What this profile covers
Abnormal extension, retraction, indication, locking, door, steering, tyre, wheel, or brake conditions affecting ground or flight operation.
Why it matters
System events can alter aircraft capability, redundancy, workload, procedures, and the reliability of other safety barriers. For landing gear malfunction, useful analysis connects the immediate event with exposure, defenses, recurrence, and the wider operating system rather than treating one observation as a final conclusion.
System degradation, warning integrity, technical condition, dispatch decisions, and continued airworthiness.
Understand the subject before interpreting a signal.
In plain language, this profile examines abnormal extension, retraction, indication, locking, door, steering, tyre, wheel, or brake conditions affecting ground or flight operation.
Build a multi-source picture
- Warnings and system parameters
- Technical logs and maintenance history
- Crew reports and operational response
- Engineering inspection, test, and component evidence
Timing, relationships, and recurrence
Relevant recorded context may include normal acceleration, radio altitude, vertical speed, calibrated airspeed, pitch attitude. Use validated mappings and examine signal relationships over the applicable flight phase.
Do not turn an observation into a conclusion
Flight data can reconstruct symptoms and response but does not replace troubleshooting, approved maintenance data, inspection, or an engineering airworthiness decision.
Keep controlling material visible
Apply the current approved manuals, procedures, authority requirements, investigation evidence, and validated organizational definitions for any operational decision.
Normal acceleration
Acceleration measured broadly along the aircraft's vertical body axis; its touchdown peak can help characterize a landing load when interpreted with other signals.
Open parameter guide ↗ftRadio altitude
Height derived from radio altimetry, normally representing the distance from the aircraft to terrain directly below within the system's operating range.
Open parameter guide ↗ft/min or m/sVertical speed
The aircraft's vertical rate. Different recorded sources and smoothing can produce materially different values, especially during flare and touchdown.
Open parameter guide ↗ktCalibrated airspeed
Indicated airspeed corrected for instrument and position error, as provided by the aircraft data system.
Open parameter guide ↗degPitch attitude
Aircraft body attitude above or below the local horizontal reference.
Open parameter guide ↗% / ratio / aircraft-specificEngine thrust
One or more recorded measures of commanded or produced propulsion; the correct signal depends on engine and aircraft type.
Open parameter guide ↗deg or discreteGround spoiler position
Position or deployment state of panels used to reduce lift and increase wheel loading after touchdown.
Open parameter guide ↗psi, bar, or %Brake pressure
Hydraulic pressure or command associated with wheel braking; it is not a direct measurement of tyre/runway friction.
Open parameter guide ↗From a broad topic to a defensible safety review.
Define
State what landing gear malfunction means for the aircraft, operation, authority, and organization in scope.
Verify
Confirm the provenance, quality, timing, units, completeness, and limitations of every data source used.
Describe
Reconstruct what happened and quantify relevant exposure before discussing causes or corrective action.
Corroborate
Compare flight data with reports, operational context, technical evidence, and authoritative source material.
Test barriers
Identify which preventive, recovery, and consequence-mitigation controls should have worked and how their performance can be measured.
Assure
Assign proportionate action and verify whether the control and safety performance improve without harmful unintended effects.
Questions before conclusions
- Q1
How is landing gear malfunction defined for the aircraft, operation, authority, and organization being reviewed?
- Q2
Which precursors, recorded signals, reports, and external data would confirm the event and describe its context?
- Q3
Which preventive, recovery, and consequence-reduction barriers should work, and where could they weaken?
- Q4
What does recurrence, exposure, severity potential, or change over time show before choosing a safety action?
6 connected event profiles
These are terminology and family connections for exploration—not claims that FDM alone can determine the topic.
Prolonged brake application during taxi
Brake pressure or command remains applied for an extended portion of taxi while the aircraft continues moving.
Open FDM profile ↗FDM-028 · Initial climb & climbLanding-gear retraction delay
Gear remains extended beyond the operator-defined state, height, or time context after a positive climb is established.
Open FDM profile ↗FDM-044 · DescentProlonged speedbrake use in descent
Speedbrake or spoiler deployment remains active for an extended descent segment outside the expected context.
Open FDM profile ↗FDM-047 · DescentLanding-gear limit speed exceedance
Airspeed exceeds the applicable gear operating or extended limit during gear movement or extension.
Open FDM profile ↗FDM-078 · Landing contactNose-gear-first touchdown
Recorded gear or load sequence indicates nose gear contact before the main landing gear.
Open FDM profile ↗FDM-090 · Landing rolloutHigh brake temperature after landing
Recorded or derived brake temperature exceeds an aircraft- and maintenance-specific monitoring condition after landing.
Open FDM profile ↗Go deeper into the closest ASIP research guides.
Hard Landing
A structured guide to recognizing, reporting, analyzing, and responding to a suspected touchdown load exceedance without confusing passenger perception with an engineering determination.
Open intelligence brief ↗Aircraft SystemsFlight-Deck Automation
Use mode awareness, active monitoring, and aircraft-response verification to keep automation aligned with crew intent.
Open intelligence brief ↗Aircraft SystemsEngine Failure and Thrust Loss
Separate commanded thrust, actual engine response, system effects, and crew management across partial, asymmetric, and complete thrust-loss events.
Open intelligence brief ↗Aircraft SystemsFire and Smoke
View fire safety as detection, containment, checklist action, diversion, evacuation, and rescue barriers.
Open intelligence brief ↗12 useful starting points
Original ASIP summaries lead to publisher pages. ASIP does not copy or host the reports.
SAFO 23001 — Potential Damage to Nose Landing Gear (NLG) by Improper Towing Procedures of the Mitsubishi Heavy Industries Regional Jet (MHIRJ) (formerly Bombardier) CL-600-2B19, CL-600-2C10 and CL-600-2D24 Airplanes
Official U.S. Federal Aviation Administration material indexed for approach and landing and ground operations. Open the publisher source for the complete document, scope, and current status.
Open official sourceSAFO 10007 — Tundra Tire Installation/Approval for Airplanes Equipped with Leaf Spring Type Main Landing Gear
Official U.S. Federal Aviation Administration material indexed for approach and landing and airworthiness and systems. Open the publisher source for the complete document, scope, and current status.
Open official sourceA320 landing gear downlock
Official Airbus Safety First material indexed for approach and landing and airworthiness and systems. Open the publisher source for the complete document, scope, and current status.
Open official sourceProper Landing Gear Servicing for Safe Operations
Official Airbus Safety First material indexed for approach and landing and maintenance. Open the publisher source for the complete document, scope, and current status.
Open official sourceSAFO 20013 — SAFO 20013, Right-Hand Control Wheel Removal for Skydiving Operations
Official U.S. Federal Aviation Administration material indexed for aviation safety. Open the publisher source for the complete document, scope, and current status.
Open official sourceAirbus Brake Testing
Official Airbus Safety First material indexed for runway safety. Open the publisher source for the complete document, scope, and current status.
Open official sourceLanding with Nosewheels at 90 degrees
Official Airbus Safety First material indexed for approach and landing. Open the publisher source for the complete document, scope, and current status.
Open official sourceTake Care of the Wheel Bearings
Official Airbus Safety First material indexed for aviation safety. Open the publisher source for the complete document, scope, and current status.
Open official sourceTake Care of the Wheel Tie Bolts
Official Airbus Safety First material indexed for aviation safety. Open the publisher source for the complete document, scope, and current status.
Open official sourceTake Care of Your Brakes
Official Airbus Safety First material indexed for aviation safety. Open the publisher source for the complete document, scope, and current status.
Open official sourceAnnex 19 — Safety Management, Third Edition
Annex 19 consolidates ICAO safety-management provisions, including State safety responsibilities, SMS, safety-data collection and processing, and the protection and sharing of safety information.
Open official sourceAnnual Safety Review 2025
EASA's review uses occurrence and accident information to describe performance across aviation domains and to support the European safety-risk-management process.
Open official sourceCommon Taxonomy Team
International work on common aviation occurrence categories and definitions for consistent reporting and analysis.
Open referenceSafety Risk Management
European safety-risk process connecting data, safety issues, risk portfolios, priorities, and safety action.
Open referenceAnnual programmes and reports
Annual safety reviews and risk portfolios used to identify key risk areas, safety issues, and emerging issues.
Open referenceEuropean Plan for Aviation Safety 2025
A broad evidence-based portfolio showing the scale and connected nature of current aviation safety issues.
Open referenceOperational issues index
A practical discovery index for operational safety subjects; official authority and manufacturer sources remain controlling where applicable.
Open reference