Boeing 737-232
Service difficulty reports · 1,700
Newest first. General aviation reporting is voluntary.
Query with SQL
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 = '737232' 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.
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 = '737232' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DL73K010407Controller · failedELECTRIAL CONNECTOR TO RIGHT FWD WINDOW BEGAN SMOKING, TURNED OFF WINDOW HEAT SMOKE STOPPED. / REPLACED R1 WINDOW AND WINDOW HEAT CONTROLLER PER M/M. OPNL TEST OF WINDOW HEAT GOODSDR DL73K010406Skin · crackedFUSELAGE / FS 1138 / STRG. 12R / HORIZ STAB CUTOUT : CRACK REPAIR INSPECTIONS OF THE FUSELAGE STRUCTURE AROUND THE HORIZONTAL STABILIZER CUTOUT PER BAC S/B 737-53-1134 REVEALED A .5 INCH CRACK IN THE SKIN AND UNDERLYING STRINGER STRAP JUST FWD OF FS 1138 AND JSDR DL73K010376Indicator · malfunctionedON GO AROUND FLAPS WOULD NOT RETRACT ABOVE 25 DEGREES NO ASSYMETRY NOTED. CORRECTIVE ACTION: FOUND EXTREME AMT OF ICE ON TE FLAPS DEICED FLAPS AND RAN THRU SEVERAL CYCLES OPS OK VISUAL CK OF FLAPS AND TORQUE TUBES FOUND OK REPLACED FLAP IND PRECAUTION OPSSDR DL73K010377Keelbeam · crackedTHE RT STRINGER 18A SHEAR BEAM WAS FOUND WITH A WEB CRACK AT FS 727. THE CRACK IS TYPICAL OF THOSE FOUND IN BAC S/B 737-53-1066, HOWEVER THE S/B IS NOT EFFECTIVE FOR THIS AIRCRAFT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A STEEL REPAIR CHANNEL PER ER/SDR DL73K010366Door Frame · crackedC2 CARGO DOOR OPENING FORWARD FRAME WAS FOUND TO HAVE CRACKS IN THE UPPER FRAME BETWEEN STR 24R AND 26R. ADDITIONALLY, THE REINFORCEMENT STRAP WAS FOUDN CORRODED BETWEEN STR 24R AND 25R. THE FRAME WAS REPAIRED PER SRM 51-40-3 AND THE DAMAGED SECTION OF SDR DL73K010364Fitting · corrodedTHE LT AND RT HORIZONTAL STABILIZER FITTING ATTACH LUGS WERE FOUND CORRODED. CORROSION WAS REMOVED FROM SEVERAL LUG BORE AND FACES. NEW BUSHINGS WERE INSTALLED. REPAIR WAS ACCOMPLISHED PER ERA 397265-14 AT HMV.SDR DL73K010348Frame · crackedA 2.5 INCH CRACK WAS FOUND IN THE FS 639 FRAME AT STR 16L IN THE INBOARD CHORD AND WEB. A NEW SECTION OF WEB WAS SPLICED IN AND TWO REPAIR ANGLES WERE ADDED TO THE INBOARD CHORD PER ERA 397256-14 AT HMV.SDR DL73K010347Spar · crackedWHILE ACCOMPLISHING INSPECTIONS PER S/B 737-57-1216 SEVERAL CRACKS WERE FOUND IN 9 FASTENER HOLES COMMON TO THE LT MLG BEAM AFT FITTING AND THE REAR SPAR. THE AFT FITTING WAS REPLACED AND THE FASTENER HOLES WERE OVERSIZED PER ERA 397280-14 AT HMV.SDR DL73K010346Fitting · corrodedCORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACH LUGS AND FUSELAGE CLEVIS LUGS. CORROSION WAS FOUND ON VARIOUS LUG BORES AND FACES. THE CORROSION WAS REMOVED AND THE BUSHINGS AND SLEEVES REMANUFACTURED PER ERA 397239-14 AT HMV.SDR DL73K010343Fitting · corrodedCORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS ATTACH LUGS FOR THE HORIZONTAL STABILIZER. THE CORROSION WAS FOUND ON SEVERAL LUG BORES AND FACES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL73K010330Frame · crackedTHE FS 663 FRAME WAS FOUND CRACKED AT STR 1R AND 3R. REPAIRED SIMILIARLY TO SRM 53-10-4, FIG 14. THE SKIN WAS CUT AT EACH LOCATION TO FACILITATE THE REPAIR AT HMV.SDR DL73K010311Light · intermittentON LANDING GEAR EXTENSION, RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. BULB CK WAS GOOD. CYCLED GEAR WITH SAME INDICATION. PUSHED LIGHT ASSY SEVERAL TIMES. THEN RT GEAR LIGHT CAME ON. ALL INDICATIONS GOOD. CONFIRMED GEAR DOWN WITH CONFIG HORN ASDR DL73K010303Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 520 NEAR STRINGER 16L. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM 53-30-3 AND ER/A 380104-14.SDR DL73K010292Fan · faultySMOKE AND FUMES IN COCKPIT DURING PREFLIGHT. FOUND CONTROL CABIN AUGMENTATION FAN PUTTING FUMES INTO COCKPIT. FWD TO MCO AND PLACARD.SDR DL73K010287Warning Light · intermittentCARGO FIRE DET AFT LIGHT ILLUMINATED ERRATICALLY/INTERMITENT. DEFERRED TO MCO AND PLAC PER MEL 26-00-19A.SDR DL73K010230Frame · crackedA CRACK WAS FOUND AT THE LOWER FASTENER ON THE LEFT SIDE OF THE FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM. THE CRACK IS TYPICAL TO THAT SHOWN ON S/B 737-53-1182. THE DAMAGE WAS REPAIRED PER S/B 737-53-1182 AT HMV.SDR DL73K010217Skin · crackedTHE SKIN AND UNDERLYING BEARSTRAP OF THE L2 DOOR CUTOUT WERE FOUND CRACK AT THE LOWER HINGE CUTOUT. CRACK REMOVAL RESULTED IN A 2 INCH X 2 INCH CUTOUT IN SKIN AND BONDED DOUBLER AND A .5 INCH CUTOUT IN THE BEARSTRAP. THE DAMAGE WAS REPAIRED WITH THREE EXTERSDR DL73K010216Skin · crackedA 3 INCH LONG CRACK WAS FOUND IN THE SKIN JUST BELOW STRINGER 18R AT FS 749. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 1 AND ER/A 379971-14, REV A.SDR DL73K010200Skin · crackedFOUND ON T1 LETTER CK, COCKPIT WINDOW POST IS CRACKED AT THE UPPER OUTBD CORNER OF THE CAPTS WINDSHIELD. REPAIRED PER SRM 53-30-3.SDR DL73K010193Power Supply · inoperativeEMERGENCY ESCAPE PATH LIGHTS SEAT ROW 1 TO 4 AND CLOSET LIGHTS INOP. REPLACED BATTERY AND POWER SUPPLY.SDR DL73K010191Skin · crackedTHE KEEL BEAM LOWER SKIN FROM FS 661 TO FS 727 HAS BEEN REPLACED AS A PREVENTATIVE MODIFICATION PER S/B 737-53-1104, REV 4. THIS MODIFICATION WAS DONE AT HMV.SDR DL73K010147Fan · odorDURING LANDING A LINE F/A SMELLED STRONG ODOR IN FWD PORTION OF CABIN. SMELLED LIKE BURNING PLASTIC. RAN BOTH ENGS AND PACKS, NO ODORS NOTED. FWD GASPER FAN TO MCO AND PLAC MEL 21-00-24. DUE TO HISTORY OF C/B POPPING C/B PULLED AND COLLARED E/E COMPTS AND SDR DL73K010134Skin · crackedA .75 INCH CRACK WAS FOUND AT THE L2 DOOR CUTOUT UPPER HINGE. THE CRACK WAS TRIMMED OUT AND DOUBLERS INSTALLED PER ERA 259485-14 AT HMV.SDR DL73K010133Fitting · corrodedCORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AND FUSELAGE LUGS. SOME OF THE BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED PER ERA 396619-14 AT HMV.SDR DL73K010132Fitting · corrodedTHE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS WERE FOUND CORRODED. CORROSION WAS REMOVED FROM SEVERAL BORES AND FACES. THE DAMAGE WAS REPAIRED PER ERA 396666-14 AT HMV.SDR DL73K010131Clip · tool damageTHE STRINGER TO FRAME CLIPS AT FS 380 AND STR 5L AND 5R WERE FOUND DAMAGED AND IN NEED OF REPLACEMENT. THE EXTRUDED CLIPS COULD NOT BE PURCHASED SO THEY WERE MANUFACTURED PER ERA 396674-14 AT HMV. THIS EFFECTS SSI F-36.SDR DL73K010111Control Valve · failedAUTO PRESS MOD FAILED ABOUT 7500 FT. STANDBY ALLOWED, CABIN PRESSURE TO REACH 10,000 FT. A/C AT 25,000 FT SWITCH TO MANUAL A/C. BUT VALVE WERE ALREADY FULL CLOSED. DESCENDED TO 10,000 FT CABIN PRESSURE HELD AT 9,200 FT. EVEN TRIED USING APU BLEED AT 10,SDR DL73K010110Fitting · corrodedCORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS LUGS THAT ATTACH THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED FROM THE LUG BORES AND FACES PER ERA 396637-14 AT HMV.SDR DL73K010109Fitting · corrodedCORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AT THE FRONT SPAR. THE DAMAGE WAS REMOVED AND REPAIRED BY ERA 396636-14 AT HMV.SDR DL73K010108Fitting · corrodedCORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS. THE CORROSION WAS REMOVED AND REPAIRED PER ERA 396651-14 AT HMV.SDR DL73K010092Fitting · corrodedCORROSION WAS FOUND IN THE BORES OF THE LT SIDE STRUT SUPPORT FITTING LOCATED AT FS 685. THE BORE DIAMETER WAS INCREASED TO 2.325 INCHES AND REPAIRED PER ERA 396650-14 AT HMV.SDR DL73S010096Skin · crackedTHE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT AND AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER ARE INSTALLED PER B737 SRM 53-30-3, FIG 24 AND ER/A 379810-14, REV A.SDR DL73K010087Floorbeam · crackedCRACKS WERE FOUND IN THE WEB OF THE LONGITUDINAL FLOORBEAM BETWEEN FS 700 AND 717. THE WEB AND CHORDS WERE INSPECTED AND REPAIRED PER S/B 737-57-1210 AT HMV.SDR DL73K010075Duct · rupturedFLIGHT ATTENDANT HEARD POP IN OVERHEAD NEAR FRONT OF A/C JUST AFTER INITIATION OF T/O POWER. ANOTHER POP AT V1. AFTER T/O SMOKE FILLED CABIN. AFTER DISCOVERY OF SMOKE IN CABIN SHUT OFF PACKS. SMOKE STARTED TO DISSIPATE. FOUND LEFT PACK MIX CHAMBER DUCTSDR DL73K010056Duct · detachedFLT ATTENDANT AND PAX NOTED SEAT RAIL AND FLOOR AROUND 7ABC IS WARM, TOO HOT TO THE TOUCH. FLT ATTENDANTS REPORTS HEAT SMELL IN AREA. FOUND LT SIDE MIX CHAMBER DISINTEGRATED AND LT HOT AIR SUPPLY DUCT SEPARATED FROM CHAMBER. REPLACED MIX CHAMBER.SDR DL73K010041Duct · blownSMOKE IN CABIN, RETURN TO BOSTON. REPLACED LT MIXING CHAMBER AND SUPPLY DUCT, LEAK CHECKED. NEEDS ENGINE RUN AND DUCT BURNOUT. PERFORMED SAME, CHECKS GOOD.SDR DL73K010033Stall Warning · malfunctionedPASSING THROUGH FL260 STICK SHAKER WENT OFF. ALL FLT LEVELS, AIRSPEED, MACH, FUEL FLOW AND RPM READINGS WERE NORMAL. DIVERTED TO MCO. REPLACED STALL WARNING MODULE. OPN TEST GOOD. A/C DIVERTED FROM TPA.SDR DL73K010018Frame · crackedA CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT SIDE FS 616 FRAMES AT THE OVERWING FRAME TO STUB JOINT. THIS IS THE TYPICAL CRACK OF S/B 737-53-1182. THE CRACK WAS CUT OUT AND THE AREA REPAIRED PER THE REFERENCED S/B AT MV.SDR DL73K010012Skin · crackedA 1 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE LOWER AFT CORNER OF THE L1 DOOR. THE DAMAGE WAS REPAIRED PER BACO DWG 65C27257 AND BACO S/B 737-53-1083. THE DAMAGE WAS FOUND AT HMV.SDR DL73K010004Skin · crackedTHE LOWER HINGE CUTOUT OF THE FWD ENTRY DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM 53-30-3 FIG 31 AND ER/A 379680-14, REV A.SDR DL73K002530Relay · failedDURING CLIMB RIGHT CENTER LOW PRESSURE LIGHT ILLUMINATED. CB POPPED RETURNED TO EWR. - REPLACED CONTROL RELAY FOR RT CENTER FUEL BOOST PUMPSDR DL73K002522Skin · crackedFUSELAGE / SKIN ASSY / AFT PASSENGER DOOR(L2) OPENING / LWR FWD CORNER : CRACK REPAIR . THE FUSELAGE SKIN, BONDED DOUBLER AND BEAR STRAP WERE FOUND CRACKED AT THE LOWER FORWARD CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS REMOVED IN ALL LAYERS WITH A 1" X 2" CSDR DL73K002529Accessory Unit · failedAT TOP OF DESCENT - ISOLATION VALVE LIGHT ILLUMINATED - THEN AFTER PLACING GEAR DOWN HAD NO GEAR LIGHTS RED OR GREEN. VISUALY CHECKED GEAR DOWN AND FOUND GEAR LIGHT C/B OUT. REPLACED LANDING GEAR ACCESSORY UNIT PER M/MSDR DL73K002511Valve · failedA/C FAILED TO PRESSURIZE . INSPA/C DOORS AND SEALS ,RAN CABIN PRESSIZATION CHECK PER MM .PRESS A/C CHECK GOOD .REP RT PAC 35DEG SENSOR AND AIR MIX VLV ,REMOVE MCO PLAC FRM RT PAC .RAN ENGS PRESS SYS CK GOOD .SDR DL73K002508Unknown · odorODOR OF BURNING PLASTIC REPORTED IN AFT GALLEY JUST AFTER TAKEOFF. ODOR WENT AWAY JUST PRIOR TO LANDING. INSPECTED FWD AND AFT BAG BINS, NO SMELL NOTED. INSPECTED AFT GALLEY AREA FOUND NEW RUBBER SEAL AREA WITH RTV SMELL. CHECKED AIR COND SYSTEM AND GASPERSDR DL73K002498Skin · corrodedCORROSION WAS FOUND ON THE FUSELAGE SKIN AT STATION 887 AND 907 IN THE UPPER SKIN WHERE THE VERTICAL STABILIZER FAIRING ATTACHES AT ABOUT RBL 4 AND 5. THE MAXIMUM DEPTH OF DAMAGE WAS .012" CONTAINED WITHIN A 1/5" DIAMETER. THE DAMAGE WAS REMOVED AND AN EXTERSDR DL73S002493Skin · crackedFUSELAGE / SKIN / FS 520-530 / STR. 16R :CRACK REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A 4" CRACK JUST ABOVE STRINGER 16R BETWEEN FS 520 & 530. THE CRACK RUNS ALONG THE EDGE OF THE INTERNAL BONDED WAFFLE DOUBLER AT THIS LOCATION. THE CRACK WAS ROUTED OSDR DL73K002488Fitting · corrodedTHE RT FUSELAGE CLEVIS LUGS ATTACHING THE HORIZONTAL STABILIZER WERE FOUND CORRODED ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED PER ERA 396532-14AD AT HMV.SDR DL73K002494Skin · dentedFUSELAGE / SKIN ASSY / FS 960-1000 / STRG. 21L-25L : GROUND DAMAGE REPAIR. THE FUSELAGE SKIN AND UNDERLYING FRAMS AND STRINGERS WERE BADLY DAMAGED BY GROUND EQUIPMENT IMPACT BETWEEN FS 960 & 1000 AND BETWEEN STRINGERS 21L & 25L. THE DAMAGED AREAS OSDR DL73K002483Frame · misinstalledTHE RH FRAME AT FS 907 WAS FOUND WITH A SMALL PILOT HOLES ADJACENT TO FOUR OF THE FIVE HOLES COMMOJN TO THE FRAME SPLICE BETWEEN STR 13R AND 14R. THE PILOT HOLES WERE IN THE SIDE FRAME ONLY. THE FRAME WAS CUT ABOVE STR 15R AND A NEW SECTION WAS SPLICED
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