Boeing 737-2T4
Service difficulty reports · 1,269
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 = '7372T4' 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 = '7372T4' 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 SWAA011187Power Supply · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & SVC DOOR EMERGENCY EXIT LIGHTS INOP. R&R POWER SUPPLY PER MM.SDR SWAA011148Skin · crackedDURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 500B, STR 10R. REPAIRED SKIN PER SRM.SDR SWAA011147Skin · crackedDURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 727B, STR 10L. REPAIRED SKIN PER SRM.SDR SWAA011111Slide · out of positionAFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.SDR SWAA010704Lens · missingEEPLS LENS COVER MISSING AT ROW 18. INSTALLED LENS PER MM.SDR TSAA0172033Engine · malfunctionedFLT 531 - LNY-HNL - TAXIED TO RUNWAY. WHEN POWER ADVANCED FOR TAKEOFF, A LOUD BANG CAME FROM THE NR 1 ENGINE. ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS AND SHUT DOWN THE NR 1 ENGINE. NR 2 ENGINE NORMAL. RETURNED TO GATE. REMOVED AND REPLACED THE NR 1 ENGISDR SWAA010687Light · inoperativeDURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT ROW 4. SECURED WIRING CONNECTOR PER MM.SDR SWAA010656Indicator · out of positionDURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.SDR TSAA0133023Light · inoperativeREPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR SWAA010532Cover · looseAFT SVC DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER ASSY PER MM.SDR SWAA010510Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT INBD T/E AFT FLAP OTBD EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA010408Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 595, STR 4R. REPAIRED SKIN PER SRM.SDR SWAA010402Light · inoperativeDURING SCHEDULED A2 CHECK, FOUND EEPLS BULB INOP AT OVERWING EXIT. RELAMPED EEPLS PER MM.SDR SWAA010293Slide · out of positionAFT ENTRY AND SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. RE-ADJUSTED EVAC SLIDE ASSY PER MM.SDR TSAA0157009Spar · corrodedIDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTAL FLANGE AND INSTALLING A TAPERED FILLER, HFEC COMPLETED ON ALL FASTENER HOLES AND REWORKED AREA. NO DEFECTS NOTED. CLEAN AND TREATED ALL SDR SWAA010212Light · looseDURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN CABIN. REINSTALLED EEPLS PER MM.SDR SWAA010162Indicator · out of positionDURING SCHEDULED C2 CHECK, FOUND AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY''S PER MM.SDR SPAA0100041Light · inoperativeDURING ACCOMPLISHMENT OF PRE-FLIGHT CHECK FOUND EMERGENCY EXIT LIGHT AT L-2 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B737 MM 33-51-101. OPERATIONAL CHECK GOOD.SDR SWAA010010Fire Loop · erraticIN FLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY, AIR TURNBACK. NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. ACCOMPLISHED FIRE PROCEDURE PER QRH, FIRED BOTH EXTINGUISHER BOTTLES. INSPECTED ENGINE FOR EVIDENCE OF FIRE, NONE NOTED. VERIFIED OVERHEAT SYSTEM NORMSDR SPAA0000028Light · inoperativeDURING PREFLIGHT INSPECTION FOUND L-2 DOOR EMERGENCY EXIT LIGHT INOP.REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLYSDR SPAA0000027Slide · unserviceableDURING PREFLIGHT INSPECTION, FOUND L-2 DOOR MOUNTED EVACUATION SLIDE CYLINDER PRESSURE LOW. REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY.SDR ERKE200000009Spar · tool damageHORIZONTAL STABILIZER CENTER SECTION FRONT SPAR, LOWER CLEVIS LUG,LEFT HAND SIDE, FORWARD FACE HAS EXISTING TOOLING MARK. REPAIRED PER ECRA N703S-55-B737-007-EAC.SDR ERKR200000008Fitting · corrodedHORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER CLEVIS LUG AFT EAR, AFT FACE, HAS A PREVIOUS BLEND IN THE SPOTFACE AREA. REPAIRED PER ECRA N703S-55-B737-008-EAC. (X)SDR ERKR200000007Spar · chippedHORIZONTAL STABILIZER REAR SPAR FITTING, UPPERMOST LUG, LEFT HAND SIDE INNER BORE SPOTFACE HAS A CHIPPED CORNER. REPAIRED PER ECRA N703S-55-B737-006-EAC. (X)SDR ERKR200000006Spar · corrodedHORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING RIGHT HAND SIDE INNER BORE HAS CORROSION. REPAIRED PER ECRA N703S-55-B737-005-EAC. (X)SDR ERKR200000005Spar · corrodedCORROSION ON THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING RIGHT HAND SIDE LOWER AFT LUG. REPAIRED PER ECRA N703S-55-B737-004-EAC. (X)SDR ERKR200000004Spar · gougedEXISTING GOUGES ON THE AFT SURFACE OF THE LEFT HAND VERTICAL STABILIZER FRONT SPAR FITTING LUG. REPAIRED PER S/B 737-55-1028, ECRA N703S-55-B737-003-EAC. (X)SDR TSAA0053255Keel · corrodedIDENTIFIED CORROSION AT THE VERTICAL LEG OF THE KEEL BEAM AT BS 535 APPROXIMATELY LBL 6.30. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TREATED AFFECTED AREA. REPAIR COMPLETED ON 12/26/00, IAW SRM 51-10-6. (M)SDR ERKR200000003Fitting · corrodedCORROSION VERTICAL REAR SPAR FITTING, LEFT SIDE OUTBOARD LUG AFT FACE OF FITTING. (X)SDR TSAA0033248Battery Pack · inoperativeREPLACED AFT SERVICE EMERGENCY EXIT IDENTIFIER LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR ERKR200000002Web · crackedCRACK IN AFT CARGO DOOR SILL WEB, BS 822, STR 25R. (X)SDR TSAA0053253Skin · crackedIDENTIFIED 3.7 INCH CRACK AT BS 747, STRINGER 18L. CONFIRMED USING HFEC METHOD. (M)SDR SWAA002699Slide · out of positionR2 DOOR EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.SDR SPAA0000040Spar · damagedDURING ACCOMPLISHMENT OF SB 737-55-1055 FOUND UNEVEN PREVIOUSLY BLENDED AREA AT LEFT SIDE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING LOWER CLEVIS AFT LUG, AFT FACE. REPAIRED BY SPOT FACING/MACHINING SURFACE TO OBTAIN A FLAT SURFACE. APPROVAL FOR RESDR SPAA0000039Fitting · damagedDURING ACCOMLISHMENT OF SB 737-55-1055 FOUND TOOLING MARK ON THE LT HORIZONTAL STAB CENTER SECTION FRONT SPAR LOWER CLEVIS FORWARD LUG, FORWARD FACE. BLENDED AND SPOT FACED EXISTING DAMAGE. APPROVAL OF REPAIR PROVIDED BY FAA FORM 8110-3 DATED DECEMBER 13, 2000SDR SPAA0000037Spar · corrodedDURING ACCOMPLISHMENT OF SB 737-55-1055, RT SIDE OF HORIZONTAL STABILIZER CENTER SECTION LOWER AFT CLEVIS LUG, FWD EAR BUSHING HOLE WAS FOUND TO HAVE CORROSION AND WAS ABOVE ALLOWABLE DIMENSIONS PER DRAWING 65C22125. REPAIRED BY REMOVING CORROSION AND INCREASISDR SPAA0000036Fitting · corrodedDURING ACCOMPLISHMENT OF SB 737-55-1055, CORROSION WAS FOUND AT THE LOWER AFT LUG BUSHING HOLE COMMON TO THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR FITTING RIGHT HAND SIDE. REPAIRED BY INCREASING THE DIAMETER OF THE BUSHING HOLE TO 1.540 DIAMETER. REPASDR SWAA002704Solenoid · failedAIR TURNBACK, AFTER TAKE-OFF MLG WOULD NOT GO UP DUE TO AIR GROUND SAFETY SENSOR AND LATCH FAILURE. R&R LANDING GEAR LEVER LATCH SOLENOID, ADJUSTED CONTROL CABLE PER MM.SDR SPAA0000033Web · crackedDURING SPECIAL MAINTENANCE VISIT, THE AFT CARGO DOORWAY SILL WEB AT STA 822.00 WAS FOUND CRACKED.THE REPAIR PROVIDED FOR TRIMMING OUT THE DAMAGED AREA IN THE SILL WEB AND INSTALLING A FILLER AND REINFORCING DOUBLER PER FIG. 1 OF ECRA N703S-53-B737-001-EAC. FASDR SPAA0000034Fitting · corrodedDURING THE ACCOMPLISHMENT OF SERVICE BULLETIN 737-55-1028, CORROSION WAS FOUND ON THE AFT SURFACE OF THE OUTBOARD LUG COMMON TO THE VERTICAL STABILIZER REAR SPAR FITTING. CORROSION WAS REMOVED PER ECRA N703S-55-737-002-EAC AND THE REWORK WAS FINISHED PER SB 73SDR SPAA0000032Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 PART 2 OF 2, CORROSION WAS FOUND ON THE RT OUTBOARD MIDFLAP, OUTBOARD CARRIAGE SPINDLE. REMOVED AND REPLACED CARRIAGE PER BOEING MM 27-51-81. RIGGED FLAP SYSTEM PER BOEING MM 27-51-12 A/TSDR SPAA0000031Carriage · corrodedDURING ACCOMLISHMENT OF CPCP TASK C57-306-04 PART 2 OF 2, CORROSION WAS FOUND ON THE RIGHT OUTBOARD MIDFLAP, INBOARD CARRIAGE SPINDLE. REMOVED AND REPLACED SPINDLE PER BOEING MM 27-51-81 AND RIGGED SYSTEM PER BOEING MM A/T 27-51-12SDR SPAA0000030Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 PART 1 OF 2, CORROSIOIN WAS FOUND ON THE LET WING OUTBOARD FLAP, INBOARD FLAP CARRIAGE SPINDLE. REMOVED AND REPLACED FLAP CARRIAGE SPINDLE PER BOEING MM 27-51-81 AND RIGGED SYSTEM PER BOEING MM 27-51-12 A/TSDR SPAA0000029Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 1OF2 CORROSION WAS FOUND ON THE LEFT WING OUTBOARD MIDFLAP, OUTBOARD CARRAIGE SPINDLE. REMOVED AND REPLACED OUTBOARD FLAP CARRAIGE IAW BOEING MM 27-51-81. RIGGED FLAP SYSTEM PER BOEING MM 27-51-12 A/TSDR SPA0000031Carriage · corrodedDURING ACCOMLISHMENT OF CPCP TASK C57-306-04 PART 2 OF 2, CORROSION WAS FOUND ON THE RIGHT OUTBOARD MIDFLAP, INBOARD CARRIAGE SPINDLE. REMOVED AND REPLACED SPINDLE PER BOEING MM 27-51-81 AND RIGGED SYSTEM PER BOEING MM A/T 27-51-12SDR SPA0000030Carriage · corrodedDURING ACCOMPLISHMENT OF CPCP TASK C57-306-04 PART 1 OF 2, CORROSION WAS FOUND ON THE LT WING OUTBOARD FLAP, INBOARD FLAP CARRIAGE SPINDLE. REMOVED AND REPLACED FLAP CARRIAGE SPINDLE PER BOEING MM 27-51-81 AND RIGGED SYSTEM PER BOEING MM 27-51-12 A/TSDR SPAA0000038Fitting · damagedDURING ACCOMPLISHMENT OF SB 737-55-1055 DAMAGE WAS FOUND TO THE LEFT HAND HORIZONTAL STABILIZER REAR SPAR UPPER TERMINAL FITTING. BLENDED DAMAGED AREA, FLAP PEENED, AND FINISHED REWORK PER SB 737-55-1055. APPROVAL PROVIDED BY FAA FORM 8110-3 DATED DECEMBER 8,2SDR SWAA002628Slide · out of positionAFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.SDR SWAA002439Light · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED EEPLS ASSY PER MM.SDR SWAA002438Sign · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN INOP. RE-LAMPED EXIT SIGN PER MM.
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