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lights) limit the ability to see objects outside of the area.
NOTE
Bright ground lights may cause loss of ground references during
landing. Avoid looking directly at bright light sources to prevent
degrading NVG vision.
The NAVFLIR is not affected by light sources and complements NVG use.
A1-F18EA-NFM-000
III-9-17 ORIGINAL
9.4.3 Weather Conditions. NAVFLIR and NVG provide a limited capability to see through visibility
restrictions such as fog, rain, haze, and certain types of smoke. As the density of the visibility
restrictions increases, a gradual reduction in light occurs. Use of an offset scanning technique will help
in alerting the pilot to severe weather conditions.
NOTE
Visibility restrictions produce a ``halo'' effect around artificial lights.
9.4.4 Object/Target Detection. Detection ranges are largely a function of atmospheric and environmental
conditions. Moving targets with contrasting backgrounds or targets with a reflected or
generated light or heat sources can be identified at greater ranges when using NVD.
9.4.5 Flight Preparation. Flights with NVD require unique planning considerations that include
weather, moon phase/angle, illumination, ground terrain and shadowing effects. Tactical consideration
and procedures can be found in the Night Attack operational tactics guides (OTG).
9.5 SHORT AIRFIELD FOR TACTICAL SUPPORT (SATS) PROCEDURES
9.5.1 Landing Pattern. Approach the break point either individually or in echelon, parade formation,
at 250 KIAS. A 17 to 20 second break interval provides a 35 to 40 second touchdown interval. The
landing checklist should be completed and the aircraft should be at on-speed AOA/approach speed by
the 180° position.
9.5.2 Approach. Plan for and execute an on-speed approach. Pay particular attention to maintaining
the proper airspeed and correct lineup.
9.5.3 Waveoff. To execute a waveoff, immediately add full power and maintain optimum attitude.
Make all waveoffs straight ahead until clear of the landing area.
9.5.4 Arrested Landing. The aircraft should be on runway centerline at touchdown. Aircraft
alignment should be straight down the runway, with no drift. Upon touchdown, maintain the throttle
at the approach position. When arrestment is assured, retard the throttle to idle. Allow the aircraft to
roll back to permit the hook to disengage from the pendant. When directed by the taxi director, apply
both brakes to stop the rollback and raise the hook. If further rollback is directed, release brakes and
allow the aircraft to be pulled back until a brake signal is given. Apply brakes judiciously to prevent
the aircraft from tipping or rocking back.
Use extreme caution when taxiing on a wet SATS runway.
A1-F18EA-NFM-000
III-9-18 ORIGINAL
9.5.5 Bolter. Bolters are easily accomplished. Simultaneously apply full power and retract the
arresting gear hook. Smoothly rotate the aircraft to a lift-off attitude and fly away.
If landing on a runway with a SATS catapult installed, care must be
taken to prevent engagement of the dolly arrester ropes with the aircraft
tailhook. Structural damage to the aircraft and catapult will result.
9.6 HOT SEAT PROCEDURE
1. PARK BRK handle - SET
2. Paddle switch - PRESS (disengage NWS)
3. Left throttle - OFF
4. Throttle friction - MAX
5. Avionics - AS DESIRED
9.7 ALERT SCRAMBLE LAUNCH PROCEDURES
9.7.1 Setting the Alert. The alert/scramble aircraft shall be preflighted in accordance with NATOPS
normal procedures every 4 hours or as local directives dictate. The pre-alert turn shall consist of full
Plane Captain checks and full systems checks. Minimum requirements are:
1. Radar BIT status - GO
2. AIM-7 - TUNED (if loaded)
3. INS alignment status - OK
4. COMM 1 and 2 - SET TO LAUNCH FREQUENCY
5. Launch trim - SET ( IAW Catapult Trim Calculations, Chapter 8)
Before engine shutdown -
6. INS known - OFF (10 seconds before engine shutdown)
NOTE
Do not switch INS to NAV during pre-alert turn so that STD HDG
option will be available for next alignment.
7. CRYPTO switch - HOLD then NORM
8. Sensors and weapon systems - ON
9. COMM 1 and 2 knobs - ON
A1-F18EA-NFM-000
III-9-19 ORIGINAL
10. EMCON - AS DESIRED
11. Exterior and interior lights - SET
12. DDIs, MPCD, and HUD knobs - ON
13. OBOGS control switch and OXY FLOW knob - OFF
14. Landing gear pins - REMOVED and STOWED
After engine shutdown -
15. External electrical power -CONNECT (if applicable)
16. EXT PWR switch - RESET then NORM
17. GND PWR switches 1, 2, 3, and 4 - OFF
18. BATT switch - OFF
19. SINS cable - CONNECT (if required)
9.7.2 Alert Five Launch.
If on external power -
　
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