Boeing 737-401

Service difficulty reports · 2,961

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '737401'
  ORDER BY difficulty_date DESC"

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SDR USAASB98324Harness · failedRIC - FLT 1475 - EN ROUTE PHL-CLT, THR NR 2 GENERATOR TRIPPED. THE APU GENERATOR SYSTEM WAS ON MEL. FLIGHT DIVERTED TO RIC AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE GENERATOR FEEDER WIRE PINS BURNED AT THE FIREWALL CONNECTOR D41Dec 11, 1998 · N419US · Boeing 737401 · AC Generation SystemSDR USAASB324Generator · malfunctionedRIC - FLT 1475 - EN ROUTE PHL-CLT, THE NR 2 GENERATOR TRIPPED. THE APU GENERATOR SYSTEM WAS ON MEL. FLIGHT DIVERTED TO RIC AND LANDED WITH NO FURTHER INCIDENT. (M)Dec 11, 1998 · N419US · Boeing 737401 · AC Generation SystemSDR USAASB98323Gcu · malfunctionedJAX - FLT 820 - DURING CRUISE, THE APU GENERATOR QUIT AND THE NR 2 ENGINE GENERATOR WAS ALREADY ON MEL. DECISION WAS MADE TO DIVERT TO JAX SINCE THE AIRCRAFT WAS DOWN TO ONE ELECTRICAL SOURCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAREDec 10, 1998 · N419US · Boeing 737401 · AC Generation SystemSDR USAASB98308Switch · malfunctionedBWI - FLT 1168, FLIGHT DEPARTED BWI WITH THE NR 1 GENERATOR ON MEL. AT APPROXIMATELY FL230, THE APU SHUTDOWN AUTOMATICALLY DUE TO AN OVERSPEED LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI SINCE THE AIRCRAFT WAS DOWN TO ONE ELECTRICAL SOURCE. FLIGHNov 19, 1998 · N413US · Boeing 737401 · APU ControlsSDR 99ZZZM41Module · malfunctionedBWI - FLT 1168, FLIGHT DEPARTED BWI WITH THE NR 1 GENERATOR ON MEL. AT APPROXIMATELY FL230, THE APU SHUTDOWN AUTOMATICALLY DUE TO AN OVERSPEED LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI SINCE THE AIRCRAFT WAS DOWN TO ONE ELECTRICAL SOURCE. FLIGHNov 19, 1998 · N413US · Boeing 737401 · APU ControlsSDR USAA980597Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH AREA OF CORROSION AT STATION 947.5 LBL 14 TO RBL 33 FLOORBEAM. CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER TR 53-60-02. (M)Nov 18, 1998 · N412US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980587Frame · chafedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CHAFED AT FRAME BS 1040. INSTALLED DOUBLER PER TR 53-80-02. (M)Nov 18, 1998 · N412US · Boeing 737401 · Fuselage Main, FrameSDR USAA980586Beam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH BY 5 INCH AREA OF CORROSION BS 986.5, WL 208, LBBL 14.5 - LBBL 19.5 BEAM INST, CORROSION TASK NR C53-107-02. INSTALLED REPAIR 'T' CAP PER SRM 53-60-51 BOEING 737-400. (M)Nov 18, 1998 · N412US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA980585Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CRACKS STATION 178 BULKHEAD APPROX 2 INCHES AT RBBL 5.7 WL 200 WEB ASSY. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)Nov 18, 1998 · N412US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA980584Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CRACKS STATION 178 BULKHEAD APPROX 2 INCHES AT LOWER LEFT RADAR ANTENNA MOUNT WEB ASSY LBL 5.7 WL 200. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)Nov 18, 1998 · N412US · Boeing 737401 · Fuselage Main, BulkheadSDR USAASB98315Wire · brokenPVD - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ON THE OUTSIDE OF THE FORWARD COAT CLOSET INOP. MAINTENANCE REPAIRED AND SECURED BROKEN WIRE INSIDE FORWARD COAT CLOSET. OPS CHECK GOOD. (M)Nov 17, 1998 · N404US · Boeing 737401 · Light System WiringSDR USAASB98295Transformer · failedPHL - FLT 162 - SHORTLY AFTER T/O, THE NR 1 TRANSFORMER RECTIFIER C/B TRIPPED FOLLOWED BY THE BATTERY CHARGER AND THE 'B' SYSTEM ELECTRIC HYDRAULIC PUMP. WITHIN 10 MINUTES, THE NR 1 ELECTRIC BUS TRIPPED FOLLOWED BY THE AC STANDBY BUS, EQUIPMENT COOLING NORMALNov 10, 1998 · N413US · Boeing 737401 · AC Generation SystemSDR 99ZZZM14Rectifier · failedPHL - FLT 162 - SHORTLY AFTER T/O, THE NR 1 TRANSFORMER RECTIFIER C/B TRIPPED FOLLOWED BY THE BATTERY CHARGER AND THE 'B' SYSTEM ELECTRIC HYDRAULIC PUMP. WITHIN 10 MINUTES, THE NR 1 ELECTRIC BUS TRIPPED FOLLOWED BY THE AC STANDBY BUS, EQUIPMENT COOLING NORMALNov 10, 1998 · N413US · Boeing 737401 · DC Rectifier/ConverterSDR USAASB98291Acm · failedTPA - FLT 1425 - AFTER TAKEOFF FROM TPA, CREW COULD NOT GET THE AIRCRAFT TO PRESSURIZE. CREW WENT THROUGH ALL PROCEDURES BUT AIRCRAFT FAILED TO PRESSURIZE. DIFFERENTIAL PRESSURE NEVER INCREASED BEYOND 1.5 SPI. OUTFLOW VALVE INDICATED FULL CLOSED. FLIGHT REOct 31, 1998 · N407US · Boeing 737401 · Cabin Cooling SystemSDR USAASB98298Battery Pack · dischargedCLT - MAINTENANCE FOUND THE FORWARD LEFT EMERGENCY EGRESS LIGHTS INOP. MAINTENANCE REPLACED FUSES IN BATTERY CHARGER AND INSTALLED REPLACEMENT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Oct 28, 1998 · N418US · Boeing 737401 · Emergency LightingSDR USAASB98283Yaw Damper · failedCLT - FLT 1669 - ON TAKEOFF ROLL AT 110-120 KNOTS, THE AIRCRAFT PULLED HARD TO THE LEFT AND THE CREW HEARD A LOUD BANG. THE AIRCRAFT ROTATED AND THE CREW SUSPECTED A BLOWN TIRE. CHECKLIST WAS ACCOMPLISHED AND THE FLIGHT RETURNED TO FIELD AT CLT. NO EMERGENCOct 26, 1998 · N421US · Boeing 737401 · Autopilot SystemSDR USAASB98280Torque Link · brokenPHL - FLT 165 - ON LANDING ROLL IN PHL, A VIBRATION DEVELOPED FROM THE NLG AND STEADILY INCREASED. NOSE WHEEL STEERING WAS LOST. AIRCRAFT STOPPED ON THE RUNWAY AND WAS UNABLE TO COMMUNICATE ON ANY RADIO, INTERPHONE OR PASSENGER ADDRESS. RECEIVERS WERE OPERABOct 21, 1998 · N405US · Boeing 737401 · Nose/Tail Landing Gear Strut/AxleSDR USAA980562Stringer · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 1 INCH AREA OF CORROSION STATION 927 STRINGER 20R. CORROSION TASK NR C53-202-01. INSTALLED SPLICE PER BOEING 737-400 SRM 53-00-03 FIG 201 AND SRM 53-00-07 FIG 205. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Main, Longeron/StringerSDR USAA980561Frame · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1 INCH AREA OF CORROSION STATION 927 BETWEEN STRINGER 22R AND 21R ON FRAME. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER BOEING 737-400 SRM 51-70-11. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA980560Clip · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION STATION 927 STRINGER 21R TIE CLIP. CORROSION TASK NR C53-202-02. REPLACED WITH IDENTICAL PARTS PER BOEING 737-400 SRM 51-10-02. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA980559Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREA OF CORROSION STATION 986.5 LBL 65 RBL 65 WL 208 FLOORBEAM INST. CORROSION TASK NC C53-107-02. SPLICED IN REPAIR 'T' CAP PER TR 53-60-01. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980558Sill · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 2 INCH BY 2 INCH AREAS OF CORROSION BETWEEN STATION 947 AND 987 LBL 65 WL 208 SILL INST AFT ENTRY DOOR. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER BOEING 737-400 SRM 51-40-00 AND 51-10-02. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA980557Floorbeam · corrodedCLT - DURING Q2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREAS OF CORROSION STATION 967 BETWEEN LBL 20 AND RBL 30 WL 208 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER BOEING 737-400 SRM 53-30-51. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980556Floorbeam · corrodedCLT - DURING Q2 CHECK, VISUAL INSPECTION FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT STATION 947.5 BETWEEN LBL 20 AND RBL 20, WL 208. DEFECTIVE PART FLOORBEAM. CORROSION TASK NR C53-107-02. SPLICED IN REPAIR 'T' CAP PER T/R 53-60-02. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980555Sill · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 AREAS OF CORROSION 2 INCHES BY 3 INCHES BETWEEN STATION 947 AND 987 RBL 65 SILL INST GALLEY DOOR. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART PER BOEING 737-400 SRM 51-40-00 AND 51-10-02. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA980522Floorbeam · corrodedCLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 52 INCH ACROSS FLOORBEAM EACH SCREW HOLE 1 INCH BY 2 INCH AREA OF CORROSION STATION 294.5, LBL 7 RBL 45 FLOORBEAM UPPER CHORD. CORROSION TASK NR C 53-107-02. BURNISHED FLOORBEAM EXCEPT AT STATION LBL 7, REPAIOct 21, 1998 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980521Seat Track · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 328 TO 336 RBL 22. CORROSION TASK NR C 53-107-02. INSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M)Oct 21, 1998 · N406US · Boeing 737401 · Fuselage, Seat/Cargo Attach FittingsSDR USAASB98262Charger Assy · failedALB - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR, FORWARD AND AFT EMERGENCY EVACUATION LIGHTS INOP ALONG WITH THE RIGHT AFT SERVICE DOOR SLIDE EVACUATION LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY FOR THE LEFT AFT ENTRY DOOR, FORWARD ANDOct 7, 1998 · N417US · Boeing 737401 · Emergency LightingSDR USAASB98303Battery Pack · dischargedIAH - MAINTENANCE FOUND THE AFT LEFT SERVICE DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Oct 5, 1998 · N408US · Boeing 737401 · Emergency LightingSDR USAASB98257Panel · leakingPBI - FLT 1908 - FLT WAS DELAYED FOR 4 HOURS IN MIA FOR FUEL LEAK REPAIR. AFTER TAKEOFF FROM MIA, F/A NOTICED FUEL LEAKING FROM LEFT WING AND SPRAYING OFF THE TRAILING EDGE. CAPT WAS NOTIFIED AND SENT F/O BACK TO ACCOMPLISH A VISUAL CHECK. FUEL LEAK WAS REPSep 29, 1998 · N411US · Boeing 737401 · Wing, Plate/SkinSDR USAASB98255Radar Unit · failedCLT - FLT 401 - EN ROUTE FROM LGA TO TPA, THE AIRCRAFT WEATHER RADAR BEGAN SPIKING IN VARIOUS QUADRANTS AT VARIOUS TIMES IN ALL RANGES BETWEEN 20-320 MILES. ADJUSTED GAIN FROM MINIMUM TO MAXIUM WITH NO IMPROVEMENT NOTED. RADAR GIVES UNRELIABLE PRESENTATION. Sep 25, 1998 · N405US · Boeing 737401 · Weather Radar SystemSDR USAASB98253Overheat Loop · failedCLT - FLT 835 - DURING CLIMB-OUT FROM CLT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER ACCOMPLISHING APPROPRIATE CHECKLIST, LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE ENGISep 24, 1998 · N407US · Boeing 737401 · Overheat DetectionSDR USAASB98245Acm · overservicedDCA - FLT 1488 - CREW REPORTED A STRONG OIL TYPE ODOR IN CABIN AT FL280 WHEN USING THE RIGHT PACK. WHEN CREW TURNED OFF RIGHT PACK, ODOR DISSIPATED. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE OVERSERVICED. DRAISep 18, 1998 · N406US · Boeing 737401 · Cabin Cooling SystemSDR USAASB98242Charger · failedALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD FIRST CLASS SEATS (ROWS 1 AND 2) AND ABOVE THE FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M)Sep 15, 1998 · N425US · Boeing 737401 · Emergency LightingSDR 98ZZZM730Battery · dischargedALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD FIRST CLASS SEATS (ROWS 1 AND 2) AND ABOVE THE FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M)Sep 15, 1998 · N425US · Boeing 737401 · Emergency LightingSDR USAASB98223Switch · out of adjustSDF - FLT 1732 - DURING CLIMB-OUT, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. CAPTAIN DECIDED TO RETURN TO FIELD AT SDF TO VERIFY SECURITY OF THE CARGO DOOR. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. CAPTAIN NOTED THAT ON LANDING, TAug 30, 1998 · N418US · Boeing 737401 · Door Warning SystemSDR USAA980358Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A SMALL CRACK .25 INCH AT RIVET HOLE FUSELAGE FRAME 500A BETWEEN S8L AND S9L. CUT OUT DAMAGE FILL AND DOUBLER PER SRM 53-00-07 FIG 202. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA980357Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AROUND CLIP NUT HOLE .5 INCH BY .5 INCH STATION 328 FLOORBEAM UPPER CHORD BL0. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51 FIG 206. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980356Floorbeam · corrodedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON STATION 967 LBBL 5-0 FLOORBEAM. CORROSION TASK NR C53-107-02. REPAIRED ONE FLANGE UPPER CHORD PER SRM 53-00-51 FIG 203. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980355Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH AREA OF CORROSION AROUND NUTPLATE HOLES STATION 312 LBL 12 TO RBL 12 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN A NEW 'T' CAP SECTION PER SRM 53-10-51. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA980354Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727G BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA980353Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727E BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA980352Frame · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 787 BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA980351Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 867 BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA980350Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 827 BETWEEN S8R AND S9R ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAA980348Frame · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND A SMALL CRACK .250 INCH AT RIVET HOLE FUSELAGE FRAME 380 BETWEEN S8L AND S9L. CUT OUT DAMAGED AREA AND REPAIRED WITH FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (X)Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, FrameSDR USAASB98204Oil Cooler · failedBNA - FLT 1514 - EN ROUTE FROM CLT-MCI, CAPT NOTICED THE NR 1 ENGINE CSD OIL TEMPERATURE READ HIGH AT 160 DEGREES. IMMEDIATELY THEREAFTER, THE OVERHEAT LIGHT ILLUMINATED. CREW DISCONNECTED THE CSD THEN TRIED TO BRING APU ON LINE AT FL350 BUT WAS UNABLE. TRIAug 9, 1998 · N417US · Boeing 737401 · Alternator-Generator DriveSDR USAA980298Skin · crackedCLT - DURING A DROP IN CHECK VISUAL INSPECTION, FOUND A 3.5 INCH CRACK RIGHT HORIZ STABILIZER 120-123, 2 INCHES FORWARD OF REAR SPAR, LOWER IN SPAR SKIN. INSTALLED DOUBLER PER T/P 55-10-07, EA 62085. (M)Jul 16, 1998 · N420US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAASB98184Power Supply · failedCLE - MAINTENANCE FOUND THE EMERGENCY LIGHT POWER SUPPLY AT STATION 753L WILL NOT HOLD A CHARGE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT STATION 753L. OPERATIONAL CHECK NORMALJul 15, 1998 · N423US · Boeing 737401 · Emergency LightingSDR USAASB98164Turbine · failedFLL - FLT 1638 - AFTER TAKEOFF AT 800 FT, THE NR 1 ENGINE EXPERIENCED A TURBINE FAILURE. CREW SHUT DOWN THE NR 1 ENGINE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT FLL WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 17 MIJun 30, 1998 · N404US · Boeing 737401 · Turbine Section
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