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DCS: AJS-37 Viggen
Normal prodedures
created by super
Normal prodedures
Ground Power (If needed)
On
Flight plan made (B for navigation, M for attack waypoint, L for landning)
data cartridge
Inserted
HUVUDSTRÖM (main power)
TILL (On)
LT - KRAN (low pressure fuel valve)
TILL (On)
HUVUDVARNING (master caution)
reset / pressed
High pressure fuel valve
open
press throttle "flap" to open
GENERATOR SWITCH
TILL (On)
Cockpit lights
As desired
Canopy
Close
OXYGEN FLOW VALVE
TILL (open)
START SWITCH
TILL - HOLD FOR 2 SECONDS
CK37
Data selector
REF/LOLA
IN/OUT SELECTOR
IN
NUMPAD
9099
CONFIRM
LS/SKU
IN/OUT SELECTOR
OUT
Data selector
AKT/POS
16
Before taxi
Ground power (if on)
Off
Pitch Trim
without drop tank 0°
with drop tank 3° ↑
EJECTION SEAT
ARMED
Master mode selector
NAV
SET ALL BACKPUT SYSTEM
BEFORE TAKE OFF
ALIGN AIRCRAFT WITH RUNWAY
TAKE OFF
BRAKES
ON
throttle
MILL
AFTER BURNER
STAGE 1
for normal length take-off / normal length runway
AFTER BURNER
STAGE 3
for short take-off / roadway runways
speed 250-300 km/h
pull up
AFTER TAKE OFF
LANDING GEAR
Up
HUD REFLECTOR GLASS
Up
26
Visual approach
Flight should be planned with at least a 10% remaining on touchdown. A normal landing pattern uses about 8% fuel.
Reduce airspeed
550 km/h during approach.
LANDING GEAR
DOWN
Check landing gear indicator (3 green fields)
Landing light
ON (LANDNING)
Preselect thrust reversal
if desired.
Set HUD reflector
lower setting (landing mode)
Set master mode
LANDN PAR/ OPT
Do not fly below an airspeed corresponding to 12° α (AoA).
Turn final during descent with a minimum airspeed of 12° α (AoA)
Check indicated airspeed at 1 G that a reasonable value for current weight.
Aim for a 3° angle of descent and reduce airspeed to correspond to 12° α (AoA). The line in the HUD during LANDN P/O corresponds to 2.86°.
Place the descent line on the runway threshold and centre the sight dot on the centreline, steer the flight path indicator onto the line. Maintain attitude. Strive for a touchdown at about 100-200 metres in on the runway
At 15 metres altitude above the runway (30 if not using the radar altimeter), the HUD will change to the descent rate mode. The previous 2.86° line represents the maximum vertical velocity (2.96 m/s).
Thrust reversal (if preselected) will activate once nose wheel is depressed.
to use thrust reversal go full throttle
TILS landing
Set landing base as destination
Press L MÅL
Set QFE pressure on altimeter
Select runway heading
cycle runway heading, BANA/ UT (OUT) and press LS
Set master mode LANDN NAV about 30 km away from the destination
Set Autothrottle ON if desired. Autopilot mode SPAK ON.
Follow steering commands on the HUD or ADI
If using TILS to land, check that TILS is locked (TILS light lit) and used after the LB turn is complete. If using a short approach set master mode to LANDN P/O and then return the master mode selector to LANDN NAV in order to select the touchdown point LF as destination.
Check backup artificial horizon
36
TILS landing
Lower the landing gear about 15 km out from the runway
Set HUD reflector glass to landing mode about 14 km out.
. Check that the TILS is locked (TILS light solid)
Follow steering commands on HUD or ADI. Maintain altitude and airspeed. The glideslope should be intercepted about 10 km from the runway.
On the descent command follow the glide path steering commands in the HUD and ADI.
If desired set AFK mode 3 (α 15.5)
On touchdown follow normal landing procedures.
Alternate Runway heading selection.
Data selector in mode AKT POS / OUT.
Confirm landing base on the destination indicator.
Data selector in mode BANA/GRÄNS.
Runway heading is displayed on the data indicator.
Cycle runway headings by pressing once or multiple times until the desired runway heading is displayed.
Select AKT POS / OUT.
Flip-flop (shorten approach length)
. Master mode NAV or LANDN NAV (or P/O)
Confirm selected landing base
Select master mode P/O, and then select LANDN NAV
LF should be displayed on the destination indicator.
46
There are two main styles of braking during landing.
Aerobraking
After touchdown gently pull back the stick to AoA (α) 16°.
Lower the nose at around 160 km/h.
Steer with the rudder.
Apply brakes evenly.
If needed, engage thrust reversal.
Normal braking (with or without thrust reversal)
Lower nose immediately after touch-down
Engage thrust reversal if needed.
Apply wheel brakes evenly.
Steer with the rudder.
56
After landing
Master Mode selector
BER
Taxi / Landing lights
Desired position
Shutdown procedure
Ejection seat
SAFE
AFK (Autothrottle) lever
OFF (Upper)
Generator
OFF
Avionics and other systems (RWR, IFF, External illumination, etc.)
OFF
Oxygen
OFF
Low pressure fuel valve (LT-KRAN)
OFF
Canopy
Open
Main Power
OFF
66