KLM Pilot Interview Questions 2026

I Would Speak Up Immediately — If my captain is rushing departure preparation and skipping checklist items, I would not wait for a problem to occur. I would say: "Captain, I noticed we skipped [item] on the checklist — can we go back to it?" If the captain dismisses the concern — "We're late, it's fine" — I would be direct: "I'm not comfortable departing with checklist items incomplete. Can we take two more minutes?" Commercial pressure to depart on time is one of the most documented contributing factors in aviation incidents. I would not let schedule pressure override standard procedures. Use Assertive Communication — The Structured Approach — Address the situation directly but respectfully, using a structured advocacy approach: first, get the Captain's attention ('Captain, I'd like to raise something'). Second, state the concern with specific reference: 'I noticed we skipped the before-start flow items 4 through 7. I'm not comfortable departing without completing those — they include the flight control check and the takeoff briefing.' Third, propose the solution: 'Can we take two minutes to run through the remaining items? I'd rather depart two minutes later than miss something.' This approach is direct (Dutch culture values directness), specific (referencing exact items, not vague concerns), and solution-oriented (not just complaining but offering a path forward).

If the Captain Dismisses Your Concern — If the Captain responds with 'I've been flying for 20 years, we don't need every item' or 'We're already late, just get on with it,' you must escalate your advocacy. Repeat the concern with emphasis on the specific safety implication: 'I understand we're under time pressure, and I respect your experience. But the flight control check is a safety-critical item — if we have a jammed elevator and we haven't tested the controls, we're departing with an unknown failure. I really need us to complete that item.' If the Captain still refuses, you have the right — and the obligation — to refuse to depart until the safety concern is addressed. Under EASA regulations, the Commander has final authority for the flight, but no crew member can be required to participate in an operation they believe is unsafe. This is an extreme escalation and should be used only when genuinely safety-critical items are being skipped.

KLM's Safety Culture Context — KLM operates a non-punitive reporting system and actively promotes a Just Culture where crew members are protected when they speak up about safety concerns in good faith. The VNV pilot union supports First Officers who exercise their right to challenge procedural deviations. In the COVA interview, this scenario tests whether you understand the balance between respect for authority and advocacy for safety — and whether you have the courage to speak up in a real situation. The assessors want to hear: that you would address it directly and specifically (not stay silent), that you would be respectful but firm (not aggressive or confrontational), that you know the limits of acceptable compromise (non-safety items can be expedited, safety-critical items cannot be skipped), and that you understand the reporting obligation (a persistent pattern of checklist non-compliance should be reported through the safety management system, not just managed in the moment).

The Facts — On 27 March 1977, KLM Flight 4805, a Boeing 747-206B (PH-BUF), collided with Pan Am Flight 1736 on the runway at Los Rodeos Airport, Tenerife. The collision killed 583 people — 248 on the KLM aircraft and 335 on the Pan Am — making it the deadliest accident in aviation history. The KLM aircraft was commanded by Captain Jacob van Zanten, the airline’s most senior training captain and the face of KLM’s recruitment advertising. He initiated the takeoff roll without receiving ATC takeoff clearance, in heavy fog with visibility below 300 metres. The flight engineer questioned whether the Pan Am aircraft had cleared the runway, but the challenge was insufficient to prevent the decision.

Root Cause Analysis — The accident was attributed to multiple failures: Captain van Zanten’s decision to commence the takeoff without explicit clearance, the ambiguous ATC communication where the phrase ‘we are now at takeoff’ was interpreted differently by the crew and the tower, the flight engineer’s hesitant challenge that did not escalate beyond a single question, and the fog that eliminated visual confirmation. The underlying systemic cause was authority gradient — the most senior captain in the airline was not effectively challenged by his crew. The CVR transcript shows the flight engineer said ‘Is he not clear then, that Pan American?’ and van Zanten responded with ‘Oh yes’ and continued the takeoff roll.

Impact on KLM’s Safety Culture — Tenerife fundamentally transformed KLM’s approach to CRM, authority gradients, and crew communication. The airline became a global pioneer in Crew Resource Management training, institutionalising the principle that rank does not override safety concerns. KLM’s current CRM philosophy — rooted in the Polder Model — requires every crew member to use assertive language when safety is at risk: ‘I believe we should stop’ rather than ‘Do you think we should maybe consider stopping?’ The airline’s recurrent training programme includes Tenerife as a mandatory case study, and the accident is discussed openly as an institutional responsibility, not a historical embarrassment. What It Means for Your Interview — The COVA panel expects you to know Tenerife in detail — not just ‘there was an accident’ but the specific CRM failures, the flight engineer’s inadequate challenge, and the cultural factors that allowed a senior captain to override normal procedures. When you discuss this event, show that you understand its direct connection to how KLM trains and evaluates pilots today. The airline’s greatest tragedy became its greatest lesson, and that willingness to confront failure openly is central to what makes KLM’s safety culture distinctive.

Preparation Before Intercepting — Before intercepting the ILS, complete the approach briefing even in abbreviated form: confirm the ILS frequency is set and identified (morse code ident verified), confirm the inbound course is set on the MCP course window, note the Decision Altitude (DA), brief the missed approach procedure, and cross-check the glideslope intercept altitude (typically 2,500–3,500 feet depending on the procedure).

With autopilot off and flight directors off, the raw ILS approach requires the pilot to interpret the localizer and glideslope deviations directly from the deviation indicators on the PFD — the diamond-shaped symbols on the CDI scale. Set the aircraft in a stabilised configuration before glideslope intercept: landing gear down, flaps at the intermediate setting (typically flaps 15 for initial approach, extending to flaps 30 or 40 for the final segment), and speed stabilised at Vref + approach correction. Trim the aircraft meticulously — raw data flying is significantly harder if the aircraft is out of trim.

Localizer Tracking — Intercept the localizer from the assigned heading, typically at a 30–45° intercept angle. As the localizer needle (CDI) begins to move from full deflection, begin a controlled turn toward the inbound course. The key is to lead the turn — do not wait until the needle centres. For a 30° intercept at a typical approach speed of 140 knots, begin the turn when the CDI shows approximately half-scale deflection. Roll out on or slightly short of the inbound heading, then make small corrections (2–5° heading changes maximum) to track the centreline. The scan pattern is critical: PFD airspeed → PFD attitude → PFD CDI localizer → PFD altimeter → PFD VSI, cycling through these instruments continuously at approximately 1-second intervals per instrument. Do not fixate on the CDI — a common error is staring at the needle and losing speed and pitch awareness.

Glideslope Tracking — Intercept the glideslope from below. As the glideslope indicator shows the diamond moving from above toward centre, begin configuring for the final descent: extend to landing flaps (flaps 30 or 40), set final approach speed (Vref + correction), and begin descent to maintain the glideslope by adjusting pitch and power together. On a standard 3° glideslope, the approximate descent rate is: groundspeed ÷ 2 × 10 = descent rate in feet per minute. At 140 knots groundspeed, target approximately 700 fpm. The glideslope is tracked through pitch: pitch up slightly to correct above glideslope (needle below centre), pitch down slightly if below (needle above centre). Power controls speed — if speed decreases, add power; if speed increases, reduce. The interconnection between pitch and power means small, coordinated adjustments: a common error is making large pitch changes that oscillate the glideslope and speed simultaneously.

From 1,000 Feet to Decision Altitude — Below 1,000 feet AGL, the approach must be stabilised: on glideslope (within one dot), on localizer (within one dot), at Vref ± 5 knots, configured for landing, and with a stable descent rate. Any parameter outside these limits requires a go-around — KLM's stabilised approach criteria are non-negotiable. Continue scanning instruments with increasing attention to the altimeter as DA approaches. At DA (typically 200 feet for CAT I), look up for the runway environment — if visual references are sufficient to continue (approach lights, runway threshold, or runway markings visible), transition to visual and land.

If not visual at DA, execute the go-around immediately: TOGA thrust, pitch to 15° nose up, positive rate — gear up, follow the missed approach procedure. In the KLM simulator assessment, the assessors specifically watch for: scan discipline (no fixation), smooth corrections (not oscillating), speed control within ±5 knots, and a crisp go-around decision at DA with no hesitation or 'ducking under.' Verbalising your intentions throughout — even simple callouts like 'correcting left,' 'slightly high, reducing' — demonstrates cockpit communication skills even in a single-pilot assessment environment.

Recognition and Immediate Action (0–5 seconds) — At V1, the PM (Pilot Monitoring — in this case, the check captain acting as PM) calls 'V1.' Simultaneously or immediately after, an engine fails — recognised by yaw toward the failed engine, asymmetric thrust indication, and possibly EGT/N1 divergence on the engine instruments. The critical decision is already made: at or above V1, you CONTINUE. Do not hesitate, do not consider rejecting. Apply immediate rudder input against the yaw — full rudder if necessary to maintain directional control on the runway centreline. As PF (Pilot Flying), maintain wings level with aileron (up to 5° bank into the live engine is acceptable to assist directional control). The instinctive response to the yaw is the first thing assessors evaluate — any delay or confusion at V1 is a significant negative mark.

Rotation and Initial Climb (5–15 seconds) — At Vr (called by PM), rotate smoothly to the normal rotation attitude of approximately 8–10° pitch. Do not over-rotate — on one engine, excessive pitch attitude will bleed airspeed below V2, which is the minimum safe climb speed for engine-out operations. Target V2 — the takeoff safety speed — and hold it. The 737NG with one engine will climb at a reduced gradient, but V2 guarantees the minimum regulatory climb gradient of 2.4% with gear down (or better with gear retracted). After positive rate is confirmed (PM calls 'Positive rate'), call 'Gear up.' Retracting the gear significantly reduces drag and improves climb performance — this is the highest priority action after establishing a positive climb. Maintain the runway heading or the SID initial heading as appropriate — do not attempt any unnecessary turns at low altitude on one engine.

Acceleration and Configuration (15–60 seconds) — Once the gear is up and a positive climb rate is established with speed at or above V2, continue climbing. At the acceleration altitude (typically 1,500 ft at Schiphol per NADP-2, but may be different for engine-out procedures), begin slowly accelerating by reducing pitch attitude. Retract flaps on schedule as speed increases through each flap retraction speed.

Do not rush the flap retraction — premature retraction on one engine can cause a loss of climb performance. Once clean configuration is achieved and speed is increasing through Vclimb, the aircraft's performance improves substantially. At this point, consider the situation: which engine has failed (verify through engine instruments — N1, N2, EGT, fuel flow, oil pressure), what indications are present (fire warning? Damage indications? Vibration?), and what the plan is (return to Schiphol or continue to an alternate).

Non-Normal Checklist and Decision (1–5 minutes) — At a safe altitude (typically above 1,500–3,000 ft AGL with positive climb established), follow the memory item sequence: engine fire/damage/failure identification — CONFIRM the failed engine through instruments before taking any shutdown action. The golden rule is 'Identify, Verify, Confirm' — never shut down an engine based solely on yaw direction. Once confirmed, if the engine has failed (N1 near zero, no fire): leave the thrust lever at idle, engine start lever to cutoff, consider whether to discharge the fire bottle (only if fire warning is present).

Run the Engine Failure/Shutdown checklist from the QRH (Quick Reference Handbook). Coordinate with ATC: declare MAYDAY, state your intentions (return to Schiphol), request vectors for the ILS approach. Brief the approach — you will fly a single-engine ILS, typically to the longest suitable runway. Schiphol's Polderbaan at 3,800 m or Kaagbaan at 3,500 m provide ample length for a single-engine landing at any weight. The assessors evaluate the entire sequence: immediate yaw control, V2 discipline, gear retraction priority, methodical checklist management, and clear communication — panicking or rushing the checklist is worse than taking an extra 30 seconds to do it correctly.

Crosswind Approach — Crab Method — The standard KLM Boeing 737NG crosswind technique is the crab method during approach, transitioning to de-crab in the flare. On approach, maintain the aircraft in a wings-level crab — the nose is pointed into the wind to maintain the desired ground track along the extended runway centreline, while the aircraft's longitudinal axis is offset from the runway heading by the drift angle. This is aerodynamically clean and comfortable for passengers. A 20-knot crosswind from the left at a ground speed of 140 knots creates a crab angle of approximately 8°. The Boeing 737-800's maximum demonstrated crosswind is 33 knots — KLM uses this as the operational limit for dry runways, reduced to as low as 15 knots on contaminated runways.

The Transition — De-Crab in the Flare — The critical phase is the transition from crab to alignment with the runway during the flare. At approximately 30–50 feet radio altitude as you begin the flare, smoothly apply rudder into the wind to align the aircraft's nose with the runway heading, simultaneously applying opposite (downwind) aileron to prevent the into-wind wing from rising as the fuselage weathervanes. The timing must be coordinated: rudder aligns the nose, aileron controls the bank.

The result is a brief sideslip — the aircraft is momentarily flying with the nose aligned with the runway, a slight wing-low into the wind, and drifting is arrested. The touchdown should be on the into-wind main gear first (because of the slight wing-low attitude), followed by the downwind main gear, then the nose gear. Do not attempt to de-crab too early (above 100 feet) as this creates a prolonged sideslip that is uncomfortable and difficult to maintain precisely. Do not leave it too late (below 20 feet) as you may touch down still in the crab — which, while survivable on the 737's strong landing gear, creates high side loads on the gear and tyres.

Alternative — Combined Method — Some KLM pilots use a combined (wing-low/crab hybrid) technique where a partial de-crab is established on short final (from 200–300 feet) with the remainder corrected in the flare. This involves establishing a partial wing-low into the wind with partial rudder to reduce the crab angle, then completing the alignment in the flare. Boeing's FCTM accepts both techniques. The advantage of the combined method is that the final de-crab in the flare is smaller and requires less aggressive rudder input. The disadvantage is that maintaining a sideslip on final approach creates slightly more drag and can make speed management more demanding. KLM SOPs do not mandate one technique over the other — the crew selects based on personal proficiency and conditions. In the simulator assessment, assessors evaluate whether the technique is controlled and consistent, not which specific method is used.

Simulator Assessment Expectations — In the KLM B737 simulator grading, the crosswind landing is typically set at 15–20 knots (moderate, not extreme) to test basic airmanship rather than to find limits. The assessors evaluate: stable approach speed (Vref + wind correction — typically Vref + half the steady headwind component plus the full gust factor, capped at Vref + 20 knots maximum), controlled crab tracking on final, smooth and timely de-crab in the flare, touchdown within the centreline tolerance (within one runway stripe width — approximately 3 metres either side), appropriate use of rudder without over-controlling, and positive ground roll directional control after touchdown (rudder pedal steering transitioning to nose wheel steering below 60 knots). The biggest mistake candidates make is chasing the centreline with aggressive aileron and rudder corrections on short final — the assessors prefer a stable, slightly offset approach to an approach that oscillates across the centreline. Accept a small drift correction in the flare rather than fighting for perfection at 200 feet.