NTSB CAROL · Event
Event DCA25LA185
Registry · N7724A
FAA Aircraft Registry record.
Make / Model
BOEING 737-7BD
Year of manufacture
2009 · 16 years old at event
Engine
CFM INTL CFM56-7B24
Seats / Engines
149 seats · 2 engines
Last airworthiness date
20130923
ADS-B equipped
Yes — Mode-S AA735A
Registrant of record
SOUTHWEST AIRLINES CO
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Serious Injury to a flight attendant sustained during an evacuation.
Factual narrative
Southwest Airlines flight 3006, a scheduled international passenger flight from William P. Hobby Airport (HOU), Houston, Texas, to Los Cabos International Airport (SJD), San Jose del Cabo, Mexico, experienced a right engine failure resulting in an air turnback. During the turnback, a burning odor was reported in the cabin and an evacuation was commanded after landing. During the evacuation, one flight attendant (FA) sustained a serious injury. According to the flight crew, they were on day two, leg two, of a three-day line experience rotation. The first officer (FO), pilot flying, was returning from leave and the captain (CA) was a line check airman for the company. During the preflight, the flight crew discussed the automatic terminal information service (ATIS) reporting windshear and planned for a precautionary takeoff profile. The flight crew briefed the engine out procedures and the takeoff profile for runway 22. The taxi and takeoff were normal. During climb out, the flight crew observed the right engine exhaust gas temperature (EGT) indication momentarily increase into the red overtemp range, then decrease. The flight crew then heard a “popping” noise and observed the right engine N1 indication decrease to approximately 50%. The CA declared an emergency with air traffic control (ATC) and initiated the Engine Fire, Severe Damage or Separation quick reference checklist (QRC) and the quick reference handbook (QRH) procedures. The FO continued as the pilot flying and coordinated vectors for a return to HOU. The “A” FA contacted the cockpit to inform them of a burning odor in the cabin. The CA informed the FAs that they had an engine malfunction and were returning to HOU. The CA then made a public announcement informing the passengers that they would be landing in 20 minutes. After completing all appropriate checklists, the CA assumed control of the aircraft, and the FO transitioned to the pilot monitoring. The approach and landing were uneventful. ATC requested that the flight crew exit the runway at the end and coordinate with airport rescue firefighting (ARFF). After clearing the runway and stopping, the CA contacted the FA’s and was informed that there was still a strong burning odor in the cabin. At that time, the CA elected to initiate an evacuation of the airplane. The CA informed ARFF of the decision and the FO began the QRH for an evacuation. The flight crew completed the QRH procedure, including left engine shutdown and FLAP 40 extension, and the CA commanded an evacuation via the left side of the aircraft. The FO evacuated the aircraft to assist with the evacuation while the CA remained onboard until all passengers had evacuated. The CA observed passengers re-entering the aircraft from the overwing exits and then utilizing the door slides. After all passengers and flight attendants had evacuated the aircraft, the CA conducted a final walkthrough and evacuated the aircraft. On the ground, the CA learned that ARFF personnel had directed passengers back into the aircraft due to concerns of injuries sliding off the wing. According to the “B” FA, seated in the aft galley, during takeoff there was a loud noise and followed by a burning odor. As the aircraft continued to climb the odor intensity decreased and they inspected the area and were unable to identify a source. The B FA contacted the A FA and informed them of the odor. The CA made an announcement that they had experienced an engine failure, and they would be landing in approximately 20 minutes. After landing and stopping, the CA called the FAs and asked if the odor still existed, to which the B FA replied that they still smelled a burning odor. After the evacuation, the B FA reported an injury to their ankle. They were diagnosed with a hairline fracture. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Aircraft-Aircraft power plant-Engine (turbine/turboprop)-(general)-Failure
- — Environmental issues-Task environment-Physical workspace-Air quality/dust/smoke-Contributed to outcome
- — Personnel issues-Physical-Impairment/incapacitation-Illness/injury-Cabin crew
Verbatim from NTSB's published report. Source file
NTSB_2025_DCA25LA185.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2019 · Technical Memorandum (TM)
A preliminary study of a wake vortex encounter hazard boundary for a B737-100 airplane
A preliminary batch simulation study was conducted to define the wake decay required for a Boeing 737-100 airplane to safely encounter a Boeing 727 wake and land.
- NASA NTRS 2018 · Other
A Numerical Simulation Study to Develop an Acceptable Wake Encounter Boundary for a B737-100 Airplane
The National Aeronautics and Space Administration (NASA) is conducting research with the goal of enabling safe improvements in the capacity of the nation's air transportation system.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NTSB Aircraft Accident Reports 2019 · Accident report
Loss of Engine Power and Subsequent Ditching of Southwest Airlines Flight 1380
Southwest 1380 (B737-700) Philadelphia, April 17, 2018 — uncontained engine failure, passenger fatality. Examines the uncontained failure of a CFM56-7B fan blade due to high-cycle fatigue that breache…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
Browse the full corpus — academia portal ↗