Airbus Flight Instructor
Airbus · Knowledge Base

Main Transfer — the Burn Order

Engines only ever drink from the inner tanks' collector cells. Every other tank is a warehouse, and main transfer is the logistics that moves stock to the shop floor: centre fuel pushed inboard by pumps, outer fuel released inboard by gravity, in a fixed order that ends with the bending-relief fuel last. This article covers the sequence, the two transfer mechanisms, their automatic triggers, and the manual overrides.


1. The burn order

   six-tank aircraft:                     five-tank aircraft:
   ① TRIM (CG schedule — own logic)       ① TRIM (CG schedule)
   ② CENTRE ──pump──► INNER               ② INNER burns
   ③ INNER burns                          ③ OUTER ──gravity──► INNER (last)
   ④ OUTER ──gravity──► INNER (last)

Two rules generate the whole table: the inner tanks are kept topped up from the centre while it lasts, and outer fuel — the wing-bending-relief ballast — is released only when the inners are nearly down to it (overview). Trim-tank fuel rides its own CG timetable (aft-CG transfer / forward transfer).


2. Centre → inner: pumped, in a top-up cycle (six-tank aircraft)

Two transfer pumps in the centre tank push fuel into the inner tanks through the inner-tank inlet valves. The FCMS runs it as a hover-around-full cycle: fill an inner to its high level, pause, resume when it has burned down about 2 000 kg below high level, repeat. The pause threshold on the receiving side is the underfull point — set approximately 2 500 litres below the volume that wets the high-level sensors (referenced to a level aircraft). Net effect: while the centre tank has fuel, the inner tanks stay essentially full and all the burn is logically "centre fuel".

Manual layer: the CTR TANK XFR pushbutton set to MAN commands the transfer regardless of the automatic schedule — the procedures use it when level-sensing or FCMS logic is suspect, typically gated on "WHEN EITHER INR < 17 T" (17 tonnes = the system's universal "is there room in the inner tank" gate, recurring across the abnormal chapter). Setting it to MAN also stops any aft transfer in progress — manual main-transfer intervention and automatic CG scheduling do not run together.

The pumps protect themselves by logic rather than endurance: centre empty + pump still running = FUEL CTR TK XFR FAULT, whose procedure switches them off before the dry-run thermal fuses decide the matter permanently (main fuel pumps, transfer faults).


3. Outer → inner: gravity through latched valves

The outer tanks sit outboard and slightly higher; their fuel needs no pump — only permission. Each side has an intertank transfer valve (codes O/P) that the FCMS opens when the inner side needs the reserve:

Manual layer: OUTR TK XFR pushbutton ON opens the transfer valves (and the related inlet valves) immediately — the "release the reserves now" button. The abnormal procedures lean on it constantly: it is the second line of the low-level fuel-grab, the CG-forward tool in the trim-fuel-unusable drill, and the gallery detour when the crossfeed is failed closed. Like CTR TANK XFR MAN, setting it ON suspends automatic aft transfer.

[!warning]- The two transfers are different machines Centre→inner is pumped, cyclic, modulated; outer→inner is gravity, latched, all-or-nothing. That is why centre fuel can be "kept" while inners burn, but outer fuel, once released, is committed — and why procedures that need CG or balance effects from outer fuel (forward CG shift, gallery detour) reach for OUTR TK XFR rather than anything centre-side.


4. Dispatch

Some operators' MEL carries the main-transfer items along the architecture's lines: the outer-to-inner transfer function (intertank valves) and the centre transfer pumps each have their own items — a single centre transfer pump inoperative is typically dispatchable (the other pump covers, with conditions), while failures that remove a whole transfer path bring fuel-management and loading conditions. One indexing quirk worth knowing: the centre-tank pumps are filed under the transfer system (28-26), not the engine-feed pump chapter — the MEL classifies them by what they do, not what they look like.


Self-test

[!note]- Q1. Recite the burn order on a six-tank aircraft. Trim per its CG schedule; centre fuel pumped to keep the inners full; inners burn; outers released by gravity last (bending relief preserved longest).

[!note]- Q2. How does the centre→inner transfer decide to pause and resume? Fill to high level, pause, resume when the inner has burned ~2 000 kg below high level; the underfull point is ≈2 500 L below the high-level-sensor volume. A hover-around-full cycle.

[!note]- Q3. What is special about the intertank transfer valves once they open? They latch — outer→inner transfer runs to completion. Gravity does the moving; the valve only grants permission.

[!note]- Q4. What side effect do CTR TANK XFR MAN and OUTR TK XFR ON share? Both suspend automatic aft (CG) transfer — manual main-transfer intervention overrides the CG schedule.

[!note]- Q5. What does the recurring "17 t" gate mean in transfer procedures? It is the system's standard check that an inner tank has receiving room — manual centre-transfer steps wait for an inner below 17 tonnes before pushing more fuel in.

Key takeaways

Point Value
Order trim (CG schedule) → centre keeps inners full → inners → outers last
Centre→inner 2 transfer pumps; full / full−2 000 kg cycle; underfull ≈2 500 L below high level
Outer→inner gravity; latched valves; trigger at inner 3 500 kg / low level
Manual buttons CTR TANK XFR MAN, OUTR TK XFR ON — both suspend aft transfer
Self-protection centre empty + pump running → CTR TK XFR FAULT → pumps off
MEL quirk centre pumps filed under the transfer system (28-26)

References

Independent study material, not an Airbus publication and not endorsed by the manufacturer. Always defer to the current operator FCOM, FCTM, and QRH for operational use.