N831L, cancelled Feb 23, 2004
Service difficulty reports · 38
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N831L' AND deregistration_id = 'N831L-2004-02-23' 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 n_number = 'N831L' AND deregistration_id = 'N831L-2004-02-23' 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 DL72W011420Battery Pack · dischargedFOUND RT OVERWING EMERGENCY DOOR LIGHTS INOP. CA REPLACED BATTERY PACK, CKS GOOD.SDR DL72W010991Bypass Valve · failedON FLAP RETRACTION LOST A-SYS HYD. FOUND O/B FLAP BYPASS VALVE FAILED. REMOVED AND REPLACED O/B FLAP BYPASS VALVE.SDR DL72W010601Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A SMALL BULGE AND CRACK AT FS 1030 AND STRINGER 30. THE DAMAGE WAS REMOVED WITH A 1.5 INCHES X 1.5 INCHES CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380542-14, REV A.SDR DL72W010404Shim · looseINSPECTIONS OF THE INBD FLAP INBD TRACK ON THE RT WING PER AD 90-07-05 REVEALED A LAMINATED SHIM WHICH HAD MIGRATED MORE THAN THE .25 INCH ALLOWED. THE MIGRATED SHIM WAS REMOVED AND REPLACED AND THE ATTACH BOLTS RE-TORQUED PER THE REQUIREMENTS ON THESDR DL72W010267Beam · crackedA TYPICAL CRACK WAS FOUND AT THE LOWER END OF THE LBL 8 VERTICAL BEAM ON THE FS 1183 BULKHEAD AT WL 182. THE CRACK WAS REPAIRED WITH AN ANGLE REPAIR PER BAC S/B 727-53-0175 AND ER/A 380021-14.SDR DL72W002081Switch · damagedAIRCRAFT AIR TURNBACK FOR ALL FUEL QUANTITY INDICATORS INOP IN FLIGHT. FOUND FUEL PANEL POWER SWITCH BUMPER NOT MAKING CONTACT WITH PANEL POWER SWITCH. REPLACED MASTER POWER SWITCH GUARD.SDR DL72W000616Cone · missingON ARRIVAL SFO, NR 2 ENGINE TAIL CONE MISSING. REPLACED SAME.SDR DL72W992425Smoke Detector · activatedON FINAL APPROACH, LAV SMOKE LIGHT ILLUMINATED, F/A SMELLED SMOKE IN RT AFT LAV. INSPECTED RT AFT LAV, NO EVIDENCE OF SMOKE. LIGHTS ALL CHECKED GOOD. REPLACED SMOKE DETECTOR AS A PRECAUTION, TEST GOOD.SDR DL72W991790Stringer · corrodedFUSELAGE STRINGER S-29L, FS 950F PLUS 10 CORROSION REPAIR. STRINGER 29L WAS FOUND WITH EXTENSIVE CORROSION AROUND STATION 950F. THE CORRODED SECTION OF STRINGER WAS CUT AND REMOVED. A NEW SECTION OF STRINGER WAS SPLICED IN PER ER/A 367879-14, REV B.SDR DL72W991528Casting · crackedDRG TPA LTR CHK E1, NR 12 SPOILER ACTUATOR SUPPORT FITTING O/B MOUNT CASTING LWR MOUNT BOLT LOBE BROKEN OFF. REPLACED CASTING PER MM 57-42-0.SDR DL72W990774Line · leakingSYSTEM 'A' FAILED UPON GEAR RETRACTION PRESSURE WENT TO ZERO QUANTITY WENT TO 1 QT, PERFORMED CKLIST PROCEDURES IAW POM. MAINTENANCE FOUND HYD LINE LEAKING ON LT GEAR DOOR ACTUATOR. REPLACED LINE, SERVICED HYD, ALL CKS NORMAL.SDR DL72W990748Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 540 AND 560. THE CRACKS WERE CUT OUT OF THE SKIN LAP AND RESDR DL72W980996Frame · crackedA .5 INCH CRACK IN DOUBLER RT FWD SVC DOOR AFT FRAME UPPER CORNER. REPAIR PER M/M 52-12-0 FIG 805.SDR DL72W980019Power Supply · inoperativeAFT SECTION OF EMERGENCY LIGHTS INOP FROM ROW 27. REPLACED 2 SOCKETS AND POWER SUPPLY.SDR DL72W972592Coffeemaker · failedNOTED ELECT SMELL IN FWD GALLEY AREA. REPLACED COFFEEMAKER.SDR DL72W972454Exhaust Pipe · crackedWHILE PERFORMING A POST-REMOVAL INSPECTION OF A GTCP85-98CK APU EXHAUST PIPE (3850089-1), THREE INCH CRACKS WERE NOTED ON EACH MOUNTING FLANGE (TWO CRACKS TOTAL). CAUSE FOR CRACKS IS UNKNOWN. EXHAUST PIPE WAS MODIFIED BY ALLIED- SIGNAL TO SATISFY REQUIREMSDR DL72W972391Wire · shortedEMERGENCY EXIT BATT CHARGER C/B POPPING. REPAIRED SHORTED WIRE.SDR DL72W972278Battery · dischargedR2 DOOR OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERIES.SDR DL72W972277Battery Pack · dischargedEXTERIOR EMERGENCY LIGHT BETWEEN LT OVERWING EXITS INOP. REPLACED BATTERY PACK, CKS NML.SDR DL72W970510Angle · crackedNR 8 SLAT ACTUATOR I/B AND O/B MOUNT ANGLES CRACKED. REPAIRED PER MM 57-20-21 FIG 808.SDR DL72W970506Angle · crackedOUTBOARD MOUNT ANGLE CRACKED NR 8 SLAT ACTUATOR. INBOARD MOUNT ANGLE CRACKED NR 8 SLAT ACTUATOR. REPAIRED PER MM 57-20-21 FIG 808.SDR DL72W970504Angle · crackedONE INCH VISIBLE CRACK AT INBD ATTACH ANGLE FOR NR 1 SLAT ACT. INSTALLED DOUBLER PER MM 57020-21 FIG 808.SDR DL72W970289Batteries · dischargedFOUND ON L/O, R-1 EMEGENCY EXIT LIGHT WOULD NOT TEST. FOUND BATTERIES DEAD. REPLACED SAME, OPS CK OK.SDR DL72W962240Skin · gougedUPPER L/E SKIN GOUGED. REPAIRED SKIN PER SRM 55-20-3 FIG 1.SDR DL72W962239Skin · gougedTWO HOLES PUNCTURED IN STIFFENER ON UPPER SKIN. REPAIRED STIFFENER PER SRM 55-20-3 FIG 3.SDR DL72W962180Frame · crackedFWD FRAME CRACKED AT UPPER HINGE. REPAIRED PER SRM 52-40-2 PG 15.SDR DL72W961944Web · crackedA .25 INCH CRACK AT LIGHTENING HOLE, TORQUE BOX VERTICAL WEB STA 1223. REPAIRED PER M/M 53-11-0 PG 828.SDR DL72W961943Door · crackedRT AFT SERVICE DOOR HAS .375 INCH VISIBLE CRACK IN UPPER HINGE CUTOUT ON FWD FRAME. REPAIRED PER SRM 52-40-2 FIG 4.SDR DL72W961942Door · crackedA .375 INCH VISIBLE CRACK IN UPPER HINGE CUTOUT OF LT AFT SERVICE DOOR. REPAIRED PER SRM 52-40-2 FIG 4.SDR DL72W960809Fire Detector · failedPILOT REPORT, AFT LAV FIRE DETECTOR GIVES FIRE INDICATION WITH NO EVIDENCE OF FIRE OR SMOKE. REPLACED DETECTOR AFT LAV, TEST NORMAL.SDR DL72W960116Spar · crackedTHE RIGHT HAND ELEVATOR REAR SPAR HAD A CRACK EMANATING .25 INCH FROM THE INBOARD SIDE OF THE SHEAR PLATE, AT THE THIRD FROM INBOARD TAB HINGE FITTING-TO-REAR SPAR ATTACHMENT. CRACK WAS WITHIN THE S/B 55-0087 INTERIM REPAIR 0.250 ALLOWABLE LIMIT ON CRACK LENGSDR DL72W960701Turb Blades · failedON ENGINE DISASSY, FOUND ALL 4TH STG TURB BLADES FRACTURED NEAR PLATFORM. UNKNOWN BMOD/FOD NOTED ON 3RD STG TURB BLADE LEADING EDGES. EVIDENCE SUGGESTS THAT THE OBJECT(S) CAUSING THIS DAMAGE, ALSO CAUSED THE 4TH STAGE BLADE FRACTURE.SDR DL72W954316Blade · failedON TAKEOFF, NR 3 ENGINE FLAMED-OUT, RETURNED PVR. INITIAL INSPECTION FOUND NR 3 TURNBINE BLADES DISINTEGRATED. REPLACED NR 3 ENGINE FOR RETURN TO SERVICE.SDR DL72W953921Eel Batteries · dischargedOVERWING EMERGENCY LIGHT INOP. REPLACED RACK AND BATTERIES, OPERATION NORMAL.SDR DL72W953441Actuator · rupturedAT 5,000 FLT ON DEPT, SYS-A HYD LOW PRESS LIGHT ILLUM WITH FWD PANEL SYS A-LIGHT. SYS-A HYD QTY AND PRESS INDICATES ZERO. EMERGENCY CHECK LIST COMPLETED AND FUEL DUMPED, RETURNED TO DFW. FOUND NR 4 SLAT ACT RUPTURED. REPLACED ACT AND SERVICED HYD TO FULL. SDR DL72W953145Angle · cracked1.5 INCH CRACK IN ANGLE OF FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. REPAIRED PER DL ERA 301995-14AD.SDR DL72W952753L/E Rib · crackedA .5 INCH CRACK ON NR 4 SLAT L/E RIBS AT I/B AND O/B SIDES OF TRACK. FOUND DURING A-2 LETTER CHECK. REPAIRED PER MM 57-54-0.SDR DL72W951453Air Distr · odorON APROACH, HAD UNKNOWN NOXIOUS FUMES IN AFT PASSENGER CABIN. MADE EMERGENCY DESCENT, LANDED AGS. VISUALLY INSPECTED CABIN AND CARGO BINS FOR SPILLS, RAN ENGINES AND PRESSURIZED CABIN DID NOT HAVE ANY ODOR. RETURNED TO SERVICE.
Back to N831L, cancelled Feb 23, 2004