N8568Z
Service difficulty reports · 62
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 = 'N8568Z' 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 = 'N8568Z' 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 SWAA2026101239768Skin · delaminatedRIGHT OTBD T/E FLAP LOWER SKIN DELAMINATED, APPROX 26 1/4 INBD FROM INBD EDGE & 7 1/4 FROM T/E. R & R IAW AMM 27-51-22-401.SDR SWAA2026050896237Battery Pack · inoperativeCAPTAIN SIDE FWD OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY PACK AT STA 500C+7 CAPTAIN SIDE BEHIND AIR GRILLE ON ROW 7ABC. PER AMM 33-51-06.SDR SWAA2026040184339Engine · bird ingestionDURING CLIMB, BIRD STRIKE NR 1 ENGINE. VIBRATION INCREASED, HAD ABNORMAL ODORS, ENGINE STILL MAINTAINED THRUST. C/W BIRD STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-18. C/W BIRD STRIKE VISUAL INSPECTION OF NR 1 ENG IAW MT 772-00-00, C/W BIRD STRIKE BORESSDR SWAA2026030575689Sign · out of adjustCEILING EMERGENCY EXIT SIGN IS CROOKED AT THE OVER WING EXIT. ADJUSTED CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01.SDR SWAA2025082908633Lamp · inoperativeAFT CENTER OVERHEAD EMERGENCY EXIT SIGN HAS MULTIPLE BULBS BURNT OUT. RELAMPED AFT CENTER OVERHEAD EMERGENCY EXIT SIGN AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-01-960-801.SDR SWAA2025082907737Handle · looseASSIST HANDLE IS LOOSE ON G7 GALLEY. SECURED ASSIST HANDLE ON G-7 IAW AMM 25-31-71 & SRM 51-40-02.SDR SWAA2025082907163Handle · looseUPPER AND LOWER ASSIST HANDLES ARE LOOSE ON L1 DOOR LINER. SECURED UPPER AND LOWER DOOR ASSIST HANDLES IAW AMM 52-11-31 & SRM 51-40-02.SDR SWAA2025082907164Handle · looseASSIST HANDLE IS LOOSE ON L2 FWD DOOR SURROUND. SECURED ASSIST HANDLE ON L-2 DOOR FWD SURROUND LINING IAW AMM 25-21-25 & SRM 51-40-02.SDR SWAA2025082907165Handle · looseASSIST HANDLES ARE LOOSE ON R2 DOOR LINER AND R2 FOWARD SURROUND. SECURED R-2 DOOR AND FWD SURROUND ASSIST HANDLES IAW AMM 52-41-31; 25-21-25 & SRM 51-40-02.SDR SWAA2025061079213Slide · looseFORWARD ENTRY DOOR EMERGENCY SLIDE LOOSE AND SAGS; NEEDS REPACKING<[01] PERF ENTRY DOOR ESCAPE SLIDE PACK CHECK REF AMM 25-66-01; SLIDE OK FOR SERVICESDR SWAA2025010682899Battery Pack · inoperativeFWD AND AFR RIGHT EXIT DOOR AND SCAPE SLIDE EMERGENCY LIGHTS INOP<[01] R/R FWD AND AFT RIGHT EXIT AND SCAPE SLIDE EMERGENCY LIGHT POEW PACKS IAW AMM 3351-06SDR SWAA2024062705789Flashlight · inoperativeLH AFT F/A STATION EMERGENCY FLASHLIGHT INOP.<[01] REMOVED AND REPLACED LEFT AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. OPS CHECK PERFORMED; OPS CEHCK GOOD NO DEFECTS NOTED AT THIS TIME REF AMM 25-64-00SDR SWAA2024062404585Cradle · inoperativeAFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WILL NOT TEST<[01] SECURED FLASHLIGHT IN MOUNTING BRACKET PER AMM 25-64-00; OPS CHECK GOOD.SDR SWAA2024041774906Battery · failedFWD EMERGENCY FLASHLIGHTS WILL NOT TEST<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]SDR SWAA2024041770110Battery Pack · inoperativeFOWARD AND AFT ENTRY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FOWARD AND AFT ENTRY EMERGENCY BATTERY PACKS PER MM 33-51-06; OPS CHECKS GOOD PER MM 33-51-00;[02] INSPECTED WORK PERFORMEDSDR SWAA2024041770109Power Supply · inoperativeLEFT AND RIGHT EMERGENCY OVER WING EXIT LOCATORS STA. 576;INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)] <BR>POWER SUPPLY (M01694) OPS CHECKED GOOD PER AMM 33-51-06.;[02] INSPECTED WORK PSDR SWAA2024041768967Scuff Plate · crackedFWD CARGO FWD SCUFF PLATE CORNER CRACKED<[01] REPAIRED PER PO# P8083505 AND INSTALLED SCUFF PLATE PER AMM 53-11-02-420-801.;[02] REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02-420-801.;[03] INSPECTED WORK PERFORMED. REMOVED AND REPLACED SCUFF PLATE PER AMM SDR SWAA2024041768968Scuff Plate · crackedFWD CARGO AFT SCUFF PLATE CORNER CRACKED<[01] REPAIRED PER PO# P8083506 AND INSTALLED SCUFF PLATE PER AMM 53-11-02-420-801.;[02] REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02-420-801.;[03] INSPECTED WORK PERFORMED. REMOVED AND REPLACED SCUFF PLATE PER AMM SDR SWAA2024041768293Seal · crackedLEFT HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED ON THE FWD AND AFT EDGES.<[01] REMOVED CRACKED UPPER FWD SLIDER SEAL AT L/H HORIZONTAL STAB IAW AMM 53-31-31.;[02] DRILLED NEW SLIDER SEAL PER SRM 51-10-02 AND INSTALLED NEW SLIDER SEAL PER AMM 53-31-31.SDR SWAA2024041768294Seal · crackedRIGHT HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED ON THE FWD AND AFT EDGES.<[01] REMOVED SLIDER PINS PER SOPM20-50-01;[02] REMOVED; DRILLED; AND ASSEMBLED NEW SLIDER PLATE PER SRM 51-10-02 AND 51-40-02. OK TO REINSTALL.;[03] INSTALLED NEW SLIDER PLATE PER AMSDR SWAA2024041766043Battery Pack · failedLEFT WING EMERGENCY EXIT ILLUMINATED SIGN ELECTRICAL; PLUGGED INTO THE OVER-WING EXIT DOOR SURROUND HEATER WIRING.<[01] BATTERY CHARGER FOR LEFT FOWARD OVER WING EMERGENCY EXIT LIGHT WAS REPLACED ON CARD TTG8Q00SHP5V LINE 2972.;[02] VERIFIED CORRECTIVE ACTION SDR SWAA2024041766042Skin · delaminatedLEFT HAND WING OUTBOARD TRAILING EDGE FLAP HAS AN AREA OF DELAMINATION AT IB END LOWER SURFACE (MKD).<[01] REMOVED DAMAGE SKIN PER SRM 57-53-01-2R-14;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] REPAIRED DAMAGED AREA PER SRM 57-53-01-2R-14.;[04] RII- INSPECTEDSDR SWAA2024041765150Shim · out of positionSHIM IS NOT CONFIGURED PROPERLY PER E.A. 24-153-00664-WIP2 LINE #2804 TTG8Q00S5KFB<[01] REMOVED LAV MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED OLD SHIM IAW SRM 51-40-02;[03] FABRICATED NEW SHIM; ALODINE AND PRIMED IAW EA 24-153-00664.;[04] C/W INSPECTION OFSDR SWAA2024041764164Crease Beam · crackedR/H CREASE BEAM INNER CHORD CRACK AT STA 377 R/H AT STA 377 CREASE BEAM INNER CHORD CRACKED.<[01] HEAT TREAT ANGLE 7075-0 TO 7075 T6 VENDER SERVICES REQUESTED SEE SA-M 1057 P.O. NUMBER P804525;[02] HEAT TREAT ANGLE 7075-0 TO 7075 T6 VENDER SERVICES REQUESTED SSDR SWAA2024041768553Seal · debondedPANEL 433BT PANEL ASSEMBLY - UPPER SPAR WEB - #1 ENGINE HAS DISBONDED RUBBER SEAL.<[01] REPLACED PANEL; PANEL TO BE INSTALLED ON CLOSE TASK CARD TTG8Q00R9FRX (#960)SDR SWAA2024041762439Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA. 947.5 AT L-24 HAS EVIDENCE OF CORROSION<[01] REMOVED LAV. MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED LAV. MOUNT TO F.O.M IAW SRM 51-40-02. AFTER REMOVAL OF LAV MOUNT CORROSION CONFIRMED FOUND ON FLOOR BEAM UPPER CAP.;[03] REMOVESDR SWAA2024041762959Web · corrodedAFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.042' REMAINING THICKNESS). THRESHOLD WEB IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED AFT CARGO THRESHOLD WEB IAW SRM 51-40-02.;[03] DRILLED UP ANDSDR SWAA2024041762266Web · corrodedFWD CARGO STA. 485 RBL 31; CORROSION ON ENTRY DOOR THRESHOLD WEB PANEL.<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .015?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-30-15-1A-1.;[02] REMOVED LOWER THRESHOLD WEB PANEL I.A.W. SRM 51-40SDR SWAA2024041762273Angle · corrodedAFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLES AT STA 727J INCHES TO STA 787. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.038' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS OUT OF LIMITS SDR SWAA2024041761926Floor Support · corrodedAFT CABIN WET AREA FLOOR INTERCOSTAL LBL-24 UPPER ATTACH ANGLE HAS CORROSION AT STA. 947 ATTACH POINT.<[01] REMOVED UPPER ATTACH ANGLE TO F.O.M AT LBL 24 IAW SRM 51-40-02.;[02] REMOVED CORROSION ON ATTACH ANGLE; MAT. REMOVED IS .004; MAT THICKNESS REMAINING ISSDR SWAA2024041761927Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA. 947 HAS EVIDENCE OF CORROSION AT LAVD OB MOUNT.<[01] REMOVED LAV MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED LAV MOUNT TO F.O.M IAW SRM 51-40-02. AFTER REMOVAL OF LAV MOUNT CORROSION IS CONFIRMED FOUND ON FLOOR BEAM UPPER CAP AT SDR SWAA2024041761939Floorbeam · brokenBREAKAWAY INTERCOSTAL AT STA 540 BETWEEN BL0 AND LBL 24.75 IS BROKEN<[01] REMOVED INTERCOSTAL FROM STA 540 BL0 TO LBL 24.75 PER SRM 51-40-02;[02] INSTALLED NEW INTERCOSTAL AT STA 540 BL 0 TO LBL 24.75 IAW SRM 51-40-02.;[03] CORRECTIVE ACTION #2 C/W.SDR SWAA2024041762264Channel · corrodedFWD CARGO STA.500I LBL 24 TO RBL 24; BULKHEAD NUTPLATE CHANNEL HAS AREAS OF CORROSION.<[01] REMOVED CHANNEL PER SRM 51-40-02;[02] APPROVED CA #1.;[03] REMOVED AND REPLACED PER SRM 51-40-02;[04] VERIFIED REPLACEMENT OF CHANNEL PER SRM 51-40-02SDR SWAA2024041762271Angle · corrodedAFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLES AT STA 727F+9 INCHES TO STA 727F+13 INCHES. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.038' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS OSDR SWAA2024041762248Angle · corrodedAFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLE AT STA 727G+9 INCHES. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.039' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS OUT OF LIMITS PER SRM 53SDR SWAA2024041762272Angle · corrodedAFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLES AT STA 727I+7 INCHES TO STA 727I+18 INCHES. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS OSDR SWAA2024041762274Angle · crackedAFT CARGO COMPARTMENT FLOOR LEFT TRANSITION ANGLE (SIDE PLATE) HAS 1/4 INCH CRACK WITH CORROSION AT BEND RADIUS LOCATED AT STA 727G+5. AREA MARKED.<[01] REMOVED AFT CARGO LH SIDE PLATE ASSY. FROM STA. 727 TO 847 IAW SRM 51-40-02.;[02] OK TO INSTALL REPAIR PARTSDR SWAA2024041762280Floor Support · corrodedAFT CARGO FLOOR STRUCTURE INTERCOSTAL FWD OF CARGO DOOR CUTOUT HAS CORROSION AT NUTPLATE SCREW HOLES. STA.767 TO STA.787 RBL22.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.047' REMAINING THICKNESS). SHIELD (INTERCOSTAL) IS OUT OF LIMITS PER SRM 53-60-15-1ASDR SWAA2024041762277Angle · corrodedAFT CARGO COMPARTMENT RIGHT TRANSITION ANGLE HAD CORROSION AT NUTPLATE HOLES FROM BS 727I TO 767. REMOVED CORROSION PER SRM 53-00-53-1A-2, 0.038' REMAINING THICKNESS. TRANS PANEL IS OUT OF LIMITS IAW SRM 53-00-53-1A-2. CUT OUT DAMAGED TRANSITION ANGLE IAW SRSDR SWAA2024041764532Floor Panel · pulledPANEL 221BF HAS PULLED FIBERS.<[01] PANEL REMOVED AND NEW PANEL INSTALLED ON TTG8Q00R9G1R LINE 1118 OF THIS CHECK. TORQUE WRENCH QDR50 S/N 96702.;[02] PANEL REMOVED AND NEW PANEL INSTALLED ON TTG8Q00R9G1R LINE 1118 OF THIS CHECK. TORQUE WRENCH QDR50 S/N 96702.SDR SWAA2024041761754Scuff Plate · crackedAFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED.<[01] INSTALLED NEW AFT THRESHOLD CORNER PLATE PER AMM 53-11-02.;[02] REMOVED AND REPLACED AFT THRESHOLD CORNER PLATE PER AMM 53-11-02.SDR SWAA2024041761612Floor Panel · pulledPANEL 222CF PANEL ASSEMBLY - PASSENGER CABIN FLOOR HAS PULLED FIBERS<[01] REMOVED AND REPLACED PANEL 222CF PER AMM 53-21-00. REF TASK CARD TTG8Q008EVNF FOR TOOLING AND PART INFO;[02] INSPECTION C/W REMOVED AND REPLACED PANEL 222CF PER AMM 53-21-00. REF TASK CASDR SWAA2024041761908Floor Support · corrodedAFT CABIN WET AREA FLOOR INTERCOSTAL L-24 STA 947 HAS EVIDENCE OF CORROSION.<[01] REMOVED LAV D IB MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED CORROSION ON FLOOR BEAM STA. 947 AT LBL 24. DEPTH REMOVED IS .041; MAT REMAINING IS .139; FOUND TO BE OUT OF LIMITSSDR SWAA2024041761604Floor Panel · pulledPANEL 232BF PANEL ASSEMBLY - RH PASSENGER CABIN FLOOR HAS PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] C/W INSPECTIONSDR SWAA2024041761610Floor Panel · pulledPANEL 232AF PANEL ASSEMBLY - RH PASSENGER CABIN FLOOR HAS PULLED FIBERS.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] C/W INSPECTIONSDR SWAA2024041761611Floor Panel · pulledPANEL 222DF PANEL ASSEMBLY - PASSENGER CABIN FLOOR HAS PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] C/W INSPECTIONSDR SWAA2024041761208Angle · crackedLEFT WING TRAILING EDGE SHELF PANEL AT DEFLECTION RIB HAS CRACKED ANGLE BRACKET. (MARKED)<[01] LOCATED AND DRILLED REPLACEMENT NEW DEFLECTION RIB CLIP (MPN 115A6260-1) I.A.W SRM 51-40-05;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] INSTALLED BRACKET PER SRM 51SDR SWAA2024041766895Fastener · loose#1 INLET COWL OUTER LIP SKIN HAS SEVERAL LOOSE FASTENERS AT THE 6 O'CLOCK POSITION (MKD)<[01] REMOVED DISCREPANT FASTENERS I.A.W SRM 51-40-02.;[02] C/W NDT PER PART 6 51-00-00 PROCEDURE 23 AND PART 6 53-30-00 PROCEDURE 3. NO DEFECTS NOTED.;[03] INSTALLED FIRSTSDR SWAA2024012945075Slide · dislodgedL1 DOOR SLIDE FELL OUT<[01] RE-INSTALLED L1 DOOR SLIDE IAW MT 725-61-06.SDR SWAA2023110919477Girt Bar · looseMAIN CABIN DOOR AFT GIRT BAR CLIP LOOSE. / [01] REPLACED MISSING RIVET ON L1 DOOR GIRT BAR CLIP PER SIP.
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