N8565Z
Service difficulty reports · 95
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 = 'N8565Z' 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 = 'N8565Z' 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 SWAA2024030747723Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 787-807 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 787-807 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; RESDR SWAA2024030747706Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727E-727F AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.033; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STASDR SWAA2024030647955Handle · looseFWD. ENTRY DOOR HANDLE CAM PLATE IS LOOSE(HAS PLAY).<[01] FOUND CASTELLATED CAM PLATE NUT HAD SEVERAL MISSING CASTELLATIONS. REMOVED AND REPLACED NUT IAW CMM. 52-16-12.;[02] FOUND CASTELLATED CAM PLATE NUT HAD SEVERAL MISSING CASTELLATIONS. REMOVED AND REPLACESDR SWAA2024030647717Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727B-727C AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.034; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED L/H SIDE PLATE PER SRM 51-40-02 FROMSDR SWAA2024030647718Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727C-727D AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS; REMAINING THICKNESS IS 0.035; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] L/H SIDE PLATE IS REPLACED WITH NEW FROM STASDR SWAA2024030647719Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE; LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES. AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDE PLATE HAS SURFACE CORROSION FROM STA 727J-747 AROUND FASTENER HOLES.<[01] REMOVED CORROSIONS. SDR SWAA2024030747553Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500B TO 500A<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] REMOVED R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-40-02.;[SDR SWAA2024030747559Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500D TO 500C<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2;[02] FAULT RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTION #2SDR SWAA2024030647554Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500I TO 500H<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] DRILLED NEW RH TRANSITION ANGLE IAW SRM 51-40-05-0G-0.;[03] FAULT IS RESOLSDR SWAA2024030647555Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500H TO 500G<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTISDR SWAA2024030647552Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500G TO 500F<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTISDR SWAA2024030647556Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500F TO 500E<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTISDR SWAA2024030647557Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500E TO 500D<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTISDR SWAA2024030647558Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500D TO 500C<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTISDR SWAA2024030647560Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500C TO 500B<[01] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.;[02] FAULT IS RESOLVED ON FAULT ID # TTG8Q00RA85G;[03] VERIFIED CORRECTIVE ACTISDR SWAA2024030647561Angle · corrodedFWD CARGO; RH TRANS. ANGLE HAS CORROSION; STA. 500A TO 500<[01] REMOVED RH TRANSITION SHIELD ASSY ANGLE IAW SRM 51-40-02-0G-0.;[02] DRILLED NEW RH TRANS SHIELD ASSY ANGLE IAW SRM 51-40-05-0G-0.;[03] REMOVED CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS ISDR SWAA2024030647562Support Angle · corrodedFWD CARGO BULKHD PANEL SUPPORT ANGLE AT STA. 500I HAS CORROSION.<[01] CLEAN CORROSION PER SRM 51-10-02. THE REMAINING THICKNESS IS OUT OF LIMIT PER SRM 53-30-08-1A-1 FIG 103 DETAILD.;[02] REMOVED SUPPORT ANGLE PER SRM 51-40-02.;[03] DRILLED NEW ANGLE PER SRM 5SDR SWAA2024030747109Cable · corrodedR/H WING FWD AILERON CABLE HAS SURFACE CORROSION AT TURN AROUND PULLEY/AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLES TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 ANSDR SWAA2024030747106Cable · corrodedR/H WING AFT AILERON CABLE HAS SURFACE CORROSION AT TURN AROUND PULLEY/AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 ANDSDR SWAA2024030747107Cable · corrodedR/H WING O/B AILERON CABLE SWAGED END HAS SURFACE CORROSION AT AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20SDR SWAA2024030747110Cable · corrodedR/H WING I/B AILERON CABLE SWAGED END HAS SURFACE CORROSION AT AILERON QUADRANT FWD OF AILERON INPUT ROD.<[01] FABRICATED TERMINAL B FITTINGS TO NEW CABLES ABSA-R1 AND ABSB-R1 AND CUT CABLE TO LENGTH; PERFORMED PULL-TEST CK. GOOD PER. M.M. 27-09-14 AND SOPM 20SDR SWAA2024030747111Balance Weight · corrodedR/H AILERON I/B BALANCE WEIGHTS 4(EA.) FWD OF AILERON INPUT ROD HAVE SURFACE CORROSION (MKD)<[01] REMOVED AND REPLACED WEIGHTS IAW SRM 51-60-03;[02] VERIFIED REMOVED AND REPLACED WEIGHTS IAW SRM 51-60-03.SDR SWAA2024010337000Flashlight · failedAFT GALLEY FLASH LIGHT AIRCRAFT RIGHT WILL NOT TEST<[01] PERFORMED PUSH TO TEST FLASHLIGHT CHEKC ON R/H AFT GALLEY FLASHLIGHT PER AMM 25-64-00. TESTS OK.SDR SWAA2023112021309Battery Pack · inoperativeAFT AISLE AND LH ENTRY DOOR INTERIOR EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED AFT LH EMERGENCY LIGHT BATTERY PACK IN REFERENCE WITH AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.SDR SWAA2023090797779Overheat Sensor · intermittentFIRE WARNING LIGHT AND BELL ALONG WITH WHEEL WELL LIGHT ILLUMINATED; THEN WENT OUT. ON APPROACH; AFTER LANDING GEAR EXTENDED DOWN; HAPPENED AGAIN.<[01] REMOVED AND REPLACED INTERMITTENTLY SHORTINGWHEEL WELL OVERHEAT SENSING ELEMENT IAW AMM CHPT. 26-18-02.SDR SWAA2023080184160Light · out of adjustCEILING EXIT SIGN BETWEEN OVERWINGS IS NOT FULLY ATTACHED<[01] SECURED EMERGENCY EXIT SIGN IAW AMM 33-51-01SDR SWAA2023072080643Light · out of adjustCENTER AISLE EXIT SIGN DISLODGED<[01] REINSTALLED LIGHT ASSY IAW AMM 33-51-01SDR SWAA2023051950302Slide · out of positionFWD SERVICE DOOR SLIDE FELL OUT OF HOUSING<[01] REPOSITION SLIDE TO HOUSING PER AMM 25-66-00 AND MT 725-61-06SDR SWAA2023051147635Slide · out of adjustFWD SERVICE DOOR SLIDE FELL OUT OF HOUSING<[01] REPOSITION SLIDE TO THE HOUSING PER AMM 25-66-00SDR SWAA2023050242755Flashlight · inoperativeAFT PANEL HAND HELD FLASH LIGHT TEST RED<[01] R&R AFT HAND HELD FLASH LIGHT BATTERY IAW AMM <BR>25-64-00; OPS CHK OKSDR SWAA2022101056680Flashlight · inoperativeAFT GALLEY CAPTS SIDE FLASHLIGHT INOP / [01] PROPERLY SEATED AND PERFORMED FLASH LT CHECK AT AFT LEFT IAW AMM 25-64-00SDR SWAA2022082544522Flashlight · failedBOTH FWD FLASHLIGHT WOULD NOT TEST / [01] REPLACED BATTERIES IN BOTH FLASHLIGHTS PER AMM 25-64-00SDR SWAA2022060614526Cover · missingEXIT SIGN COVER MISSING AT AFT RIGHT OVERWING EXIT / [01] INSTALLED A NEW EMERGENCY EXIT LIGHT AS REQUIRED. LIGHT OPS CKS GOOD IAW AMM 33-51-01.SDR SWAA2022011861520Battery · faultyAFT GALLEY FLIGHT ATTENDANT FLASH LIGHT RED ; / [01] OK TO CONTINUE PER MEL 25-12-01<BR>AUTH #43569; [02] REACHED BATTERY ON F.O. OUTBD. FLASHLIGHT AFT GALLEY PER SIP.SDR SWAA2022011360530Indicator · incorrectFLAPS WOULD NOT EXTEND PAST 10 DEGREES. ; / [01] PERFORMED FLAP SKEW DETECTION FUNCTIONAL TEST. NO DEFECTS NOTED. REF AMM 27-59-00. PERFORMED FIM 27-51 TASK 849. FOUND #1 TRAILING EDGE FLAPS TRANSMISSION TORQUE TRIP INDICATOR EXTENDED. REPLACED #1 FLAP TRANSMISDR SWAA2021080500675Floor Panel · unsecureAISLE FLOOR BETWEEN ROWS 16 & 17 'POPS' EXCESSIVELY WHEN WALKED ON.C/W REPAIR-53EA-04959 REV 1 / 1-A53-31403 REV 1REPETITIVE INSPECTION ACTION; ACTION REQUIRED: PERFORM GENERAL VISUAL EXAMINATION OF THE PANEL TO ENSURE PANEL IS FREE OF DEFECTS (CRACKS; DENTS; SDR SWAA2021080500676Floor Panel · unsecureAISLE FLOOR BETWEEN ROWS 16 & 17 'POPS' EXCESSIVELY WHEN WALKED ON.C/W REPAIR-53EA-04959 REV 1 / 1-A53-31403 REV 1REPETITIVE INSPECTION ACTION; ACTION REQUIRED: PERFORM GENERAL VISUAL EXAMINATION OF THE PANEL TO ENSURE PANEL IS FREE OF DEFECTS (CRACKS; DENTS; SDR SWAA2021071593387Flashlight · inoperativeCREW REPORTS AFT LEFT OUTBOARD EMERGENCY FLASHLIGHT WONT TEST ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / REMOVED AND REPLACED AFT ELFT EMERGENCY FLASHLIGHT BATTERY PACK REF AMM 25-64-00. OPS CHECK GOOD. THIS CLEARS MEL 25-12-01. AUTH # 113405. CL # 9SDR SWAA2021051170697Flashlight · no testCREW REPORTS FWD FA OD FLASHLIGHT FAILS TEST. REINSTALLED FWD FA OB FLASHLIGHT PER MM 256400.SDR SWAA2021042064878Battery · no testAFT LFT FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED BATTERY PER MM 256400.SDR SWAA2021081715396Panel · crackedAFT CARGO FWD BULKHEAD PANEL 142NW DAMAGED/CRACKED IN 3 LOCATIONS. / R+R 142W PANEL IAW AMM 25-52-78 AMT 69696SDR SWAA2019072235158Battery Pack · dischargedFORWARD LT UPPER ENTRY EMERGENCY LIGHTS INOP. R&R BATTERY PACK PER AMM.SDR SWAA2018112026934Flashlight · inoperativeAFT RT GALLEY UNDER RH FLIGHT ATTENDANCE SEAT EMERGENCY FLASHLIGHT INOP. REPAIRED FLASHLIGHT ASSEMBLY PER MMM.SDR SWAA2018082124479Battery · dischargedAFT RT SIDE INBOARD EMERGENCY FLASHLIGHT INOP. R&R BATTERY IAW AMM.SDR SWAA2018052322204Adiru · failedDIVERSION, NR 2 AIR DATA INERTIAL REFERENCE UNIT FAILED INFLIGHT. R&R NR 2 DATA INERTIAL REFERENCE UNIT PER AMM.
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