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 DL73S030923Skin · crackedA 2 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST BELOW STRINGER 19R AT FS 765. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087498-14.SDR DL73S030909Coffeemaker · overheatedPASSING 10,000 FT ON CLIMB STRONG BURNING ODOR. F/A'S CONFIRMED OVENS OFF, ODOR STRONGER, RETURNED TO ATL. FOUND FIRST CLASS COFFEEMAKER OVERHEATING. REPLACED COFFEEMAKER, OPERATION GOOD.SDR DL73S030899Duct · damagedRT ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB, WENT OUT WITH THROTTLE AT IDLE. FOUND DAMAGED STARTER DUCT. REPLACED SAME.SDR DL73K030896Frame · crackedTHE LOWER FORWARD FRAME OF THE C1 DOOR HAD A TIME-LIMITED REPAIR PREVIOUSLY INSTALLED AND NEEDED PERMANENT REPAIR INSTRUCTIONS. PERMANENT REPAIR ISSUED VIA ERA 377407-14AD, REV A.SDR DL73S030885Switch · brokenELECTRICAL SMELL COMING FROM FWD FLIGHT ATTENDANT INTERPHONECOMM PANEL. FOUND CABIN SIDEWALL LIGHT SWITCH AT FWD F/A PANEL BROKEN AND SHORTING. REPLACED SWITCH, CHECKS OK.SDR DL73S030883Control Panel · smokePRIOR TO PUSHBACK FLT 1111 CREW SMELLED ELEC BURNING ODOR IN COCKPIT THEN NOTICED SMOKE COMING FRM F/O EYEBROW WINDOW AREA. FOUND SMOKE TO COMING FROM ENG/WING ANTI-ICE PANEL. REPLACED PANEL.SDR DL73S030875Skin · dentedTWO DENTS WERE FOUND BELOW THE C2 DOOR CUTOUT IN THE FUSELAGE SKIN. THE DENTS WERE REMOVED WITH A 7.75 X 2.6 INCH CUTOUT AND A 9.7 X 3.4 INCH CUTOUT. THE CUTOUTS WERE REPAIRED SEPARATELY WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385609-14.SDR DL73S030864Gasper Fan · failedON CLIMBOUT FLIGHT ATTENDANTS REPORTED SMOKE ODOR IN CABIN, STRONGER IN AFT PART OF CABIN, NO SMOKE VISIBLE. GASPER FAN WAS TURNED OFF AND ODOR DISSIPATED. FOUND GASPER FAN AT FAULT. REPLACED SAME.SDR DL73S030861Bear Strap · crackedTHE FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING. THE UNDERLYING BEAR STRAP WAS UNCRACKED. THE CRACK WAS REMOVED WITH A 1.7 INCH CUTOUT IN THE SKIN AND BONDED DOUBLER AND REPAIRED WITH AN ESDR DL73S030813Skin Panel · corrodedTHE LOWER SKIN PANEL OF THE KEEL BEAM STRUCTURE WAS FOUND WITH AREAS OF CORROSION BETWEEN FS 661 & 724 AND BETWEEN LBL 6 & RBL 6. THE DAMAGED PANEL WAS REMOVED AND A NEW PANEL FABRICATED AND INSTALLED. THE REPAIR WAS ACCOMPLISHED PER BAC S/B 737-53-1104 AND SDR DL73S030805Power Supply · dischargedDURING LAYOVER CHECK FOUND EMERGENCY ESCAPE PATH LIGHTING FROM ROW 11 THRU AFT CABIN BLINKING ON AND OFF WHEN THE SWITCH WAS OFF. REPLACED POWER SUPPLY (M9013) AND BATTERY PACK. ALL OPS NORMAL.SDR DL73S030778Coffeemaker · burnedBURNING ODOR IN AFT GALLEY, TURNED GALLEY POWER OFF, ODOR WENT AWAY. REPLACED AFT GALLEY NR 2 COFFEE DISPENSER.SDR DL73S030783Skin · gougedSKIN GOUGE CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND GOUGED NEAR THE FWD EDGE OF THE C1 DOOR CUTOUT BETWEEN FS 430 AND 440 AT STRINGER 22R. THE DAMAGE WAS REMOVED WITH A 10.5 X 1.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLESDR DL73S030763Battery Pack · inoperativeEMERGENCY SEAT LIGHTS ROW 1-16 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS NORMAL.SDR DL73S030771Bulkhead · corrodedWEB CORROSION REPAIR INSPECTION OF THE FS 1016 BULKHEAD WEB REVEALED CORROSION AT THE BL 0 STIFFENER NEAR THE BOTTOM OF BULKHEAD AT WL 190-200. AN OIL CAN CONDITION WAS DISCOVERED JUST OUTBOARD OF THE CORROSION AREA. BOTH DAMAGES WERE REMOVED WITH A WEB CSDR DL73S030755Accessory Unit · failedIRR LANDING GEAR LEVER LOCK WOULD NOT RELEASE WHEN GEAR HANDLE WAS RAISED AFTER T/O. REPLACED LANDING GEAR ACCESSORY UNIT.SDR DL73S030747Wire · inoperativeSEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 18-21. REPAIRED WIRING NOW OPS, NORMAL.SDR DL73S030688Attach Fitting · corrodedDURING ACCOMPLISHMENT OF INSPECTIONS IAW SB 737-55-1028 (DAL EO 3-85220-3), CORROSION WAS FOUND ON FIVE (5) VERT STABILIZER CLEVIS LUGS AND THREE (3) VERT STABILILZER ATTACH LUGS. THE BORES WERE OVERSIZED AND THE LUG FACES MACHINED TO REMOVE CORROSION. O/S BSDR DL73S030681Skin · dentedA SCRATCH AND DENT WAS FOUND IN THE FUSELAGE SKIN JUST BELOW THE C1 CARGO DOORWAY EXTENDING FROM FS 460 TO FS 500. AN EXISTING REPAIR WAS FOUND AT THE FORWARD LOWER CORNER OF THE DOORWAY. THIS REPAIR WAS REMOVED AND AN EXTERNAL ALUMINUM DOUBLER TRIPLER AND FILSDR DL73S030680Spar · gougedRT WING / MLG AFT SUPPORT FITTING / WBL 157, TOOLING DAMAGE. THE MLG AFT SUPPORT FITTING ON THE RT WING SUFFERED TOOLING DAMAGE DURING REMOVAL OF FASTENERS FOR INSPECTION. THE BORE OF ONE OF THE FASTENERS WAS DAMAGED IN THE AFT FITTING, REAR SPAR UPPER CHORDSDR DL73S030674Floorbeam · damagedDURING ACCOMPLISHMENT OF EO 03-062982-03AD, MTC ADDED ADDITIONAL FASTENER HOLES THROUGH THE UPPER CAP AND SPLICE ANGLES OF THE CENTER WING BOX FLOORBEAMS FROM BS 650 TO 675 AT BL 0.07. REPAIR PER ER/A 385423-14AD.SDR DL73S030666Pressure Panel · crackedFUSELAGE STA 727 BLKHD, MLG WW, UPPER CHORD - REPAIR: A 0.5 INCH CRACK WAS PREVIOUSLY REPAIRED IN TEH UPPER CHORD OF THE SUBJECT BULKHEAD NEAR BL 0. THE CRACK WAS IN THE UPPER FLANGE OF THE COMPRESSION CHORD AND RAN THROUGH A FASTENER HOLE. DURING THE CURRENSDR DL73S030665Frame · crackedFUSELAGE SKIN STA 663, S2R TO S1 - MISALIGNMENT: DURING INSPECTION OF THE FS 663 FRAME, MTC FOUND CRACKS IN THE FRAME AT S2R AND S1R. THESE WERE WITHIN THE AREA ADDRESSED BY B737-200 SRM 53-10-4, FIG 14. DURING INSTALLATION OF SRM FRAME REPAIR, SKIN ATTACH SDR DL73S030664Skin · damagedFUSELAGE SKIN STA 255, S-23R TO S-24R - CUTOUT: EXISTING TEMPORARY (BLIND FASTENER) SRM REPAIR REMOVED AND PERMANENT SKIN REPAIR INSTALLED IAW DAL ER/A 385263-14.SDR DL73S030658Attach Fitting · corrodedHORIZ STAB LT, RT, AND CENTER SECTIONS ATTACH FITTINGS :LUG CORROSION, INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS ON THE LT, RT, AND CENTER SECTIONS OF THE STAB PER BAC S/B 737-55- 1055, CORROSION WAS FOUND IN SEVERAL OF THE LUG BORES AND ON THE LUG SDR DL73S030643Engine · bird ingestionIRREG: ON T/O DETECTED SMELL IN COCKPIT AND CABIN. RETURN TO CVG. FOUND EVIDENCE OF BIRD STRIKE NR 1 ENG. INSP ENG AND ENG BLEED DUCTS. PERFORMED DUCT BURNOUT AND REPLD. WATER SEPARATOR BAGS.SDR DL73S030630Insulation · out of positionSMOKE SMELL IN AFT CABIN. FOUND INSULATION TOUCHING APU BLEED DUCT CAUSING SMELL. REPOSITIONED INSUL. FWD APU AIR TO MCO AND PLAC AS PRECAUTION.SDR DL73S030623Sill · crackedFUSELAGE C-2 DOOR UPPER SILL FS 818 WEB CORROSION. DURING INSPECTION OF A TIME LIMITED REPAIR TO THE C-2 DOORWAY UPPER SILL WEB, CRACKING OF THE WEB WAS NOTED AS WELL AS A SHORT ED FASTENER IN THE SILL OUTER CHORD. THE WEB WAS REPAIRED WITH A DOUBLER AND THESDR DL73S030596Fuse · inoperativeEMERGENCY SEAT LIGHTS INOPERATIVE, FROM CLOSET 1R THROUGH ROW 10. RPLCD FUSE AT D1133. CLOSET LIGHTS STILL INOPERATIVE. REPAIRED BROKEN WIRES AT CLOSET BULKHEAD. NOW OPS NORMAL. 1L EMERGENCY SLIDE LIGHT, INOPERATIVE, RELAMPED, CKS GOOD.SDR DL73S030594Charger · inoperativeAFTER LANDING FWD EMERGENCY LIGHT COVER FELL ON FLOOR. REINSTALLED COVER AND LIGHT DOES NOT OPS OK. CHANGED EMERGENCY LIGHT BATTERY PACK, NO HELP. CHANGED BATTERY CHARGER, OPS CHECK OK.SDR DL73K030582Megaphone · inoperativeON PREFLIGHT FWD MEGAPHONE INOP. REPLACED MEGAPHONE.SDR DL73S030531Skin · debondedLT OUTBOARD AFT FLAP T/E WEDGE DISBONDED. T/E WEDGE REPAIRED PER ER/A 423067-14.SDR DL73S030530Fitting · gougedTHE UPPER ATTACH LUG OF THE HORIZONTAL STABILIZER CENTER SECTION WAS FOUND WITH A GOUGE FROM INTERFERENCED WITH AN IMPROPERLY INSTALLED FASTENER ON ADJACENT STRUCTURE. THE GOUGE WAS BLENDED TO A SMOOTH CONTOUR AND NDT INSPECTED. THE GOUGED FITTING WAS AUTHORSDR DL73S030520Skin · crackedTHE FUSELAGE SKIN AT FS 750 WAS FOUND WITH A 2 INCH CRACK RUNNING ALONG THE EDGE OF THE BONDED DOUBLER AT STRINGER 18R. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385222-14.SDR DL73K030517Skin · crackedFS 661 - 727, KEEL BEAM SKIN PANEL FABRICATION: DURING INSPECTIONS PER EO 3-58542-3, THE SUBJECT PANEL WAS FOUND CRACKED. BAC SB 737-53-1104 PROVIDES REPAIR INSTRUCTIONS TO REFABRICATE THE PANEL, HOWEVER ER/A 385214-14 WAS ISSUED TO CUT AN ACCESS HOLE IN THESDR DL73K030507Skin · crackedA 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT FS 525 JUST ABOVE STRINGER 16L RUNNING ALONG THE EDGE OF THE INTERNAL BONDED WAFFLE DOUBLER. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ERSDR DL73K030504Engine · malfunctionedENG FUEL FLOWS WERE 1500 SPLIT AFTER TAKEOFF. TRIED ENG ANTIICE ON AND MISMATCH ON THROTTLES REVERSED. EPR ON LEFT ENG 1.40 AND ON RIGHT ENG WAS 1.77. AFTER CONSULTATION WITH MAINTENANCE COORDINATOR AND DISPATCH, DIVERTED TO MCO. DUPLICATED ITEM ON R/U. RSDR DL73S030508Frame · crackedMTC FOUND CRACKS IN THE FRAME AT S6L, 3L, 2L, 1, 2R, AND 3R EXTENDING FROM THE STRINGER PASS THRU CUTOUTS. THE CRACKS WERE CUTOUT AND A REPAIR SIMILAR TO B737-200 SRM 53-10-04, F14, WAS INSTALLED TO EXTEND FROM O/B OF STR 6L TO O/B OF STR 4R. FUSELAGE SKIN WSDR DL73S030505Frame · crackedTHE SUBJECT DOOR FRAME WAS FOUND CRACKED AT THE INTERSECTION OF FS 440 AND STR 24R. THE FRAME WAS ORIGINALLY 0.071 INCH 7075-T6 CLAD. THE CRACK WAS TRIMMED OUT, STEEL REPAIR ANGLES WERE INSTALLED, AND TWO DOOR STOP FITTINGS WERE MODIFIED TO ALLOW FOR THE INSSDR DL73S030497Frame · cutFRAME AND REINFORCEMENT ANGLE CUT AT STA 380 TO REPLACE SECTION OF STR 17L. REPAIRED FORMER PER SRM 53-10-4 FIG 9. REPAIRED REINFORCEMENT ANGLE PER SRM 51-40-3, OK PER LIA ENGINEERING.SDR DL73S030495Attach Fitting · corrodedSTABILIZERS / HORIZONTAL / ATTACH FITTINGS / LT, RT AND CENTER SECTION - CORROSION: WHILE ACCOMPLISHING AN INSPECTION OF THE HORIZONTAL STABILIZER ATTACH LUGS PER EO 3-69697-3. MAINTENANCE DISCOVERED CORROSION IN ALL FUSELAGE AND STABILIZER LUGS AND ON MOST SDR DL73S030488Bulb · malfunctionedNR 1 OIL TEMP ERRATIC FLUX PLUS OR MINUS 10 DEGREES UPPER GREEN BAND, THEN WENT INTO YELLOW BAND. ALL AREAS PLUS OR MINUS 10 DEGREES. FLUX STAYED IN YELLOW UP TO 15 MINUTES. PRECAUTIONARY SHUTDOWN PER POM. REPLACED OIL TEMP BULB.SDR DL73S030485Skin · dentedFUSELAGE SKIN FS 344, S-19R TO S-20R - DENT: A DENT WAS REPORTED APPROXIMATELY 2 INCHES BELOW THE LOWER EDGE OF THE UPPER SKIN OF THE LAP SPLICE AT S-19R. THE DENT MEASURED 2.2 X 1.5 X 0.057 INCH DEEP. THE SKIN PANEL IS 0.036 INCH SKIN WITH A 0.036 INCH INSDR DL73K030481Power Supply · inoperativeDOOR 1L EMERGENCY OVERHEAD LIGHT INOPERATIVE. REPLACED M1133 POWER SUPPLY.SDR DL73S030479Attach Fitting · corrodedFUSELAGE ATTACH FITTINGS: VERTICAL STABILIZER CLEVIS LUGS - CORROSION. THE NR 11 CLEVIS LUG FWD FACE WAS FOUND GOUGED. THE DAMAGE WAS CLEANED UP USING A SPOTFACE, WITH A MIN REMAINING LUG THICKNESS OF 0.940 INCH IAW DAL ER/A 412535-14, INITIAL RELEASE.SDR DL73S030476Bulkhead · crackedWHILE ACCOMPLISHING INSPECTIONS OF THE AFT PRESSURE BULKHEAD IAW AD 99-08-23, 2 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES IN THE BULKHEAD AT THE ATTACH AREA. THE CRACKED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM DOUBLER IAW SRM AND ER/A 38508SDR DL73S030466Actuator · crackedAFTER LANDING ROLL OUT, LOSS OF SYSTEM -A- QUANTITY PRESSURE FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATORSDR DL73S030455Skin · crackedAFT ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT CRACK REPAIR THE UPPER HINGE CUTOUT OF THE L2 DOOR CUTOUT WAS FOUND WITH A 1 INCH CRACK THROUGH THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIRSDR DL73S030445Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK RUNNING ALONG THE MILL/BONDED DOUBLER LINE OF STRINGER 23R AT FS 867. THE CRACK IS TYPICAL OF BAC S/B 737-53A1210. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLERSDR DL73S030431Valve · stuckIR: 20KFT CABIN ALTITUDE HORN WENT OFF.CBN ALT AT 11 KFT. STARTED DESCENT SWITCHED TO STBY CBN WOULD NOT PRESS. MANUAL MODE ALSO INOP. REPLACED E & E COOLING EXHAUST VALVE. ALSO FOUND LEFT ENGINE 450 DEG THERMOSTAT SENSE LINE BACKED OFF. TIGHTENED SAME,RAN
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