Aircraft specs QANTAS VIRTUAL AIRWAYS 

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Warning

 

Information on this page is intended for PC simulator use only. Do not use for
                   real world navigation. It may be outdated, unreliable or entirely wrong !

for all fleet fuel calculations, download this handy program

 

FUEL11.zip

 


IMPORTANT INFORMATION UPDATES

 

QVA Fleet Operating Speeds PDF file.

Angle of Attack (AoA) reference guide (pdf file)

Dash 8 Operations guide

 


 DEFINITIONS:
 

Term:

Definition:

Velocity/speed

V1

The go/ no-go decision speed for completion of takeoff

Vr

The Rotation speed or Lift-off speed

V2

Safe Climb-out speed (the speed after Vr)

Vfri

Minimum flap retraction speed (Typical for turboprops)

Vclimb

Minimum safe climb speed with 1 engine inop and the other at MCP

Vs1

Stall speed - clean (no flaps or undercarriage)

Vso

Stall speed @ full flap/gear down (flying dirty)

Vfe

Maximum flap extension speed – the maximum speed for using a certain flap setting without causing structural  damage

Vref

Threshold Reference speed, 1.3 times stall speed (Vso)

MLW

Maximum Landing Weight

MTOW

Maximum Take Off Weight

Vapp

Approach Speed , Vref +20

Vno

Maximum Normal Operating Speed

Vmo

Maximum Operating Speed

Vne

Never Exceed this Speed

FL

Flight Level eg FL350 = 35,000 feet

N1

Maximum thrust

 

 

 

 

Dash 8 Q400 Technical Specifications

Engines

PW150A

Max Cruise Speed

360kts TAS

Vlo

200kts

Max Power

5,071 SHP

Ceiling

FL250

Flap Extension Speeds (Vfe)

MTOW

28,998kg

Vmo (Max Operating)

Flap 5°

200kts

MLW

28,009kg

Below 8,000ft

245kts

Flap 10°

181kts

MZFW

25,855kg

10,000ft

282kts

Flap 15°

172kts

Max Payload

8,670kg

18,000ft

286kts

Flap 35°

158kts

Max Fuel Load

1,724 US gal

20,000ft

275kts

Va

204kts

 

5,200kg

25,000ft

248kts

Max Tyre Speed

182kts

Max Range

1,362nm

Vle

215kts

Crosswind Limit

32kts

 

Dash 8 Q400 Checklists

 

FlightDeck Safety Checks

Before Start

Starting

After Start

Taxi Checks

Documentation

Safety Equipment

Ldg Gear & Pins

Engine Intake Drs

Circuit Breakers

Batteries

Main Bus Tie

Fire Det & Smoke

Ext Pwr/APU

Battery Temps

Bleed Air 1+2

APU Bleed

Bus Voltage

Recirc Fan

Press/Packs

Avionics

System Test

Check

Test/Chk

Check

Open

Check

On/Check

Tie

Tested

On

Check

Off

As Reqd

Check

On

Set

Checked

Checked

GPU/APU

Emergency Lights

Fuel Transfer/Qty

Brake/Pressure

Pwr/Cond levers

Nose Steering

Briefing

On

Arm

Off

On/Check

Disc/Flo

Off

Complete

Takeoff Data/Trim

Door/Fuel Lights

Passenger Signs

Escape Hatch

Cabin Report

Flt Deck Door

Anti Collision

APU Bleed

Batts/Bus Volts

Check/set

Out

On

Closed

Received

Locked

Red

Off

On/26 min

Ext pwr/APU

Electric panel

Bleeds

Radar

----------Pushback

Condition Lvrs

Autofeather

Fuel Pumps

Hydraulics

Flaps

Rudder

Nose Steering

Flight/Taxi

PFD/MFD/ED

Yaw Damper

De-ice Press

Ice protection Test/Set

Off

Check

On/Norm

Standby

-----------

Max

Select

On

Checked

Set/Indctg

Full Travel

On

Taxi

Check

On

Check

As Rq'd

Brakes

T/O Warning Test

Altimeters

Pitot Static

Pwr for T/O

Flight Instruments

Cabin

Flying Controls

Cabin Crew

Clearances

Tpndr/TCAS

Check

Tested

QNH Set

On

%

Check

Secure

Full/Free

Chime

Reviewed

Alt/Auto

Line Up

After Take Off

Climb

Descent

Approach

Anti-Collision

Landing Lights

Flight/Taxi

When Cleared for de

Bleeds

Caution/Warning pnl

White

On

Flight

parture

Min/Off

Check

Landing Gear

Flaps

Bleeds

Climb Power

Up

Zero

On/Norm

Set

Altimeters

Ice Protection

Pressurisation

Hyd Pump PTU

Fuel Pumps

Autofeather

1013

As Rq'd

Check

Norm

Off

Off

Pressurisation

Ice Protection

GPWS Flap Pos

Briefing/MSA

& Bugs

Set

As Rq'd

As Rq'd

Reviewed & Set

Altimeters

Ice Protection

Fuel Transfer

Fuel Pumps

Hyd Pump/PTU

Hydraulics

Passenger Signs

Caution/W panel

Cabin

QNH set

As Rq'd

Off

On

On

Check

On

Check

Secure

Landing

After Landing

Shutdown

Last Flight

Cabin Crew

Ice Protection

Landing Gear

RDC Np

Condition Levers

Flaps

Bleeds

Chime

As Rq'd

Down 3

Armed

Max

Set/Ind

Min/Off

Control Locks

Anti Collision

Transponder/TCAS

Flaps

Radar

Fuel Pumps

Flight/Taxi

Ice Protection

Main Bus Tie

Yaw Damper

Bleeds/APU

OSG

On

Red

As Rq'd

Zero

Stby

Off

Taxi

Off

Tie

Off

As Rq'd

Check

Brake

Hyd Pump/PTU

Pwr/Cond Levers

Nose Steering

Radar

GPU/APU - Bleeds

Engine Bleeds

Cond Lvrs (30sec)

Passenger Signs

Lights

Battery Master

On

Norm

Disc/SFX

Off

Off

As Rq'd

Off Diff 0

Fuel Off

Off

As Rq'd

As Rq'd

PA Check

Ice Protection/

Intake Doors

Recirc Fan

Ignition

Packs

APU

Battery/Master

Anti Skid

Emerg/Dome +

Board lights

Complete

Off

Closed

Off

Off

Man/Off

Off

Off

Off

Off

 

 

 

Boeing 717 Flight Operations 

AIRCRAFT SPECIFICATIONS 

Weights:
Max Taxi	115,000Lbs
MGTOW		114,000Lbs  (Max Gross Take Off Weight)
Max Landing	102,000Lbs
Zero Fuel	 96,000Lbs

Fuel Capacity In Pounds (6.7Lbs/U.S. Gallon)
Right Main	Left Main	AUX Tank	Total
9,286		9,286		6,030		24,602	

Engine Type: BMW/Rolls Royce BR715, 18,500lbs thrust each.

Aircraft Speeds (All speeds are indicated airspeeds, in knots.
Speed Limitations:
Vmo/Mmo	325KIAS/M.84	(Max Overspeed) M=MACH
Flaps/Slats	  5Deg	280KIAS (visual model now has slats)
Down		15Deg	240KIAS
		20Deg	240KIAS
		25Deg	220KIAS
		40Deg	190KIAS
		50Deg	190KIAS
Gear Down	VLe	300KIAS  Maximum
Gear Up/down	VLo	250KIAS	 ""
Maneuvering	235KIAS Below 100,000Lbs
Va		239KIAS Above 100,000Lbs
TakeOff  (Here I only list at MGTOW)
V1		138KIAS	(Engine out, commit to T/O)
Vr		140KIAS	(Rotate)
V2		146KIAS	(Initial Climb)
Climb Schedule (2 Engines)	290KIAS to MACH .72
Climb Schedule (1 Engine)	210KIAS
Descent & Landing  (Based on Max Gross Landing Weight. MGLW)

Recommended Maneuvering Speeds:
0 Flaps		230KIAS
5Deg		205KIAS
15Deg		160KIAS
25Deg		Vref + 20Kts
50Deg (Vref)   	138KIAS (at 110,000Lbs)
		135KIAS (at 108,000)
			132KIAS (at 105,000)
			129KIAS (at 100,000)
		126KIAS (at 95,000)
			123KIAS (at 90,000)
			119KIAS (at 85,000)
		116KIAS (at 80,000)
			113KIAS (at 75,000)
			109KIAS (at 70,000)

Turbulent Air Penetration:
M.79 or 285KIAS, whichever is lower. DO NOT CHASE THE AIRSPEED.	
Note: Below 10,000Ft at Max landing Weight or less, 250KIAS is applicable.

Maximum Operating Altitude, 35,000Ft

NORMAL OPERATIONS, DESCRIPTION
Autolands are supported (using GPWS V7.2 with AC set to B.)
NOTE:  IF you have full tanks, you must burn off at least 1,000Lbs of fuel
prior to takeoff.  The aircraft is not certified for flight above gross
weights of 114,000Lbs.
1. Take Off thrust must not exceed 5 minutes total time.
2. Normal Take Off, set flaps (usually 3 notches) depending on fuel/
   passenger load, length of runway.
3. Apply thrust to accelerate, maintain below 70% N2.  When airspeed exceeds
   40 - 60 Kts, apply takeoff thrust.
4. At Vr, rotate smoothly to takeoff attitude (5 - 10 deg nose up).  Confirm
   positive rate of climb at takeoff.
5. At 35Ft AFL (Above Field Level), raise gear, speed should be at V2 to V2 + 
   10Kts, climb to 1000 AFL at V2 + 10Kts, 20Deg pitch.
6. At 1000 AFL, reduce pitch attitude by not more than 1/2 (one half) the
   angle required for V2 + 10Kts to reach 1000 AFL.  Set climb thrust
   (normally 85% N2 (FAN Indicator).  Maintain climb gradient while
   accelerating. Retract Flaps/Slats on schedule.
7. Continue acceleration to Vzf (Zero Flaps)speed.  If Vzf is reached before
   3000Ft, climb at Vzf to 3000Ft.
8. 3000Ft AFL, accelerate to 250Kts, maintain 1000-1500 ft/mn rate of climb
   during acceleration. Climb at 250Kts to 10,000Ft.
9. Accelerate to climb schedule (290KIAS to .79M) past 10,000Ft to cruising
   altitude.
   Maintain speed until cruise altitude is reached.

Vzf Schedule:
Flaps Retract	V2+25 (5Deg T.O. Flaps)
	V2+35 (15Deg T.O Flaps)
Cruise power is approximately 70% to 75% N1 (FAN Indicator) .80M.  Long Range
cruise is .76M.

Descent in Range (to landing):
1. Start Descent at XXX DME.  Target descent rate is 500 Ft/mn to reach
assigned level. To determine XXX, use the following formula (Altitude (in
1,000's) X 3 = DME distance to start descent)
Example 1	Cruise altitude 31,000
	 	DME transmitter on field
		31 (000)
		X 3
		Start Decent at	93 Miles DME
		Cruise Altitude 31,000
		Airport 10 Miles beyond DME transmitter
		From Example 1 93 Miles DME
		Airport Beyond Transmitter -10 Miles
		Start Descent at 83 Miles DME
2. 50 miles from the outer marker, level off at 10,000ft and decelerate to
   250 KIAS.
3. Descend at 250KIAS 40 miles from outer marker, turn on landing lights.
   Slats can be used to maintain a descent rate of 1,000ft/mn to our initial
   approach altitude.
4. Set 5 Deg Flaps on entering IAP (initial approach point).  Speed set at
   160 KIAS. Descend to MDA (Minimum Descent Altitude).
5. At localizer capture, drop gear, set spoiler to auto deploy, final check
   list.
6. At Glideslope + 1 dot, set 25Deg Flap, Speed Vref(50) + 20Kts.
7. At Glideslope capture, Full Flaps, follow glideslope.  Maintain Vref on
   final.
8. Land.
9. After landing, retract flaps, slats, taxi to terminal.

 


 

Boeing 737 Flight Operations

737-376

Air Speeds

Vs/Vso

V1

KIAS

VR

KIAS

V2

KIAS

Vno/ Mno

KIAS/ Mach

Vmo/ Mmo

KIAS/ Mach

Vne/ Mne

KIAS/ Mach

Vapr

KIAS

Vref

KIAS