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76 Cards in this Set
- Front
- Back
- 3rd side (hint)
Q200 max ramp wt |
36500 |
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Q300 max ramp wt
|
43200
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Q200 max takeoff wt
|
36300
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Q300 max takeoff wt
|
43000
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Q200 max landing wt
|
34500
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Q300 max landing wt
|
42000
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Q200 max ZFW
|
32400 per STC
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Q300 max ZFW
|
39500 per STC
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-Max fuel imbalance -Fuel low level light |
600lb in flight only 130lb |
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Max operating altitude
|
25000ft
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Max tailwind |
20kt |
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Tailwind 11-20kt takeoff/landing limitations |
BANAN BFF MCR
B-Both ECUs operative A-Antiskid operative N-Nosewheel steering operative A-Autofeather operative N-Normal t/o power
B-Bleeds off F-Flaps 15 for t/o F-Flaps 35 for landing
M-Max approach angle 4* (Q200 only) C-Condition levers set 1200RPM R-Runway uncontaminated |
Banan bff mcr |
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Max crosswind
|
36kts |
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Max operating ambient temp
|
48.9C or ISA+35C, whichever is lower
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Min operating ambient temp
|
-54C |
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"Bleeds On" takeoff max operating ambient temp
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41.9C (107F) [Q300 only]
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"Bleeds On" landing max operating ambient temp
|
41.9C (107F) [both aircraft] |
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Max altitude w/ landing gear and/or flaps extended
|
15000ft |
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Vfe for Q200
|
Flaps 5 - 148 |
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Vfe for Q300
|
Flaps 5 - 163 |
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Vlo for Q200 |
158
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Vlo for Q300
|
163
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Vle for Q200
|
172 |
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Vle for Q300
|
173
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Rough Air Speed Q200 |
180
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Rough Air Speed Q300
|
190
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Q200 Va |
164 |
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Q300 Va |
177 |
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Engine minimum ambient temp
|
-54C |
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Engine max ambient temp
|
48.9C or ISA+35C, whichever is lower |
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Max Takeoff power use and time limit
|
Used by the uptrim system, maximum 5 minutes |
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ITT limits
|
800-840 - 20 sec |
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Transient limits time limit
|
20 sec unless otherwise stated |
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Oil pressure _ _-_ _psi allowed for engine speed below _ _%Nh
|
40-55psi |
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Oil temp between _ _ _ - _ _ _C is limited to _ _minutes
|
115-125C |
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Min oil temp for unfeathering and power settings above flight idle
|
0C |
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Min oil temp for adequate inlet splitter anti-icing
|
45C |
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Reduced torque takeoff limitations |
UP WATER FARM
U-Uptrim enabled and operative P-Procedure must not require NTOP
W-Windshear not present or suspected A-Autofeather operative T-Tailwind max 10kts E-ECUs operative R-Runway cant be gravel/unpaved
F-First flight of the day not autorized A-Antiskid operative R-Runway slope 2% or less M-Min torque 88.5% (Q200) 82% (Q300) |
Up water farm |
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Usable fuel tank capacities |
2839 lb per tank 5678 lb total |
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_____ must be on for takeoff and landing.
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Tank 1 and 2 aux pumps |
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Min/max temp at fuel heater outlet for continuous operation |
Min: 11C |
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APU limitations (Q300 only) |
GG PP TT RS |
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Starter cranking limits for engines and APU
|
Start 1 - 1 min on - 2 min off |
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Max torque with prop feathered
|
Q200-50% Q300-48% |
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Min flight idle Nh |
66% Nh
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DC Generator load limits
|
Ground - 0.7
Flight - 1.0 |
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TRUs load limits |
Ground/Flight - 1.0 |
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AC generators load limits
|
Ground <10C - 1.0 |
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Inverters load limits
|
Ground/Flight - 1.0
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Situation and time limit when DC generator may exceed load limits |
During Internal battery starting for up to 1 minute |
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-Max cabin pressure differential for taxi, takeoff, and landing -Normal Cabin Pressure Differential -Max Cabin Pressure Differential |
0.5 psi 5.5 psi 5.95 psi |
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Max cabin altitude in pressurized flight |
8000ft
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Engine intake bypass doors must be ____ and engine ignition switch at ____ for engine ops in icing conditions. |
OPEN |
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Definition of icing conditions on ground
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SAT is 10C or below when precip in any form is present, or fog w/ vis of 1mile or less, and when operating on ramps/taxiways/runways where surface snow/ice/slush/standing water may be ingested by or freeze on engines/nacelles/engine sensor probes |
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Definition of icing conditions in flight |
SAT is 5C or lower and visible moisture is present in any form |
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AFCS - Automatic Flight Control System (autopilot) limitations |
DOG CHESS BEEF
D-NAV/APP mode not auth using VOR w/o associated DME O-Must not manually Overpower the autopilot G-Glideslope 2.5-4* only for AP/FD appchs, 3*+ is flaps 15 only
C-Cat I approach limits only for AP appchs H-Harness must be worn/seated during AP ops E-Engine inop - must not continue APR approach past 1000 AGL S-Severe icing prohibited S-Severe turbulence prohibited
B-Backcourse AP appchs not approved E-Engaged after 1000AGL E-disEngaged before 200AGL F-APP mode prohibited: -Flaps 35 prohibited [both aircraft] -Flaps 5 AP engaged -Flaps 0 AP engaged |
dog chess beef |
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AHRS takeoff limitations |
Takeoff prohibited in: |
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____ and ____ based approaches are not permitted using ________ _____/_____ display
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ILS and FMS |
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DImensions Q200 -Wingspan -Length -Tail Height |
85' 73' 24'5" |
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Dimensions Q300 -Wingspan -Length -Height |
90' 84'3" 24'7" |
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Propeller continuous operation between ___ and ___ rpm is prohibited |
500/780 |
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Hydraulic System #1 operates ___ |
FARPIB Flaps Anti Skid Lower Rudder Power Transfer Unit (PTU) INBD Roll Spoiler Brakes |
farpib |
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Hydraulic System #2 operates ___ |
LOSER Landing Gear Extension/Retraction Outboard Roll Spoilers Steering Emergency/Park Brake Upper Rudder |
loser |
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Hydraulic Pressures -Engine Driven Pump |
3000 psi (2900-3100) |
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Hydraulic Pressures -Standby Power Unit (SPU) |
2900 psi (2800-3000) |
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Power Transfer Unit (PTU) |
Used for gear extension in the event of a right hand #2 engine failure or hydraulic pump failure |
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Oxygen Requirement -Crew -Passengers |
2 crew 1300 psi 3 crew 1800 psi crew portable 1800 psi Pax 1800 (1100 min departure) |
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Intermittent Gear Horn |
Park brake set Flaps less than 5 or more than 20 Condition levers not at max ECU not at TOP Trim not at Take Off
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Hydraulic Fluid Quantities Left ___ Right ___ Emergency Hyd Sys ___ |
2.5 usq (min disp 1.5) 4.5 usq (min disp 3.0) 1.21 usq |
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Normal Take Off Torque |
Q200 99.5% Q300 92% |
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Max Continuous Power (MTOP) |
Q200 97.5% @1212 prop rpm Q200 114.2% @1024 prop rpm
Q300 90% @1212 prop rpm Q300 96% @1125 prop rpm |
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FMS HSI Scaling -Enroute -Terminal -Approach |
5.0 nm 1.0 nm .3 nm |
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Climb Profiles |
Type 1 195 KIAS to 10 000' ASL subtract 5 KIAS for every 1000' above 10 000' to a min of 135 KIAS Type 2 165 KIAS to 17 000' ASL subtract 5 KIAS for every 1000' above 17 000' to a min of 135 KIAS Type 3 135 KIAS
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Max Power Settings 314 301/311 201/202 103/106 102
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314 = 105 %, 800 ITT 301/311 = 100 %, 800 ITT 201/202 = 107.5 %, 800 ITT 103/106 = 107.5 %, 800 ITT 102 = 90 %, 800 ITT |
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Contact Approach |
An approach wherein an aircraft on an IFR flight plan, having an ATC authorization and operating clear of clouds with at least 1 mi. flight visibility and a reasonable expectation of continuing to the destination airport in those conditions, may deviate from the instrument approach procedure and proceed to the destination airport by visual reference to the surface of the earth. |
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MAX Tire Ground Speed Q200 Q300 |
139 165 |
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