Dh8 200/300 Limitations

Front 1

Q200 max ramp wt

Back 1

36500

Front 2

Q300 max ramp wt

Back 2

43200

Front 3

Q200 max takeoff wt

Back 3

36300

Front 4

Q300 max takeoff wt

Back 4

43000

Front 5

Q200 max landing wt

Back 5

34500

Front 6

Q300 max landing wt

Back 6

42000

Front 7

Q200 max ZFW

Back 7

32400 per STC

Front 8

Q300 max ZFW

Back 8

39500 per STC

Front 9

-Max fuel imbalance

-Fuel low level light

Back 9

600lb in flight only

130lb

Front 10

Max operating altitude

Back 10

25000ft

Front 11

Max tailwind

Back 11

20kt

Front 12

Tailwind 11-20kt takeoff/landing limitations

Back 12

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

Hint 12

Banan bff mcr

Front 13

Max crosswind

Back 13

36kts

Front 14

Max operating ambient temp

Back 14

48.9C or ISA+35C, whichever is lower

Front 15

Min operating ambient temp

Back 15

-54C

Front 16

"Bleeds On" takeoff max operating ambient temp

Back 16

41.9C (107F) [Q300 only]

Front 17

"Bleeds On" landing max operating ambient temp

Back 17

41.9C (107F) [both aircraft]

Front 18

Max altitude w/ landing gear and/or flaps extended

Back 18

15000ft

Front 19

Vfe for Q200

Back 19

Flaps 5 - 148
Flaps 15 - 148
Flaps 35 - 130

Front 20

Vfe for Q300

Back 20

Flaps 5 - 163
Flaps 15 - 150
Flaps 35 - 138

Front 21

Vlo for Q200

Back 21

158

Front 22

Vlo for Q300

Back 22

163

Front 23

Vle for Q200

Back 23

172

Front 24

Vle for Q300

Back 24

173

Front 25

Rough Air Speed Q200

Back 25

180

Front 26

Rough Air Speed Q300

Back 26

190

Front 27

Q200 Va

Back 27

164

Front 28

Q300 Va

Back 28

177

Front 29

Engine minimum ambient temp

Back 29

-54C

Front 30

Engine max ambient temp

Back 30

48.9C or ISA+35C, whichever is lower

Front 31

Max Takeoff power use and time limit

Back 31

Used by the uptrim system, maximum 5 minutes

Front 32

ITT limits

Back 32

800-840 - 20 sec
840-900 - 12 sec
900-950 - 5 sec

Front 33

Transient limits time limit

Back 33

20 sec unless otherwise stated

Front 34

Oil pressure _ _-_ _psi allowed for engine speed below _ _%Nh

Back 34

40-55psi
75%Nh

Front 35

Oil temp between _ _ _ - _ _ _C is limited to _ _minutes

Back 35

115-125C
20 minutes

Front 36

Min oil temp for unfeathering and power settings above flight idle

Back 36

0C

Front 37

Min oil temp for adequate inlet splitter anti-icing

Back 37

45C

Front 38

Reduced torque takeoff limitations

Back 38

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)

Hint 38

Up water farm

Front 39

Usable fuel tank capacities

Back 39

2839 lb per tank

5678 lb total

Front 40

_____ must be on for takeoff and landing.

Back 40

Tank 1 and 2 aux pumps

Front 41

Min/max temp at fuel heater outlet for continuous operation

Back 41

Min: 11C
Max: 57C

Front 42

APU limitations (Q300 only)

Back 42

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

Front 43

Starter cranking limits for engines and APU

Back 43

Start 1 - 1 min on - 2 min off
Start 2 - 1 min on - 2 min off
Start 3 - 1 min on - 30 min off

Front 44

Max torque with prop feathered

Back 44

Q200-50%

Q300-48%

Front 45

Min flight idle Nh

Back 45

66% Nh

Front 46

DC Generator load limits

Back 46

Ground - 0.7
Flight - 1.0

Front 47

TRUs load limits

Back 47

Ground/Flight - 1.0

Front 48

AC generators load limits

Back 48

Ground <10C - 1.0
Ground ≥ 10C - 0.33
Flight - 1.0

Front 49

Inverters load limits

Back 49

Ground/Flight - 1.0

Front 50

Situation and time limit when DC generator may exceed load limits

Back 50

During Internal battery starting for up to 1 minute

Front 51

-Max cabin pressure differential for taxi, takeoff, and landing

-Normal Cabin Pressure Differential

-Max Cabin Pressure Differential

Back 51

0.5 psi

5.5 psi

5.95 psi

Front 52

Max cabin altitude in pressurized flight

Back 52

8000ft

Front 53

Engine intake bypass doors must be ____ and engine ignition switch at ____ for engine ops in icing conditions.

Back 53

OPEN
AUTO or MAN

Front 54

Definition of icing conditions on ground

Back 54

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

Front 55

Definition of icing conditions in flight

Back 55

SAT is 5C or lower and visible moisture is present in any form

Front 56

AFCS - Automatic Flight Control System (autopilot) limitations

Back 56

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

Hint 56

dog chess beef

Front 57

AHRS takeoff limitations

Back 57

Takeoff prohibited in:
-DG mode
-BASIC mode
-With any advisory light (AUXPR, SLAVE, etc..)

Front 58

____ and ____ based approaches are not permitted using ________ _____/_____ display

Back 58

ILS and FMS

composite EHSI/EADI

Front 59

DImensions Q200

-Wingspan

-Length

-Tail Height

Back 59

85'

73'

24'5"

Front 60

Dimensions Q300

-Wingspan

-Length

-Height

Back 60

90'

84'3"

24'7"

Front 61

Propeller continuous operation between ___ and ___ rpm is prohibited

Back 61

500/780

Front 62

Hydraulic System #1 operates ___

Back 62

FARPIB

Flaps

Anti Skid

Lower Rudder

Power Transfer Unit (PTU)

INBD Roll Spoiler

Brakes

Hint 62

farpib

Front 63

Hydraulic System #2 operates ___

Back 63

LOSER

Landing Gear Extension/Retraction

Outboard Roll Spoilers

Steering

Emergency/Park Brake

Upper Rudder

Hint 63

loser

Front 64

Hydraulic Pressures

-Engine Driven Pump

Back 64

3000 psi (2900-3100)

Front 65

Hydraulic Pressures

-Standby Power Unit (SPU)

Back 65

2900 psi (2800-3000)

Front 66

Power Transfer Unit (PTU)

Back 66

Used for gear extension in the event of a right hand #2 engine failure or hydraulic pump failure

Front 67

Oxygen Requirement

-Crew

-Passengers

Back 67

2 crew 1300 psi

3 crew 1800 psi

crew portable 1800 psi

Pax 1800 (1100 min departure)

Front 68

Intermittent Gear Horn

Back 68

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

Front 69

Hydraulic Fluid Quantities

Left ___ Right ___ Emergency Hyd Sys ___

Back 69

2.5 usq (min disp 1.5)

4.5 usq (min disp 3.0)

1.21 usq

Front 70

Normal Take Off Torque

Back 70

Q200 99.5%

Q300 92%

Front 71

Max Continuous Power (MTOP)

Back 71

Q200 97.5% @1212 prop rpm

Q200 114.2% @1024 prop rpm

Q300 90% @1212 prop rpm

Q300 96% @1125 prop rpm

Front 72

FMS HSI Scaling

-Enroute

-Terminal

-Approach

Back 72

5.0 nm

1.0 nm

.3 nm

Front 73

Climb Profiles

Back 73

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

Front 74

Max Power Settings

314

301/311

201/202

103/106

102

Back 74

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

Front 75

Contact Approach

Back 75

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.

Front 76

MAX Tire Ground Speed

Q200

Q300

Back 76

139

165