**AIRCRAFT “De Havilland - Dash DH8A-100”**

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: High wing

Engine position: (Front) Wing leading

Tail configuration: T high

Landing gear: Tricycle retractable

Wing Span: 25.9 m

Length: 22.3 m

Height: 7.5 m

Power plant: 2 x 2.000 SHP P&W 120A or

2 x 2.150 SHP P&W 121A turboprops with 4 blade propellers.

Accommodation: Flightcrew of two and typical 37 passengers in single class configuration.

Notes: Short range turboprop airliner. In service since 1984. Initial basic model of DHC-8

Dash 8 regional turboprop airliner family. Followed by the series 100A in 1990 with extra headroom and 100B (since 1992) with more powerful engines. From 1996 all Dash 8s

delivered with a computer controlled noise and vibration supression system.

Type designation with a Q for quiet. Canada mil. type: CT142, US-mil. type: E-9.
Alternative names:
CT-142, Dash 8 (100), DE HAVILLAND CANADA DHC-8-100 Dash 8 (E-9,CT-142,CC-142),

DE HAVILLAND CANADA E-9,CT-142,CC-142, DHC-8-100 Dash 8.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 15.650 kg

VMO - Maximum Operating Speed 250 KIAS

MMO - Maximum Operating Speed Mach  nd Mach

Turbulent Air Penetration Speed   000 KIAS/.00 Mach

VLO - Maximum Gear Operating Speed   000 KIAS

VLE - Maximum Landing Gear Extension Speed   000 KIAS/.00 Mach

 

*****Maximum Flap Placard Speeds*****

Flaps degrees KIAS

1                      000

2                      000

5                      000

10                    000

15                    000

25                    000

30                    000

40                    000

 

*****Take-off*****

WTC:               M

Distance:         900 mt

V2 (IAS):         100 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 130 kt

ROC:               1800 ft/min

-(to FL150)

IAS:                 200 kt

ROC:               1500 ft/min

-(to FL240)

IAS:                 200 kt

ROC:               1000 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                250 kt

MACh:             nd data

Ceiling:            FL250

Range: 1000 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 250 kt

ROD:               1500 ft/min

 

*****Approach*****

IAS:                 250 kt

MCS:               150 kt

ROD:               1500 ft/min

 

*****Landing*****

Vht (IAS):        100 kt

APC:                B

Distance:         900 mt