N58101
Service difficulty reports · 128
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 = 'N58101' AND registry_match = 'registration' 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 = 'N58101' AND registry_match = 'registration' 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 CALA2021070101008Skin · crackedPANEL IDENTIFIED ON R-315 AS "LEADING EDGE ABOVE PYLON" SKIN CRACKED IN CORNER(ON REPAIR RACK) FABRICATED NEW SKIN PANEL IAW DWG114N1802 REV L AND B757 BAC 530 0-2 REV J PARAGRAPH 8.2.1 FIG 3. INSTALLED WEBS AND SECURING BRACKETS IAW 51-40-02 PARAGRAPH 5 AND DSDR CALA2021070101007Intercostal · crackedINTERCOSTAL AT STA 1480-1500 26R-27R CRACKED REMOVED AND REPLACED INTERCOSTAL AND CHORD IAW DWG 146N54 11 AND B757 SRM 51-40-02 SEE PARTIAL WORK ACCOMPLISHED.SDR CALA2021070101006Intercostal · corrodedCORROSION ON INTERCOSTAL CHORD AT NUTPLATES STA 1440-1460 BETWEE N STR 27R AND 26R REMOVED AND REPLACED INTERCOSTAL, CHORD IAW DRAWING 146N5215 AT STA 1440-1460 PN 146N5214-2 DUE TO CORRODED. OUT OF LIMITS 100 P ERCENT LOSS OF MATERIAL. SEE PARTIAL WORK ACCOMPSDR CALA2021063001002Skin · crackedPANEL IDENTIFIED ON R-315 AS "LEADING EDGE ABOVE PYLON" SKIN CRA CKED IN CORNER(ON REPAIR RACK) FABRICATED NEW SKIN PANEL IAW DWG114N1802 REV L AND B757 BAC 530 0-2 REV J PARAGRAPH 8.2.1 FIG 3. INSTALLED WEBS AND SECURING BRA CKETS IAW 51-40-02 PARAGRAPH 5 ANDSDR CALA2021063001001Intercostal · corrodedCORROSION ON INTERCOSTAL CHORD AT NUTPLATES STA 1440-1460 BETWEE N STR 27R AND 26R REMOVED AND REPLACED INTERCOSTAL, CHORD IAW DRAWING 146N5215 AT STA 1440-1460 PN 146N5214-2 DUE TO CORRODED. OUT OF LIMITS 100 P ERCENT LOSS OF MATERIAL. SEE PARTIAL WORK ACCOMPSDR CALA2021063001000Intercostal · crackedINTERCOSTAL AT STA 1480-1500 26R-27R CRACKED REMOVED AND REPLACED INTERCOSTAL AND CHORD IAW BOEING DWG 146N54 11 AND B757 SRM 51-40-02 SEE PARTIAL WORK ACCOMPLISHED.SDR CALA2021062500957Housing · gougedREF AMES NR 0697. EXTERIOR HANDLE SURROUND IS GOUGED IN 2 PLACES - L1 DOOR DOOR MECHANISM DOOR HANDLE PAN REMOVED AND REPLACED IAW B757 SRM 51-40-02. REV 133 DATED 5-20-21 ADD EMP:V934494SDR CALA2021062000920Shim · migratedDURING AC C-CHECK AT ILN, MAINT DISCOVERED MAJOR SHIM P/N BA CS40R21C38F MIGRATION COMMON TO THE LEFT WING BETWEEN THE FWD O/ B DRAG FITTING ASSY PN 12N7009-11 AND FRONT SPAR ASSY PN 112N300 2-15. THE SHIM MIGRATED I/B BY APPROX 0.600 INCH AND THE THICKNE SS CSDR CALA2021062000919Shim · migratedDURING AC C-CHECK AT ILN, MAINT DISCOVERED MAJOR SHIM P/N BA CS40R21C38F MIGRATION COMMON TO THE LEFT WING BETWEEN THE FWD O/ B DRAG FITTING ASSY PN 12N7009-11 AND FRONT SPAR ASSY PN 112N300 2-15. THE SHIM MIGRATED I/B BY APPROX 0.600 INCH AND THE THICKNE SS CSDR CALA2021062000918Shim · migratedDURING AC C-CHECK AT ILN, MAINT DISCOVERED MAJOR SHIM P/N BA CS40R21C38F MIGRATION COMMON TO THE LEFT WING BETWEEN THE FWD O/ B DRAG FITTING ASSY PN 12N7009-11 AND FRONT SPAR ASSY PN 112N300 2-15. THE SHIM MIGRATED I/B BY APPROX 0.600 INCH AND THE THICKNE SS CSDR CALA2021062000917Shim · migratedDURING AC C-CHECK AT ILN, MAINT DISCOVERED MAJOR SHIM P/N BA CS40R21C38F MIGRATION COMMON TO THE LEFT WING BETWEEN THE FWD O/ B DRAG FITTING ASSY PN 12N7009-11 AND FRONT SPAR ASSY PN 112N300 2-15. THE SHIM MIGRATED I/B BY APPROX 0.600 INCH AND THE THICKNE SS CSDR CALA2021052800747Stringer · corrodedAFT LOWER CARGO STRINGER 28R AT FUSELAGE STATION 1380 IS CORRODE D ON BOTTOM INBOARD SIDE OF STRINGER FLANGE REMOVED AND REPLACED S28R, STATION 1380 IAW B757 SRM 51-40-02 PA RA 4, PARA 7 ADD EMP:V921265SDR CALA2021032200348Controller · failedAUTO PRESS CONTR 1 AND 2 INOP CABIN AUTO INOP INSTALLED SERVICEABLE #2 CABIN PRESSURE CONTROLLER REF AMM 21-31-02-401, VERIFIED BIT TEST PASSED OF #1 & #2 CONTROLLER BIT PROCEDURE REF FIM 21-30-815-802. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1106035 SN OSDR CALA2019121602215Selector · malfunctionedPRESSURIZATION CONTROL EICAS MESSAGE CABIN ALTITUDE SHOWN. CABIN ALT & CABIN ALTITUDE LIGHTS ON. COULD NOT CONTROL THE CABIN PRESSURE IN THE MANUAL MODE (DESCRIBE CAUSE OF DEPRESSURIZATION , IF KNOWN) TALKED TO THE CREW AFTER LANDING AND THEY TRIED BOTH AUSDR CALA2019062201043Bolt · missingFMC FUEL DISAGREE MESSAGE ON PROG PG 2 WITH ASSOCIATED DECREASE IN LEFT MAIN TANK QUANTITY. VISUAL CONFIRMATION OF FLUID/VAPOR FROM LEFT WING/ENGINE AREA. COMPLIED WITH QRH PROCEDURE 120.3 FOR FUEL LEAKAGE. SCREEN CONFIRM SOURCE OF FUEL LEAKAGE. ACCOMPLISHESDR CALA2019021700257Relief Valve · malfunctionedL ENG HI STAGE EICAS C THE LEFT ENGINE HPSOV IS CLOSED BECAUSE THE HIGH STAGE BLEED PRESSURE IS TOO HIGH UPON INITIAL CK FOUND OVERPRESSURE SWITCH TRIPED. WITH LIGHT ON. RESET AND ACP''D AMM 36-00-23 HPSOV AND PILOT TEST TEST WAS NORMAL. FIM 36-10-00 PG 3 BLOSDR CALA2018051701296Frame · dentedTWO DENTS FOUND ON THE FWD CARGO FRAME, BS 520, STRINGER 24L. FOUND OUT OF LIMITS IAW SRM 53-00-07 P101. TRIMMED AREA AND ACCOMPLISHED A REPAIR IAW ECRA 5310-07406, PART 1.SDR CALA2018021600649Housing · faultyAFT RIGHT DOOR EXTERIOR EMERGENCY LIGHT IS OUT REPLACED LIGHT BASE . LIGHT CHECKED GOOD. WDM 33-51-15SDR CALA2018021600648Contactor · dirtyR2 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. CLEANED THE CONTACTOR . LIGHTS OP CHECKED GOOD IAW 33-51-201-962-001.SDR CALA2018012100263Control Unit · faultyFIVE SECONDS INTO TAKE OFF POWER, RT GENERATOR OFF AND BUSSES OFF. REMOVED AND REPLACED THE NR 2 GENERATOR CONTROL UNIT IAW AMM 24-22-02. PERFORMED AN OPS CHECK IAW AMM 24-22-00-715-001.OPS CHECKED GOOD.SDR CALA2017090803083Sign · detachedR2 DOOR EMERGENCY EXIT SIGN FELL OFF THE MOUNTING. SECURED THE SIGN.SDR CALA2017090403042Unknown · odorWET SOCK ODOR DURING TAKEOFF FOR 5 MINUTES, THEN CLEARED. REPLACED THE RT AND LT RECIRCULATION FAN FILTERS. TURN ON APU AND RAN PACKS NO ODORS NOTED THIS TIME. DETECTED NO FUMES. APU BLEED THRU BOTH PACKS, DETECTED NO FUMES. OPERATION DETECTED NO FUMES OSDR CALA2017072402358Sensor · looseDURING CRUISE AT FL360, THE AIRCRAFT ABRUPTLY YAWED AND THE LT WING SLIDE MESSAGE APPEARED FOR 3 SECONDS. SECURED THE LEFT OVER WING SLIDE PROXIMITY SENSOR IAW AMM 25-65-00. OPS CHECKED OK.SDR CALA2016112500959Hydraulic Line · leakingLEFT HYD SYSTEM LOSS. EMERGENCY DECLARED. LEFT HYD SYSTEM LEAKING FROM FLEX LINE FOR TILT ACTUATOR ABOVE RT MAIN LANDING GEAR REPLACED HYD FLEX LINE. BLED AND LEAK CK OK.SDR CALA2016111400911Light · inoperativeRT EXTERIOR EMERGENCY LIGHT AT DOOR 2R OR MID DOOR IS INOP. RELAMPED, OPS CK GOOD REF AMM 33-51-06.SDR CALA2015061500510Pan · wornAFT CARGO DOOR LOWER SIDE OF DOOR PAN WORN IN SEVERAL AREAS & TEFLON PAINT WORN OFF. AFT CARGO DOOR LOWER SIDE PAN & TEFLON PAINT ADDRESSED IN PREVIOUS WIPS AS REQUIRED LEVELING COMPOUND IAW AMM 51-41-00-352-013. CURE TIME COMPLIED WITH ALSO CLOSED AREA OPENSDR CALA2015061500509Beam · wornLOWER CTR SECTION OF DOOR PAN ON FWD CARGO DOOR WORN IN 2 SPOTS & TEFLON PAINT WORN AWAY. AREA PAN THAT MAKES CONTACT WITH PRESS SEAL, THE LOWER CTR SECTION OF DOOR PAN OR BEAM WAS REPLACED PN 1 REPAIRED IAW ECRA 5230-01969. DAILY INSPECTION REQUIRED WITH PESDR CALA2015061100501Flap · damagedRIGHT INBD FLAP HAS 2 EACH ELONGATED FASTENER HOLES, LOCATED INSIDE PANEL 655AR. REPAIRED 2 EACH RT INBD FLAP FASTENER HOLES IAW ECRA 5750-0 4789 SEE WIPS FOR WORK ACCOMPLISHED.SDR CALA2015061000499Hinge Fitting · crackedNUMBER 1 ENG INBD T/R AFT HINGE FITTING UPPER ATTACH BOLT NR 1 HOLE CRACK INDICATION. CONFIRMED NDT PART 6 SECTION 51-00-16 & 51-00-17 AFTER SECOND OVERSIZE, REF EA 5451-01040 REV A STEP 4.3. REPAIRED FASTENER LOCATION IAW ECRA 5451-01176.SDR CALA2015060400485Stringer · damagedLEFT FUSELAGE, AFTER PREVIOUS REPAIR REMOVED, FOUND STRINGER 17LT BETWEEN STATION 600 & 620 HOLES ARE DAMAGED & DIMPLED ON OUTER SURFACE. INSTALLED REPAIR CHORD IAW AVO IAH043015-0101-1A & ECRA 530 0-02178.SDR CALA2015060400484Skin · cracked4R DOOR HAS A CRACK ON LIGHTNING HOLE 4TH HOLE FROM TOP. REPAIRED 4R DOOR IAW ECRA 5210-02624.SDR CALA2015060400483Frame · wornAFT FUSELAGE FRAME WORN AT STATION 1640, BELOW STRINGER 5R. REPAIR OF AFT FUSELAGE FRAME AT STATION 1640 BETWEEN STRINGER 5R & 6R IAW ECRA 5310-06504.SDR CALA2015052100410Doubler · dentedLARGE DENT ON EXISTING FUSELAGE SKIN DOUBLER AT STATION 620 & STRINGER 16L. REMOVED DAMAGE FROM STATION 590 - 650, STRINGER 13L - 20L, REPAIRED IAW SRM.SDR CALA2015051800405Structure · crackedCRACK ON L4 DOOR OUTER CHORD, 146N6100-59, IN RADIUS AT APPROX STATION 1669 AT DOOR HANDLE PAN CUT-OUT. R & R CHORD IAW SRM 51-40-02 & DWG 146N6100.SDR CALA2015051800402Stringer · damagedLEFT FUSELAGE AFTER PREVIOUS REPAIR REMOVED, FOUND STRINGER 15L FROM STATION 600 - 630 ALL THE HOLES ARE DIMPLED ON OUTER SURFACE. REMOVED & REPAIRED DAMAGED STRINGER 15L IAW SRM 53-00-03.SDR CALA2015051800401Stringer · damagedRIGHT SIDE FUSELAGE, STRINGER 16LT, DAMAGED, DENTED BETWEEN STATION 620 - 640. DAMAGED FOUND AFTER PREVIOUS REPAIR REMOVED. R & R DAMAGED STRINGER 16L IAW SRM 53-00-03.SDR CALA2015051500400Frame · crackedCABIN FRAME STATION 800 IS CRACKED AT FASTENER BETWEEN STRINGER 8R & 9R. FABRICATED & INSTALLED REPAIR CHANNELS 1 & 2 AT STATION 800 BETWEEN STRINGER 8R & 9R IAW SRM 53-00-07.SDR CALA2015051100384Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION STATION 365 BL-0 THRU 45 APPROX. REMOVED CORROSION AT CABIN FLOORBEAM, MATERIAL REMOVED FROM ORIGINAL .125 & THICKNESS RBL22.25. DAMAGED CLEANED UP & IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-51. DAMAGE IS LIMITED TO EXISDR CALA2015050600374Frame · crackedCABIN FRAME CRACKED AT PSU RAIL BETWEEN STRINGER 8R & 9R. REPAIRED CABIN FRAME AT STATION 760 BETWEEN STRINGER 8R & 9R IAW SRM 53-00-07. REPAIR ONE DETAIL ONE PLACED ON DIP TO DO DETAIL VISUAL INSPECTION OF REPAIR AT 12000 FLIGHT CYCLES OR 50000 AIRFRAME FLISDR CALA2015050600371Frame · crackedCABIN FRAME IS CRACKED AT FASTENER, STATION 1580 BETWEEN STRINGER 8 RT & 9 RT. REPAIRED CABIN FRAME IAW SRM 53-00-07 REPAIR 1.SDR CALA2014100801321Oven · malfunctionedAPPROXIMATELY 7 HOURS INTO FLIGHT A BURNING RUBBER SMELL EMANATED FROM THE MID GALLEY OR MID LAVATORY AREA THAT GREW WORSE. ACCOMPLISHED SMOKE FUME CHECKLIST. REMOVED LT & RT UTILITY BUS, LT & RT RECIRCULATION FAN. AFTER LANDING EQUIPMENT COOLING LIGHT CAME SDR CALA2014100601314Cable · out of rigLP 7901478 VERY LOW SPEED REJECTED TAKEOFF. NO AIRSPEED INDICATED. CHECKED LIMITS IN MM 05-51-14 BLOCK 201, NO ACTION REQUIRED. CREW CLAIMING WHILE STARTING TAKEOFF & USING RUDDER PEDALS FOR STEERING NOT GETTING PROPER RESPONSE STEERING. NOSE STEERING CABLSDR CALA2014052800686Radio Altimeter · faultedON FINAL THRUST LEVERS AT IDLE AT 3000'', LT RA SIGNALED INOPERATIVE. CONFIG LIGHT GEAR NOT DOWN, LIGHT WARNING HORN CAME ON. WENT AROUND PUT THE GEAR DOWN NORMAL LANDING. PERFORMED FIM TASK 34-33-00-815-807, RA FLAG DISPLAYED ON CAPTAIN`S EADI, PASSED. PERSDR CALA2014032100376Probe · faultyRT ENG PROBE HEAT REPLACED P1 PROBE IAW MM73-21-04-404-013-R-00.SDR CALA2012111300792Button · unsecureF/O MICROPHONE SELECTOR PANEL, LEFT VHF SELECTOR BUTTON CAME OFF. SECURED F/O LEFT VHP SELECTOR BUTTON. OK TO CONTINUE.SDR CALA2009081400455Fan · malfunctionedAT 4.5 HOURS INTO FLIGHT FUMES IN AFT GALLEY COMING FROM AIR VENTS (OVEN OPENED AND NOT SMELLING) PER A/C SMOKE/FUME CHECK LIST BOTH RECIRC FANS TURNED OFF, FUMES STOPPED. REMOVED AND REPLACED RIGHT RECIRCULATION FAN PER AMM 21-25-01, ALSO REMOVED AND REPLACESDR CALA2009080400424Battery Pack · dischargedRIGHT AFT EMERGENCY FLASHLIGHT IS NOT FLASHING. REMOVED AND REPLACED BATTERY PACK, CHECKS NORMAL.SDR CALA2009061200309Angle · crackedMAIN CABIN O/B CORD CREASE BEAM ATTACHED TO FUSELAGE AT STA 984 LBL 45.70 IS CRACKED. REPAIRED STA 984 LBL 45.70 O/B CREASE BEAM REF ECRA 5311-01454.SDR CALA2009061500311Attach Bracket · damagedFWD I/B MOUNT BRACKET FOR PANEL 572HB IS BROKEN OFF ON LEFT WING I/B FLAP. REPAIRED DAMAGED AREA OF FLAP AT ATTACH BRACKET REF ECRA 5752-0 1395 INTERIM REPAIR. ISSUED DIP FOR PERMANENT REPAIR WITHIN 24 MONTHS HS CTL 94487. ACCOMPLISH A PERMANENT REPAIR WITHSDR CALA2009061200308Bear Strap · corrodedB757-53-3-0246, AFT CARGO STA 1425 O/B OF S27R, CORROSION ON INTERNAL SKIN DOUBLER, MARKED. ACCOMPLISHED BEAR STRAP INTERIM REPAIR REF ECRA 5331-01455. ISSUED DIP TO ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS FROM 6/08/2009. PLANNING TO CONTACT ENGINEER
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