Boeing 737-200

Service difficulty reports · 86

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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 = '737200'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2023F00313Skin · dentedCUTOUT OIL CANNED AREA (1.25" DIAMETER) ON L/H AFT FUSELAGE SKIN EXTERIOR BETWEEN FS 967 AND FS 986.5 AND STR 24L AND STR 25L IAW AERO DESIGN SERVICES EO #ADS-N467TW-01 REVISION IR DATED 02/OCT/2023. ACCOMPLISHED HFEC NDT INSPECTION AROUND CUTOUT AREA WITH NO Oct 13, 2023 · N467TW · Boeing 737200 · Fuselage Main, Plate/SkinSDR SWAA20211102None · bentTHIS IS A TEST.Nov 1, 2021 · N12345 · Boeing 737200 · Standard Practices/StructuresSDR 2DYA202108270001Window · crackedAIRCRAFT WAS FLYING FROM KSJT TO KVBG WHEN THE FLIGHT CREW WAS ISEEN CRACK DEVELOPING IN THE R1 FLIGHT DECK WINDOW WHILE IN CRUISE FLIGHT. THE CAPTAIN ELECTED TO DIVERT INTO KLAX AS A PRECAUTIONARY, THE LANDING WAS UNEVENTFUL.Jun 20, 2021 · N605KW · Boeing 737200 · Flight Compartment WindowsSDR FY4Y202110002None · corrodedCORROSION FOUND AT LH WING REAR SPAR LOWER CHORD UPPER HORIZONTAL FLANGE WBL 162Jun 10, 2021 · N737CS · Boeing 737200 · Wing Main, Frame StructureSDR FY4Y202110001Beam · crackedLONGITUDINAL FLOOR LONGITUDINAL FLOOR BEAM FOUND TWO CRACKS BETWEEN BS705 AND 715 RBL 24.82, CRACKS SIZE 3.0 INCH AND 1.5 INCH IN AREA.May 4, 2021 · N737CS · Boeing 737200 · Fuselage Main, StructureSDR FY4Y202110004Battery · noneELT BATTERY TIME DUE ON 2021/JULY. NRC:CA1251-01-015May 3, 2021 · N737CS · Boeing 737200 · Emergency EquipmentSDR FY4Y202110003Battery · weakEMER EXIT LIGHT BATTERY WEAK ON MAIN ENTRY DOOR UP SIDE. NRC:CA1251-01-014May 3, 2021 · N737CS · Boeing 737200 · Emergency LightingSDR CA190510001Roller · broken(CAN) DURING AIRCRAFT WALK AROUND A ROLLER WAS FOUND BROKEN ON THE #1 FLAP TRACK CARRIAGE ASSY. FLAP SYSTEM WAS INSPECTED, ROLLER WAS REPLACED AND NO OTHER DAMAGE WERE FOUND. NO CAUSE FOR THE FAILURE WAS FOUND, THE FLAP SYSTEM WAS RIG PROPERLY. (TC# 2019051000May 5, 2019 · Boeing 737200 · Trailing Edge FlapsSDR CA190221011Tube · chafed(CAN) ENGINE OIL CONSUMPTION ABNORMAL (CONSUMPTION INCREASING). CAUSE: #6 BEARING PRESSURE TUBE P/N 761392 CHAFFED. RECTIFICATION: #6 BEARING TUBE P/N 761392 REPLACED (TC# 20190221011)Feb 21, 2019 · Boeing 737200 · Engine (Turbine/Turboprop)SDR CA190314019Mau · inoperative(CAN) MODULAR ACQUISITION UNIT (MAU), FAILED AND CAUSED THE FLAP ASSYMETRY INDICATION TO COME ON IN THE COCKPIT, THE CREW REACTED BY RETURNING TO THE AIRPORT. THE AIRCRAFT AT 14000 FT IN A CLIMB. THE TROUBLESHOOTING THAT FOLLOWED RESULTED IN DETERMINING THAT Feb 14, 2019 · Boeing 737200 · Flight Control SystemSDR CA190115015Plug · dislodged(CAN) APU OVERSPEED LIGHT ILLUMINATED DURING APU START. THE MAINTENANCE INVESTIGATION FOUND A BORESCOPE PLUG WAS FOUND IN THE APU BAY, NO LONGER INSTALLED IN THE APU WHICH CAUSED A BLEED AIR LEAK.Jan 15, 2019 · Boeing 737200 · APU Core EngineSDR EE4Y201808137049Skin · crackedDURING A STRUCTURE INSPECTION, FOUND A CRACK IN THE UPPER FUSELAGE BS 727B+8.5, STRINGER 16R AT UPPER CHEM-MILLED AREA. REPAIRED THE DAMAGED AREA IAW SRM 53-30-3, FIGURE 48, DETAIL VII.Aug 13, 2018 · Boeing 737200 · Fuselage Main, Plate/SkinSDR EE4Y201813087048Skin · crackedDURING A STRUCTURE INSPECTION, FOUND A CRACK IN THE LOWER SKIN BS 1013, STRINGER 21R AT LOWER CHEM-MILLED STEP AREA. REPAIRED THE DAMAGE AREA IAW SRM 53-30-3.Aug 13, 2018 · Boeing 737200 · Fuselage Main, Plate/SkinSDR CA151218005Wire · burned(CAN) FOUND LT WING ANTI-ICE VALVE OPEN WHEN ACFT WAS ON THE GROUND. FAULT WAS FOUND TO BE BURNED WIRING CAUSING THE VALVE TO OPEN AND THE CIRCUIT BREAKER TO OPEN ALONG WITH LT OTBD LANDING LIGHT CIRCUIT BREAKER TO OPEN. DAMAGED WIRING REPLACED AND ALL SYSTEMDec 16, 2015 · Boeing 737200 · Ice/Rain Protection System WiringSDR CA151007024Hose · leaking(CAN) AIRCRAFT TOOK OFF AND HAD TO RETURN WHEN THEY DECLARED HAVING A HYDRAULIC PROBLEM IN CLIMB. UPON RETURN, HYDRAULIC LINE ON THE AILERON PCU HYDRAULIC B SYS IN THE LT WHEEL WELLWAS FOUND LEAKING UNDER THE ATTACH FITTING. UNABLE TO SEE DAMAGE OR LEAK BY GOct 5, 2015 · Boeing 737200 · Hydraulic System, MainSDR CA150902004Switch · stuck(CAN) SWITCH GETS STUCK TO THE ARMED POSITION AND UNABLE TO MOVE IT.Aug 26, 2015 · Boeing 737200 · Emergency Locator BeaconSDR CA150729007Indicator · failed(CAN) DURING APPROACH THE CREW SELECTED FLAPS 1 POSITION. THE L/E FLAPS LOWERED TO THE EXTEND POSITION, BUT THE TRAILING FLAPS DIDN`T MOVE. THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO MOVEMENT. THE CREW THEN SELECTED ALTERNATE EXTENSION OF THE FLAPS WITH THE SJul 23, 2015 · Boeing 737200 · Trailing Flap Position Indicating SystemSDR CA140224017Oil System · bypassing(CAN) WITH POWER LEVERS ADVANCED FOR TAKEOFF, AN INDICATION OF AN IMPENDING "OIL FILTER BYPASS" LIGHT ON NR 1 ENGINE HAD OCCURRED. POWER LEVERS RETARDED AND ACFT RETURNED TO THE RAMP. THE NR 1 ENGINE OIL FILTER WAS REMOVED AND INSPECTED. FILTER INSPECTION IFeb 21, 2014 · Boeing 737200 · Turbine Engine Oil SystemSDR CA140110005Wire · shorted(CAN) THE POSITIVE WIRE FROM THE BATTERY PACK IN THE AFT CARGO PIT SHORTED AGAINST THE BATTERY MOUNT BRACKET ON THE LID OF THE BATTERY HOLDER ASSEMBLY. THE BATTERY SHORTED ONCE THE LID WAS MOUNTED TO THE BOX, THE BATTERY OVERHEATED & STARTED TO EMIT SMOKE. TDec 16, 2013 · Boeing 737200 · Light System WiringSDR CA130702001Power Lever · obstructed(CAN) UNABLE TO REACH TAKEOFF EPR ON NR 2 ENGINE DURING TRIM RUNS AFTER FCU REPLACEMENT DIFFERENT READING WERE OBSERVED WITH COWLING OPEN VERSUS COWLING CLOSED. AFTER TROUBLESHOOTING FCU POWER LEVER FOUND INTERFERING WITH COWLING.Jun 27, 2013 · Boeing 737200 · Power LeverSDR CA120906004Actuator · cracked(CAN) AFTER LANDING, CREW WAS TAXING TO THE GATE, THE CREW NOTICED THE STEERING AS NOT RESPONSIVE. THE ACFT WAS STOPPED AND IT WAS DISCOVERED TO HAVE A PUDDLE OF HYDRAULIC FLUID UNDER THE L/T WING. INSPECTION REVEALED THAT THE LT OTBD SPOILER ACTUATOR WAS CRASep 5, 2012 · Boeing 737200 · Drag Control ActuatorSDR SWAA2012030501932Lock · looseL1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOCK LOOSE. SECURED LOCK PER MM.Mar 2, 2012 · N891AT · Boeing 737200 · Emergency EquipmentSDR 2011F00131Structure · crackedDURING NDT INSPECTION AT BS 291.5 ON SR 16, RT FORWARD GALLEY AREA FOUND CRACKED.Jun 1, 2011 · Boeing 737200 · Fuselage Structure (General)SDR CA101117002Fire Loop · shorted(CAN) SHORTLY AFTER TAKEOFF THE FLIGHT CREW REPORTED AN OVERHEAT WARNING ON THE #2 ENGINE. THE ENGINE WAS SHUTDOWN AS PER STANDARD OPERATING PROCEDURE AND FIRE EXTINGUISHERS WERE ACTIVATED. MAINTENANCE CREW DETERMINED THE LOWER FIRE DETECTION LOOP HAD AN INTERNov 15, 2010 · Boeing 737200 · Fire DetectionSDR 2011F00133Autopilot Sys · inoperativeDURING INSPECTION AUTOPILOT B WAS FOUND NOT ENGAGING IN ANY MODE. ALL RELEVANT LRU'S REPLACED BUT DEFECT PERSISTED.Jun 26, 2010 · Boeing 737200 · Autopilot SystemSDR 2011F00132Structure · dentedDURING INSPECTION A VERTICAL DENT 7.O"X2.5" WAS OBSERVED ON LT SIDE IN THE AREA DEFINED FOR RVSM BS259.5, WL 194.Apr 12, 2010 · Boeing 737200 · Fuselage Structure (General)SDR CA100121008Bellcrank · broken(CAN) DURING OPENING OF THE MAIN CARGO DOOR, THE FWD CLEVIS ON THE BELLCRANK ASSY WAS FOUND FRACTURED.Jan 20, 2010 · Boeing 737200 · Cargo/Baggage DoorsSDR EE4Y090207Skin · crackedUPPER FUSELAGE AT BS 843 STR 11 LT EXTERNAL SKIN WITH CRACK.Jul 30, 2009 · N472BC · Boeing 737200 · Fuselage Main, Plate/SkinSDR EE4Y090205Doubler · corrodedLOWER FUSELAGE, POTABLE WATER SERVICE PANEL CUT OUT INTERNAL DOUBLER WITH CORROSION.Jul 30, 2009 · N472BC · Boeing 737200 · Fuselage Main, Plate/SkinSDR EE4Y090206Skin · crackedUPPER FUSELAGE AT B/S 375, BETWEEN STR. 12L AND 13L, EXTERNAL SKIN WITH CRACK.Jul 30, 2009 · N472BC · Boeing 737200 · Fuselage Main, Plate/SkinSDR EE4Y090195Bear Strap · crackedFORWARD ENTRY DOOR UPPER HINGE CUTOUT BEAR STRAP CRACKED.Jul 29, 2009 · N472BC · Boeing 737200 · Fuselage Main, Plate/SkinSDR CA090618008Angle · broken(CAN) ON ARRIVAL, BLOW-OUT PANEL NR 3302L WAS FOUND OPEN. THIS PANEL PROVIDES ACCESS TO THE RAM AIR DUCT. INSP OF AREA FOUND ANGLE PN 65-49573-23 BROKEN. THIS ALLOWED RAM AIR TO LEAK INTO THE PANEL AREA AND CAUSE PANEL NR 3302L TO BLOW OPEN.Jun 15, 2009 · Boeing 737200 · Nacelle/Pylon Miscellaneous StructureSDR NACA20090002Stringer Splice · crackedCRACK AT STA 907, STR 4R STRINGER SPLICE. REMOVED AND REPLACED CRACKED STRINGER SPLICE AT STA 907 STR 4R IAW SRM 51-10-01 SECTION 7, FASTENERS INSTALLED IAW 51-30-2.Feb 25, 2009 · N321DL · Boeing 737200 · Fuselage Main, Longeron/StringerSDR CA090204008Landing Gear · malfunctionedDEPARTING YFB FOR YOW ON JAN 31, 2009, THE CREW OBSERVED A NOSE LANDING GEAR FAIL TO LOCK CONDITION AFTER GEAR WAS SELECTED UP. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE SERVICED THE NOSE GEAR AND THE AIRCRAFTJan 31, 2009 · Boeing 737200 · Nose/Tail Landing GearSDR CA080225014Clutch · disengagedDEPARTING YOW THE AIRCRAFT EXHIBITED AN UNCOMMANDED ROLL TO THE LEFT REQUIRING 2-3 UNITS OF RUDDER TRIM TO CORRECT. THE CREW OBSERVED NO ASSYMMETRY INDICATION IN THE FLIGHT DECK BUT IT WAS VISUALLY CONFIRMED THAT THE RIGHT INBOARD AFT FLAP WAS PARTIALLY EXTENFeb 22, 2008 · Boeing 737200 · Trailing Edge Flap Control SystemSDR CA061117005Support · cracked(CAN) ON WALK AROUND AFTER LANDING FOUND CENTER SUPPORT ASSY OF GRAVEL DEFLECTOR CRACKED. CENTER SUPPORT ASSY CRACK REPAIRED. ASSEMBLY SUPPORT FITTING P/N69-60100-2 REPLACED AIRCRAFT RETURNED TO SERVICE.Nov 6, 2006 · Boeing 737200 · Nose/Tail Landing GearSDR ASAA0610886Glowstrip · detachedDURING DEPLANING EMERGENCY PHOTOLUMINSCENT LIGHT STRIP IN AFT CABIN DETACHED FROM FLOOR. REPLACED SECTION OF PHOTOLUMINSCENT LIGHT STRIP IN FIXED PORTION OF AFT CABIN.Aug 14, 2006 · N747AS · Boeing 737200 · Emergency EquipmentSDR TSAA0627047Packing · damagedNON ETOPS FLT 208 LIH-HNL. DURING CLIMB OUT OF LIH, CREW NOTED HYDRAULIC QUANTITY DROP TO ZERO. CREW COMPLETED CHECKLIST PROCEDURES AND LANDED HNL WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED TO MAINTENANCE. MAINTENANCE FOUND A PACKING ON THE NR 4 SPOILER Jun 14, 2006 · N828AL · Boeing 737200 · Drag Control ActuatorSDR AU510002186Tee Fitting · crackedAIRSPEED SWITCH PITOT TEE FITTING CRACKED AND LEAKING ON SMALL DIAMETER END.Dec 12, 2005 · Boeing 737200 · Pitot/Static SystemSDR AU510002044Pipe · leakingHYDRAULIC PIPE LOCATED IN NR 2 ENGINE NACELLE LEAKING.Dec 12, 2005 · Boeing 737200 · Hydraulic System, MainSDR AU510002215Actuator · leakingACTUATOR LOCATED IN LT WING LEAKING. LIMITED INFORMATION PROVIDED.Feb 12, 2005 · Boeing 737200 · Flight Control SystemSDR CA050211007Apu · fire(CAN) ENCOURTERED AN APU FIRE. FIRE DID NOT INITIATE A FIRE WARNING. FIRE BELIEVED TO BE INITIATED BY CRACK IN APU PLENUM. CRACK IN TURN CAUSED HOT COMPRESSOR DISCHARGE AIR TO AFFECT FUEL HEATER & CHECK VALVE CAUSING AN O-RING TO LEAK. ALLOWING FUEL TO STAFeb 4, 2005 · Boeing 737200 · APU Engine Fuel and ControlSDR CA050119011Window · cracked(CAN) RT WINDOW NR 4 PANE CRACKED, APPEARS TO BE OUTER PANE. AIRCRAFT RETURNED TO BASE. WINDOW REPLACED, AIRCRAFT RETURNED TO SERVICE.Jan 16, 2005 · Boeing 737200 · Passenger Compartment WindowsSDR CA041110001Proximity Sensor · failed(CAN) UPON SELECTION OF FLAPS 15 ON LANDING CHECKLIST THE L/E FLAP TRANSIT REMAINED ILLUMINATED AND THE NR 4 SLAT INDICATOR WAS SHOWING IN TRANSIT. REPLACED AND ADJUSTED NR 4 SLAT PROX SENSOR IAW MM 27-88-11. NR 4 SLAT FOUND DENTED ON UPPER SURFACE, REPLACED Nov 8, 2004 · Boeing 737200 · Leading Edge Slat Position Indicating SystemSDR ASAA0410371Cowling · wornFOUND NR 2 ENGINE NOSE COWL AFT LIP REPAIR WORN/DENTED. REMOVED AND REPLACED LOWER AFT CAP. (M)Aug 13, 2004 · N746AS · Boeing 737200 · Engine Air Intake SystemSDR ASAA0410372Web · damagedFOUND AFT WEB SECTION DAMAGED. REPLACED WEB. (M)Aug 13, 2004 · N746AS · Boeing 737200 · Fuselage Miscellaneous StructureSDR ASAA0410369Stringer · chafedPAE - FOUND CHAFED STRINGER. REMOVED AND REPLACED CHAFED STRINGER. (M)Aug 13, 2004 · N746AS · Boeing 737200 · Fuselage Main, Longeron/StringerSDR CA040412005Pitot Line · leaking(CAN) B737-200 PITOT TUBE ASSEMBLY FAILED BENCH CHECK WITH A PITOT LEAK IN EXCESS OF 10 KTS/MIN. THE LEAK WAS DETERMINED TO BE ORIGINATING WHERE THE PITOT TUBE AIRFRAME ATTACHMENT CONNECTS TO THE BASE OF THE PITOT TUBE ASSEMBLY. THE COMPONENT WAS A USED PARTApr 8, 2004 · Boeing 737200 · Pitot/Static SystemSDR CA040412003Pitot Line · leaking(CAN) B737-200 PITOT TUBE ASSEMBLY FAILED BENCH CHECK WITH A PITOT LEAK IN EXCESS OF 350 KTS/MIN. THE LEAK WAS DETERMINED TO BE ORIGINATING WHERE THE PITOT TUBE AIRFRAME ATTACHMENT CONNECTS TO THE BASE OF THE PITOT TUBE ASSEMBLY. THE COMPONENT WAS A USED PARApr 8, 2004 · Boeing 737200 · Pitot/Static SystemSDR CA040412002Pitot Line · leaking(CAN) B737-200 PITOT TUBE ASSEMBLY FAILED BENCH CHECK WITH A PITOT LEAK IN EXCESS OF 350 KTS/MIN. THE LEAK WAS DETERMINED TO BE ORIGINATING WHERE THE PITOT TUBE AIRFRAME ATTACHMENT CONNECTS TO THE BASE OF THE PITOT TUBE ASSEMBLY. THE COMPONENT WAS A USED PARApr 6, 2004 · Boeing 737200 · Pitot/Static System
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