100 questions written for Emirates Airline’s actual selection process. Below are 5 of them in full — the prompt, what the panel is really probing, a model answer, the red flags that fail it, and the follow-ups that come next. No account, nothing to sign.
Question 1 of 100·technical
Define V1 and explain why it changes with runway length, slope, and contamination.
What they are really probing: They want the decision logic behind the number, not the certification wording.
Model answer
Give the definition in both halves, because V1 is two limits meeting rather than one speed. It is the maximum speed at which the first stopping action must be taken to stop within the accelerate-stop distance available, and it is the minimum speed at which the takeoff can be continued on one engine and still meet the screen height within the distance available. So it is a stop limit from above and a go limit from below, and every factor moves one of those two. Then work the factors. A shorter runway takes stopping distance away, so the stop limit drops and V1 comes down until it meets the go limit — at which point the runway is limiting and the weight has to come off. Contamination is the big one: standing water, slush or snow ruins braking friction and adds impingement drag, so the stopping distance grows sharply and V1 falls, sometimes below what feels comfortable. Slope cuts both ways — upslope helps you stop and hurts you go, downslope the reverse. Then the two floors people forget: V1 can never be below VMCG, because below it you cannot keep straight on the remaining engine, and never above VR. Close with the operational point on a hot Dubai afternoon: temperature reduces thrust, which lengthens the go case, and on a 777 near maximum weight that is what drives the numbers, not the runway length.
What fails this question
- — Reciting the certification wording with no decision logic
- — Forgetting V1 is bounded below by VMCG and above by VR
- — Saying V1 always equals VR on a long runway
- — Not knowing contamination lowers V1
Follow-ups they ask next
- — Engine failure five knots before V1 — what do you do?
- — Define VMCG and explain why it limits V1 from below.
- — How does an improved-climb takeoff change V1?
Question 2 of 100·technical
What is ETOPS and what entry/exit point rules apply on a DXB-LAX 777 sector?
What they are really probing: Emirates flies some of the longest twin-engine sectors in the world. Fluency here is expected, not impressive.
Model answer
Define it properly: ETOPS is the approval that allows a twin to operate further than a threshold time — commonly 60 minutes — from an adequate alternate at the approved one-engine-inoperative cruise speed in still air. Emirates operates the 777 at long diversion approvals, so say the concept rather than guessing a number you cannot support: the certified diversion time sets how far from an adequate airfield you may plan. Then the route structure. The entry point is where you first cross the threshold distance from an adequate airfield; the exit point is where you come back inside it; between them you are in ETOPS airspace and the flight plan carries the en-route alternates that make it legal. The equal-time point is the position from which diverting either way takes the same time at single-engine speed, and it is computed on the failure case, not on normal cruise. Then the preconditions, which is what separates a real answer: the ETOPS-significant systems must be serviceable, the MEL has a separate ETOPS column, the alternates must meet planning minima that are deliberately higher than landing minima, and the fuel must cover the critical scenario. Close with the operational reality: alternates on the northern routings are few, remote and weather-limited, and the reason you check them at dispatch rather than at the entry point is that at the entry point you have already committed.
What fails this question
- — Confusing diversion time with distance
- — Computing the ETP at normal cruise speed
- — Not knowing planning minima differ from landing minima
- — 'The computer works it out'
Follow-ups they ask next
- — What is the critical fuel scenario?
- — You lose a pack before the entry point. Do you continue?
- — Why are ETOPS alternate minima higher?
Question 3 of 100·technical
Explain coffin corner and what airspeed margins you target at FL410.
What they are really probing: The question behind the question is whether you understand why you do not just climb to save fuel.
Model answer
Describe the squeeze. As you climb, the indicated stall speed rises in terms of Mach because true airspeed for a given indicated speed increases, while the critical Mach number at which shock-induced buffet begins stays roughly fixed. So low-speed buffet and high-speed buffet converge, and coffin corner is the altitude at which the gap between them shrinks to nothing. Long before that point the margin becomes too small to absorb a disturbance, which is the operational issue: it is not that you cannot fly there, it is that you have no room for turbulence, a turn or a temperature change. Then give the numbers you actually work to: a buffet margin expressed as load factor — commonly 1.3g, meaning you can pull about 1.3g or bank around 40 degrees before buffet — and that margin is what the optimum and maximum altitude figures in the FMC are protecting. Then the factors that move it: weight, because a heavier aeroplane needs more lift and therefore more angle of attack; temperature, because a warm day at altitude reduces thrust and raises the true airspeed for a given Mach; and turbulence, because a gust is a load factor you did not ask for. Close with the airmanship: step-climb as the weight burns off rather than climbing early, respect the FMC maximum altitude rather than treating it as a target, and in turbulence descend and slow to the turbulence penetration speed, because the margin you are protecting is the one that keeps the aeroplane out of a high-altitude upset.
What fails this question
- — Describing it as a single altitude rather than a shrinking margin
- — No mention of buffet margin as a load factor
- — Forgetting weight and temperature effects
- — Treating FMC maximum altitude as a cruise target
Follow-ups they ask next
- — What bank angle can you use at maximum altitude?
- — How does temperature change the picture?
- — You hit turbulence at maximum altitude. Actions?
Question 4 of 100·technical
Walk me through your wind-shear escape manoeuvre on the 777.
What they are really probing: Memorised actions plus the reason each one exists. The reasons are what they probe.
Model answer
Split it into the warning and the escape. On a predictive warning before takeoff, you do not go — the aeroplane has told you there is shear on the path and there is no version of departing into it that is worth the delay saved. Airborne, on a warning or on recognising shear, escape immediately: maximum available thrust, disconnect the autothrottle if it is not giving you what you need, roll wings level, and pitch to the escape attitude, following the flight director if the escape guidance is displayed, then continue to increase pitch towards the stick shaker if the aircraft is still descending. Say the two rules that carry the manoeuvre. First, do not change configuration — gear and flap stay exactly where they are, because retracting either removes lift at the moment you have none to spare, and the aircraft is designed to escape in the configuration it is in. Second, do not chase airspeed: in a decreasing performance shear the air is taking your airspeed and the instinct to lower the nose and recover it flies you into the ground. You accept the low speed and you protect the flight path. Fly to the shaker if that is what it takes. Then the aftermath: climb away, tell ATC what you experienced with a specific number if you have one so the aircraft behind you gets the benefit, and reassess whether you are landing here at all. Close with prevention — radar, reports and thresholds set before the approach are what stop you needing any of this.
What fails this question
- — Changing configuration during the escape
- — Lowering the nose to recover speed
- — Departing after a predictive warning
- — Not reporting the encounter
Follow-ups they ask next
- — Why does the gear stay down?
- — Would you take off with a predictive warning?
- — What do you report to ATC afterwards?
Question 5 of 100·technical
What is RVSM and what equipment is required to operate within it?
What they are really probing: An easy question that candidates answer thinly. The contingency half is where the marks are.
Model answer
Define it: Reduced Vertical Separation Minimum is the application of 1,000 feet of vertical separation instead of 2,000 between FL290 and FL410 inclusive, which roughly doubles the usable levels in the busiest part of the airspace. It exists because altimetry got good enough to justify it, and that is why the equipment list is specific. Name the requirements: two independent primary altimetry systems, an automatic altitude control system able to hold the assigned level within tolerance, an altitude alerting system, and a transponder with altitude reporting. Beyond the aircraft, the operator needs approval and there is a monitoring requirement — height-keeping performance is measured, which is how the system stays safe. Then the parts candidates skip. The cross-check discipline: altimeters compared before entry and periodically, and a defined tolerance beyond which you are not RVSM capable. What to do when something fails — you tell ATC immediately and request a level or a route out, because an aircraft that has lost its height-keeping capability inside RVSM is an unannounced hazard to everyone at the levels above and below. And the weather case: severe turbulence or mountain wave activity can make holding a level impossible, and reporting that is a service to the whole system rather than an admission. Close with the wake element — closer vertical spacing means wake encounters are a real consideration, and the lateral offset procedures exist for that.
What fails this question
- — Wrong altitude band
- — Listing only one altimeter
- — No contingency procedure for a failure
- — Unaware of the monitoring requirement
Follow-ups they ask next
- — Your altimeters disagree by 250 feet. Now what?
- — What do you tell ATC on a failure?
- — Turbulence stops you holding the level. Actions?
Same depth as the 5 above — model answer, red flags and follow-ups on every one. You just read a twentieth of the pack; if those five were not worth your time, the rest will not be either, and you should not buy it.
— Define decision altitude (DA) versus decision height (DH). When do you use which?
— What conditions are required for a stabilised approach by 1000 ft AFE in IMC?
— What is RNP-AR and where does Emirates use it?
— Explain how thrust required vs thrust available defines absolute ceiling.
— What are the memory items for a rapid decompression?
— Explain the difference between TCAS RA and TCAS TA. What's your action on each?
— How do you compute landing distance required on a contaminated runway?
— Why does rudder authority reduce as airspeed increases, and what protects the fin?
— Explain transition altitude, transition layer, and transition level.
— What is QNH versus QFE versus QNE?
Not affiliated with Emirates Airline. Process details are sourced and dated; candidate-reported detail is labelled as reported.