Airbus Flight Instructor
Airbus · Knowledge Base

Fuel Alerts — the Full Index

Every fuel alert in one map, graded by threat and pointed at its deep-dive article. Built by sweeping the abnormal-procedures chapter's triggering conditions end to end — the "severity" column shows only what is verbatim in each procedure (LAND ASAP / crew awareness / configuration actions), never an opinion.

How to use it: before a sim or a review, read the threat tiers; after an event, find the alert's row and follow the link. In flight, fly the ECAM and the QRH — this is a study index, not a procedure.


1. Threat tiers — learn the worst first

Tier 1 — LAND ASAP written in the procedure (4):

Alert / procedure One line Deep dive
FUEL ENG 1(2) FEEDLINE BURST feed pipe ruptured; side pumps off, crossfeed forbidden, gravity ceilings leak & burst
FUEL LEAK (confirmed) leak proven = land; the investigation happens en route leak & burst
FUEL L + R WING TK LO LVL both sides low = final notice; every pump on quantity & level
ENG FUEL CONTAMINATED (confirmed) dual-engine common cause; thrust frozen gently home contamination

Tier 2 — heavy reconfiguration / fuel re-planning (the bulk of Section 2).

Tier 3 — "crew awareness" (5): AFT XFR FAULT · APU LP VALVE FAULT · ENG LP VALVE FAULT · FCMC 1(2) FAULT · INNER TK HI TEMP (in flight). Awareness never means "nothing": each carries a STATUS/INOP bill — AFT XFR FAULT alone costs the cruise CG optimisation and its fuel saving.


2. The full map

Pumps → pumps / pump failures

Alert Trigger (precis) Core response
FUEL L(R) PUMP 1(2) LO PR one main pump low standby took over; pump OFF
FUEL L(R) STBY PUMP LO PR standby low pump OFF; INOP aft transfer + standby
FUEL L(R) CTR PUMP LO PR one centre pump pump OFF; the other carries
FUEL L + R CTR PUMPS LO PR both centre pumps gravity transfer; <15 t unusable; 17 t MAN gate
FUEL L(R) WING PUMPS LO PR a side's pumps the fork: rupture → no crossfeed; no leak → crossfeed ON
L(R) FUEL GRVTY FEED ONLY side unpowered gravity regime: IGN, ceilings, 2 t/tank unusable

Transfers and the trim line → transfer faults / trim unusable

Alert Trigger (precis) Core response
FUEL OUTR TO INR FAULT gravity transfer failed OUTR TK XFR ON (centre pumps yield first)
FUEL CTR TK XFR FAULT centre empty, pump running pumps OFF; trim fuel's last delivery
FUEL CTR TO INNER FAULT transfer anomaly / inlet stuck open pumps OFF; condition-matched at 17 t
FUEL AFT XFR FAULT aft transfer failed awareness; false during refuelling — 3-step test
FUEL ABNORM MAN FWD XFR manual FWD + pump dead + pitch >3.4°/30 s wait or 270 kt level; never blocks rescues
FUEL T TANK XFR FAULT trim transfer failed FWD + OPEN (~1 %); ≈200 kg APU floor; recirculation → UNUSABLE
FUEL TRIM LINE FAULT (A) line valve open + centre wet JETTISON OFF → pumps OFF → reclaim
FUEL TRIM LINE FAULT (B) isolation failed deliberate ISOL + APU OFF; ground-selected recoverable
FUEL TRIM LINE FAULT (FUEL TRIM PUMP) trim pump failed gravity-only forward transfer
TRIM TANK FUEL UNUSABLE the endgame OUTR fwd shift + centre ballast; 4 h; landing trio
FUEL EXCESS AFT CG CG >2.5 % behind target, 2nd FMGEC detection per ECAM; the red-CG face
FUEL APU AFT PUMP FAULT APU's normal source APU ≤ FL250 with trim fuel
FUEL APU LP VALVE FAULT valve disagrees awareness; isolation capability check
FUEL MAN XFR COMPLETED switch left on, tank empty back to AUTO

Quantity and level → quantity & level

Alert Trigger (precis) Core response
FUEL L(R) WING TK LO LVL both sensors dry 60 s (1 100–2 520 kg) the fuel-grab; no-leak crossfeed + low-side pumps OFF
FUEL L + R WING TK LO LVL all four dry 60 s LAND ASAP; all pumps ON
FUEL CELL NOT FULL collector <500 kg, pumps running jettison OFF; no-leak crossfeed; avoid negative g
FUEL WING TK OVERFLOW surge sensor wet 25 s stop/reroute the filling transfer; 17 t resume
FUEL OVERREAD (QRH) conservation shows a gain FQI condemned; run on initial FOB − F.USED; LO LVL alerts reliable
FUEL F.USED/FOB DISAGREE books differ >3 500 kg signpost: leak drill or overread drill
FUEL ZFW ZFCG DISAGREE FMGECs disagree confirm vs loadsheet; 2 % line
FUEL NO WEIGHT/CG DATA no ZFW/ZFCG initialise

Temperature → temperature faults

Alert Trigger (precis) Core response
FUEL LO TEMP inner −37 / outer −40 / trim −40 °C check freeze point; three warm-side moves; raise TAT
FUEL L(R) INNER TK HI TEMP 49 °C flight / 45 °C ground ground JET B: delay + engine off; flight: awareness

Computers and inerting → FCMC faults

Alert Trigger (precis) Core response
FUEL FCMC 1(2) FAULT one computer awareness; changeover
FUEL FCMC 1+2 FAULT both reset → initialise → timetable 32 % / 60 t / FL250; TOGA-only (option)
FUEL INERTING SYS FAULT FTIS failed changes nothing

Jettison → jettison / jettison faults

Alert Trigger (precis) Core response
FUEL JETTISON FAULT defuel valve open → self-inhibit NOT AVAIL; hold-to-burn or overweight landing
FUEL JETTISON NOT CLOSED valve won't close OFF; confirm flow; centre pumps OFF (the 15 t bill)

Leak and balance → imbalance / leak & burst

Alert / procedure Trigger (precis) Core response
FUEL IMBALANCE (QRH) crew-detected / 3 000 kg flash leak first; crossfeed + light-side pumps off; gallery backup
FUEL WING X FEED FAULT valve disagrees stuck open: monitor; stuck closed: gallery backup ready
FUEL LEAK (QRH) ten cues isolate, watch the books, three endings; no reversers
FUEL LOSS REDUCTION (QRH) leak drill recommends manual symmetric transfers; trim ends ISOL
FUEL ENG FEEDLINE BURST rupture detected pumps off = leak stopped; ceilings; relight candidate

Cross-chapter members

ENG FUEL CONTAMINATED (engine chapter — contamination) · ENG 1(2) LP VALVE FAULT · electrical configurations listing jettison inoperative · the false AFT XFR FAULT note (temporary-behaviour chapter).


3. Reading discipline — three rules

  1. This table is not a procedure. Airborne: ECAM, then QRH. The index earns its keep before (threat tiers, mechanism links) and after (find the deep dive, check the dispatch path).
  2. Translate "awareness" into its bill. Short procedure ≠ small consequence — read the INOP column of the STATUS page as the real content.
  3. Names are checkable. Every alert name above was verified against the procedure text or the maintenance documentation (the trim-pump case carries the AMM's sub-failure name FUEL TRIM PUMP); on the dispatch side, some operators' MEL prefaces its fuel chapter with an alert-to-relief-item mapping table — the fastest route from an ECAM event to the applicable dispatch conditions, including a separate family for false alerts (a failed warning chain has its own relief path, distinct from the true condition).

4. Memory hooks


Self-test

[!note]- Q1. Name the four procedures that write LAND ASAP. Feedline burst, confirmed fuel leak, double wing-tank low level, confirmed engine fuel contamination.

[!note]- Q2. Which three situations forbid opening the crossfeed? Feedline burst, confirmed contamination, and a leak not yet located.

[!note]- Q3. What does "crew awareness" never mean? "Nothing happened." Each awareness alert carries an INOP/STATUS bill — e.g. AFT XFR FAULT silently costs the cruise CG optimisation.

[!note]- Q4. An alert turns out to be a false warning (sensor chain failure). Does dispatch treat it like the real thing? No — false-alert cases have their own relief family in the MEL mapping, separate from the true-condition items; telling true from false is what the cross-check disciplines are for.

[!note]- Q5. Where do you read this page in the operation's timeline? Before (study, briefing) and after (review, dispatch path). Never instead of ECAM/QRH in the air.

Key takeaways

Point Value
Tiers 4 × LAND ASAP / reconfiguration bulk / 5 × awareness-with-a-bill
Coverage every fuel alert, each linked to its mechanism article
Hooks 4 land-ASAPs · 3 crossfeed bans · 2 pump moves · 1 timetable
Discipline index ≠ procedure; awareness = read the bill; names verified

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.