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59 Cards in this Set
- Front
- Back
Q200 max ramp wt
|
36500
|
|
Q300 max ramp wt
|
43200
|
|
Q200 max takeoff wt
|
36300
|
|
Q300 max takeoff wt
|
43000
|
|
Q200 max landing wt
|
34500
|
|
Q300 max landing wt
|
42000
|
|
Q200 max ZFW
|
32400 per STC
|
|
Q300 max ZFW
|
39500 per STC
|
|
Q200 min structural wt
|
21400
|
|
Q300 min structural wt
|
24700
|
|
Max lateral assymetry
|
600lb in flight only
|
|
Max operating altitude
|
25000ft
|
|
Max tailwind
|
20kt
|
|
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 |
|
Max crosswind
|
36kts
|
|
Max operating ambient temp
|
48.9C or ISA+35C, whichever is lower
|
|
Min operating ambient temp
|
-54C
|
|
"Bleeds On" takeoff max operating ambient temp
|
41.9C (107F) [Q300 only]
|
|
"Bleeds On" landing max operating ambient temp
|
41.9C (107F) [both aircraft]
|
|
Max altitude w/ landing gear and/or flaps extended
|
15000ft
|
|
Vfe for Q200
|
Flaps 5 - 148
Flaps 15 - 148 Flaps 35 - 130 |
|
Vfe for Q300
|
Flaps 5 - 163
Flaps 15 - 150 Flaps 35 - 138 |
|
Vlo for Q200
|
158
|
|
Vlo for Q300
|
163
|
|
Vle for Q200
|
172
|
|
Vle for Q300
|
173
|
|
Rough Air Speed Q200
|
180
|
|
Rough Air Speed Q300
|
190
|
|
Engine minimum ambient temp
|
-54C
|
|
Engine max ambient temp
|
48.9C or ISA+35C, whichever is lower
|
|
Max Takeoff power use and time limit
|
Used by the uptrim system, maximum 5 minutes
|
|
ITT limits
|
800-840 - 20sec
840-900 - 12sec 900-950 - 5sec |
|
Transient limits time limit
|
20sec unless otherwise stated
|
|
Oil pressure _ _-_ _psi allowed for engine speed below _ _%Nh
|
40-55psi
75%Nh |
|
Oil temp between _ _ _ - _ _ _C is limited to _ _minutes
|
115-125C
20minutes |
|
Min oil temp for unfeathering and power settings above flight idle
|
0C
|
|
Min oil temp for adequate inlet splitter anti-icing
|
45C
|
|
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) |
|
Usable fuel tank capacities
|
2839lb per tank
|
|
_____ must be on for takeoff and landing.
|
Tank 1 and 2 aux pumps
|
|
Min/max temp at fuel heater outlet for continuous operation
|
Min: 11C
Max: 57C |
|
APU limitations (Q300 only)
|
GG PP TT RS
G-Ground operations only G-Gravity fueling must not be operated P-Pressure refueling must be attended P-Pax on board must be attended T-Temp min is -43C T-Temp max is 48.9C or ISA+30C, whichever is lower R-Refer to mtx manual for approved oils S-Shutdown prior to takeoff |
|
Starter cranking limits for engines and APU
|
Start 1 - 1min on - 2min off
Start 2 - 1min on - 2min off Start 3 - 1min on - 30min off |
|
Max torque with prop feathered
|
57%
|
|
Min flight idle Nh
|
66% Nh
|
|
DC Generator load limits
|
Ground - 0.7
Flight - 1.0 |
|
TRUs load limits
|
Ground/Flight - 1.0
|
|
AC generators load limits
|
Ground <10C - 1.0
Ground ≥ 10C - 0.33 Flight - 1.0 |
|
Inverters load limits
|
Ground/Flight - 1.0
|
|
Situation and time limit when DC generator may exceed load limits
|
During Internal battery starting for up to 1 minute
|
|
Max cabin pressure differential for taxi, takeoff, and landing
|
0.5 psi
|
|
Max cabin altitude in pressurized flight
|
8000ft
|
|
Engine intake bypass doors must be ____ and engine ignition switch at ____ for engine ops in icing conditions.
|
OPEN
AUTO |
|
Definition of icing conditions on ground
|
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
|
|
Definition of icing conditions in flight
|
SAT is 5C or lower and visible moisture is present in any form
|
|
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 commence/continue AP appch 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 <1500AGL [Q300 only] -Flaps 0 AP engaged <500AGL [Q300 only] |
|
AHRS takeoff limitations
|
Takeoff prohibited in:
-DG mode -BASIC mode -With any advisory light (AUXPR, SLAVE, etc..) |
|
HGS reduced visibility takeoff limitation
|
Requires PRIMARY (PRI) mode be selected
|
|
____ and ____ based approaches are not permitted using ________ _____/_____ display
|
ILS and FMS
composite EHSI/EADI |