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Fifth sector of the day. Northern European winter. You've been de-iced but you're number 14 for departure and holdover time is expiring. ATIS reports the destination runway RWYCC 3 with a pilot AIREP of LESS THAN POOR braking action. Your fuel state after taxi delay means predicted destination fuel is approaching ALTN + FINRES + DEV.
What is your immediate decision on the braking action report? Do you need re-treatment? And at what point does your fuel state require a specific action before you even get airborne?
Braking action: LESS THAN POOR requires the runway to be closed until it improves. This is not a judgment call - it is an explicit gate. You cannot plan to land there.
De-icing: if holdover time is exceeded or contamination is suspected, return to stand or remote de-icing for retreatment. You do not depart with expired holdover.
Fuel: if predicted destination fuel drops below ALTN + FINRES + DEV during taxi, the Commander shall return to stand (with limited exceptions for immediate departure). Three separate decision gates, all converging on the same answer: stop pressing and reset the plan.
"You're inbound to a Northern European base in winter. ATIS gives a GRF/SNOWTAM with RWYCCs and ATC passes a braking action AIREP that's marginal. Talk me through how you interpret the information, manage braking, and decide to accept or reject."
GRF Baseline and AIREP Cross-Check
Treat RWYCC as the baseline, then cross-check with pilot braking action reports (AIREPs) - the Winter Ops Guide highlights these as the key runway-friction inputs the crew will see operationally.
Accept / Reject Gate
Braking action reports are categorized as GOOD, MEDIUM, POOR, and LESS THAN POOR. A LESS THAN POOR report requires the runway to be closed until braking action improves. This is an explicit operational gate, not a judgment call. Taxi on a slippery surface at max 5 kt.
Braking and Reverse Technique
On a slippery/contaminated runway, maintain a crabbed approach to touchdown, lower the nosewheel promptly, then apply brakes as required and do not pump the brakes. Under extreme conditions, maximum reverse thrust may be required to bring the aircraft to a complete stop. If the runway is sanded/gritted (SPWR), reduce reverse thrust to idle below 80 kt and stow reversers at 60 kt to minimize engine damage risk.
"Ten miles out, ATC changes the landing runway. Different LDA, different wind. Tell me what you do about landing performance and what your decision gates are."
Immediate Performance Reset
A late runway change requires re-validation of landing performance against the new LDA and wind. Ryanair line flying expects current charts and performance products available via trip kit discipline.
Speed Penalty
Excess approach speed is a major overrun factor. If touchdown is delayed while bleeding off 10 kt in the flare, total landing distance can increase by approximately 2,000 ft. If the aircraft is already on the ground in a stopping mode, 10 kt excess typically adds approximately 200 ft (dry) or up to approximately 600 ft (slippery runway).
Reverse Thrust
Select reverse thrust without delay once the main gear has touched down and hold until the interlocks release. The thrust reverser system is for ground operations after touchdown - the earlier claim that reverse can be initiated in flight was incorrect for B737 operations.
Decision Gate
If the runway change makes the landing limiting, buy time (vectors/hold) to re-validate the landing plan or divert. The stabilized approach gate is a hard backstop - if you cannot be stabilized and correctly configured, go around and reassess.
"Six sectors, quick turns all day. What are your specific procedural anchors to prevent rushing - particularly around performance setup, briefing quality, and tool validity?"
Trip Kit Hygiene
Ensure required flight paperwork and charts are present and valid including chart update discipline. Manage timing to avoid last-minute surprises. Ryanair line notes emphasize keeping operational documents current and being able to retrieve/print performance products when needed.
Hard Gates as Tempo Firewalls
Stabilized approach criteria are non-negotiable. If not stabilized and configured by the gate, go around regardless of schedule pressure. This is the primary defense against tempo-driven normalization.
Fatigue Self-Monitoring
Ryanair policy is explicit: crew must not commence or continue duty if they are aware they are fatigued. OM-A lists practical symptoms: reduced monitoring, slower scan, fixation, difficulty reading, irritability. These are exactly the errors that show up on quick-turn sectors. Simple mitigation: regular light meals and fluids.
"You've been de/anti-iced, you're number 12 for departure, holdover time is running out. Walk me through what you do, what you record, the must-do post-treatment actions, and the no-go winter phenomena."
Recording and All Clear
After de/anti-icing with engines running, obtain the anti-ice code and de-ice supervisor name, complete the DAR/DAR-01 recording. Must receive the ALL CLEAR signal before moving - multiple rigs/vehicles may still be in proximity.
Post-Treatment Actions
Wait at least 1 minute after completion before continuing the winter checklist (to ensure de-icing fluid clears from engines). Then: engine bleeds ON, packs AUTO, flight controls CHECK, and flap handling per exposure. Taxi with flaps up through slush/standing water in freezing conditions. Tactile checks are not permitted with engines running.
The No-Go Gate
HOT guidelines are not assessed for moderate or heavy freezing rain. OM-A does not permit operations in those conditions. If HOT is exceeded or contamination is suspected/confirmed, return to stand or remote de-icing for retreatment and/or inspection.
"On a short Ryanair sector, fuel margins move fast. Explain the fuel decision gates before start and during taxi, and tell me exactly when you transmit MINIMUM FUEL versus MAYDAY FUEL."
Pre-Start and Taxi Gates
Following a runway/SID change, prior to engine start the predicted fuel at destination must be at least CONT + ALTN + FINRES + DEV + TAXI. During taxi, if predicted fuel at destination drops below ALTN + FINRES + DEV, the Commander shall return to stand (unless ATC provides an immediate departure/short delay, or returning would cause further significant delay).
MINIMUM FUEL vs MAYDAY FUEL
Declare MINIMUM FUEL when committed to land at a specific aerodrome and any change to clearance may result in landing with less than planned final reserve. It does not imply priority handling.
If it becomes apparent that usable fuel on landing at the nearest adequate aerodrome will be less than final reserve, declare a fuel emergency: "MAYDAY, MAYDAY, MAYDAY, FUEL, [callsign]."
"Short runway landing: justify your autobrake selection, explain how autobrake and anti-skid behave, what causes autobrake to disarm, and what changes on a slippery runway."
Autobrake Operation and Disarm
Boeing autobrake provides commanded deceleration by automatically modulating brake pressure. Select it early and do not override unintentionally. Autobrake disarms with manual brake pedal application or selecting the switch off/disarm - avoid riding the pedals if you want autobrake active.
Short / Slippery Runway Technique
On short or slippery runways, do not attempt to modulate or pump the brakes - let anti-skid work. Critical exam point: maximum autobrake deceleration is less than maximum manual braking. If stopping is not assured, apply full manual braking immediately.
Use reverse thrust to support stopping; on slippery runways maximum reverse may be required. On SPWR surfaces, reduce reverse to idle below 80 kt and stow at 60 kt.
"Low visibility at a Northern European base - LVP declared, arrival rate collapses. Give me Ryanair's LVO framework, the key LVTO constraints, and the CAT II autoland crew flow."
LVO Authorization
Ryanair conducts LVO only when approved and within OM-A LVO policy, including LVTO, CAT II, and CAT III operations. For low-RVR LVTO (below 150 m but not less than 125 m), OM-A requires centerline/edge lighting spacing, a 90 m visual segment, and RVR achieved at relevant points.
LVP Requirement
LVP are aerodrome safety procedures supporting CAT II/IIIA approaches and LVTO. Ryanair shall not use an aerodrome for LVOs below visibility 800 m unless LVP are established. LVTO is defined as takeoff where RVR is less than 400 m.
CAT II Autoland Crew Flow
After APP mode selection, couple the second autopilot. Verify localizer capture and callouts/monitoring at key gates: 1,000 ft stabilization call, 500 ft FLARE ARMED check, minima calls, post-touchdown autopilot disconnect.
Before starting CAT II, read the ILS CAT II crew review in the QRH operator information. Minima-setting technique: set BARO minima first to bug the altimeter, then set RADIO minima. The All Weather Ops Guide highlights visual illusions and false pitch perception in very low vis, managed by a disciplined scan.
"Hydraulic abnormal on approach into a secondary airport with limited emergency services. Explain System A vs System B, manual reversion, and how it changes your approach plan."
System A vs System B
System A powers: landing gear, nose wheel steering, normal brakes, ground spoilers, and specific spoiler panels.
System B powers: leading edge devices, trailing edge flaps, and other spoiler panels.
A single-system failure is not symmetric in operational impact - know which system you have lost and what that specifically removes.
Manual Reversion / Dual-System Loss
The QRH checklist provides a structured recovery path including planning to land at the nearest suitable airport, system configuration actions, alternate flap extension, and manual gear extension. Notes flag performance and handling considerations including brake pressure limitations if system pressure is low.
Approach Decision
Choose the most suitable runway and support option available, simplify the approach, and avoid late changes. Configuration and energy management will be constrained by the abnormal checklist requirements. At a secondary airport with limited rescue services, this means early, conservative decisions.
"Six sectors, multiple delays, duty creeping toward the limit. What is your obligation regarding fatigue, what symptoms do you monitor, and how does Commander's Discretion work?"
Fatigue Obligation
Crew must not commence a duty, and must not continue after an intermediate landing, if they are aware they are fatigued or will be fatigued before the next landing. OM-A lists practical fatigue symptoms relevant to flight deck error: reduced monitoring, slower scan, fixation, difficulty reading, irritability. Simple mitigation: regular light meals and fluids.
Commander's Discretion (ORO.FTL.205(f))
Used in special circumstances. The Commander alone makes the decision, after consultation with crew on alertness, and may reduce FDP or increase rest to eliminate detrimental effect on safety. It is exceptional and should be avoided at home base where standby/airport-duty crew may be available.
Required Actions
When exercised: communicate the decision to Operations, file an ASR (Fatigue and ECDR), and keep Operations informed if duty may be continued based on acceptable alertness (unless crew are stood down).
"Engine failure after V1 departing a short-runway secondary airport. Talk me through 737-specific engine-out handling priorities, the QRH flow, and return vs continue logic in dense European airspace."
QRH Engine Failure or Shutdown Flow
The QRH includes configuration/automation considerations and directs an operationally conservative strategy: plan to land at the nearest suitable airport.
TCAS Setting
If required by the applicable QRH/MEL procedure, select TCAS TA ONLY for scenarios including engine failure. The correct mode name is "TA ONLY" - not "TA/TA only" as originally stated. OM-A 8.3.6.3.1 explicitly includes engine failure as a listed TA ONLY scenario.
APU Actions
Any APU actions must be taken only if explicitly directed by the applicable QRH checklist. The original output claimed the checklist directs starting the APU - this specific claim could not be verified in the approved sources.
One-Engine Approach and Return vs Continue
Transition into one-engine-inoperative approach/landing procedures. Be in landing configuration by 1,000 ft AGL. PM reads and confirms the landing checklist and configuration.
In dense European airspace, nearest suitable may be the departure field or another close alternate. The checklist-driven priority is to minimize exposure and land as soon as practicable.
Unreliable Airspeed: What are the B737 pitch and thrust targets for unreliable airspeed after takeoff from a contaminated runway?
Fly pitch and thrust, stop chasing the frozen tape — crosscheck all sources, then set targets from the Performance Inflight tables for your configuration, weight, and altitude.
System Fact
The Boeing QRH NNC flow for Airspeed Unreliable: adjust attitude and thrust, maintain airplane control, PROBE HEAT ON, crosscheck MACH/AIRSPEED indicators. If indicated airspeed is questionable, crosscheck IRS and FMC groundspeed and winds to determine airspeed accuracy. The flight path vector is inertial-based and can be used to help hold the correct path. Published attitude/thrust values must be taken from the applicable Performance Inflight tables for the aircraft and configuration in use. Important: altitude and/or vertical speed indications may also be unreliable — do not blindly trust vertical mode behavior when air data is suspect. Note: QRH PI tables are titled for the 737-800/CFM56-7B27. Do not assume they apply to the 737-8200/MAX without confirming in the MAX tail-specific publication.
Operational Risk / Trap
Rotating off a contaminated runway in winter with a frozen airspeed indicator is the scenario where pitot ice does not announce itself — the tape simply stops moving. The standby ASI matters because it is an independent reference when a primary pitot system is iced. GPS/IRS groundspeed matters because it is not pressure-derived, so it still tells you whether you are accelerating or decelerating while the pitots lie. Do not let one frozen primary drive your pitch and thrust. The structured crosscheck is how you find the liar without becoming one yourself.
Manual Verification
Boeing 737 QRH (D6-27370-804-BRI(P2)) — NNC.10 Instruments / AIRSPEED UNRELIABLE P 10.1 (NNC flow, crosscheck sequence); PI-QRH.10.1 Flight With Unreliable Airspeed (altitude/VS unreliable caution, Flaps Up tables); PI-QRH.10.2 Final Approach tables (Gear Down, Flaps 15/30/40)
Emergency Descent: What is the B737 emergency descent procedure and when can oxygen masks be removed?
Masks first — oxygen masks and regulators to 100%. Establish crew communications. Then descend without delay to the minimum safe altitude or 10,000 feet, whichever is higher.
System Fact
Emergency Descent QRH: autopilot and autothrottle should remain engaged (if not engaged, do not engage). Thrust levers minimum. Speedbrake lever to FLIGHT DETENT. Target speed set to MMO/VMO, engage. Turn and descend as needed. Altitude selector set to minimum safe altitude. Cabin crew notified. PA: ‘CABIN CREW RAPID DESCENT, RAPID DESCENT.’ Limit airspeed and add thrust as needed to prevent buffet or other adverse conditions. If cabin altitude exceeds or is expected to exceed 14,000 feet, passenger oxygen activates. Oxygen masks may be removed when the cabin altitude is at or below 10,000 feet — this is cabin altitude, not aircraft altitude.
Operational Risk / Trap
At FL390 over Northern Europe at minus 56 degrees, the procedure intentionally drives you to the speed limits. MMO/VMO is the target, not a limit to avoid. But an overspeed exceedance during the descent can add structural or engine problems on top of an already time-critical event. The mask-removal condition is cabin altitude at or below 10,000 feet, not aircraft altitude — this distinction matters because a depressurized aircraft at 10,000 feet may still have a cabin altitude above 10,000 if the outflow valve or fuselage damage prevents equalization.
Manual Verification
Boeing 737 QRH (D6-27370-804-BRI(P2)) — NNC.2 Air Systems / CABIN ALTITUDE WARNING or Rapid Depressurization P 2.1 (mask sequence, passenger oxygen trigger); NNC.0 Emergency Descent P 0.1 (descent procedure, speedbrake, speed target, cabin crew notification, buffet caution, mask removal condition)
The OEP contains 300+ system traps like these. Full memory item logic, Ryanair QRH alignment, and interactive oral exam Q&A — ready in 60 seconds.
Hone Your Edge — From $6/month →Runaway Stabilizer: What is the B737 runaway stabilizer procedure at low altitude on approach?
At 500 feet on approach this is survival prioritization — aviate first, stop the trim runaway per the memory flow, then assess the go-around gate.
System Fact
Runaway Stabilizer QRH memory items: Control column — hold firmly. Autopilot (if engaged) — disengage. Do not re-engage the autopilot. Control airplane pitch attitude manually with control column and main electric trim as needed. If the runaway continues: STAB TRIM CUTOUT switches (both) — CUTOUT. If the runaway continues: stabilizer trim wheel — grasp and hold. Stabilizer — trim manually. Anticipate trim requirements. The procedure is the same at any altitude — but the margins are not.
Operational Risk / Trap
Ryanair’s Landing Gate requires stability by 500 feet VMC or 1,000 feet IMC — if not stable, go-around is mandatory. A runaway stabilizer with changing column forces is a classic stable-approach breaker. At cruise you have altitude and time to troubleshoot and re-trim. At 500 feet on approach in gusty crosswind conditions at a European regional airport, you have neither. The go-around creates both — but it also becomes a single-pilot manual-trim event with significant column forces. That is why the low-altitude runaway stabilizer is one of the most demanding emergency scenarios on the 737: the correct procedure is identical to cruise, but the decision environment is completely different.
Manual Verification
Boeing 737 QRH (D6-27370-804-BRI(P2)) — NNC.9 Flight Controls / RUNAWAY STABILIZER P 9.1 (complete memory items); Ryanair B737-800 SOP Section 8 Approach & Landing / Stabilised Approach / Landing Gate PP 136-138
If you didn’t know the Landing Gate go-around trigger — your runaway stabilizer scenario ends at the wrong gate. The OEP drills every low-altitude emergency with the exact QRH and SOP logic behind the decision.
Hone Your Edge — From $6/month →Engine Fire Procedures: How does the B737 ground engine fire procedure differ from an in-flight engine fire?
In-flight: shut down, discharge, configure for single-engine landing. On the ground: evacuation is on the table immediately — and the checklist contains items in-flight crews never practice.
System Fact
In-flight ENGINE FIRE sequence: autothrottle disengage, thrust lever confirm and close, engine start lever confirm and CUTOFF, fire switch confirm and pull. If fire warning or ENG OVERHEAT light stays illuminated: rotate to stop, hold 1 second. If still illuminated after 30 seconds: rotate other stop, hold 1 second. If high airframe vibration occurs and continues after engine shutdown: reduce airspeed and descend as needed. Ground EVACUATION checklist differs significantly: FLAP lever 40 (IAS below 60), parking brake SET, speedbrake lever DOWN, pressurization mode selector MAN, outflow VALVE switch hold in OPEN until fully open. Engine start levers both CUTOFF. Captain PA: ‘EVACUATE, EVACUATE, UNDO SEAT BELTS AND GET OUT.’ FO advise ATC. Engine and APU fire switches all override and pull. Boeing guidance states there is no reason to discharge fire bottles for evacuations not involving fire indications existing or reported in or near an engine or APU.
Operational Risk / Trap
On the ground during taxi after landing with the fire bell going and EICAS fire warning confirmed, the FO advising ATC is the trigger for airport fire response — that call is what brings the fire trucks. The agent discharge is secondary to getting the passengers off the aircraft and the fire services rolling. The evacuation checklist items crews never practice in normal sim sessions include: pressurization MAN, outflow valve OPEN, speedbrake DOWN, and the IAS below 60 qualifier for flap selection. Missing any one of these in a high-stress ground fire changes the evacuation outcome.
Manual Verification
Boeing 737 QRH (D6-27370-804-BRI(P2)) — NNC.8 Fire Protection / ENGINE FIRE or Engine Severe Damage or Separation PP 8.2-8.3 (in-flight procedure, vibration block, agent discharge triggers); EVACUATION Back Cover.2 (ground evacuation procedure); B737NG FCTM NNO P 8.11 (fire bottle discharge guidance for evacuations)
TCAS RA Compliance: Do you disconnect the autopilot for a preventive TCAS RA on the B737?
If maneuvering is required: disengage autopilot and autothrottle. Then smoothly adjust pitch and thrust to satisfy the RA — this applies to all RAs including ADJUST VERTICAL SPEED.
System Fact
Boeing guidance: if maneuvering is required, disengage autopilot and autothrottle, then smoothly adjust pitch and thrust to comply with the RA. Follow the planned lateral path. Flight director pitch commands are not to be used during the conflict — the FD is not driven by RA guidance. Only follow the FD if it results in a vertical speed that satisfies the RA. Ryanair OM-A confirms compliance with the RA and requires ‘TCAS RA’ phraseology to ATC.
Operational Risk / Trap
High-tempo European short-haul climbing through a flight level with an ADJUST VERTICAL SPEED RA feels less urgent than a full CLIMB or DESCEND command — that is the trap. The RA is still a resolution advisory requiring compliance. Boeing does not distinguish between ‘preventive’ and ‘corrective’ RAs in the published guidance: if maneuvering is required, disconnect and comply. The FD bars may be showing a climb rate that does not satisfy the RA vertical speed band. Following the FD instead of the RA green/red guidance is how crews become non-compliant while believing they are flying correctly.
Manual Verification
Boeing 737 QRH (D6-27370-804-BRI(P2)) — Maneuvers / Non-Normal Maneuvers / TCAS MAN.1.5-MAN.1.6 (RA compliance, AP/AT disconnect, FD limitation); B737NG FCTM Maneuvers / Resolution Advisory P 7.23; Ryanair OM-A 8.3.6.3.2 TCAS RA Compliance / ATC Phraseology P 378
Two regulatory traps. Two checkride failures waiting to happen. The OEP puts you through every one — interactively — before your TRE does.
Hone Your Edge — From $6/month →Compliance & Accuracy — Manual Versions Used
Boeing 737 QRH (D6-27370-804-BRI(P2), 17 Jul 2009) — NNC.10 AIRSPEED UNRELIABLE (P 10.1) · NNC.9 RUNAWAY STABILIZER (P 9.1) · NNC.2 CABIN ALTITUDE WARNING / Rapid Depressurization (P 2.1) · NNC.0 EMERGENCY DESCENT (P 0.1) · NNC.8 ENGINE FIRE or Engine Severe Damage or Separation (PP 8.2-8.3) · EVACUATION (Back Cover.2) · TCAS (MAN.1.5-MAN.1.6)
Boeing 737 QRH — Performance Inflight PI-QRH.10.1 Flight With Unreliable Airspeed (737-800/CFM56-7B27) · PI-QRH.10.2 Final Approach (Gear Down)
B737NG Flight Crew Training Manual (FCTM) — Non-Normal Operations / Evacuation / Fire Bottle Guidance (P 8.11) · Maneuvers / Resolution Advisory (P 7.23)
Ryanair B737-800 Standard Operating Procedures — Section 8 Approach & Landing / Stabilised Approach / Landing Gate (PP 136-138)
Ryanair Operations Manual Part A (OM-A) — 8.3.6.3.2 TCAS RA Compliance / ATC Phraseology (P 378)
Note: QRH PI tables are confirmed for 737-800/CFM56-7B27 only. Do not assume applicability to 737-8200/MAX without confirming in the MAX tail-specific QRH/FCOM.
Content sourced exclusively from Ryanair-issued documentation. Not affiliated with Boeing or Ryanair.
If you didn’t know the Landing Gate go-around trigger, the evacuation checklist items crews never practice, or the FD trap on an ADJUST VERTICAL SPEED RA —
you’re a passenger in your own checkride.
