Typos, Grammar and minor clarity changes

docs/pilots-corner/a380x/a380x-briefing/flight-deck/glareshield/afs.md

@@ -271,7 +271,7 @@ When pressed, selects either:
 - Shows `HDG` and `---` in managed target mode
 - Shows `TRK` and `---` in managed target mode
 
-Note: The HDG/TRK window shows TRUE, at the top left corner of the HDG/TRK window, if TRUE is selected with the 
+Note: The HDG/TRK window shows TRUE, in the top left corner of the HDG/TRK window, if TRUE is selected with the 
 TRUE/MAG pb.
 
 ### HDG/TRK Knob

docs/pilots-corner/a380x/a380x-briefing/flight-deck/glareshield/glare-underside.md

@@ -23,10 +23,10 @@ brightness of the glareshield integral lights and LCD brightness.
 
 From left to right:
 
-- Brightness for the instrument panel flood lights on the Captain side.
+- Brightness for the instrument panel floodlights on the Captain side.
 - Brightness for the glareshield integral lights.
 - Brightness for the LCD displays.
-- Brightness for the instrument panel flood lights on the First Officer side.
+- Brightness for the instrument panel floodlights on the First Officer side.
 
 
 ---

docs/pilots-corner/a380x/a380x-briefing/flight-deck/main-panel/isis.md

@@ -38,7 +38,7 @@ Both ISIS are connected to fully independent probes:
 
 !!! warning ""
     Only one ISIS is available in the A380X at this time.
-    Also the ISIS is not fully functional at this time.
+    Also, the ISIS is not fully functional at this time.
 
 ## Usage
 

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/air.md

@@ -44,7 +44,7 @@ description: The A380 Flight Deck Air Panel description.
     - Or when the pack overheats.
         - Associated with the following ECAM alert:
             - AIR PACK 1(2) OVHT
-        - The FAULT light goes off when the overheat disappears.
+        - The FAULT light goes off when the overheat condition disappears.
     - Or when the pack has failed.
         - Associated with one of the following ECAM alerts:
             - AIR PACK 1(2) FAULT

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/apu-fire.md

@@ -42,7 +42,7 @@ The APU compartment has a fire protection system, with:
 
 - OFF
     - The fire extinguisher bottle is not armed. 
-- SQUID
+- SQUIB
     - The squibs of the fire extinguisher bottle are armed. The fire extinguisher bottle is ready to discharge 
       extinguisher agent.
     - When pressed, the extinguisher bottle discharges and the SQUIB light goes off.

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/cargo-smoke.md

@@ -24,7 +24,7 @@ The Cargo Smoke Panel is used to detect smoke in the cargo compartments.
 ### AGENT TO FWD/AFT pb
 
 - Guarded and dark:
-    - No smke is detected.
+    - No smoke is detected.
 - Smoke:
     - Smoke is detected in the associated cargo compartment.
     - Associated with the following ECAM warning:

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/eng-fire.md

@@ -40,13 +40,13 @@ The Engine Fire Panel is used to control the engine fire detection and extinguis
 
 - AUTO: 
     - Normal position.
-- SQUID: 
+- SQUIB: 
     - The squibs of the fire extinguisher bottles are armed. 
     - The fire extinguisher bottles are ready to discharge extinguisher agent.
     - When pressed, the extinguisher bottles discharge and the SQUIB light goes off.
 - DISCH: 
     - The fire extinguisher bottle discharges or is empty.
-- SQUID & DISCH: 
+- SQUIB & DISCH: 
     - The flight crew is pressing the ENG FIRE panel TEST pb (Refer to [TEST pb](#test-pb)).
 
 ### TEST pb

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/ext-lt.md

@@ -41,7 +41,7 @@ The Exterior Lighting of an Airbus A380 includes these lights:
 Turns on and off the three synchronized strobe lights, one on each wing tip and one below the tail cone.
 
 - ON:
-    - Strobe lights or on.
+    - Strobe lights are on.
 - AUTO:
     - Automatically turns on strobe lights when the main gear strut is not compressed.
 - OFF:
@@ -55,7 +55,7 @@ There are three anti-collision beacon lights: Two on the top of the fuselage, an
 fuselage.
 
 - ON:
-    - Beacon lights or on.
+    - Beacon lights are on.
 - OFF:
     - Beacon lights are off.
 
@@ -71,7 +71,7 @@ Illuminate the leading edges of the wings and the engine air intake to show if i
 This switch turns the navigation lights on and off.
 
 - ON:
-    - Navigation lights or on.
+    - Navigation lights are on.
 - OFF:
     - Navigation lights are off.
 
@@ -94,7 +94,7 @@ There are two logo lights: One on the upper surface of each horizontal stabilize
 These lights provide lighting on the company logo that is on the tail fin.
 
 - ON:
-    - LOGO lights or on.
+    - LOGO lights are on.
 - AUTO:
     - The logo lights come on automatically, when the aircraft is on ground or in flight, when the
       slats are extended.
@@ -116,13 +116,13 @@ When the flight crew uses the taxi cameras at night, the camera lights provide g
 for the nose landing gear and the main landing gear.
 
 - ON:
-    - RWY TURN OFF lights or on.
-    - Camera lights or on, if ETACS is set to ON
+    - RWY TURN OFF lights are on.
+    - Camera lights are on, if ETACS is set to ON
 - OFF:
     - RWY TURN OFF lights are off.
     - Camera lights are off.
 
-These lights go off automatically when the landing gear is retracted.
+These lights turn off automatically when the landing gear is retracted.
 
 During takeoff, landing and approach, only the camera lights
 are on if:
@@ -156,7 +156,7 @@ The taxi lights enable the flight crew to detect obstacles on the taxiway.
 - OFF:
     - Taxi and takeoff lights are off.
 
-Note: The lights attached to the nose gear strut, go off automatically when the landing gear is retracted.
+Note: The lights attached to the nose gear strut turn off automatically when the landing gear is retracted.
 
 ---
 

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/fuel.md

@@ -60,7 +60,7 @@ fuel transfers to:
 
 - AUTO:
     - The transfer pump runs, if necessary:
-        - For an automatic fuel transfer from the inner, mid, or outer tanks, via the forward gallery, or
+        - For an automatic fuel transfer from the inner, middle, or outer tanks, via the forward gallery, or
         - For a manual transfer from the outer tanks, via the forward gallery (except if any outer tank pump has been switched off), or
         - During jettison.
 - OFF:
@@ -83,7 +83,7 @@ fuel transfers to:
 
 - ON:
     - The transfer pump runs, if necessary:
-        - For an automatic or manual fuel transfer from the inner, or mid tanks, via the aft gallery, or
+        - For an automatic or manual fuel transfer from the inner, or middle tanks, via the aft gallery, or
         - During jettison.
 - OFF:
     - The transfer pump is off.
@@ -119,10 +119,10 @@ fuel transfers to:
 ### INR(MID)(OUTR) TK XFR pb-sw
 
 - AUTO:
-    - Automatic fuel transfers from the inner (mid)(outer) tanks are available.
+    - Automatic fuel transfers from the inner (middle)(outer) tanks are available.
     - For more information: Refer to Fuel Transfer Sequence
 - MAN:
-    - Fuel manually transfers from the inner (mid)(outer) tanks to the feed tanks.
+    - Fuel manually transfers from the inner (middle)(outer) tanks to the feed tanks.
 - FAULT:
     - Comes on:
         - When automatic fuel transfers from the affected tanks are no longer possible.

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/hyd.md

@@ -55,7 +55,7 @@ The hydraulic systems ensure:
         - HYD G(Y) RSVR LEVEL LO
         - HYD G(Y) RSVR AIR PRESS LO.
     - The FAULT light goes off, when the flight crew selects OFF. However, in case of an overheat, the FAULT light 
-      will remain on, until the overheat disappears.
+      will remain on, until the overheat condition disappears.
 
 ### ENG PMP A+B DISC pb
 
@@ -109,7 +109,7 @@ The electric pumps are fully automatic and do not require any crew action, unles
         - HYD G(Y) RSVR LEVEL LO (on ground, with engines OFF)
         - HYD G(Y) RSVR AIR PRESS LO (on ground, with engines OFF) (Refer to procedure).
     - The FAULT light goes off, when the flight crew selects OFF. However, in case of an overheat, the FAULT light will
-      remain on, until the overheat disappears.
+      remain on, until the overheat condition disappears.
 
 
 ---

docs/pilots-corner/a380x/a380x-briefing/flight-deck/ovhd/maintenance.md

@@ -62,7 +62,7 @@ takes a priority over a refueling initiated from the external REFUEL panel.
     - Note: Only manual transfers can be initiated from the external REFUEL panel.
 - ON:
     - When pressed, automatic ground transfer is activated to automatically obtain the ground CG target.
-    - Note: All transfer pumps must selected ON to perform an automatic ground transfer.
+    - Note: All transfer pumps must be ON to perform an automatic ground transfer.
 - END/ON:
     - Automatic ground transfer is completed, or is aborted by the FQMS.
     - If the FQMS aborts the automatic ground transfer, the light flashes. 
@@ -181,7 +181,7 @@ Maintenance personnel uses this pushbutton to restart the fan.
 #### CKPT DOOR LCKG SYS
 
 Maintenance personnel uses this pushbutton-switch to turn off the Cockpit Door Locking System
-(CDLS), in order to ease ground operations (e.g. servicing, cleaning, maintenance, etc).
+(CDLS), in order to ease ground operations (e.g. servicing, cleaning, maintenance, etc.).
 
 - AUTO:
     - The CDLS is operative.

docs/pilots-corner/a380x/a380x-briefing/flight-deck/pedestal/cockpit-lighting.md

@@ -25,13 +25,13 @@ or when flying through clouds.
 
 ## MAIN PNL FLOOD LT (Main Panel Flood Light):
 
-This control adjusts the flood lighting for the main panel, which provides a wash of light over the entire instrument
+This control adjusts the floodlighting for the main panel, which provides a wash of light over the entire instrument
 panel. This general lighting is useful when the pilots need to see the entire panel without the need for backlighting on
 individual instruments.
 
 ## PEDESTAL FLOOD LT (Pedestal Flood Light):
 
-This knob controls the flood lighting over the pedestal area, where the throttle and other control systems like the
+This knob controls the floodlighting over the pedestal area, where the throttle and other control systems like the
 radio and flight management systems are located. This light allows for better visibility of the pedestal controls,
 especially important during critical flight operations.
 

docs/pilots-corner/a380x/a380x-briefing/flight-deck/pedestal/ecam-cp.md

@@ -136,7 +136,7 @@ requested by the flight crew, or prompted by the ECAM.
 
 * On EWD or SD clears the lines indicated by the displayed vertical bar.
 * The CLEAR pb light comes on, when there is an alert to clear on EWD.
-* Note: The CLEAR pb does not cancel any aural alerts associated witha caution/warning, and does not deactivate a 
+* Note: The CLEAR pb does not cancel any aural alerts associated with a caution/warning, and does not deactivate a 
   Not-Sensed ABN PROC.
 
 ### RCL LAST

docs/pilots-corner/a380x/a380x-briefing/flight-deck/pedestal/engine-master.md

@@ -37,7 +37,7 @@ description: The A380 Flight Deck Thrust and Thrust Reverser Control Levers desc
     - An automatic start sequence aborts, or
     - The HP fuel valve position is abnormal.
     - Associated with the ECAM alert ENG 1(2)(3)(4) HP FUEL VLV FAULT 
-    - The overthrust protection is active and the FADEC automatically shut downs the engine.
+    - The overthrust protection is active and the FADEC automatically shuts down the engine.
     - Associated with the ECAM alert ENG 1(2)(3)(4) CTL SYS FAULT
 
 ---

docs/pilots-corner/a380x/a380x-briefing/flight-deck/pedestal/rmp.md

@@ -189,7 +189,7 @@ In normal operation:
 ![img_9.png](../../../assets/a380x-briefing/flight-deck/pedestal/rmp-vhf-page.png){loading=lazy}
 
 1. Active frequency
-2. Loadspeaker symbol (indicating if reception is on or not)
+2. Loudspeaker symbol (indicating if reception is on or not)
 3. Transceiver Indicator (indicating if transmission is on or not)
 4. Standby frequency
 5. Clear the RMP message line