Boeing 737-522
Service difficulty reports · 1,682
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 = '737522' 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 = '737522' 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 2005UALA01081Light · inoperativeEMERGENCY EXIT PATH LIGHTING IN REAR THIRD OF AIRCRAFT NOT WORKING. REPLACED POWER STRIP.SDR 2005UALA01071Stringer · crackedAFT CABIN STA 907 STR 4L IS CRACKED AT 2 EA FASTENER HOLES. REPLACED STRINGER SPLICE. REF SRM 51-40-02.SDR CA051003001Screw · damaged(CAN) AFTER LANDING, AFTER THE AIRCRAFT WAS REFUELED, FUEL WAS OBSERVED COMING FROM THE RIGHT WING FORWARD OF THE IB FLAP TRACK. THE FUEL ACCESS PANEL DIRECTLY AFT OF THE RT WING NACELLE WAS FOUND LEAKING. ON INVESTIGATION SEVERAL SCREWS WERE FOUND TO BE STRSDR 2005UALA01048Frame · crackedFWD SIDE OF DOOR LOWER END FRAME CRACKED AT FASTENER HOLE FWD GALLEY DOOR. ACCOMPLISHED A REPAIR PER MM 51-40-02, FABRICATED AND INSTALLED FRAME SPLICES REF BOEING DRW 69-69430,SDR 2005UALA01032Frame · crackedMID CABIN FRAME IS CRACKED AT FASTENER HOLE AT STA 727B NEAR STR 8L. ACCOMPLISHED A REPAIR PER MM 53-10-84, FABRICATED ANGLE, FILLER AND SUPPORT AND INSTALLED PER MM.SDR 2005UALA01031Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 827 NEAR STR 8L MARKED. FABRICATED AND INSTALLED ANGLE, FILLER AND SUPPORT PER MM 53-10-84SDR 2005UALA01030Frame · crackedAFT CABIN STA 867 FRAME IS CRACKED NEAR STR 8L. FABRICATED AND INSTALLED REPAIR PARTS WITH REF. TO MM CHAPT 53-10-84. FABRICATED NEW RAIL SUPPORT BRACKET.SDR 2005UALA01029Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 787 NEAR STR 8L MARKED. FABRICATED ANGLE,FILLER & SUPPORT BRACKET PER MM 53-10-84 AND INSTALLED.SDR 2005UALA01028Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 907 NEAR STR 8L. FABRICATED AND INSTALLED REPAIR PARTS WITH REF TO MM 53-10-84. FABRICATED NEW RAIL SUPPORT BRACKET.SDR 2005UALA01027Stringer Splice · crackedAFT CABIN CROWN STRINGER SPLICE IS CRACKED AT STA 907 STR 4R. REMOVED DAMAGED STRINGER SPLICE. ACCOMP HFEC INSPECTION ON EXISTING STRINGER SECTIONS. NO CRACKS FOUND. DRILLED UP NEW STRINGER SPLICE CHANNEL PN 65-51698-2 AND INSTALLED. REF SRM 51-40-02.SDR 2005UALA01026Crease Beam · corrodedAFT CABIN FLOOR STA 962 TO STA 1006 WL 208 RBL 54 RT CREASE BEAM CORRODED. REMOVED DAMAGE CREASE BEAM INNER CORD. MATCH DRILLED AND INSTALLED NEW CORD REF SRM 51-40-0 2.SDR 2005UALA01025Skin · dentedAFT PIT DOOR EXTERIOR SKIN HAS DENTS. DAMAGE REMOVED, MANUFACTURED AND INSTALLED REPAIR PER SRM.SDR CA050923009Seal · fod(CAN) WHILE THIS A/C WAS IN HANGAR FOR A SCHEDULED PHASE CHECK, IT WAS NOTICED BY A MECHANIC THAT THERE APPEARED TO BE FOREIGN MATERIAL STICKING OUT OF THE RUDDER BALANCE WEIGHT CUT-OUT SEAL. ON CLOSER INSPECT IT WAS FOUND TO BE TWO BAGS OF PNL ATTACHMENT HARSDR 2005UALA01020Frame · crackedAFT CABIN FRAME IS CRACKED AT STA 867 NEAR STR 8R, AROUND FASTENER HOLE. REMOVED DAMAGED AREA ON FRAME. VERIFIED CRACK WAS REMOVED BY HFEC INSPECTION. FABRICAT ED AND INSTALLED REPAIR ANGLES. ANGLES FORMED FROM 7075-0 MAT ERIAL AND HEAT TREATED TO 7075 T6. FSDR 2005UALA01019Skin · dentedAFT LOWER FUSELAGE APPROX STA 1064 BETWEEN STR 27L AND 28L HAS DENT. REMOVED DAMAGE, FABRICATED & INSTALLED DOUBLER. REF SRM 53-80-01 FIG 201SDR CA050923008Vent · cracked(CAN) ON A SCHEDULED PHASE INSPECTION THIS VENT, WHICH IS ON THE ENGINE THRUST REVERSER COWL WAS FOUND TO HAVE A 2 INCH CRACK. A SIMILIAR CRACK WAS FOUND ON A PHASE CHECK THE DAY BEFORE ON ANOTHER AIRCRAFT.SDR CA050921003Module · cracked(CAN) DURING AN INSPECTION OF THE STANDBY HYDRAULIC SYSTEM, BOEING TASK CARD B27-21-94-2A, FLUID WAS NOTED LEAKING FROM THE STANDBY HYDRAULIC MODULE. ON INVESTIGATION THE UNIT WAS FOUND TO BE CRACKED. THE UNIT WAS REPLACED WITH A SERVICEABLE UNIT.SDR 2005UALA01009Wire · damagedEEL LIGHTS FROM ROW 15 AFT ARE INOP. REPLACED FEEDER CABLE IN EEL TRACK DUE TO CONNECTORS WERE SWAMPED WITH GALLEY GOO.SDR CA050922004Panel · departed(CAN) WHEN DEPARTING, AC HAD A NR1 ENG NACELLE STRUT ACCESS PANEL DEPART FROM AC. AC WAS INSPECTED FOR DAMAGE RESULTING FROM DEPARTURE OF THIS PANEL, AND FOR POSSIBLE CAUSE. REST OF PANELS WERE CHECKED FOR SECURITY. NO ADDITIONAL FAULTS FOUND. AC WAS RELEASSDR 2005UALA00925Power Supply · inoperativeTHE FOLLOWING EMERGENCY LIGHTS ARE INOP: EEL LIGHTS AFT OF ROW 14, SLIDE LIGHT DOOR 2L. EXIT SIGN DOOR 2R, AFT ENTRY EXIT SIGN, AISLE LIGHT ROW 17. REPLACED POWER SUPPLY AND BATTERY.SDR 2005UALA00892Stringer · crackedSTR 10L UPR FLANGE IS CRACKED AT STA 294.SDR 2005UALA00853Fitting · crackedCRACK IN FUSELAGE MAIN FRAME FITTING UNDER CABIN FLOOR AT STA 616 RBL 70, INNER CHORD AT BOTTOM 2 RIVETS.SDR 2005UALA00859Wire · failedEEL LIGHTS FROM ROW 15 BACK INOP. INSTALLED SERVICEABLE EEL LEAD FOR FAILED SECTION.SDR 2005UALA00844Skin · puncturedPUNCTURE OF SKIN BELOW AND AFT OF DOOR 2R.SDR 2005UALA00789Battery · failedRETURNED TO THE FIELD DUE TO A BATTERY SYSTEM FAILURE. SHOP FINDINGS REVEALED BAD CELLS IN THE BATTERY. THE BATTERY HAS BEEN SCRAPPED.SDR 2005UALA00779Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 13 TO AFT CABIN. REPLACED BATTERY AND AFT GALLEY STRIP.SDR 2005UALA00755Attach Fitting · corrodedVERTICAL STABILIZER LT AND RT AFT PRIMARY ATTACH LUG FITTINGS ON FUSELAGE HAD CORROSION REMOVAL BEYOND LIMITS. REPLACED LT AND RT AFT PRIMARY ATTACH LUGS AND INSTALLED NEW BUSHINGS PER BACO DRAWING 65-52274.SDR 2005UALA00745Skin · dentedSTA 837 IS DENTED BETWEEN STR 25L AND 26L. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR PER SRM 53-00-01 FIG 229.SDR 2005UALA00744Web · corrodedAFT CARGO DOOR SILL WEB HAS NUMEROUS AREAS OF CORROSION WL 141 STATION 800 TO 847 RBL 20" TO RBL 24". REMOVED AND INSTALLED NEW WEB REPAIR.SDR 2005UALA00736Web · corrodedCABIN FLOOR WEB CORRODED AT STATION 749 JUST INBD OF STR 17R CREASE BEAM. REMOVED AND REPLACED WEB.SDR 2005UALA00735Stringer Clip · crackedCABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 639 STR 4 LT. REPLACED STRINGER CLIP.SDR 2005UALA00734Stringer Clip · crackedCABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 685, STR 4 LT. REMOVED AND REPLACED STRINGER CLIP.SDR CA050804009Torque Tube · worn(CAN) DURING ROUTINE INSPECTION THE NR 2 TRANSMISSION TORQUE TUBE, A DEEP 'V' GOUGE .016 INCH DEEP WAS FOUND. A FLEET CAMPAIGN WAS INITIATED TO CHECK ALL TRAILING EDGE FLAP TORQUE TUBES.SDR 2005UALA00712Skin · dentedSTATION 807 IS DENTED AT STR 28R. CUT OUT DAMAGE AND INSTALLED A TRIPLER REPAIR REF SRM 53-00-01 FIG 229.SDR 2005UALA00709Frame · crackedFUSELAGE FRAME STA 663 IS CRACKED AT STR 1 CUTOUT. MAJOR REPAIR ACP'D PER SRM 53-00-07 AND BACO DRAW 65-73740.SDR 2005UALA00708Skin · dentedAFT CARGO DOOR EXT SKIN HAS 8 EA DENTS. REPAIR ACP'D PER SRM 52-00-01, 41" BY 23" DOUBLER INSTALLED.SDR 2005UALA00694Skin · dentedSTATION 203 HAS A SCRATCH BETWEEN STR 24 AND 25 LT. CUT-OUT DAMAGED AREAS AND INSTALLED TRIPLER REPAIR REF SRM 53-10-01 FIG 211 DETAIL XII AND XIII.SDR 2005UALA00696Lamp · burned outAISLE ILLUMINATION EMERGENCY LIGHT INOP AT ROW 10 BULLNOSE. REPLACED BURNED OUT LAMP.SDR 2005UALA00693Frame · crackedFWD GALLEY DOOR, FWD SIDE LOWER END FRAME CRACKED 1 EA FASTENER HOLE. MAJOR REPAIR ACP'D, REPLACED FRAME REF SRM 51-40-02 AND BACO DRAW 69-69430.SDR 2005UALA00692Frame · crackedFWD GALLEY DOOR, AFT SIDE LOWER END FRAME CRACKED 1 EA FASTENER HOLE. MAJOR REPAIR ACP'D, AFT FRAME REPLACED PER SRM 51-40-02 AND BACO DRAW 65-45871.SDR 2005UALA00691Angle · corrodedAFT CABIN FLOOR ANGLE CAP IS CORRODED AT STA 996 RPL 53, WL208. REPLACED ZEE ANGLE ASSY AT HMV3.SDR 2005UALA00688Frame · gougedSTA 211 FRAME IS GOUGED APPROXIMATELY 6 FEET ABOVE STRINGER 17R. REPAIRED WEB WITH DOUBLER PER SRM 51-70-13 FIG 1 DETAIL 1SDR 2005UALA00687Skin · dentedEXTERIOR FUSELAGE SKIN DENTED AT STA 378-380 BTWN STR 17L & 18L, AND STA 376 BTWN STR 16L & 17L ALSO HAS A DENT. MAJOR REPAIR ACP'D PER SRM 53-00-01 TO BOTH DENT AREAS. TRIPLER REPAIR SCHEME USED PER FIG 101 APPROX SIZE 13"X20"SDR 2005UALA00686Slide · dislodgedDOOR 1 LEFT SLIDE PACK CAME COMPLETELY OFF. THE CAUSE FOR THIS EVENT IS UNKNOWN. THE CORRECTIVE ACTION WAS INSPECTION OF THE SLIDE AND RE-INSTALLATION ON SAME AIRCRAFT.SDR 2005UALA00682Skin · dentedFUSELAGE SKIN HAS DENT AT STATION 855 BELOW STR 20L SKIN LAP. MAJOR REPAIR ACP'D PER SRM 53-00-01 FIG 229 TRIPLER INSTALLED 14 X 16.SDR 2005UALA00681Skin · dentedEXTERNAL FUSELAGE SKIN HAS DENT AT STA 897 STR 19L. MAJOR REPAIR ACP'D PER SRM 53-00-01 FIG 229. TRIPLER INSTALLED APPROX 12 X 11.SDR 2005UALA00680Pressure Panel · crackedLT MLGWW UPPER PRESSURE DECK HAS CRACK AT STA 664 LBL 32. MAJOR REPAIR ACP'D PER MM53-21-98, INSTALLED DOUBLER REPAIR.SDR 2005UALA00675Frame · crackedFUSELAGE FRAME AT STA 663 IS CRACKED IN TWO PLACES AT STR 3R CUTOUT. MAJOR REPAIR ACP'D PER SRM 51-10-02 & SRM51-10-07 FIG 209 PG 225 REPAIR ANGLE INSTALLED, APPROX SIZE 16" X 4"SDR 2005UALA00674Door Frame · damagedFWD CARGO DOOR LOWER AFT CORNER FRAME AT LOWER INBOARD FASTENER DAMAGED. MAJOR REPAIR ACP'D BY FRAME SECTION REPLACEMENT.SDR DU4R0507143Skin · delaminatedRIGHT WING INBOARD MID FLAP WEDGE LOWER T/E SKIN SURFACE DELAMINATED AND DENTED.
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