls with harness (lap belt and shoulder harness) fastened |
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True or Flase? The autopilot is allowed to be manually overpowered |
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Definition
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| In approach the autopilot must be disengaged at or above _____ ft above runway elevation |
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True or False? The autopilot can be used for approach on one engine. |
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Definition
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| Autopilot mode is not permitted with flaps at ____ |
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Definition
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| Autopilot mode is not permitted with flaps at 5 degrees below ____ ft (311 only) |
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Definition
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| Autopilot mode is not permitted with flaps at 0 degrees below ____ ft (311 only) |
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Definition
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True or False? The autopilo/t must be disengaged in severe icing |
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Definition
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| After takeoff or go around the minimum (manufactureer's) approved height for autopilot engagement is ____ ft. The Piedmont limit is ____ft. |
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Definition
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Term
True or False? The use of VOR without associated DME is not permitted in NAV and APP mode. |
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Definition
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Term
| Severe icing conditions are determined by the following visul cues: |
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Definition
1. Unusually extensive ice accreted on the airframe in areas not normally observed to collect ice 2. Accumulation of ice on the lower surface of the wing aft of the protected area 3. Accumulation of ice on the prop spinner farther aft than normally observed |
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Term
| When ice is detected the ______ must be set to _____ or _____ |
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Definition
| AIRFRAME AUTO; FAST; SLOW |
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Term
| Normal cabin pressure differential limit: |
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Definition
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| Maximum cabin pressure differential limit: |
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Definition
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| Max cabin pressure differential during taxi, takeoff, and landing: |
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Definition
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| Max cabin alitude (pressurized flight): |
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Definition
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| Bleed air must be_______ for takeoff and landing |
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Definition
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Term
| Engine _________ doors must be _____ and engine ignition switch at _____ for engine operation in ______ conditions |
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Definition
| Engine INTAKE BYPASS doors must be OPEN and engine ignition switch at MANUAL for engine operation in ICING conditions |
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Term
| Icing conditions exist on the ground or for takeoff exist when: |
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Definition
| 10 degrees C or below and visible moisture including contaminiated runways, ramps, or taxiways. |
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Term
| Icing conditions exist in flight when: |
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Definition
| 5 degrees C or below and visible moisture |
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Term
| The APU is approved for _____ _____ only |
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Definition
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Term
| The APU temperature range is: |
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Definition
| -43C to +48.9C or ISA +35 which ever is lower |
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Term
| APU must be ________ while operating during pressure refueling |
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Definition
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Term
True or False? APU must not be operated during gravity refueling |
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Definition
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Term
| APU must be ________ prior to ________ |
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Definition
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Term
| APU must be ________ prior to ________ |
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Definition
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Term
True or False: The APU can be operated unattended while passengers are on board? |
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Definition
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Term
| The APU can be operated unattened under what provisions? |
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Definition
1. All other limitations are observed 2. BATTERY MASTER switch- ON 3. MAIN and AUX BATTERY switches - OFF 4. EMERGENCY LIGHTS- OFF 5. Unattended operation not to exceed 20 mins 6. Receiving checklist must be accomplished upon return to the aircraft. |
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Term
| During de-icing/anti-icing events the ______ ______ switch must be OFF |
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Definition
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Term
| Minimum pressure for crew portable Oxygen |
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Definition
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Term
| Minimum pressure for passenger portable oxygen |
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Definition
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| Alternate Gear extension speed: |
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Definition
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Definition
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Term
| Vmo varies ________ between altitudes |
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Definition
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Term
| Ambient temperature limits |
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Definition
| lower of +48.9C and ISA +35C and -54C |
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Term
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Definition
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Term
| Max tailwind with 15 degrees for takeoff and 35 degrees for landing |
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Definition
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Term
| Max tailwind for takeoff and landing |
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Definition
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Definition
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Definition
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| Max altitude for takeoff and landing |
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| Max combined total load (100) |
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Definition
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| Max combined total load (300) |
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| Maximum T/O Torque Limitation (100) |
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Definition
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Term
| Normal T/O Torque limit (100) |
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Definition
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Term
| How long can the max takeoff limitations be used for? |
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Definition
| it is limited to 5 minutes |
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Term
| Inflight torque limit (100) |
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Definition
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Term
| Max continuous torque limit (100) |
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Definition
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Term
| Transient torque limit (100) |
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Definition
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Term
| How long are transient times limited to? |
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Definition
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Term
| Max reverse torque limit (100) |
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Definition
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Term
| Max ITT for Max T/O (100) |
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Definition
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Term
| Max ITT for normal T/O (100) |
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Definition
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Term
| Max ITT for Max continuous (100) |
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Definition
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Term
| Max ITT for starting (100) |
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Definition
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