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 CALA2026033014919Skin · damagedTHE REPAIR INCORPERATED VIA ECRA 5720-03636 FOR THE R/H WING INT ERSPAR LWR SKIN APB PANEL P/N 757-3401-2 REPLACEMENT BETWEEN WS 711.50 & 743.50 IS APPROVED AS TIME LIMITED FOR 18 MONTHS UNTIL PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA).SDR CALA2026033014917Skin · damagedTHE REPAIR INCORPERATED VIA ECRA 5720-03636 FOR THE RT WING APB SPLICE & ADJACENT LWR SKIN PANEL HOLES CRACKED INBD OF WS 711.5 0 & THE LWR SKIN PANEL L-8 STRINGER AT APPROX. WSTA 700 IS APPROVED AS TIME LIMITED.SDR CALA2026033014912Skin Splice · crackedRIGHT WING OTBD MAIN SKIN SPLICE WAS CRACKED. REMOVED AND REPLACED SKIN SPLICE IAW DWG 757-3400, SRM 51-40-02, ECRA 5720-03636 REV-, & REO G25831, REV IR.SDR CALA2026033014911Angle · crackedRT WING LOWER STR NO. 8 SPLICE PN 757-3403-4 PER REO G25831, REMOVED AND REPLACED STR 8 SPLICE. REMOVED AND INSTALLED FREEZE PLUGS AT DISCREPANT HOLE, RESTORED COATING REF B737NG 51-40-02, ECRA 57220-03636 REV - AND AAR REO G25831 REV IR.SDR CALA2026033014910Skin · crackedRIGHT WING OTBD FWD SKIN SPLICE WAS CRACKED. R & R THE SKIN SPLICE IAW DWG 757-3400, REV E, SRM 51-40-02, EC/RA 5720-03636 REV-, & REO G25831, REV IR.SDR CALA2026033014890Skin · crackedCRACK IN RT LWR WING SKIN FOUND DURING EA 5720-03614 REV 'A' INSPECTION PERFORMED IN SFO BY UAL. AIRCRAFT FERRIED TO GSO FOR REPAIR. MAJOR REPAIR. REMOVED, LOCATED, DRILLED AND INSTALLED NEW RT WING LOWER OUTBD SKIN PANEL AND RESTORED COATINGS REF SRM 51-40SDR CALA2025100609655Wire · damagedAILSE EMERGENCY LIGHT AT SEAT 8C INOP. REPAIRED RED VENDOR WIRE AT SEAT 8C REF WDM 33-51-21-1. REQUIRES OPS CHECK. PERFORMED OPS CHECK OF EMERGENCY AISLE LIGHT AT SEAT 8C. OPS CHECK GOOD, REF AMM 33-51-00SDR CALA2025081907935Display · faultedRT MCDU FAILED AFTER 1HOUR OF FLIGHT. CYCLED CB TOMC DIRECTION TWICE. STILL INOP. F/O MCDU REPLACEMENT PERFORMED IAW AMM34-61-02/401 REV 137TEST SATISSDR CALA2025081507822Ceiling Panel · no discrepancyREMOVED CEILING PANELS FROM L2 TO OVERWING EMER DOORS ROW 20 AND 21 INSTALLED CEILING PANELS FROM L2 TO OVERWING EMER DOORS ROW 20 AND 21 IAW AMM 25-22-01-404-067SDR CALA2025072106763Oven · fireOVEN 205 FIRE. PBE AND FIRE EXT USED. OVEN 205 FIRE L1 DOOR PBE USED, FIRE EXTINGUISHER WAS NOT USED BUT WILL NEED TO BE INSPECTED AND RESEALED. REMOVED AND REPLACED L1 PBE AND FIRE EXTINGUISHER PER 26-26-02 SEE LOG PAGE 5616867 FOR POSITION 205 OVEN. R&R GALSDR CALA2025071406567View Port · damaged4R SLIDE VIEW PORT IS EXCESSIVELY SCUFFED/ SCRACHED-DIFFICULT TO SEE SLIDE GUAGE CLEARLY NUTPLATE FOR 4R SLIDE VIEW PORT STRIPPED AND WONT HOLD SCREWS FOR VIEW PORT LENS TO STAY INPACT. REQUIRES NEW DOOR COVER PART NIS IN LAX. ACCOMPLISH REPETITIVE INSPECTIONSDR CALA2025061605561Unknown · odorBAD ODOR COMMING FROM BEHIND AFT CARGO COMPARTMENT PANEL REMOVED AFT PANEL OF AFT CARGO BAY AND WAS GREETED BY AN UNPLESENT SMELL. PANEL WAS REMOVED FOR TROUBLESHOOTING FUP 5112977 ADD EMP: U433812 REMOVED AFT PIT SIDEWALL PANELS 161CW AND 162CW FOR ACCESS TO SDR CALA2025061105454Lamp · inoperativeDOOR 3R SLIDE LIGHT WILL NOT ILLUMINATE DOOR 4R SLIDE GIRT BAR ENGAGED LIGHT NOT ILLUMINATING. APPLYING MEL, VERIFIED DOOR 4R IS ARMED FOR DEPARTURE. APPROVED MEL 2566V COMPLIED WITH MEL. DOOR 4R VERIFIED ARMED PROPERLY FOR DEPARTURE. *DM* REF FIM 25-66 FAULT SDR CALA2025051504702Modulating Valve · faultedFLT DECK VERY WARM AFTER TAKEOFF QRH PROCD NO HELPFLIGHT CREW REPORTS NO AIR FLOW FROM GASPER VENTS, NO ADVISORY MSG OR EICAS MSGS. NO DIFFERENCE IN AIR FLOW REGARDLESS OF FLIGHT PHASE. CBS OPENED REF AMM 25-13-03 GLARESHIELD REMOVAL. CHECKED DUCTING BEHIND PASDR CALA2025031202738Slide · faultedSLIDE FAULTED, REMOVED L2 DOOR IN REF TO AMM TASK 25-66-01-004-154 REMOVED AND REPLACED IAW AMM 25-66-01-404-044. C/W GMM RII, VERIFIED PART NUMBER, SERIAL NUMBER AND EFFECTIVITY.SDR CALA2025021102294Bulb · inoperative2L SLIDE LIGHT BULBS INOP INSTALLED NEW LIGHT CAP ASSY. LIGHT OPS CHECKS GOOD, OK TO CONTINUE PARTS USED: 19-3350-3-0009,QTY :1SDR CALA2025021102288Indicator · stuckDOOR 1R ARMING INDICATOR KNUCKLE GETS STUCK ON THE PLASTIC DOO R CASING WHEN ARMING READJUSTED PANEL ON DOOR 1R AS REQUIRED. INDICATOR KNUCKLE IS OPERTIONAL GOODSDR CALA2024110601044Lock · faultyWHILE ACCOMPLISHING J/C# 19-2560-1-9801 ON L4 DOOR, OBSERVED L4 'SLIDE ARM LIGHT' FLICKERING INTERMITENTLY WHEN ARMED. R/R L4 DOOR GIRT BAR (M&E 19-2566-3-0005) AND FWD AND AFT BAR LOCK ASSY (M&E 19-2566-3-0002) IAW AMM 25-66-10. OPS CHECKS NORMAL AT THIS TIMESDR CALA2024083000516Controller · faultyON TAKEOFF L ENG BLEED EICAS MSG. PERFORMED FIM 36-10 FAULT TREE 811 PERFORMED PREVIOUS FLIGHT TAKEOFFS BLEED PARAMETERS READOUT AND NO ABNORMAL INDICATIONS FOUND AT THIS TIME.AS PRECAUTION REPLACED LEFT AIR SUPPLY THERMAL OVERTEMP SWITCH AS PER AMM 36-22-01-SDR CALA2024080802179Access Panel · damagedREF AMES NON ROUTINE 173487-0400-0033.GENERATING ITEM:19-5400- 1-2009.#1 PYLON UPPER ACCESS 432AL, O/B UPPER SKIN CHAFED DUE TO HYD LINE BLOCK CLAMP WORKING FWD & AFT, TAG 10145,WORK WITH N/R 0400-0032.SDR CALA2024080602164Scuff Plate · damagedL4 DOOR FWD SCUFF PLATE CORNER FLATTENED ON RIDGE. DOESN''T ALLOW DOOR GATE TO CLOSE PROPERLY. (REF N/R 0800-0022). QC ACCEPTED. NOTE: THIS LOG PAGE WAS MARKED RII INADVERTENTLY. REMOVED AND REPLACED L4 DOOR FWD SCUFF PLATE WITH NEW P/N 146N610Y83 IAW B757 AMMSDR CALA2024080602162Scuff Plate · crackedL4 DOOR AFT SCUFF PLATE CORNER FLATTENED AND CRACKED ALONG TOP RIDGE. DOESN''T ALLOW DOOR GATE TO CLOSE PROPERLY. (REF N/R 0800-0022). REMOVED AND REPLACED L4 DOOR AFT SCUFF PLATE WITH NEW P/N 146N6104-59 IAW B757 AMM 53-13-01-424-003. SEE PARTIAL WORK ACCOMPSDR CALA2024080602168Pan · damagedL1 EXTERIOR DOOR HANDLE PAN GOUGED,AS MARKED AMES INSPECTOR V921207 BOUGHT THE FINAL INSPECTION. NONE L1 EXTERIOR DOOR HANDLE PAN DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED REPLACED AND INSTALLED PAN PN141N6302U3 IAW B757 SRM 51-40-02 PARA 4 AND 9. BOEING DRASDR CALA2024080602166Pan · damagedL4 DOOR EXTERNAL HANDLE PAN IS GOUGED IN MULTIPLE AREAS TO INCLUDE AT THE PRESS TO RELEASE BUTTON. L4 DOOR EXTERNAL HANDLE PAN DAMAGE FOUND TO BE OUT OF LIMITS DETAILS. REMOVED AND REPLACED AND INSTALLED PAN P/N -146N6201-7. IAW SRM 51-40-02 PARA 4 AND 9 AND SDR CALA2024080602163Skin · corrodedREPAIRED CORROSION ON INTERNAL SKIN DOUBLER AT CUTOUT FOR PANEL 154AR IAW UNITED EC/RA 5300-03134 AND AMES DOC #47625REA02. REPAIRED CORROSION ON INTERNAL SKIN DOUBLER AT CUTOUT FOR PANEL 154AR IAW UNITED EC/RA 5300-03134 AND AMES DOC 47625REA02. SEE PARTIAL SDR CALA2024080602165Angle · corrodedLIGHT CORROSION FORMING AROUND NUTPL ATES ON LOWER SIDE OF ALC RT TRANSITION ANGLE FLOOR TO SLOPING SIDE WALLS, BS 1300 TO 1360 RBL 24. REMOVED AND REPLACED DAMAGED ALC RT TRANSITION PANEL BS 1300-1360 WITH NEW P/N 146N5391U182 IAW SRM 51-40-02 PARA 4 AND 7SDR CALA2024080602169Bracket · corrodedCORROSION ON BOTH OF THE BRACKETS THAT HOLD THE LEFT OVERWING ESCAPE SLIDE RELEASE PIN INSIDE OF THE LEFT SLIDE COMPARTMENT.#3653 REMOVED AND REPLACED L/H OVERWING EXCAPE SLIDE RELEASE PIN BRACKET ASSY IAW B757 SRM 51-40-02 PARA 7. SEE PARTIAL WORK ACCOMPLISHESDR CALA2024080602167Bracket · corrodedTHERE IS CORROSION ON THE 2 STOWAGE BRACKETS FOR THE RIGHT OVERWING ESCAPE SLIDE RELE ASE CABLE PIN NO 3650. REMOVED AND REPLACED R/H OVERWING EXCAPE SLIDE CABLE RELEASE BRACKET ASSY P/N 416N2826-80 IAW B757 SRM 51-40-02 PARA 4. SEE AMES NON ROUTINE 173487-01SDR CALA2024050801411Compressor · stalledL ENGINE COMPRESSOR STALL ON DEPARTURE AMM TASK 71-00-00-715-049-R03 & TEST NO 13 PER TASK 71-00-00-715-223-R03. ESCPP ROHAN ATTACHED PIC OF E1 EGT AUTO EVENT. ENGINEERING UPDATE: PERFORM FIM TASK 71-06 FAULT TREE 812, "ENGINE SURGE AND RECOVERY". PERFORM BLOSDR CALA2024020300310Engine · slowON TAKEOFF LT ENG SLOW TO SPOOL WITH TL MATCHED GOT AUTO THROTTL E DISC CAUTION T/S AS PER FIM 71-06 FAULT TREE 801. PERFORMED A/T BITE, EEC BITE, BVCU BITE AND TPU BITE CHECK. HIGH & LOW IDLE CHECKS, ACCELERATION AND DECELERATION TESTS PASSED, OK TO CONTINUE.SDR CALA2024010900069Actuator · leakingON T/O ROLL THE RIGHT YELLOW REV LIGHT CAME ON A GAIN EVEN AFTER MEL 7831 F HAD BEEN APPLIED. REVERSED MEL #2 ENG T/R. PERFORMED ACTUATOR LOCK, CROSSOVER SHAFT INTEGRITY TEST IN REF AMM 78-31-00. CHECK OK. PERFORMED #2 ENG T/R OPS TEST IN REF AMM 78-31-00-715SDR CALA2024010900070Thrust Reverser · warning messageNO 2 ENGINE YELLOW REV LIGHT CAME ON DURING ROLL ON TAKE OFF RTO LOW SPD CYCLE REV TRIED 2ND. PLACARD #2 ENGINE T/R INOP PER MEL COWLING CLOSED AND SECURED. PLACARD #2 T/R INOP PER MEL .OK TO CONTINUE. DISPATCH DESK: 52 NAME: B.A. DATE: 07-JAN-24- NOC DESK: 75SDR CALA2024010800052Unknown · unknownAFTER POWER UP ON T/O ROLL-MOMENTARY RT ENG REVERSER LIGHT-RTO COMPLIED WITH DDP DDP COMPLIED WITH DISPATCH DESK: 24 NAME: DS DATE: 04-JAN-24- NOC DESK: 757 NAME: MC DATE: 04-JAN-24- RIGHT REVERSER INOP. CYCLED THRUST REV. 6 TIMES AND COULD NOT DUPLICATE FAULTSDR CALA2023112703476Computer · faultedLOW SPEED ABORT DUE TO AUTO THROTTLES NOT ENGAGING. PERFORMED CURRENT FAULTS NO FAULTS FOUND. AS PRECAUTION REMOVED AND REPLACED THRUST MANAGEMENT COMPUTER REF AMM 22-31-01. COMPUTER, THRUS OFF 19-2231-9-0002 1575 ON 19-2231-9-0002 2017 COMPUTER, THRUS OFF 19-SDR CALA2023112403458Unknown · unknownTE FLAP DISAGREE CAUTION MSG ON FLAP ON FLAP EXTENSION TO 25 IN GUIDANCE WITH FIM 27-51 FAULT TREE 808, BITE THE PSEU, NO PICTURE UPDATED PERFORMED FSEU BITE CHECK ON ALL 3 FSEU''S NO FAULTS WERE ON ANY PHOTO ATTACHED. CONDITION OF FLAP INDICATOR AND FLAP HANDSDR CALA2023111603405Unknown · unknownRIGHT REVERSER AMBER LIGHT ILLUMINATED AT 115KTS ON TAKEOFF FOUND NO MESSAGE UNDER STATUS PAGE OR UNDER ECS/MSG ON P61. PERFORMED T/R OPERATIONAL CHECKS IAW 78-30-00-715-037-R04 WITH NO DEFECTS NOTED. PERFORMED TASK MULTIPLE TIMES WITH SAME RESULTS. INSPECTED SDR CALA2023100602969Modulating Valve · faultyCOCKPIT TEMP TOO HOT-RAN CABIN TEMP HOT C-LIST. SOME CONTROL OF TEMP RE- GAINED L PACK OFF/R-STB REPLACED ZONE TEMP CONTROLLER, DID NOT FIX FLIGHT DECK COOLING ISSUE. REF AMM TASK 21-61-03-404-041. PARTS USED: 75-2162-9-0003,QTY :1 ROTABLE PARTS CHANGE WAS INDSDR CALA2023071402255Valve · inoperativeAT 37000FT CABIN ALT ALARMS WENT OFF. PILOTS NOTED THAT THE CABIN CONTROL PANEL THAT SHOWS ALT WAS PEGGED TO MAX. PILOT STATED HIS BAG OF CHIPS POPPED OPEN. PILOTS STATED THAT THEY FELT LIGHT HEADED AND WERE ABOUT TO DEPLOY MASK BUT PERFORMED EMERGENCY DECENT SDR CALA2023061901941Slide · detachedDOOR-MOUNTED ESCAPE SYSTEM DOOR 2L - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS FA HAD TO RECYCLE SLIDE ARMING LEVER MULTIPLE TIMES TO GET 2L SLIDE LIGHT TO STAY ON. AT DOOR 2L CLEANED DEBRI FROM GIRT BAR FLOOR MSDR CALA2023061901911A/C Pack · restrictedL PACK NO AIRFLOW OR TEMPERATURE CONTROL L ENG BLEED CLOSED WHEN PACK WAS TURNED OFF OPERATING NORMALLY. "FLT DECK TEMP" AUTO EVENT ON ECS PAGE. ALL BITE CHECK PASS, NO FAULTS. OPERATED REGULATION SYSTEM, THE COOLING SYSTEM AND THE REVERSE FLOW BOTH PACKS IN SDR CALA2023021000394Transmission · trippedTE FLAP DISAGREE BITE SFEU 1,2,3 REF FIM 27-51 TREE 805. SFEU 1,2&3 SHOWED NO EXISTING FAULTS. SFEU1 FAULT HISTORY LEG 0 REPORTED MSG # 305. SFEU2 FAULT HISTORY LEG 0 REPORTED MSG# 327. SFEU3 HAD NO FAULT HISTORY FOR LOG 0. TROUBLESHOT LH SIDE OF FLAP SYSTEM ISDR CALA2023020800352Panel · not reportedPDA 3 REF LP 3779230 FOUND PNL 433BL MISSING. REPLACED PNL . REF LP3779230. PARTS USED: 19-5453-3-0016,QTY :1 ENGINE NUMBER 1 PYLON OUTBOARD ROUND COVER MISSING. INSTALLED NEW PANEL AS PER IPC 54-53-01-5 LANYARD CONNECTED PANEL IS PRE PAINTED ACFT OK TO CONTISDR CALA2023012300184Processor · faultedLEFT FUEL TANK FLUCTUATES BETWEEN 14.6 AND 13.0 EVERY 30 MIN OR SO LEFT TANK AT STICK 87 IS 4.2 WITH ROLL 0 AND PITCH -5. RIHJY TANK AT STICK 7 IS 5.1. REMOVED AND REPLACED FUEL QTY PROCESSOR. REMOVED AND REPLACED FUEL QTY PROCESSOR. PERFORMED TANK UNIT CAPACSDR CALA2022121903437Outflow Valve · inoperativeCABIN ALT EICAS AT FL400. RT PACK OFF AUTO 1-2 CONTROLLER INOP. OVBD EX VAL STATUS DECLARE AN EMERGENCY. OUTFLOW VALVE WAS REPLACED AND AMM 05-51-24 PROCEDURE PERFORMED OPS CK GOOD PRESSURE HOLDS PER AMM CALLOUT.SDR CALA2022121403391Skin · noneSUPPORT TASK - LW NO. 4 SLAT TE WEDGE IB SIDE PREVIOUS REPAIR FOUND TO BE SEPARATING REF HAECO GSO NR 9286241 ACCOMPLISHED PERMANENT REPAIR OF L/W NO. 4 SLAT TE WEDGE IAW B75 ROTARY ACTUATORS, ACCOMPLISH TORQUE SAFETY AND OPS CHECK, CHECK 7-200 SRM 57-43-02-2RSDR CALA2022101402803None · inoperativeAFT L LAV NOT FLUSHING NO MOTOR SOUND LAV SWITCH WAS CYCLED SEVERAL TIMES TO OPERATE. ORDERED LAV SWITCH AND WILL PASS IT TO DAY SHIFT SUPERVISOR. REMOVED AND REPLACED FLUSHING SWITCH REF AMM 24-25- OPS CHECK GOOD PLACKARD REMOVED OK FOR SERVICE .SDR CALA2021071901137Strut · corrodedREF AMES NR 0966. NUMBER 2 ENGINE STRUT COMMON TO NOZZLE FAIRING AFT PAN SKIN HAS CORROSION AROUND BEARING HOLE BLENDED AFT PAN SKIN. FOUND TO BE OUT OF LIMITS. REMOVED AND REP LACED IAW B757-200 SRM 51-40-02 PARAGRAPH 9 AND B757-200 SRM 51- 40-04. SEE BACK ANSDR CALA2021071601115Strut · corrodedREF AMES NR 0966. NUMBER 2 ENGINE STRUT COMMON TO NOZZLE FAIRING AFT PAN SKIN HAS CORROSION AROUND BEARING HOLE BLENDED AFT PAN SKIN. FOUND TO BE OUT OF LIMITS. REMOVED AND REP LACED IAW B757-200 SRM 51-40-02 PARAGRAPH 9 AND B757-200 SRM 51- 40-04. SEE BACK ANSDR CALA2021071401093Stringer · corrodedAFT PIT STA 1620 STRINGER 29R FOUND TO BE CORRODED, 100 PERCENT MATERIAL LOSS FABBED REPAIR PART SEE AMES WORK ORDER 134918-0005. LOCATED AND DRILLED IAW BOEING DRAWING 146N5451 REV D AND SRM 51-40-02 ADD EMP:V931875SDR CALA2021071201076Frame · damagedREF AMES NR 0465. AD 2020-05-25 PREVIOUS REINFORCING FRAME REPAI R LOCATED IN INSPECTION AREA STA 1460 S25L-26L REMOVED AND REPLACED FRAME P/N 146N1029-11 AND FAIL SAFE CHORD P /N 146N1035-7 AT STA 1460 S24L-24R IAW BOEING DRW 146N1014 AND B 757 SRM 51-40-02 A
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