N8535S

Service difficulty reports · 81

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 = 'N8535S' 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 SWAA2023061650609Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221CF HAS DELAMINATION ON PANEL<[01] IDENTIFIED FLOOR PANEL 221CF IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2 AND BOEING DWG 141A5810-9.<BR><BR>DAMAGE NOTED TO UPPER SURFACE SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1May 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023061650610Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 221FF HAS DELAMINATION ON PANEL.<[01] IDENTIFIED FLOOR PANEL 221FF IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2 AND BOEING DWG 141A5810-157.<BR><BR>DAMAGE NOTED TO UPPER SURFACE SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1May 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023061650611Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222CF HAS DELAMINATION ON PANEL<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>RMay 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023061650607Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222DF HAS DELAMINATION ON PANEL.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>May 21, 2023 · N8535S · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023061649646Angle · corrodedCORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS767 TO BS787 RBL21 WL156<[01] CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1- OUT OF LIMITS.;[03]May 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649647Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1- OUT OF LIMITS.;[03] RMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649644Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727F+5' TO BS767 RBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727H+6' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649648Shield · corrodedCORROSION AFT CARGO BAY SHIELD AFT OF CARGO DOOR HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS847 TO BS867 RBL22 WL163.5<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1- OUT OF LIMIMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649643Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26.5 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 794.3+5' REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2023061649649Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11.5 WL156<[01] CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1- OUT OF LIMITS.;[03] RECEIVED NEW AFT CARGO BAMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649650Support · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+6' TO BS767+14' LBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 747+11' REMOVED 0.020' IN AN AREA OF 1'X1' ORIGINMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649651Support · corrodedCORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500I LBL21 TO RBL21<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT RBL 14 REMAINING THICKNESS LESS THAN 0.056' IN AN AREA OF 1X1 FOUND TO May 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2023061649891Support · corrodedCORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS480+6' TO BS500C+11' LBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500A+6' REMOVED 0.010' IN AN AREA OF 1'X1' ORIGINMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649890Support · corrodedCORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500D+8' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICMay 18, 2023 · N8535S · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023061649239Threshold · crackedFORWARD CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] WELDED CRACKED RADIUS ON FWD CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B.(2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; May 17, 2023 · N8535S · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2023061649216Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 REP. 5;[02] INSTALLED EWIS PROTECTION ON REPAIR AREA BS 663 RBL 6-35 IAW AMM 20-60-07.;[03] REMOVED DAMAGED AREA OF UPPER ATTACH ANGLE AT BSMay 16, 2023 · N8535S · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2023061649217Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] VERIFIED SRM APPILCABILITY OF SRM 57-10-10-2R-5 REP. 5;[02] INSTALLED EWIS PROTECTION ON REPAIR AREA BS 663 LBL6-35 IAW AMM 20-60-07.;[03] REMOVED DAMAGED AREA OF UPPER ATTACH ANGLE ATMay 16, 2023 · N8535S · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2022121280055Lens · brokenROW 5 CAPT SIDE LUGGAGE BIN LIGHT COVER/LENS BROKEN. LIGHT OPERATES / [01] OK TO CON?T PER MEL 25-10-01 SP1 AUTH #107877;[02] R&R ROW 5 EMERGENCY AISLE LIGHT LENS IAW AMM 33-51-03. LIGHT OPS CHECK GOOD AT THIS TIME.Dec 9, 2022 · N8535S · Boeing 7378H4 · Emergency LightingSDR SWAA2022090148888Slide · out of adjustFWD ENTRY DOOR SLIDE PRESSURE IN RED / [01] R&R FWD ENTRY DOOR SLIDE ASSY I.A.W. MT#725-61-06.Sep 1, 2022 · N8535S · Boeing 7378H4 · Escape SlideSDR SWAA2022032184808Mechanism · faultyFIRST OFFICER'S SLIDING WINDOW DOES NOT OPEN WHEN EMERGENCY RELEASE HANDLE IS PULLED. / [01] ADJUSTED EMERGENCY EXIT RELEASE MECHANISM PER AMM 56-12-11.Mar 17, 2022 · N8535S · Boeing 737800* · Flight Compartment WindowsSDR SWAA2022031883951Guide Arm · failedFORWARD ENTRY DOOR STICKS WHILE OPENING / [01] REMOVED AND REPLACED GUIDE ARM HINGE BOLT PER MM 52?11-21. OPS NORMALMar 14, 2022 · N8535S · Boeing 737800* · Passenger/Crew DoorsSDR SWAA2022022876570Fitting · cracked#1 ENGINE. AFT STRUT FITTING LEFT SIDE IS CRACKED. / [01] R & R #1 ENG LH AFT STRUT FITTING PER SRM 51-40-02Feb 23, 2022 · N8535S · Boeing 737800* · Nacelle/Pylon StructureSDR SWAA2021090112919Light · intermittentEXIT LIGHT 14F FLICKERING /Aug 28, 2021 · N8535S · Boeing 7378H4 · Emergency LightingSDR SWAA2021041564010Seat Track · damagedCAPTAINS'S SEAT I/B SEAT RAIL DAMAGED. / R&R CAPTAIN'S SEAT I/B SEAT RAIL TRACK PER AMM 25-11-11.INSP #13288Apr 14, 2021 · N8535S · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021041564011Seat Track · damagedF/O'S I/B SEAT RAIL DAMAGED. / R&R F/O'S I/B SEAT RAIL TRACK PER AMM 25-11-11.INSP #13288Apr 14, 2021 · N8535S · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020111730857Cradle · inoperativeAFT EMERGENCY FLASHLIGHT INOPERABLE. CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS.Nov 16, 2020 · N8535S · Boeing 7378H4 · Emergency EquipmentSDR SWAA2020031642478Skin · dentedDENT FOUND ON LEFT SIDE OF FUSELAGE JUST FORWARD OF AOA. AT STATION 181 BETWEEN STRINGER 17L & 18L. DENT MEASURES L= 2.4", W=2.0', Y=.009'. W/Y=222. REPAIRED FUSELAGE SKIN IAW REPAIR -53-EA-07918 REV 1 AND ER 20-02072Mar 4, 2020 · N8535S · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2020031642477Skin · dentedTRANSFERRED FROM LOG PAGE 1240617: DENT FOUND ON LEFT SIDE OF FUSELAGE JUST FORWARD OF AOA. DENT MEASURES 4" X 4" X .180" DEEP. STATION 184 BETWEEN STRINGER 17L & 18L. W/Y=22.2 2. REPAIRED FUSELAGE SKIN IAW REPAIR-53 EA-07918 REV 1 AND ER 20-02072 REV IMar 4, 2020 · N8535S · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR SWAA2019020629293Megaphone · brokenFORWARD GALLEY MEGAPHONE BROKEN. SECURED MOUTH PIECE PER SIP.Feb 6, 2019 · N8535S · Boeing 7378H4 · Emergency EquipmentSDR SWAA2018111326710Glowstrip · damagedRT 1ST SECTION OF PHOTOLUMINESCENT STRIP DAMAGED. R&R STRIP IAW AMM.Nov 8, 2018 · N8535S · Boeing 7378H4 · Emergency EquipmentSDR SWAA2018032720756Battery · no testFORWARD INBOARD EMERGENCY FLASHLIGHT TEST FAILED. R & R THE BATTERY IAW AMM.Mar 23, 2018 · N8535S · Boeing 7378H4 · Emergency Equipment
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