Boeing 737-201

Service difficulty reports · 2,471

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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 = '737201'
  ORDER BY difficulty_date DESC"

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SDR CA101118008Dome · stripped(CAN) DURING TAKEOFF ROLL AT APPROX 80 KNOTS, ENGINE NR 2 NOSE DOME FELL OFF IN THE ENGINE INLET. THIS CAUSED THE ENGINE TO STALL (LOUD BANGS). THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE 4 STUDS THANov 12, 2010 · Boeing 737201 · Engine Air Intake SystemSDR CA101012011Overheat Loop · false indicationIN CRUISE FLIGHT, APROX. AT FL340, LT WING BODY OVERHEAT LIGHT ILLUMINATED. NON NORMAL CHECKLIST WAS COMPLETED AND LIGHT REMAINED ON. CREW DECLARED AN EMERGENCY AND ACFT DIVERTED. ONCE ON FINAL APPROACH, LIGHT WENT OUT AND REMAINED OUT. NORMAL LANDING WAS CAOct 6, 2010 · Boeing 737201 · Overheat DetectionSDR CA081217001Compressor · fod(CAN) AIRCRAFT WAS ON TAKEOFF ROLL WHEN THE PILOTS HEARD A LOUD BANG FROM ENGINE NR 2 & EXPERIENCED A YAW TO THE RIGHT AS THEY APPROACHED 110 KNOTS. THE PILOTS THROTTLED BACK, ABORTED THE TAKEOFF, TAXIED BACK TO THE RAMP AND SHUTDOWN THE ENGINES. PASSENGERSDec 13, 2008 · Boeing 737201 · Turbine Engine Compressor SectionSDR CA081030003Transmitter · failed(CAN) DURING FINAL APPROACH, WHEN THE PILOTS SELECTED FLAPS 25, THE FLAPS STOPPED SLIGHTLY PAST FLAPS 15. THE PILOTS SELECTED FLAPS UP AND OVERSHOT THE APPROACH. THE FLAPS RETRACTED OK. ON THE NEXT APPROACH, THE FLAPS OPERATED NORMALLY. MX INSPECTED AND OPERATOct 16, 2008 · Boeing 737201 · Trailing Flap Position Indicating SystemSDR 2011F00136Apu · misoverhauledNEWLY O/H APU WAS REMOVED AFTER 155 FHRS DUE TO ABNORMAL NOISE & SEVERE VIBRATION. APU WAS REPAIRED FROM APS AND INSTALLED ON ANOTHER ACFT AND AGAIN IT WAS REMOVED AFTER 178 FHRS DUE TO ABNORMAL NOISE, HEAVY SURGE & INTERNAL OIL LEAK. AGAIN IT WAS REPAIRED AJun 24, 2008 · Boeing 737201 · APU Core EngineSDR SROM200700005Casting · brokenDURING TAKEOFF, AT APPROXIMATELY 300 FEET, CREW EXPERIENCED NR 2 ENGINE COMPRESSOR STALL WITH RAPIDLY RISING EGT. SHUTDOWN NR 2 ENGINE AND MADE UNEVENTFUL LANDING AT DEPARTURE AIRPORT. INSPECTION REVEALED THE NOSE DOME HAD SEPARATED FROM ITS MOUNT DAMAGING THEJul 31, 2007 · N245US · Boeing 737201 · Turbine Engine Air Inlet SectionSDR CA070504010Switch · intermittent(CAN) ON FINAL APPROACH, THE FLIGHT CREW SELECTED LANDING GEAR DOWN. THE LAND GEAR INDICATORS ILLUMINATED 3 GREEN AND 3 RED. THIS INDICATED A DISAGREEMENT BETWEEN LANDING GEAR HANDLE POSITION AND LANDING GEAR POSITION. THE FLIGHT CREW SELECTED GEAR UP AND ABORMay 2, 2007 · Boeing 737201 · Landing Gear SelectorSDR USAA070128Skin · delaminatedNR 9 SLAT, WEDGE UPPER SURFACE OSS 643.74-648.74 DELAMINATED. CUT OUT DELAMINATED SKIN, BONDED REPAIR DOUBLER PER SRM 51-70-10, PAR 20, DEFECT SIZE: 2.5L X 1.5W INCHES.Feb 26, 2007 · N246AY · Boeing 737201 · Leading Edge DevicesSDR USAA070127Skin · delaminatedNR 8 SLAT, WEDGE UPPER SURFACE OSS 319.71-324.71 DELAMINATED. CUT OUT DELAMINATED SKIN, BONDED REPAIR DOUBLER PER SRM 51-70-10, PARA 20, DEFECT SIZE: 1 INCH DIA.Feb 26, 2007 · N246AY · Boeing 737201 · Leading Edge DevicesSDR USAA070107Skin · delaminatedTHREE AREAS, 7 INCHES DIA DELAMINATED, NR 10 SLAT, UPPER SURFACE, 0SS 798.74-815.74. CUT OUT DELAMINATION, BONDED REPAIR DOUBLER PER SRM 51-20-10, 57-43-02, DEFECT SIZE: 7 INCHES DIA.Feb 15, 2007 · N246US · Boeing 737201 · Leading Edge DevicesSDR SROM200700001Duct · rupturedUPON TAKEOFF A POP WAS WAS HEARD FOLLOWED BY PERCEIVED SMOKE (DUST) IN THE CABIN. PACS WERE SELECTED TO OFF AND A IMMEDIATE LANDING MADE AT THE DEPARTURE AIRPORT. ALL COCKPIT INDICATIONS NORMAL. FOUND LT AIR CONDITIONING PAC MIXING CHAMBER AND HOT AIR SUPPLJan 5, 2007 · N245US · Boeing 737201 · Air Distribution SystemSDR SROM200600022Carriage · crackedDURING ROUTINE ACCOMPLISHMENT OF ULTRASOUND INSPECTION OF THE SPINDLES ON THE OB FLAPS IAW AD 2003-24-08 FOUND THE RT IB SPINDLE TO SHOW A CRACK INDICATION. LAST ULTRASONIC INSPECTION PERFORMED 46 CYCLES AGO. REPLACED SPINDLE AND CARRIAGE ASSEMBLY WITH NEW PDec 27, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600018Skin · misrepairedDURING OWNER REQUEST FOR REPLACEMENT OF FUSELAGE SKIN BS 907 - 1016, STR 20L - 25L (P/N 65C80736-834) TO ELIMINATE PREVIOUS PERMANENT AND TEMPORARY SKIN REPAIRS, DISCOVERED NON-STANDARD REPAIR AT BS992.80, STR 20L IDENTIFIED AS A CUTOUT IN THE ADJACENT UPPER SNov 30, 2006 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA061363Panel · chafedRIGHT I/B SLAT, 27 - 25 INCHES FROM I/B EDGE OF SLAT CHAFED. REMOVED DAMAGED SECTION AND REPLACED PER TYP REP 57-50-01 REV A, PART B, DEFECT SIZE: 1.250"L X .625"W X 0"D.Nov 29, 2006 · N253AU · Boeing 737201 · Leading Edge DevicesSDR USAA061366Frame · crackedRIGHT LBG W/W, WING TRAILING EDGE LWR SURFACE (BELOW TORQUE TUBE) CRACKED. REMOVED FRAME SECTION, SPLICED IN NEW PART PER SRM 51-70-12, 51-40-02, 51-40-05, DEFECT SIZE: .5 INCH.Nov 29, 2006 · N253AU · Boeing 737201 · Wing SparSDR CA061029001Bellcrank · broken(CAN) NR 2 AFT FLAP BELLCRANK WAS FOUND BROKEN WHILE ACCOMPLISHING DAILY CHECK. INVESTIGATION FOUND EXCESSIVE WEAR ON THE NR 2 AFT FLAP BELLCRANK CAM TRACK WHICH RESULTED IN THE BELLCRANK POPPING OUT OF THE CAM TRACK. UPON REPLACEMENT OF THE CAM TRACK, IT WAS Oct 17, 2006 · Boeing 737201 · Trailing Edge FlapsSDR USAA060851Angle · corrodedFOUND ANGLE CORRODED STA 727E TO 767. REPLACED TRANSITION ANGLE IAW SRM 51-10-02 LEVEL 1 C53-202-01, DEFECT SIZE: .5" BY .750".Jun 19, 2006 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR CA060609004Anti-Ice Valve · inoperativeIN CLIMB, THE PORT ENGINE COWL ANTI-ICE LITE ILLUMINATED BRIGHT. THE AIRCRAFT RETURNED TO BASE. THE PORT ANTI-ICE VALVE WAS REPLACED, CHECKED SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE.Jun 7, 2006 · Boeing 737201 · Engine Anti-Icing SystemSDR USAA060734Floor Support · corrodedFOUND LBL 33, BETWEEN BS 324-345 CORRODED. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 53-00-51, 51-40-05, 51-40-02, DEFECT SIZE: .3"L BY 1.0" W BY .015"D.May 30, 2006 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR SROM200600015Torque Tube · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND NR 5 FLAP CARRIAGE OUTER TORQUE TUBE TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.May 24, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600013Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP REQUIREMENTS TO TRAILING EDGE FLAP CARRIAGES FOUND NR 5 CARRIAGE, INBD CARRIAGE HALF CORRODED. LEVEL 2. REMOVED AND REPLACED WITH SERVICEABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.May 24, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600016Torque Tube · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING 10 YEAR CPCP INSPECTION REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 5 CARRIAGE INNER TORQUE TUBE TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICEABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCE.May 24, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600014Carriage · corrodedDURING HEAVY MAINTENANCE INSPECTION WHILE PERFORMING 10 YEAR CPCP INSPECTION REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 5 CARRIAGE OTBD CARRIAGE HALF TO BE CORRODED. LEVEL 2. REPLACED WITH SERVICABLE UNIT V/S REPAIR FOR CUSTOMER CONVENIENCMay 24, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600010Case · crackedDURING HEAVY MAINTENANCE INSPECTION FOUND CRACKED OUT SECTION IN REAR EXHAUST CASE OF NR 2 ENGINE. REPLACED WITH OVERHAULED UNIT.May 23, 2006 · N245US · Boeing 737201 · Turbine SectionSDR SROM200600009Skin · dentedDURING HEAVY CHECK INSPECTION DISCOVERED 9 CREASE/DENTS ON EXTERIOR SKIN AT STA 305 - 372, STR 23R - STR 24R. REPAIRED EXTERIOR SKIN IAW B 737 SRM FIGURE 48, DETAIL XXIX AND XIX.May 17, 2006 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR SROM200600008Bolt · crackedDURING INSPECTION REQUIREMENTS OF AD2005-20-39, SB737-32A1367 FOUND LT MLG TEE BOLT, P/N 65-46140-6SPL, S/N XZ865 CRACKED AT RADIUS OF LARGEST BEARING SURFACE CIRCUMFERENCE. UNIT HAD TOTAL HOURS OF 29571, TOTAL CYCLES 22830. LAST OVERHAULED 1998 WITH ACCUMULMay 16, 2006 · N245US · Boeing 737201 · Main Landing GearSDR SRON200600007Skin · misdrilledDURING HEAVY MAINTENANCE INSPECTION FOUND SNOWMAN SHAPED HOLE WITH A SOLID AND CHERRY MAX IN IT AT STA 727A, STR 26L. REPAIR PATCH AND DOUBLER INSTALLED PER BOEING ENGINEERING 1-185416133. FAA FORM 8109-9.0May 16, 2006 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR SROM200600012Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING CPCP 10 YEAR REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 3 TRAILING EDGE FLAP CARRIAGE IB CARRIAGE HALF TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED WITH NEW UNIT V/S REPAIR FOR COMPANY CONMay 10, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600011Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING A 10 YEAR CPCP INSPECTION REQUIREMENTS OF THE TRAILING EDGE FLAP CARRIAGES FOUND LEVEL 2 CORROSION ON NR 3 CARRIAGE OB CARRIAGE HALF. REPLACED WITH NEW HALF V/S REPAIR FOR COMPANY CONVENIENCE.May 10, 2006 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200600006Skin · crackedDURING HEAVY MAINTENANCE INSPECTION FOUND SKIN CRACK UNDER RT WING TO BODY FAIRING AT STA 727B, STR 19R. REMOVED EXSISTING ADJACENT PATCH AT STA 727A, STR 18R. INSTALLED PATCH, INCORPORATING OLD REPAIR AND NEW DAMAGE IAW B737 SRM FIG. 48, 55-30-3 AND BOEING May 10, 2006 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR SROM200600005Stringer · corrodedDURING HEAVY MAINTENANCE INSPECTION FOUND CORROSION AT STR 28 LT, STA 1000 TO 1006. CORROSION FOUND TO BE BEYOND LIMITS. STRINGER REPLACED I.A.W. B737 SRM 53-10-2 AND 51-10-1 PG. 9 PARA 7. STRINGER REPLACED STA 986 - 1016 PLUS/MINUS 28". ORIGINAL SPLICE REMay 3, 2006 · N245US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA060359Frame · crackedSTA 807 BETWEEN S8L AND 9L AT OVERHEAD BIN LOWER ATTACH POINT CRACKED. FABRICATED REPAIR PARTS AND INSTALLED IAW TR 53-10-20C, DEFECT SIZE: 1 INCH.Feb 24, 2006 · N223US · Boeing 737201 · Fuselage Main, FrameSDR USAA060351Floor Support · corrodedMAIN DECK, STA 337-365, RBL 60, WL 208 AT 1R DOOR; TASK C53-222-03 CORROSION. FAB'D NEW FLOOR SUPPORT CHANNEL PER SRM 51-40-02, 53-00-51, 51-20-01, 51-21-10, 52-11-25, DEFECT SIZE: 6"L X 2"W X .024"D & 7"L X 2.5"W X .040"D.Feb 22, 2006 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA060252Skin · crackedCRACKS FROM RIVET HOLES AT 4 LOCATIONS ON LOWER TRAILING EDGE OF NR 4 SLAT. SRM 57-43-01-2R6, DEFECT SIZE: .25.Feb 15, 2006 · N257AU · Boeing 737201 · Leading Edge DevicesSDR RYNA200600002Engine · bird ingestionBIRD INGESTION INTO NR 1 ENGINE OCCURRED DURING LANDING, AFTER MAIN WHEELS TOUCHED DOWN AND BEFORE NOSE WHEEL TOUCHED DOWN. THUD WAS HEARD IN COCKPIT. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. UPON INSPECTION FOUND NR 1 ENGINE DAMAGED BEYOND REPAIR Feb 3, 2006 · N225US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA060159Intercostal · crackedFOUND INTERCOSTAL CRACKED, BS 660 S-14L. REMOVED DAMAGE AND ISNTALLED REPAIR PARTS IAW EO 5304R143, DEFECT SIZE: 1".Jan 30, 2006 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA060129Angle · corrodedLEFT Z-ANGLE BETWEEN 312 TO STA 344 CORROSION. REPLACED WITH IDENTICAL PART, NEW Z-ANGLE IAW SRM 51-40-02, DEFECT SIZE: .5 X 2 INCH.Jan 23, 2006 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR RYNA200600001Link · brokenON CLIMB FROM UTA, POP AND VIBRATION WAS HEARD UNDER PILOT SEAT. AIRCRAFT DIVERTED TO MEM, LANDED WITHOUT INCIDENT. GEAR INSPECTED FOR SUSPECTED BIRD STRIKE, NO EVIDENCE OF DAMAGE FOUND. AIRCRAFT DEPARTED MEM, ON CLIMB TWO POPS AND VIBRATION WERE HEARD UNDEJan 10, 2006 · N235US · Boeing 737201 · Landing Gear Door Retract SectionSDR SROM200500017Spindle · crackedDURING ROUTINE NDT INSPECTION OF OB FLAP SPINDLE IAW AD 2003-24-08 AND SB 737-57A1277 FOUND A FLAP CARRIAGE SPINDLE CRACKED 40 PERCENT AT THE RADIUS OF THE YOKE TO THE FIRST BEARING LAND. FLAP CARRIAGE ASSEMBLY REPLACED WITH A NEW UNIT. RECORDS INDICATE 5221 Dec 12, 2005 · N245US · Boeing 737201 · Trailing Edge FlapsSDR SROM200500016Skin · crackedDURING ROUTINE MAINTENANCE FOUND A 3 INCH CRACK IN THE FUSELAGE SKIN AT BS 973, STR 21L. INSTALLED TEMPORARY REPAIR DOUBLER IAW 8110-3 APPROVED REPAIR, REFERENCE DWG 33-05565-1.Dec 12, 2005 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR RYNA200500028Pump · overheatedNR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEATED, RETURNED TO ACY DUE TO DECREASING A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED NR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP, AND SERVICED A-SYSTEM. BOTH SYSTEMS LEAKED AND OPERATIONALLY CHECKED GOOD. REF B737 Aug 29, 2005 · N242US · Boeing 737201 · Hydraulic Pump, AuxiliarySDR SROM200500014Skin · gougedDURING ROUTINE INSPECTION FOUND A GOUGE IN THE SKIN AT BS 1036.5, STR 8L. REPAIRED IAW MFG MESSAGE 1-115922448-4 AND SRM 53-30-3, FIG. 50. BLENDED, REMOVED DAMAGE, EDDY CURRENT INSPECTED FOR CRACKS AND INSTALLED AN EXTERNAL DOUBLER IAW MESSAGE AND SRM REFEREAug 21, 2005 · N245US · Boeing 737201 · Fuselage Main, Plate/SkinSDR RYNA200500026Skin · crackedDURING WALKAROUND AFTER FLIGHT A SKIN CRACK AT BS 727B+18" AND JUST ABOVE STRINGER 16L WAS NOTICED. AIRCRAFT FERRIED TO FLIGHTSTAR FOR REPAIR. COMPLIED WITH FUSELAGE SKIN REPAIR AT BS 727B+18" AT STRINGER 16L PER SRM 53-30-3 FIG DETAIL VII.Aug 17, 2005 · N242US · Boeing 737201 · Fuselage Main, Plate/SkinSDR CA050810001Pitot System · fod(CAN) ON TAKEOFF ROLL, NO AIRSPEED INDICATION ON THE CAPTAINS SIDE. DEBRIS FOUND IN CAPTAINS UPPER LT PITOT TUBE. BUG REMOVED AND PITOT/STATIC SYSTEM TESTED SERVICEABLE. TIMES: 63714:40 CYCLES: 61165.Aug 10, 2005 · Boeing 737201 · Pitot/Static SystemSDR RYNA200500022Oil System · overtempDURING CLIMB-OUT, NR 2 ENGINE OIL TEMP INCREASED TO 122 DEG C. DURING DESCENT, OIL TEMP INCREASED TO 140 DEG C. OIL TEMP IN YELLOW BAND FOR 5 MINUTES. OIL PRESSURE WAS NORMAL IN CLIMB AND CRUISE. NR 2 ENGINE SHUTDOWN AS A PRECAUTION BECAUSE OIL TEMP COULD NOTJul 6, 2005 · N225US · Boeing 737201 · Engine Oil TemperatureSDR RYAN200500020Speed Brake · wornSPEED BRAKE TAKEOFF WARNING SWITCH WORN/BROKEN. SWITCH NOT MAKING CONTACT WHEN SPEED BRAKE ARMED, CAUSING A FALSE TAKEOFF WARNING TO SOUND WHEN THROTTLES ARE ADVANCED.Jul 3, 2005 · N225US · Boeing 737201 · Engine Thrust ReverserSDR RYAN20050018Warning System · activatedDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN NR 1 ENGINE WAS SHUTDOWN.Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil Indicating SystemSDR RYAN200500018Bulb · faultyDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil TemperatureSDR 193Bulb · malfunctionedDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.Jun 12, 2005 · N240AU · Boeing 737201 · Engine Oil TemperatureSDR CA050510006Gcu · shorted(CAN) AFTER STARTING THE NR 1 ENGINE, THE CREW TURNED ON POWER FROM THE NR 1 ENGINE. THEY IMMEDIATELY NOTICED SMOKE COMING FROM THE GCU. THEY TURNED THE POWER OFF AND RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE SWAPPED THE NR 1 GCU WITH THE APU GCU AND CARRMay 9, 2005 · Boeing 737201 · Battery/Charger System
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