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.

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; REFeb 2, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 STAFeb 2, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 REPLACEFeb 2, 2024 · N8565Z · Boeing 7378H4 · Passenger/Crew DoorsSDR 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 FROMFeb 2, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 STAFeb 2, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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. Feb 2, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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.;[Feb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 #2Feb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 RESOLFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ACTIFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ACTIFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ACTIFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ACTIFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ACTIFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ACTIFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 IFeb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 5Feb 1, 2024 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 ANJan 31, 2024 · N8565Z · Boeing 7378H4 · Aileron Control SystemSDR 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 ANDJan 31, 2024 · N8565Z · Boeing 7378H4 · Aileron Control SystemSDR 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 20Jan 31, 2024 · N8565Z · Boeing 7378H4 · Aileron Control SystemSDR 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 20Jan 31, 2024 · N8565Z · Boeing 7378H4 · Aileron Control SystemSDR 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.Jan 31, 2024 · N8565Z · Boeing 7378H4 · AileronsSDR 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.Jan 1, 2024 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR 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.Nov 14, 2023 · N8565Z · Boeing 7378H4 · Emergency LightingSDR 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.Sep 6, 2023 · N8565Z · Boeing 7378H4 · Overheat DetectionSDR SWAA2023080184160Light · out of adjustCEILING EXIT SIGN BETWEEN OVERWINGS IS NOT FULLY ATTACHED<[01] SECURED EMERGENCY EXIT SIGN IAW AMM 33-51-01Jul 31, 2023 · N8565Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023072080643Light · out of adjustCENTER AISLE EXIT SIGN DISLODGED<[01] REINSTALLED LIGHT ASSY IAW AMM 33-51-01Jul 19, 2023 · N8565Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023051950302Slide · out of positionFWD SERVICE DOOR SLIDE FELL OUT OF HOUSING<[01] REPOSITION SLIDE TO HOUSING PER AMM 25-66-00 AND MT 725-61-06May 10, 2023 · N8565Z · Boeing 7378H4 · Escape SlideSDR SWAA2023051147635Slide · out of adjustFWD SERVICE DOOR SLIDE FELL OUT OF HOUSING<[01] REPOSITION SLIDE TO THE HOUSING PER AMM 25-66-00May 10, 2023 · N8565Z · Boeing 7378H4 · Escape SlideSDR 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 OKApr 28, 2023 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2022101056680Flashlight · inoperativeAFT GALLEY CAPTS SIDE FLASHLIGHT INOP / [01] PROPERLY SEATED AND PERFORMED FLASH LT CHECK AT AFT LEFT IAW AMM 25-64-00Oct 7, 2022 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2022082544522Flashlight · failedBOTH FWD FLASHLIGHT WOULD NOT TEST / [01] REPLACED BATTERIES IN BOTH FLASHLIGHTS PER AMM 25-64-00Aug 23, 2022 · N8565Z · Boeing 7378H4 · Emergency LightingSDR 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.Jun 2, 2022 · N8565Z · Boeing 7378H4 · Emergency LightingSDR 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.Jan 14, 2022 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR 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 TRANSMIJan 10, 2022 · N8565Z · Boeing 7378H4 · Trailing Flap Position Indicating SystemSDR 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; Jul 31, 2021 · N8565Z · Boeing 7378H4 · Fuselage Floor PanelSDR 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; Jul 31, 2021 · N8565Z · Boeing 7378H4 · Fuselage Floor PanelSDR 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 # 9Jul 11, 2021 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2021051170697Flashlight · no testCREW REPORTS FWD FA OD FLASHLIGHT FAILS TEST. REINSTALLED FWD FA OB FLASHLIGHT PER MM 256400.May 7, 2021 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2021042064878Battery · no testAFT LFT FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED BATTERY PER MM 256400.Apr 16, 2021 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2021081715396Panel · crackedAFT CARGO FWD BULKHEAD PANEL 142NW DAMAGED/CRACKED IN 3 LOCATIONS. / R+R 142W PANEL IAW AMM 25-52-78 AMT 69696Feb 7, 2020 · N8565Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2019072235158Battery Pack · dischargedFORWARD LT UPPER ENTRY EMERGENCY LIGHTS INOP. R&R BATTERY PACK PER AMM.Jul 20, 2019 · N8565Z · Boeing 7378H4 · Emergency LightingSDR SWAA2018112026934Flashlight · inoperativeAFT RT GALLEY UNDER RH FLIGHT ATTENDANCE SEAT EMERGENCY FLASHLIGHT INOP. REPAIRED FLASHLIGHT ASSEMBLY PER MMM.Nov 20, 2018 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2018082124479Battery · dischargedAFT RT SIDE INBOARD EMERGENCY FLASHLIGHT INOP. R&R BATTERY IAW AMM.Aug 20, 2018 · N8565Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2018052322204Adiru · failedDIVERSION, NR 2 AIR DATA INERTIAL REFERENCE UNIT FAILED INFLIGHT. R&R NR 2 DATA INERTIAL REFERENCE UNIT PER AMM.May 22, 2018 · N8565Z · Boeing 7378H4 · Inertial Guidance System
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