Term
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Definition
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Term
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Definition
Pressurization- Checked
Altimeters-Set
Cabin signs- As needed
Auto Feather - Armed
Flaps- Approach |
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Term
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Definition
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Term
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Definition
| Ground fine | then reverse |
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Term
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Definition
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Term
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Definition
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Term
| Approaching the Holding Point |
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Definition
Engine anti ice As Required,
Bleed air valves Open,
Transponder
ATC 1 |
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Term
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Definition
Bleed air open
Transponder on
Radar- As required
Annunciators- LookLights/Landing /strobe- As required
Ice protection- As required
Auto Ignition- Armed |
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Term
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Definition
Power Set
Power Check/adjustL & R AFX illuminated
Call 60 Kts
Call "V1 rotate"Rotate to 10... |
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Term
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Definition
Engine climb power/RPM set
Engine limits check
Prop Sync ON
Landing Gear UP
Landing & Taxi lights off |
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Term
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Definition
Prop sync ON,
Landing Gear UP,
Taxi lights OFF,
Flaps UP
,Pressurisation CHECKED |
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Term
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Definition
Altimiters SET
Power/RPM SET
(set based on cruise graph) |
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Term
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Definition
Landing speeds SET
Pressurisation SET
Briefing COMPLETE |
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Term
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Definition
Gear -down
Lights -as requires
Cabin signs- As needed
Radar- Off
Prop Sync off |
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Term
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Definition
Engine auto ignition OFF
Engine anti-ice ON
Icing equipment OFF
Auto feather - Off
Transponder - Standby
Bleed air- As required
Condition levers- As required
Flaps- Up
Trrim tabs-Set |
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Term
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Definition
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Term
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Definition
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Term
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Definition
| 21 compressor1 power turbine shaft |
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Term
| engine shaft-horsepower rating |
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Definition
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Term
| Minimum flight crew: __________. |
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Definition
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Term
| Power lever(s) must not be moved into reverse except when __________. |
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Definition
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Term
| Operating respective engine with L FUEL PRES LO or R FUEL PRES LO annunciation is limited to... |
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Definition
| 10 hours overhaul or replacement of engine-driven fuel pump |
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Term
| Normal oil pressure range of 80-100 PSI is applicable for N1 speeds above __________. |
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Definition
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Term
| With oil pressure in flight between 40 and 80 PSI, fly at __________. |
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Definition
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Term
| Normal oil pressure operating range for maximum reverse is __________. |
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Definition
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Term
| Do not take off if fuel quantity gauges indicate __________ or less than __________ in each... |
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Definition
| In the yellow arc -265 pounds of fuel |
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Term
| Both boost pumps must be operations prior to __________. |
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Definition
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Term
| Usable fuel weights are based on fuel density of |
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Definition
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Term
| Allowable oil temperature range at high idle is __________ to __________. |
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Definition
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Term
| Allowable oil temperature range at high idle is __________ to __________. |
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Definition
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Term
| Maximum Cruise prop RPM is __________. |
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Definition
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Term
| Normal oil pressure range for takeoff is |
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Definition
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Term
| ENGINE ANTI-ICE must be ON in ambient temperatures of __________ when __________ |
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Definition
| +5 deg. C or below conditions free of visible moisture cannot be assured |
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Term
| Maximum prop RPM for takeoff is __________. |
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Definition
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Term
| The airplane's category is __________. Acrobatic maneuvers, including spins, are __________ |
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Definition
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Term
| Starter use is time limited to: __________ |
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Definition
| 40 seconds ON, 60 seconds OFF, 40 seconds ON, 60 seconds OFF, 40 seconds ON, 30 minutes off |
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Term
| Maximum occupancy (including crew): |
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Definition
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Term
| EXTERNAL POWER CART: Voltage range: __________ Power output requirements: |
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Definition
| 28.0-28.4 V 1000 amps momentary, 300 amps continuous |
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Term
| Cabin differential pressure gauge green arc is _________. |
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Definition
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Term
| Sustained propeller overspeeds exceeding 2288 RPM indicate __________. |
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Definition
| failure of the primary governor and the overspeed governor |
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Term
| Sustained propeller overspeeds exceeding 2200 RPM indicate __________ |
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Definition
| failure of the primary governor |
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Term
| Maximum operating pressure altitude: |
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Definition
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Term
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Definition
Gen Load
0 to 50% ----> 59% N1
50 to 80% ----> 61% N1
80 to 85% ----> 70% N1 |
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Term
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Definition
| 150 hrs between overhauls 8000 ft pressure altitude limited with boost pumps inop crossfeed capability required on climbs above 8000 ft |
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Term
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Definition
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Term
| crossfeeding allowed only |
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Definition
1. elec boost pump failure
2. engine failure |
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Term
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Definition
| Do not take of 265 lbs or less |
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Term
| operating with lo fuel pressure |
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Definition
| limited to 10 hrs with LO FUEL PRESS annunciator before overhaul |
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Term
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Definition
| must be operational before takeoff |
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Term
3-Prop rotation speed limits
Transient
Reverse
All Other |
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Definition
5 sec transient --- 2420
reverse --- 2100
all other conditions --- 2200 |
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Term
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Definition
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Term
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Definition
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Term
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Definition
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Term
| Max rear baggage max nose avionics compartment load |
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Definition
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Term
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Definition
| Positive- 3.7 G Negative- 1.68 G |
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Term
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Definition
| 1 cycle every 3 minutes for 10 cycles... followed by 15 minute cool down period |
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Term
| Min temp for operation of deicing boots |
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Definition
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Term
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Definition
| Total fuel 484 useable Main- 392 Aux-82 |
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Term
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Definition
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Term
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Definition
| Above 2200 indicate primary governor failour Above 2288 both primary and secondary governors failure |
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Term
| Normal Operating Speed range Green Radial |
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Definition
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Term
| Full Flap operating range White radial |
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Definition
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Term
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Definition
Climb power set-
Observe Max ITT,
Torque, N1 Rpm limits
Prop Sync- On
Auto feather - OFF
Engine instruments -
Monitor Cabin signs- as needed |
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Term
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Definition
| Any "light on"indication Shut down affeced engine immediately |
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Term
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Definition
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Term
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Definition
1. -Never fill aux tanks unless mains are full
2. -Alwayse burn aux tanks first mains second
3. -Cross fee - ONLY during singe engine operation |
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Term
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Definition
Gear- Down /Check
Flaps- Down/100%
Yaw damp- Off |
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Term
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Definition
Power- Forward
FD/ Go button around selected
Gear- Up
Speed - VYSE+ 10 (Best rate)
Flaps up
Climb Check list- Complete
ATC- As required |
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Term
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Definition
Gear -Up
Yaw Damp-On
Climb power -1900 RPM set
Prop Sync- On
Flaps -Up |
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