Airbus MCDU Guide (4): Radio Navigation & Weight/Fuel Initialization Explained

Airbus MCDU Guide (4): Radio Navigation & Weight/Fuel Initialization Explained

✈️ Airbus MCDU Operating Guide · Part 4

Airbus MCDU PERF Page: Takeoff, FLEX & Approach Explained

By Daniel W August 30, 2025 9 min read MSFS 2020/2024 · X-Plane 12
Part 3 · RAD NAV & Fuel Part 4 · Performance (PERF) Part 5 · ATSU & ATC

The PERF page is where you set up the make-or-break phases of the flight. This guide walks through the TAKEOFF performance page — thrust reduction, flaps, FLEX temperature and V-speeds — and the APPR page that prepares your approach and landing.

1. The PERF page & flight phases

The PERF page stores the performance data for each phase of flight — takeoff, climb, cruise, descent, approach and go-around. The FMGS automatically advances through these phases as you fly, but the two you set up on the ground are TAKEOFF and APPR. Get these right and the aircraft flies the numbers for you.

2. Takeoff thrust: THR RED/ACC & TO SHIFT

THR RED / ACC

These are two altitudes, usually defaulting to around 3000 ft AGL. At the thrust reduction altitude (THR RED) the engines step back from takeoff to climb thrust; at the acceleration altitude (ACC) the aircraft lowers the nose to accelerate and retract flaps.

TO SHIFT

Used for intersection departures. If you're not starting from the very end of the runway, enter the distance (in metres) from the threshold to your actual takeoff point so the FMGS knows how much runway you really have.

Airbus MCDU takeoff performance parameters (THR RED/ACC)
The TAKEOFF perf page — THR RED / ACC altitudes.
Airbus MCDU TO SHIFT entry for an intersection departure
TO SHIFT — the runway shift for an intersection takeoff.

3. Flaps, FLEX temperature & engine-out

FLAPS / THS

Enter your takeoff flap setting (Config 1, 2 or 3) and the THS (Trimmable Horizontal Stabilizer, i.e. pitch trim) value from your load sheet. Each flap configuration has its own maximum speed (VFE): Config 1 is limited to about 230 kt, tightening down to roughly 177 kt at Config FULL — always respect the placard for the setting you're in.

Airbus flap configurations 1, 1+F, 2, 3, FULL
Flap configurations and their VFE speed limits.
Airbus MCDU FLAPS/THS entry example
Entering FLAPS / THS on the takeoff page.

FLEX TO TEMP

A flexible (reduced-thrust) takeoff. You enter an assumed temperature higher than the real outside air temperature — for example 46°C — and the engines produce less than full thrust. When the runway is long enough, this saves engine wear and extends engine life without compromising safety.

Airbus MCDU FLEX TO TEMP reduced-thrust setting
FLEX TO TEMP — an assumed temperature for reduced thrust.

ENG OUT ACC

The engine-out acceleration altitude — the altitude at which you'd level off to accelerate if you lost an engine after takeoff. It's normally set higher than the standard ACC altitude to clear obstacles on one engine.

4. Takeoff V-speeds (V1 / VR / V2)

The three takeoff speeds are computed from your weight, flap setting, runway and temperature. A typical set looks like this:

Speed Meaning Example
V1 Decision speed — the last point you can safely reject the takeoff 140 kt
VR Rotation speed — begin raising the nose 142 kt
V2 Takeoff safety speed — the target if an engine fails 144 kt
Airbus MCDU V1 VR V2 takeoff speeds
V1 / VR / V2 on the takeoff performance page.

Once you're airborne and past the acceleration altitude, the PERF page automatically advances to the CLB (climb) phase, where you can review or tweak the climb speed and any altitude constraints.

Airbus MCDU climb (CLB) performance page
The PERF page advances to CLB after takeoff.
Airbus MCDU climb phase reference
Climb-phase performance reference.

5. The APPR (approach) page

Before you start down, set up the approach on the PERF APPR page. The key fields:

QNH — destination airport pressure, from ATIS or ATC.
TEMP — destination airport temperature.
MAG WIND — wind speed and direction, referenced to magnetic north (not true north).
TRANS ALT — transition altitude, typically 18,000 ft.
Vapp — approach speed, computed automatically by the FMGS.
FINAL — the final approach segment.

MDA vs DH — know the difference: MDA (Minimum Descent Altitude) is the lowest altitude for a non-precision approach. DH (Decision Height) is the height at which you must decide to continue or go around on a precision approach such as an ILS — typically set anywhere from 0 to 700 ft.
Minima Approach type Meaning
MDA Non-precision Lowest altitude you may descend to without visual reference
DH Precision (ILS) Height to decide: continue to land or go around (≈ 0–700 ft)

Finally, set LDG CONF — the landing configuration, normally full flaps. With takeoff and approach both programmed, the PERF page has everything it needs to fly the profile.

Fly the numbers on real hardware.

Set FLEX, V-speeds and approach minima on a backlit Rowsfire panel instead of a mouse — tactile keys, authentic Airbus layout, plug-and-play with MSFS & X-Plane.

Explore Rowsfire cockpit panels

Frequently asked questions

What is the PERF page on the Airbus MCDU?
PERF holds performance data for every flight phase — takeoff, climb, cruise, descent, approach and go-around. The FMGS advances through them automatically; you pre-set the TAKEOFF and APPR pages on the ground.
What is a FLEX takeoff (FLEX TO TEMP)?
A reduced-thrust takeoff. You enter an assumed temperature higher than the actual OAT (e.g. 46°C) so the engines make less than full thrust. On a long-enough runway this reduces engine wear without compromising safety.
What do V1, VR and V2 mean?
V1 is the decision speed — the last point to safely reject the takeoff. VR is the rotation speed, where you raise the nose. V2 is the takeoff safety speed you target if an engine fails. They're computed from weight, flaps, runway and temperature.
What's the difference between MDA and DH?
MDA (Minimum Descent Altitude) is the lowest altitude for a non-precision approach. DH (Decision Height) is the height on a precision approach (e.g. ILS) where you decide to land or go around, typically 0–700 ft.
What is THR RED/ACC?
Two altitudes, usually around 3000 ft AGL. At THR RED the engines reduce from takeoff to climb thrust; at ACC the aircraft accelerates and retracts flaps.

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