N8574Z
Service difficulty reports · 63
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 = 'N8574Z' 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 = 'N8574Z' 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 SWAA2026092832413Sill Drain · odorTSI - REPORTS OF AFT GALLEY SMELL. DURING INSPECTION OF AFT DOOR SILL DRAIN FOUND BOTH CAPT SIDE DOOR SILL DRAIN FITTINGS FILLED WITH DEBRIS CLEANED DOOR SILL SILL DRAIN FITTINGS IRT 38-11-00. NO FOUL SMELL NOTEDSDR SWAA2026092833840Seat · odorBAD ODOR COMING FROM THE LAST 4 ROWS OF AIRCRAFT. SANITIZED LAST 4 ROWS OF AIRCRAFT SEATS IAW SIPSDR SWAA2026091116924Lamp · inoperativeEXTERIOR EMERGENCY LIGHT BY LT AFT ENTRY DOOR INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04SDR SWAA2026061009570Elec Connector · looseEMERGENCY LIGHT FO SIDE AFT FLICKERS. OK TO CONTINUE PER MEL 33-2-04. SP1 B AUTH 322846; SECURED LOOSE CONNECTOR ON THE LIGHT ASSY IAW AMM 33-21-00. OPS CHKD GOOD. NO DEFECTS NOTED AT THIS TIME.SDR SWAA2026060806756Skin · delaminatedRIGHT OTBD AFT FLAP HAS AREA OF DELAMINATION, INBOARD AFT EDGE. REMOVED AND REPLACED RT OTBD AFT FLAP ON TASK CARD TTG8Q01BR0XB. REMOVED AND REPLACED RT OTBD AFT FLAP ON TASK CARD TTG8Q01BR0XB.SDR SWAA2026030575737Handle · brokenFORWARD MAIN ENTRY DOOR WHITE ASSIST HANDLE BROKEN. ATTACHED THE FWD MAIN ENTRY DOOR ASSIST HANDLE IAW MM 52-11-31SDR SWAA2025122955381Battery Pack · inoperativeEMERGENCY LIGHTS BATTERY PACK AT POSITION M1672 WILL NOT ILLUMINATES EMERGENCY LIGHTS. REPLACED BATTERY PACK AT POSITION M1672 PER AMM 33-51-06SDR SWAA2025121251761Battery Pack · inoperativeL1 EMERGENCY LIGHTS INOPERATIVE. R & R THE L1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2025102729004Pump · leaking45 MIN INTO FLIGHT, ENG 2 HYD PUMP LOW PRESSURE LIGHTILLUMINATED. ELEC 1 LOW PRESSURE LIGHT ALSO ILLUMINATED. RAN PROCEDURE IAW QRH & EXTENDED FLAPS VIA ALT FLAP SYS TO FLAPS 15 LANDING. REMOVED & REPLACED ENG. NR 2 EDP REF. AMM 29-11-11. OPS TEST GOOD, NO SDR SWAA2025102728412Pump · leaking45 MIN INTO FLIGHT. ENG 2 HYD PUMP LOW PRESSURE LIGHTILLUMINATED. ELEC 1 LOW PRESSURE LIGHT ALSO ILLUMINATED. RAN PROCEDURE IAW QRH & EXTENDED FLAPS VIA ALT FLAP SYS TO FLAPS 15 LANDING. REMOVED & REPLACED ENG NR 2 EDP IAW AMM 29-11-11. OPS TESTED GOOD, NO LSDR SWAA2025021996987Battery Pack · no testAFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2024102953341Cover · detachedEXIT ROW EXIT SIGN KNOCKED OFF<[01] SECURED SIGN COVER AS PER AMM 33-51-01 AT ROW 11.SDR SWAA2024102953469Cover · missingEXIT ROW EXIT SIGN KNOCKED OFF<[01] SECURED SIGN COVER AS PER AMM 33-51-01 AT ROW 11.SDR SWAA2024082830176Coffeemaker · odorBURNING SMELL FROM FRONT LEFT COFFEE MAKER<[01] R/R COFFEE MAKER PER AMM 25-30-01.<BR>OPS CHECK GOOD.SDR SWAA2024062796967Stringer Clip · crackedFWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT BOTH FRAME RIVETS; STA 500I STR 25R. HFEC VERIFIED.<[01] REMOVED AND REPLACED IAW SRM 51-40-02 AND SRM 51-40-05.;[02] C/W INSPECTIONSDR SWAA2024062791654Angle · crackedIN THE RH AC BAY; L ANGLE AT STA 663; RBL 31.5 RIVET HAS A CRACK EXTENDING VERTICAL TOWARDS THE CENTER FUEL TANK. VERIFIED WITH HFEC.<[01] THIS L ANGLE WILL BE REMOVED AND REPLACED ON TTG8Q00TH4J4.;[02] VERIFIEDSDR SWAA2024062791658Angle · crackedIN THE RH AC BAY; L ANGLE AT STA 663; RBL 35 RIVET HAS A CRACK EXTENDING VERTICAL TOWARDS THE CENTER FUEL TANK. VERIFIED WITH HFEC.<[01] THIS L ANGLE WILL BE REMOVED AND REPLACED ON TTG8Q00TH4J4.;[02] VERIFIEDSDR SWAA2024062890207Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500A-500B. REMOVED DAMAGE IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .009. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. CUTOUT & REMOVED DAMAGE SECTION OF TRANSITION ANGLE FROM STA 480SDR SWAA2024062890214Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500F-500G. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION SDR SWAA2024062890215Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500E-500F. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITIONSDR SWAA2024062890216Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500D-500E. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. REPLACED IAW SRM 51-10-02SDR SWAA2024062890217Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500C-500D. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION SDR SWAA2024062890218Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500B-500C. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITIONSDR SWAA2024062890219Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500A-500B<[01] REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. STEP 1 FWD CARGO R/H TSDR SWAA2024062890223Angle · corrodedFWD CARGO COMPT RH SHORT TRANSITION ANGLE AFT OF DOOR CORRODED STA 492-500A<[01] REMOVED CORROSION AT FWD CARGO R/H SHIELD SIDEPLATE ASSY STA 492 TO STA 500A PER SRM 51-10-02. MEASURED REMAINING MATERIAL THICKNESS OUT OF LIMITS PER SRM 53-30-15-1A-1 FIG.103; DSDR SWAA2024062790213Angle · corrodedFWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500H-500I<[01] REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E.;[02] RESOLVED ON FAULT TSDR SWAA2024062790212Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500B-500C<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .008?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIONSDR SWAA2024062790206Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500C-500D<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .004?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIONSDR SWAA2024062790211Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .0010?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIOSDR SWAA2024062790210Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500E-500F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .005?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIONSDR SWAA2024062790209Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500H-500I. REMOVED DAMAGE IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .008. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITION ANGLE FROM BS 480SDR SWAA2024062790208Angle · corrodedFWD CARGO COMPT 500I BULKHEAD ANGLE AT FLOOR CORRODED. REMOVED CORROSION AT FWD CARGO COMPT. AFT BULKHEAD LOWER RAIL ANGLE BS 500I, RBL 22 TO LBL 22 IAW SRM 51-10-02. MEASURED REMAINING MATERIAL THICKNESS, OUT OF LIMITS IAW SRM 53-30-08-1A-1 FIG. 103, DETAIL SDR SWAA2024070189988Floorbeam · crackedCABIN FLOOR SUPPORT STIFFENER CRACKED AT STA 540 BL ZERO TO LBL24<[01] REMOVED AND REPLACED STIFFENER AT STA 540 BL 0 TO LBL 24 PER SRM 51-40-02.;[02] VERIFIED C/A #1.SDR SWAA2024070189987Floorbeam · crackedCABIN FLOOR SUPPORT STIFFENER CRACKED AT STA 540 BL ZERO TO RBL24<[01] REMOVED AND REPLACED FLOOR SUPPORT STIFFENER PER SRM 51-40-02.SDR SWAA2024070190181Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727H-727I LBL 21-22 WL 156. MRKD<[01] FOUND CORROSION ON L/H SIDE PLATE AT STA. 727H-727I TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] REMOVED DAMAGED SECTION OF L/H SIDE PLATE FROM STA.727G+12-SDR SWAA2024070190192Angle · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.727J-747; RBL 21-RBL 22 HAS SURFACE CORROSION.(MARKED<REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT AND SDR SWAA2024070190193Angle · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.747-767; RBL 21-RBL 22 HAS SURFACE CORROSION.(MARKED<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOSDR SWAA2024062890198Angle · corrodedAFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.767-787; RBL 21-RBL 22 HAS SURFACE CORROSION. MRKD<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.045' REMAINING THICKNESS). SHIELD (TRANSITION ANGLE) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] SHIELD ASSDR SWAA2024062889980Floor Support · corrodedAFT CABIN WET AREA FLOOR STRUCTURE INTERCOSTAL AT STA 947+4'; AFT OF RIGHT HAND LAV MOUNTS HAS CORROSION AROUND FASTENER HOLE. (MARKED)<[01] BLENDED OUT CORROSION AT AFT CABIN FLOOR STRUCTURE SUPPORT ANGLE STA 947+4?; RBL 28 PER SRM 51-10-02. MEASURED REMAININSDR SWAA2024062890180Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727G-727H LBL 21-22 WL 156. REMOVED CORROSION FROM STA.727G-727G+12 PER SRM 51-10-02. REMOVED .002? OF MATERIAL THICKNESS; REMAINING THICKNESS IS .038?.FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-0SDR SWAA2024062890182Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727I-727J LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 727I-727J TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 ASDR SWAA2024062890183Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727J-747 LBL 21-22 WL 156. MRKD<[01] FOUND CORROSION ON L/H SIDE PLATE AT STA. 727J-747 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53SDR SWAA2024062890185Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 747-767 LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 747-767 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2. L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND A SESDR SWAA2024062890199Plate · corrodedAFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 767-787 LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 767-787 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND ASDR SWAA2024062890204Shield · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURES SHIELD BETWEEN BS 767 & 767+25, RBL 21-22 HAS SURFACE CORROSION. REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.045' REMAINING THICKNESS). SHIELD IS OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED SHIELD ASSY IAW SRM 51-40-02.SDR SWAA2024062790197Support Bracket · crackedAFT CARGO COMPARTMENT WASTE TANK ACCESS PANEL STANCHION SUPPORT BRACKET AT STA 867 LBL 15 CRACKED. REMOVED AND REPLACED AFT CARGO BLKHD STANCHION SUPPORT BRACKET AT STA. 867 LBL 15 IAW SRM 51-40-02.SDR SWAA2024070189317Seal · crackedL/H HORZ. STABILIZER FWD ATTACH FITTING UPPER SLIDER SEAL IS CRACKED AT FWD AND AFT SIDES. REMOVED L/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31. INSTALLED L/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31.SDR SWAA2024070189318Seal · crackedR/H HORZ. STABILIZER FWD ATTACH FITTING UPPER SLIDER SEAL IS CRACKED AT AFT END. REMOVED R/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31. INSTALLED R/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31.;[03] INSPECTED WORK PERFORMEDSDR SWAA2024070189306Bonding Jumper · corrodedA/C ACCESS PANEL 192CL 2ND FROM FWD END BONDING WIRED TERMINAL END CORRODED.<[01] PERFORMED RESISTANCE CHECK PER AMM 52-48-42 AND SWPM 20-20-00;[02] VERIFIEDSDR SWAA2024070189083Support Angle · crackedUPPER FIXED TRAILING EDGE PANEL I/B OF #5 SPOILER LOWER ANGLE BRACKET CRACKED. REMOVED DEFLECTION RIB CLIP FROM AIRCRAFT I.A.W SRM 51-40-02.. LOCATED AND DRILLED NEW DEFLECTION RIB CLIP I.A.W SRM 51-40-05. INSTALLED DEFLECTION RIB CLIP I.A.W SRM 51-40-02
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