F-15E Procedures - Versionshistorik

DeadGun: /* Tactical Formations */

2026-02-04T19:56:51Z

Tactical Formations

DeadGun den 4 februari 2026 kl. 19.11

2026-02-04T19:11:37Z

DeadGun den 1 maj 2024 kl. 10.51

2024-05-01T10:51:16Z

DeadGun den 30 april 2024 kl. 15.47

2024-04-30T15:47:07Z

DeadGun den 30 mars 2024 kl. 11.56

2024-03-30T11:56:11Z

DeadGun: /* Climb */

2023-11-13T22:00:23Z

Climb

DeadGun den 12 november 2023 kl. 16.20

2023-11-12T16:20:02Z

DeadGun den 12 november 2023 kl. 16.16

2023-11-12T16:16:08Z

DeadGun den 12 november 2023 kl. 16.13

2023-11-12T16:13:11Z

DeadGun den 12 november 2023 kl. 14.11

2023-11-12T14:11:49Z

@@ Rad 177: / Rad 177: @@
 <u>General</u>
 * Visual references: </br>
-:- When turning into the formation/other aircraft, maintain same relative position. </br>
+:- When lead turning into wingman, maintain same relative position. </br>
-:- When turning away from formation/other aircraft, maintain the fuselages level and intake ramp leding edge on pilots helmet. </br>
+:- When lead turning away from wingman, maintain the fuselages level and intake ramp leding edge on pilots helmet. </br>
 * Visual signals: </br>

@@ Rad 173: / Rad 173: @@
 ====Tactical Formations====
 Formations explained [https://magwo.github.io/formations/ here].
-* Visual references for "finger tip": </br>
+<u>General</u>
-:- Align UHF antenna (Behind cockpit) and either the missile rail or the Position- and Anti-Col.lights on the wing root. </br>
+* Visual references: </br>
-:- Align the trailing edges of the vertical stabilizors. </br>
+:- When turning into the formation/other aircraft, maintain same relative position. </br>
 * Visual signals: </br>
-:- Yaw (pedal left and right) - Go to Route </br>
+:- Quick wingflick - Wingman cross over to other side. </br>
-:- TBD - Spread </br>
+:- Wing Rocking - Rejoin. </br>
 ===Ingress===

@@ Rad 2: / Rad 2: @@
 The following sections describe Tactics, Techniques and Procedures (TTP) that are valid only for F-15E.
-<pre style="color: red">Some Tactics and Techniques have reference to the manual "F-15E Manual EN", this manual can be found in the DCS installation folder "DCS World OpenBeta\Mods\aircraft\F-15E\Doc"</pre>
+<pre style="color: red"> If not specified in the Syllabus all procedures are to be followed as described in the F-15E Manual. (Linked below) </pre>
+[https://www.digitalcombatsimulator.com/en/downloads/documentation/ F-15E manual]
 ==Considerations==
 ===Operating Range/Altitudes===

@@ Rad 54: / Rad 54: @@
 ====Standard Conventional Loadout====
+[https://wiki.masterarms.se/index.php/CAS_SPINS#Table_of_MA_SCLs SCL]
 ==Tactics, Techniques and Procedures==

@@ Rad 56: / Rad 56: @@
 * SCL 1
-:- 1xGBU-24, 8xGBU-12, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
+:- 8xGBU-12, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
 * SCL 2
-:- 1xGBU-24, 8xGBU-38, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
+:- 6xGBU-54, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
 * SCL 3
-:- 1xGBU-24, 4xGBU-12, 4xGBU-38, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
+:-
 * SCL 4
-:- 12xMk-82, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
+:-
@@ Rad 107: / Rad 107: @@
 - The pilot must notify the WSO when R engine is up before proceeding to start the next one.</br>
 - The pilot must check with the WSO that the position is correct before starting INS ALIGN.</br>
 These steps are designed to minimize the risk of errors during start-up and to synchronize the crew and flight.
@@ Rad 119: / Rad 118: @@
 :- Throttle to 82%
 :- Release brakes
-:- Throttle to MIL/MAX
+:- Throttle to FULL MIL/MAX AB
 :- Stick half way back at rotation speed -> 10° pitch attitude
@@ Rad 125: / Rad 124: @@
 :- Throttle to 82%
 :- Release brakes
-:- Throttle to MIL/MAX
+:- Throttle to FULL MIL/MAX AB
 :- Stick full back at 10kts below nose wheel lift-off speed and rotate to 12° pitch attitude.
@@ Rad 149: / Rad 148: @@
 Land using Overhead Break as explained [http://wiki.masterarms.se/images/9/9e/OverheadBreak.png here]*
-''* Stay at between 200-250kts on downwind leg until base turn.
+''* Stay at ≈210kts on downwind leg until base turn. Aim to roll out on final with threshold at -3° and α20-22

@@ Rad 131: / Rad 131: @@
 * MIL Power
-:- Drag index of 60 or less, climb at 350kcas to M0.9, then maintain M0.9 to cruise altitude. If speed increases above M0.95 at 40° pitch attitude, maintain 40° pitch attitude.
+:- Drag index of 60 or less, climb at 350 KCAS to M0.9, then maintain M0.9 to cruise altitude.
-:- Drag index greater than 60, climb at 350kcas to M0.9, then maintain M0.9 to cruise altitude.
+:- Drag index greater than 60, climb at 300 KCAS to M0.75, then maintain M0.75 to cruise altitude.
 * MAX Power
-:- Drag index of 60 or less, climb at 350kcas to M0.95, then maintain M0.9 to cruise altitude.
+:- Drag index of 60 or less, climb at 350 KCAS to M0.95, then maintain M0.95 to cruise altitude. If speed increases above M0.95 at 40° pitch attitude, maintain 40° pitch attitude.
-:- Drag index greater than 60, climb at 300kcas to M0.75, then maintain M0.75 to cruise altitude.
+:- Drag index greater than 60, climb at 350 KCAS to M0.9, then maintain M0.9 to cruise altitude.
 * Drag Index

@@ Rad 5: / Rad 5: @@
 ==Considerations==
 ===Operating Range/Altitudes===
@@ Rad 17: / Rad 16: @@
 ===Day versus Night===
 ====Lights====
@@ Rad 139: / Rad 137: @@
 :- Drag index of 60 or less, climb at 350kcas to M0.95, then maintain M0.9 to cruise altitude.
 :- Drag index greater than 60, climb at 300kcas to M0.75, then maintain M0.75 to cruise altitude.
 ====Landing====
@@ Rad 177: / Rad 174: @@
 - If not max range/endurace is needed, cruise at M0.8-0.85  </br>
 - To make it easier for wingman to follow, FL should set a FTIT.
 ====Tactical Formations====
@@ Rad 198: / Rad 194: @@
 :- Quick wingflick - Wingman cross over to other side.  </br>
 :- Wing Rocking - Rejoin
 ===Ingress===
@@ Rad 225: / Rad 222: @@
 ===Attack===
 ====Air-To-Air====

← Äldre version		Versionen från 12 november 2023 kl. 16.13
Rad 140:		Rad 140:
	:- Drag index greater than 60, climb at 300kcas to M0.75, then maintain M0.75 to cruise altitude.		:- Drag index greater than 60, climb at 300kcas to M0.75, then maintain M0.75 to cruise altitude.

−	~~{\| class="wikitable"~~
−	\|-
−	~~! scope="col" rowspan="2" \| GWT (lbs)~~
−	~~! scope="col" colspan="2" \| Rotation- / Nosewheel Lift-Off- / Takeoff Speed (KCAS)~~
−	\|-
−	~~! MAX THRUST~~
−	~~! MIL THRUST~~
−	\|-
−	~~\| 40,000~~
−	~~\| 110 / 133 / 159~~
−	~~\| 115 / 127 / 147~~
−	\|-
−	~~\| 45,000~~
−	~~\| 115 / 136 / 162~~
−	~~\| 120 / 132 / 150~~
−	\|-
−	~~\| 50,000~~
−	~~\| 120 / 140 / 166~~
−	~~\| 125 / 136 / 154~~
−	\|-
−	~~\| 55,000~~
−	~~\| 125 / 145 / 169~~
−	~~\| 130 / 140 / 158~~
−	\|-
−	~~\| 60,000~~
−	~~\| 130 / 150/ 173~~
−	~~\| 135 / 145/ 163~~
−	\|-
−	~~\| 65,000~~
−	~~\| 140 / 159 / 181~~
−	~~\| 145 / 154 / 170~~
−	\|-
−	~~\| 70,000~~
−	~~\| 155 / 169 / 190~~
−	~~\| 155 / 162 / 180~~
−	\|-
−	~~\| 75,000~~
−	~~\| 160 / 177 / 196~~
−	~~\| 160 / 168 / 187~~
−	\|-
−	~~\| 81,000~~
−	~~\| 167 / 181 / 200~~
−	~~\| 167 / 172 / 194~~
−	\|-
−	\|}

	====Landing====		====Landing====

@@ Rad 63: / Rad 63: @@
 * SCL 3
 :- 1xGBU-24, 4xGBU-12, 4xGBU-38, 3xAIM-120C, 1xAIM-9M, 2xFuel Tank, NAV/TGT-Pods, 500x20mm
@@ Rad 119: / Rad 121: @@
 :- Throttle to 82%
 :- Release brakes
-:- Throttle to MIL, Nozzles <30%
+:- Throttle to MIL/MAX
 :- Stick half way back at rotation speed -> 10° pitch attitude
@@ Rad 125: / Rad 127: @@
 :- Throttle to 82%
 :- Release brakes
-:- Throttle to MAX
+:- Throttle to MIL/MAX
 :- Stick full back at 10kts below nose wheel lift-off speed and rotate to 12° pitch attitude.
@@ Rad 141: / Rad 143: @@
 |-
 ! scope="col" rowspan="2" | GWT (lbs)
-! scope="col" rowspan="2" | CG (%)
+! scope="col" colspan="2" | Rotation- / Nosewheel Lift-Off- / Takeoff Speed (KCAS)
 |-
-! colspan="2" | MAX THRUST
+! MAX THRUST
-! colspan="2" | MIL THRUST
+! MIL THRUST
 |-
-| rowspan="5" | 65,000
+| 40,000
-| 28
+| 110 / 133 / 159
-| -
+| 115 / 127 / 147
 |-
-| 26
+| 45,000
-| -
+| 115 / 136 / 162
-| -
+| 120 / 132 / 150
 |-
-| 25
+| 50,000
-| -
+| 120 / 140 / 166
-| -
+| 125 / 136 / 154
 |-
-| 24
+| 55,000
-| -
+| 125 / 145 / 169
-| -
+| 130 / 140 / 158
 |-
-| 22
+| 60,000
-| -
+| 130 / 150/ 173
-| -
+| 135 / 145/ 163
-| -
+|-
-| -
+| 65,000
 |-
 |}