FlarePathAir-accident investigation intelligence
Investigation brief · generated 2026-10-09 · source: NTSB public docket and accident database

BOEING 737-7Q8 — Chicago, IL, USA, 2011-04-26

NTSB number
DCA11IA047
Operator
SOUTHWEST AIRLINES CO
Registration
N799SW
Highest injury
No injury
Regulation
Part 121
Damage
Minor
Cohort
Part 121 airline
Recorder data
Tier 1 — decoded recorder tables
Every sentence below is taken directly from NTSB records — the accident database, the docket's recorder reports and the Board's findings — with its source noted. Nothing is paraphrased or inferred.

NTSB summary

The flight was routine until nearing the Chicago terminal area, where delays due to traffic, weather, and conflicting approaches with O’Hare International Airport resulted in an air traffic controller instructing the flight crew to expect to hold. Shortly afterward, the controller advised the crew that aircraft capable of required navigation performance (RNP) approaches to runway 13C would be accepted to MDW. The flight crewmembers mistakenly loaded and briefed a different procedure, the area navigation (RNAV) global positioning system (GPS) approach, before entering the holding pattern. While in the holding pattern, the flight crew performed a landing distance assessment using the onboard performance computer (OPC). The calculation results showed sufficient runway length for the landing in accordance with the flight manual procedures. Data from the cockpit voice recorder and the OPC indicate that the crew performed the assessment correctly. After receiving air traffic control (ATC) clearance to leave the holding pattern and begin the approach to MDW, the flight crewmembers discussed confusion about the approach instruction, likely because they had loaded and briefed the wrong approach procedure. The flight crew then identified the proper approach procedure chart. The crew subsequently reprogrammed the flight management system for the correct approach and amended some of the procedure crossing altitudes in order to follow ATC instructions. These activities at this point in the approach resulted in extra workload for the flight crew. Later, as flight 1919 neared the runway, the flight crew set flaps to 15. The flight crew of a preceding Southwest Airlines 737 arrival reported “fair” braking action on runway 13C to ATC. The air traffic controller did not advise the flight 1919 crew of the braking action report transmitted by the previous arrival; however, the incident crew overheard the report and correctly recalculated the landing distance assessment, which again indicated sufficient runway length available. The incident crew also set the airplane autobrakes appropriately for the conditions. In addition to discussion regarding the approach procedure automation, the crew had additional operational distractions in the final minutes of the approach. These included a momentary flap overspeed as the first officer attempted to set flaps to 25, assessment of a rain shower passing over the airport, and incorrect settings for minimum altitude reminders. The delay in setting flaps to 25 as the first officer waited for airspeed to decay occurred about the same time that the crew normally should have been executing the Before Landing checklist, which includes the item “speedbrake—armed.” No mention of speedbrakes or the Before Landing checklist is heard on the cockpit voice recording, and data from the flight data recorder (FDR) indicate that the speedbrakes were not armed. The airplane touched down within 500 feet of the runway threshold. After touchdown, the captain perceived a lack of braking effectiveness and quickly applied full manual brakes. Speedbrakes did not deploy upon touchdown, nor were thrust reversers deployed. About 16 seconds after touchdown, thrust reversers were manually deployed, which also resulted in speedbrake deployment per system design, when the airplane had about 1,500 feet of runway remaining. As the airplane neared the end of the pavement, the captain attempted to turn onto the connecting taxiway but was unable. The airplane struck a taxiway light and rolled about 200 feet into the grass. FDR data and component examination revealed that all airplane systems operated as expected. The automatic speedbrakes were not armed and, therefore, would not deploy upon touchdown without crew action. Extending the speedbrakes after landing increases aerodynamic drag and reduces lift, which increases the load applied to the main gear tires and makes the wheel brakes more effective. A lack of speedbrake deployment results in severely degraded stopping ability. According to the flight operations manual, braking effectiveness is reduced by as much as 60 percent. The flight crew’s delay in applying reverse thrust also contributed to the amount of runway used. Simulation studies concluded that the airplane would have stopped with about 900 feet of runway remaining if the speedbrakes had been deployed at touchdown (without reverse thrust) or with about 1,950 feet remaining if both speedbrakes and reverse thrust had been deployed at touchdown, per standard procedures. The calculated braking coefficient of the incident airplane was consistent with a “fair” braking action report, as given by the preceding Southwest Airlines 737 arrival. The braking coefficient is also in accordance with the OPC calculations.
Verbatim, NTSB aviation accident database (narratives.narr_accf).

Probable cause

The flight crew's delayed deployment of the speedbrakes and thrust reversers, resulting in insufficient runway remaining to bring the airplane to a stop. Contributing to the delay in deployment of these stopping devices was the flight crew's inadequate monitoring of the airplane's configuration after touchdown, likely as a result of being distracted by a perceived lack of wheel braking effectiveness. Contributing to the incident was the flight crew's omission of the Before Landing checklist, which includes an item to verify speedbrake arming before touchdown, as a result of workload and operational distractions during the approach phase of flight.
Verbatim, NTSB determination.

Flight data recorder

— 9,232 samples, 73 parameters, 11:00:00.0 to 13:33:51.0.

ParameterMaxatMinatFinalat
Pressure altitude ft37,026.011:25:56.00.013:33:51.00.013:33:51.0
Computed airspeed kts290.311:15:44.00.013:33:51.00.013:33:51.0
Vertical acceleration g1.413:13:32.00.713:32:48.01.013:33:51.0
Engine 1 N1 %RPM99.811:23:20.019.213:33:16.024.413:33:51.0
Engine 2 N1 %RPM99.811:23:18.019.113:33:16.023.213:33:50.0
Computed from the docket's tabular attachment; times as recorded (local or SRN as published).

Sequence of events (FDR factual report)

TimeEventPage
11:05 CDTTakeoff; cruising altitude of 37,000 ft reached about 18 minutes later2
about 12:15 CDTInitial descent began2
12:45 CDTSeries of right holding turns for about 30 minutes, then final descent for landing2
final approachFlaps set to 40 degrees; speed brake armed light not indicated3
13:31:48 CDTAutopilot disengaged3
13:33:04 CDTMain gear weight-on-wheels registered ground at an airspeed of 136 knots; autothrottle engage parameter turned off 1 second later3
13:33:06 CDTNose gear weight-on-wheels registered ground; autobrake showed applied for one second followed by an increase in left and right brake pressure3
13:33:21 CDTThrottle resolver parameters began to move, speed brake handle position increased and the speed brake armed light indicated armed; within 2 seconds thrust reversers fully deployed and spoiler panels fully deployed3
13:33 CDTDuring the landing roll the aircraft made a left excursion from the runway heading and stopped on a magnetic heading of 101 degrees; last recorded data point at 13:333
Extracted by claude-fable-5-1 (in-session); 4 of 9 stated events verified against the raw recorder data.

Cockpit voice recorder

721 transcribed utterances from 11:39:17.3 to 13:43:55.9, 25 sources. Final entries:

13:42:12.7HOT-8yeah.
13:42:13.5HOT-7hey which door do you want to use here...they’re asking me...it's this door right...the door I have open...[sigh] oh my God...our aft--our aft entry door...not the one where we use the provisioner...he's comin' up right now with the stairs.
13:42:57.1CAM-1hey @ @ @ captain on nineteen nineteen. hey thanks. yep we're in the mud. everybody's okay. no injuries. engines have been shut down. uh fire trucks are here. we're trying to get some airstairs that won't sink in the mud. but everything--...yes---...we're doin'---we're doin'---we're doin' it right now.
13:43:23.7CAM-1everybody's fine. no injuries. aircraft is approximately um ten to fifteen feet off of the left end. we did not go into the frangible cement. we steered it into the grass. we're a good hundred feet from the fence line. everybody is here with no injuries....yeah...yep...oh yeah. DCA11IA047
13:43:55.9CAM-1no...no no no...the aircraft was...we were landing right at max weight. had wind gusts a storm had just passed through the area. guy in front of us had just called wet fair. ah when we hit the brakes we weren't gettin' anything it was just...it just kept goin'. we both got on the brakes as hard as we could and ah and weren't seeing any deceleration. and we finally got it [end of recording]
The NTSB cautions that a CVR transcript is not a precise science and should not be used as the sole source of information.

Recorder documents in the docket

GroupTitlePagesType
fdrFlight Data Recorder 10 - Factual Report of Group Chairman11pdf
fdrFlight Data Recorder 10 - Attachment 1 FDR Tabularcsv
cvrCockpit Voice Recorder 12 - Factual Report of Group Chairman69pdf
performanceAircraft Performance 13 - Performance Study17pdf

Docket: data.ntsb.gov/Docket/?NTSBNumber=DCA11IA047. This brief is an analytical aid assembled from public records; it is not an investigative finding.