Lufthansa Group Interview Prep Pack 2026

Aviate, Navigate, Communicate — In any emergency, my immediate priorities follow the universal framework: aviate — maintain control of the aircraft; navigate — ensure a safe flight path; communicate — inform ATC, cabin crew, and my colleague. I would not attempt to diagnose the emergency until the aircraft is under control and in a safe configuration. Once stabilised, I would use FORDEC to structure my decision: Facts — what has happened and what indications do I have?

Options — what can I do? Risks — what are the consequences of each option? Decision — choose and commit. Execution — carry out the plan. Check — verify it is working. In the Lufthansa FQ interview, the assessors want to see structured thinking, not a recitation of the QRH — they already know I can read checklists. What differentiates candidates is calm prioritisation under pressure.

Crew Coordination During the Emergency — Describe how you would manage the crew dynamic during an emergency. At Lufthansa, the standard procedure is: PF (Pilot Flying) maintains aircraft control and communicates with ATC, while PM (Pilot Monitoring) manages the ECAM or QRH actions and coordinates with cabin crew. Clear task assignment prevents duplication and ensures nothing is missed. The German cockpit culture’s low Power Distance means both pilots contribute equally to emergency management — the Captain makes final decisions, but the First Officer is expected to provide active input, cross-check ECAM actions, and voice any concerns. Reference specific procedures: for an engine failure on the A320neo PW1100G, the memory items are ECAM-driven with autothrust managing the remaining engine.

Decision-Making Under Pressure — Use the FORDEC model (Facts, Options, Risks/Benefits, Decide, Execute, Check) to structure in-flight decision-making during an emergency. Describe how you would gather facts (what is the actual failure? what does ECAM indicate? what are the weather and fuel state?), identify options (continue to destination, divert to an alternate, return to departure airport), assess risks (time to nearest suitable airport, runway requirements, emergency services availability), decide, execute the decision, and continuously check whether the situation is evolving. At Lufthansa, diversion airports for Frankfurt hub operations include Köln/Bonn, Düsseldorf, Stuttgart, and Hahn; for Munich, alternatives include Nuremberg, Salzburg, and Innsbruck.

Passenger Communication — Address the passenger dimension. After securing the aircraft and initiating the correct procedure, communicate with the cabin crew (via interphone) to prepare them for the emergency, then make a PA to passengers. The PA should be calm, factual, and reassuring: explain that a situation has occurred, the crew is managing it according to procedures, and provide specific instructions if applicable (brace position, prepare for emergency landing). At Lufthansa, where the premium brand includes First Class passengers accustomed to excellence, maintaining calm professionalism during an emergency is part of the brand promise. The crew’s composure directly affects passenger behaviour during evacuation if required.

What FADEC Is and Why 'Full Authority' Matters — Full Authority Digital Engine Control is the computerised system that manages every aspect of the jet engine's operation — there is no mechanical throttle linkage from the cockpit to the engine. The pilot's thrust lever movement generates an electrical signal that FADEC interprets as a thrust demand; FADEC then calculates the correct fuel flow, variable stator vane positions, bleed air valve positions, and anti-surge margin to deliver that thrust level while remaining within every certified engine parameter limit. The word 'full authority' has a specific and critical meaning: unlike earlier Hydromechanical Metering Units (HMUs) that had a mechanical fuel control backstop, FADEC has no mechanical fallback — if both FADEC channels fail, the engine shuts down. This is a deliberate trade-off: the probability of both FADEC channels failing is certifiably lower (approximately 10⁻⁹ per flight hour) than the probability that a mechanical system would have failed to control the engine safely in the complex operating envelope of a high-pressure-ratio turbofan.

Dual-Channel Redundancy and Automatic Switchover — Each engine's FADEC consists of two independent processing channels — Channel A and Channel B — each capable of fully controlling the engine. The channels use different processors, different software, and different power supplies to prevent common-mode failure. Under normal operation, Channel A is the active channel and Channel B is in monitoring mode, continuously comparing Channel A's outputs against its own calculations. If Channel B detects a discrepancy that exceeds its fault tolerance, it automatically assumes control from Channel A without any crew awareness or action — the transition is smooth and imperceptible. The only indication is a maintenance message recorded in the Digital Flight Data Acquisition Unit (DFDAU) for post-flight review. If Channel A fails completely, Channel B assumes control immediately. If both channels fail, the engine shuts down — the only FADEC failure mode that is operationally visible to the crew. The FADEC channels are powered from the aircraft's essential electrical buses — a critical link that means severe electrical failures can affect engine control, though the design ensures electrical redundancy to the FADEC matches the redundancy of the engine itself.

FADEC Functions: Thrust Management, Protections, and Engine Starting — FADEC manages five major operational functions. Thrust setting and control: FADEC translates detent position (IDLE, CLB, FLX/MCT, TOGA) into a precise N1 or EPR target, compensated for current atmospheric conditions (temperature, pressure altitude, Mach) — so that selecting CLB detent at ISA standard conditions at FL350 gives a different fuel flow than CLB at ISA+20°C on the ground, but the same reference N1. Engine parameter limiting: FADEC continuously prevents EGT (Exhaust Gas Temperature), N1, N2, and oil pressure from exceeding certified maximums — it reduces fuel flow automatically before any limit is reached, protecting the engine from over-temperature and over-speed without crew intervention. Anti-surge protection: FADEC monitors compressor stall precursors and adjusts variable stator vane angles to prevent surge. Engine start management: FADEC executes the full start sequence automatically after the crew selects the ignition mode and opens the fuel valve — monitoring light-off, acceleration through sub-idle, and stabilisation at ground idle, cutting off the start sequence and alerting the crew if parameters deviate outside normal limits. Thrust reverser control: FADEC validates reverser deployment conditions and manages deployment sequencing to prevent reverser asymmetry.

A320 Auto-Thrust Integration and NEO-Specific Notes — On the A320, FADEC is integrated with the auto-thrust system through the FCMCs and the FMGCs. The autothrottle does not move the thrust levers on the A320 — unlike Boeing autothrottle systems where the levers physically move. Instead, the FCMCs command FADEC directly, bypassing the lever physical position. The thrust lever is a 'demand device' that sets an upper thrust ceiling; auto-thrust operates within that ceiling. This means that if the thrust levers are in the CLB detent and autothrottle is active, FADEC may deliver any thrust from IDLE to CLB limit — the lever does not move to show this. Pilots transitioning from Boeing types must understand this fundamental difference. On the A320neo with PW1100G-JM, the FADEC software is specifically tailored to the geared turbofan's unique characteristics: the epicyclic gearbox creates different N1/N2 relationships compared to the CFM56 or V2500, and the PW1100G's transient response profile (the rate at which thrust builds from low settings to high) differs from conventional turbofan behaviour. The current PW1100G powder-metal contamination inspection campaign required FADEC software updates on returning engines to enable enhanced condition monitoring of affected components — a practical intersection of FADEC software management and fleet maintenance. At Lufthansa, this technical knowledge is directly relevant to the airline's fleet operations: A320 family aircraft on European short-haul, A350-900 and A340 on intercontinental routes, and Boeing 747-8 on flagship long-haul services from Frankfurt — one of Europe's busiest hub airports handling over 60 million passengers annually.

Assess the ECAM, Then Decide on Diversion — An ECAM hydraulic leak warning on the A350-900 mid-Atlantic requires the same structured response as any ECAM non-normal: I would follow the ECAM actions in order, assess the impact on the aircraft's capability, and then make a decision about continuing or diverting. On the A350, the hydraulic system differs from the A320 — it uses two independent 5,000 PSI systems plus a local electrohydrostatic backup. A leak in one system is serious but the aircraft remains controllable on the other system plus backup. My decision framework: what systems have I lost? What is my remaining operational capability? What is the nearest suitable diversion airport versus my destination? Over the mid-Atlantic, the options may be limited — Shannon, Keflavik, the Azores, or continuing to destination — and the decision depends on the severity of the leak and the rate of fluid loss.

TDODAR: The Decision Framework for a Major Abnormality Over Water — With a hydraulic leak at the Atlantic midpoint — approximately equidistant from São Paulo and Frankfurt, with no land diversion options within 300 nm — the decision framework must be applied methodically. Time available: how quickly is fluid being lost? An ECAM hydraulic low level warning indicates the system has lost a significant proportion of its fluid — the rate of loss and remaining quantity determine the urgency timeline. The A350's hydraulic reservoir quantity is indicated on the HYD SD page. Diagnosis: is this a slow seep from a fitting, a moderate leak from a hydraulic line, or a catastrophic rupture (the most dangerous scenario, where the system empties in minutes)? Options: continue to São Paulo (possibly 2-3 hours remaining), divert to Recife (northeast Brazil, approximately 1 hour), divert to Dakar Senegal (approximately 90 minutes), or divert to the Azores (approximately 3 hours). Decision: driven by the leak rate assessment, the residual hydraulic capability, and the medical/operational resources at each diversion airport. Assign: PM contacts company (OCC Frankfurt) via SATCOM, PM handles ATC, PF manages aircraft energy.

A350-Specific System Considerations: EBHA and RAT — The A350-900's electrical backup hydraulic actuator (EBHA) architecture provides a level of resilience not present in the A320. Even if one hydraulic system is completely empty, the EBHA-powered flight controls — critical ailerons and elevator — remain functional via electrical actuation. The Ram Air Turbine (RAT) can be manually deployed to provide emergency hydraulic pressure to the essential circuits. The A350's fly-by-wire system will automatically reconfigure to alternative modes as hydraulic availability changes, and the ECAM will show the available control surfaces and any approach category implications in the STATUS page. A key A350-specific consideration is the higher hydraulic pressure (5,000 PSI versus A320's 3,000 PSI) — this means that a given seal failure loses fluid faster than an equivalent failure on a 3,000 PSI system, making rapid leak rate assessment more urgent. The augmented crew on this long-haul sector (three or four pilots) means one pilot can manage ECAM procedures and company communications while the other two maintain aircraft control and situational awareness — a significant workload advantage over a two-person short-haul operation.

Diversion Decision and Coordination: Getting to the Ground Safely — The diversion decision balances residual hydraulic capability against distance to suitable airports. If the Green system has lost significant fluid but Yellow is intact, the aircraft retains adequate control authority and landing capability — the primary operational consideration is approach category limitation (ECAM STATUS may show CAT 1 only if key hydraulic-dependent autoland systems are inoperative, requiring higher ceiling and visibility at the diversion airport). If both systems are losing fluid — a scenario suggesting a more catastrophic failure — the urgency increases and the nearest suitable airport (Recife or Dakar depending on position) becomes the priority regardless of facilities. The Lufthansa OCC Frankfurt coordinates with the diversion airport for emergency services, and the crew declares MAYDAY if the situation warrants (loss of flight control capability is MAYDAY-level; single system loss with maintained aircraft control is PAN-level). Post-landing, the aircraft is inspected by Lufthansa Technik or local maintenance organisation before any further flight — a hydraulic system failure in flight is a mandatory occurrence report under EASA Part-ORO and triggers both internal SMS review and LBA notification.

The Captain Has Final Authority on Fuel — I Would Exercise It — If I discover the fuel load is insufficient for the conditions — perhaps the dispatcher calculated minimum legal fuel but I can see that the en-route weather, the destination forecast, or the ATC flow situation creates risk — I would request additional fuel. EASA Part-CAT explicitly gives the PIC the right to carry additional fuel beyond the calculated minimum, and at Lufthansa, exercising this authority when operationally justified is expected, not questioned. I would be specific: 'I would like an additional 500kg because the TAF shows a tempo for thunderstorms at Munich between 16:00 and 18:00, our ETA is 17:15, and the alternate at Nuremberg has the same weather system. The extra fuel gives us holding capability or a second alternate option.' Data and reasoning, not anxiety.

Distinguishing a Single Concern from a Systemic Pattern — The scenario describes noticing that the airline regularly departs with minimum legal fuel — a pattern rather than a single-flight concern. These require different responses. A single-flight fuel concern is handled on the day through the Captain's discretionary fuel authority. A recurring pattern — where multiple consecutive flights arrive with fuel close to or at final reserve, where dispatch routinely proposes fuel at the legal minimum, or where route analysis suggests the standard planning assumptions are optimistic for actual conditions — is a systemic safety issue that must be escalated through the safety management system rather than just added to on each individual flight.

The correct response to a systemic concern is an SMS safety report: specific, factual, data-driven. 'Over the past six weeks I have operated eight sectors to Frankfurt. On six of those sectors, the aircraft arrived with less than 15 minutes above final reserve due to actual route winds exceeding the fuel planning assumptions by an average of 40 kt.' That report triggers an operations safety review, not just a single-flight fuel adjustment.

Understanding the Commercial Context — and Why It Does Not Override Safety Judgement — Fuel is Lufthansa Group's single largest variable operating cost — the group spent approximately €9-10 billion on jet fuel in FY2025. The commercial pressure to minimise fuel loads is real and institutionally significant: every kilogram of extra fuel costs money not only in its own purchase price but in the performance penalty it creates (higher MTOW means lower fuel efficiency, longer take-off roll, reduced payload capacity). Lufthansa's operations control, dispatch, and fuel optimisation teams apply sophisticated models to minimise fuel while staying within regulatory requirements. Understanding this commercial context — and being able to acknowledge it without being controlled by it — demonstrates the professional maturity that Lufthansa expects. The correct frame is not 'the company is cutting corners' but rather 'the company's fuel optimisation system is calibrated for average conditions; when specific circumstances produce above-average risk, the pilot's professional judgement must adjust the output.'

The Escalation Path and Union Resources — If a pilot raises a fuel safety concern through the SMS and does not receive a response that addresses the systemic issue adequately, the escalation path exists within the system. The Head of Flight Safety (or equivalent within Lufthansa's safety organisation) is the next escalation point above the standard SMS review. Vereinigung Cockpit (VC) — representing all Lufthansa mainline and cargo pilots — has safety representation functions that can raise systemic operational concerns with management through collective channels. An individual pilot who raises a documented, evidence-based safety concern and experiences pushback or retribution for doing so is protected under German labour law and the just-culture provisions of Lufthansa's SMS, which align with EASA Part-ORO requirements. The most important principle throughout this scenario is that the pilot who acts in good faith — documents the concern, follows the correct escalation path, and maintains professional standards while doing so — is in the legally and professionally defensible position regardless of the commercial sensitivity of the subject matter.

I Would Approach It as an Opportunity — If assigned to Lufthansa City Airlines in Munich rather than mainline Frankfurt, I would treat it as an entry into the Lufthansa Group ecosystem. I would research the CityLine operation, the fleet (A319/A320), the Munich hub structure, and the route network. I would be honest about the adjustment — it is not my first choice of base — but frame it as manageable and a step toward my long-term career at Lufthansa.

Operational Preparation: Munich Is Not Frankfurt — A practical, operationally specific preparation for Munich base requires genuine research. Munich Airport (EDDM, 1,487 ft AMSL) has distinct operational characteristics from Frankfurt: two parallel runways (08L/26R and 08R/26L, both 4,000m × 60m) with independent parallel operations capability, a night flight ban from 2200–0600 (stricter than Frankfurt's 2300–0500 ban), Föhn winds from the Alps that cause rapid temperature and wind-direction changes and significant turbulence on approach, radiation fog from the Erdinger Moos moorland that produces low-visibility conditions comparable to Frankfurt in autumn and winter, and Terminal 2 Satellite (jointly owned 40% by Lufthansa, 60% by FMG) as the primary Lufthansa facility. City Airlines specific preparation: understanding the CBA structure under which City Airlines operates (distinct from mainline VC-negotiated contracts, a fact that creates union tension but does not affect day-to-day flying operations), the A320 fleet configuration deployed, and the SOP differences if any from the mainline operating culture.

Team Integration: Proactive Sozialkompetenz in an Unfamiliar Environment — DLR's selection process specifically evaluates Sozialkompetenz — social competence and interpersonal intelligence — as a core pilot competency. In a new base where nobody is known yet, Sozialkompetenz is what converts a collection of individuals into a crew team. Proactive strategies include: introducing yourself specifically to every colleague you fly with in the first weeks rather than maintaining professional distance, attending team events even when tired after duty, learning names and roles of the ground operations team, dispatcher team, and cabin crew regulars as quickly as possible.

These are not social niceties — they are the foundation of crew coordination quality. A First Officer who has never met a particular Captain before a cross-European sector will produce lower-quality CRM than two pilots who have spoken briefly at the base ops room. Research consistently shows that familiarity within established crew teams — even brief familiarity — improves callout rates, reduces communication latency, and increases the quality of pre-flight briefings.

Emotional Honesty: Acknowledge the Challenge Without Dramatising It — The DLR psychological interview values honest self-assessment over managed self-presentation. Moving to an unfamiliar city — whether Munich or any other base — and joining an operation where social networks do not yet exist does create a period of genuine adjustment. Loneliness is a documented wellbeing challenge in airline operations, particularly for pilots based away from their families during early career years. Acknowledging this honestly — 'I know the first few months in a new city without established friendships will require active effort to manage well' — and describing specific strategies for managing it (maintaining regular connection with existing friendships and family, building new social connections through shared activities, using Lufthansa's peer support network if needed) is a stronger answer than claiming the transition will be easy. The evaluator, who has navigated their own career transitions, will recognise authentic preparation over performed confidence.