GENERAL INFORMATION FOR NTSB REPORT: DCA18MA142
Data Source NTSB AVIATION ACCIDENT/INCIDENT DATABASE
NTSB Report Nbr DCA18MA142
Event Id 20180417X23642
Local Date 04/17/2018
Local Time 1503
State PA
City PHILADELPHIA
Airport Name PHILADELPHIA
Event Type ACCIDENT
Injury Severity FATAL
Record Status FINAL
Event Location OFF AIRPORT/AIRSTRIP

WEATHER INFORMATION
Basic Weather Conditions VISUAL METEOROLOGICAL COND
Light Condition DAY
Cloud Height above Ground Level (ft) 0
Ceiling Height above Ground Level (ft) 0
Wind Direction (deg) 0
Wind Condition Flag U

AIRCRAFT INFORMATION
Aircraft 1
Type of Operation PART 121: AIR CARRIER
Registration Number N772SW
Aircraft Make BOEING
Aircraft Model 737
Aircraft Series 7H4
Aircraft Damage SUBSTANTIAL
Aircraft Fire NONE
Aircraft Explosion NONE
Aircraft Type AIRPLANE
Aircraft Homebuilt NO
Phase of Flight ENROUTE-CLIMB TO CRUISE
Category of Operation SCHEDULED
Flight Plan Filed IFR
Domestic/International DOMESTIC
Passenger/Cargo PASSENGER ONLY
Operator Name SOUTHWEST AIRLINES CO
Owner Name SOUTHWEST AIRLINES CO
Number of Passenger Seats 149
Number of Engines 2
ELT Installed UNKNOWN
ELT Operated UNKNOWN
Departure Airport Id LGA
Departure City NEW YORK
Departure State NEW YORK
Last Departure Point UNKNOWN
Destination Airport Id DAL
Destination City DALLAS
Destination State TEXAS
Runway Id 27L
Runway Length 12000
Runway Width 200
Air Carrier Operating Certificates YES
Air Carrier Other Operating Certificates UNKNOWN
Cert Max Gross Wgt 154500
Landing Gear FIXD

ENGINE INFORMATION

Aircraft 1 - Engine : #1
Engine Type TURBO FAN
Engine Manufactuer CFM INTL.
Engine Model CFM56 SERIES

Aircraft 1 - Engine : #2
Engine Type TURBO FAN
Engine Manufactuer CFM INTL.
Engine Model CFM56 SERIES

INJURY INFORMATION
Injury Summary for Aircraft 1
Fatal Serious Minor None
Crew 0 0 0 0
Pass 0 0 0 0
Total 0 0 0 0
Sequence of Events for Aircraft 1
Occurrence Sequence
Occurrence Sequence # Occurrence Sequence Description
1 ENROUTE-CLIMB TO CRUISE POWERPLANT SYS/COMP MALF/FAIL


Findings
Finding # Finding Description Cause/Factor
1 AIRCRAFT-AIRCRAFT POWER PLANT-ENGINE (TURBINE/TURBOPROP)-COMPRESSOR SECTION-FATIGUE/WEAR/CORROSION C
2 AIRCRAFT-AIRCRAFT STRUCTURES-NACELLES/PYLONS STRUCTURE-NACELLE/PYLON MISC STRUCTURE-DAMAGED/DEGRADED C
3 AIRCRAFT-AIRCRAFT STRUCTURES-WINDOWS-WINDSHIELD SYSTEM-PASSENGER COMPARTMENT WINDOWS-DAMAGED/DEGRADED C
4 ORGANIZATIONAL ISSUES-MANAGEMENT-RESOURCES-AVAILABILITY OF DOCUMENTS/INFO-FAA/REGULATOR
5 PERSONNEL ISSUES-ACTION/DECISION-ACTION-LACK OF ACTION-CABIN CREW



AIRCRAFT 1 PRELIMINARY REPORT


The NTSB's full report is available at http://www.ntsb.gov/investigations/AccidentReports/Pages/AccidentReports.aspx. The Aircraft Accident Report number is NTSB/AAR-19/03. On April 17, 2018, about 1103 eastern daylight time, Southwest Airlines flight 1380, a Boeing 737-7H4, N772SW, experienced a left engine failure while climbing through flight level 320 en route to the flight's assigned cruise altitude. The flight had departed from LaGuardia Airport, Queens, New York, about 30 minutes earlier. As a result of the engine failure, the flight crew conducted an emergency descent and diverted to Philadelphia International Airport (PHL), Philadelphia, Pennsylvania. Portions of the left engine inlet and fan cowl separated from the airplane, and fragments from the inlet and fan cowl struck the left wing, the left-side fuselage, and the left horizontal stabilizer. One fan cowl fragment impacted the left-side fuselage near a cabin window, and the window departed the airplane, which resulted in a rapid depressurization. The airplane landed safely at PHL about 17 minutes after the engine failure occurred. Of the 144 passengers and 5 crewmembers aboard the airplane, 1 passenger received fatal injuries, and 8 passengers received minor injuries. The airplane was substantially damaged. The regularly scheduled domestic passenger flight was operating under the provisions of Title 14 Code of Federal Regulations Part 121 with a destination of Dallas Love Field, Dallas, Texas.

AIRCRAFT 1 FINAL REPORT


The NTSB's full report is available at http://www.ntsb.gov/investigations/AccidentReports/Pages/AccidentReports.aspx. The Aircraft Accident Report number is NTSB/AAR-19/03. On April 17, 2018, about 1103 eastern daylight time, Southwest Airlines flight 1380, a Boeing 737-7H4, N772SW, experienced a left engine failure while climbing through flight level 320 en route to the flight's assigned cruise altitude. The flight had departed from LaGuardia Airport, Queens, New York, about 30 minutes earlier. As a result of the engine failure, the flight crew conducted an emergency descent and diverted to Philadelphia International Airport (PHL), Philadelphia, Pennsylvania. Portions of the left engine inlet and fan cowl separated from the airplane, and fragments from the inlet and fan cowl struck the left wing, the left-side fuselage, and the left horizontal stabilizer. One fan cowl fragment impacted the left-side fuselage near a cabin window, and the window departed the airplane, which resulted in a rapid depressurization. The airplane landed safely at PHL about 17 minutes after the engine failure occurred. Of the 144 passengers and 5 crewmembers aboard the airplane, 1 passenger received fatal injuries, and 8 passengers received minor injuries. The airplane was substantially damaged. The regularly scheduled domestic passenger flight was operating under the provisions of Title 14 Code of Federal Regulations Part 121 with a destination of Dallas Love Field, Dallas, Texas. The National Transportation Safety Board determines the probable cause(s) of this accident as follows: A low-cycle fatigue crack in the dovetail of fan blade No. 13, which resulted in the fan blade separating in flight and impacting the engine fan case at a location that was critical to the structural integrity and performance of the fan cowl structure. This impact led to the in-flight separation of fan cowl components, including the inboard fan cowl aft latch keeper, which struck the fuselage near a cabin window and caused the window to depart from the airplane, the cabin to rapidly depressurize, and the passenger fatality.

AIRCRAFT 1 CAUSE REPORT


A low-cycle fatigue crack in the dovetail of fan blade No. 13, which resulted in the fan blade separating in flight and impacting the engine fan case at a location that was critical to the structural integrity and performance of the fan cowl structure. This impact led to the in-flight separation of fan cowl components, including the inboard fan cowl aft latch keeper, which struck the fuselage near a cabin window and caused the window to depart from the airplane, the cabin to rapidly depressurize, and the passenger fatality.


END REPORT