N8549Z

Service difficulty reports · 84

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 = 'N8549Z' 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 SWAA2023083085776Angle · corrodedFORWARD CARGO BIN; R/H TRANSITION ANGLE HAS CORR. FROM STA. 500C-500D.<[01] REMOVED ENTIRE FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED 1. WILSON WHITT (TECHNICIAN); 07-AUGAug 4, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085778Angle · corrodedFORWARD CARGO BIN; R/H TRANSITION ANGLE HAS CORR. FROM STA. 500E-500F.<[01] REMOVED ENTIRE FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED 1. WILSON WHITT (TECHNICIAN); 07-AUGAug 4, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085772Angle · corrodedFORWARD CARGO BIN; R/H TRANSITION ANGLE HAS CORR. FROM STA. 500F-500G.<[01] REMOVED ENTIRE FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED 1. WILSON WHITT (TECHNICIAN); 07-AUGAug 4, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085773Angle · corrodedFORWARD CARGO BIN; R/H TRANSITION ANGLE HAS CORR. FROM STA. 500G-500H.<[01] REMOVED ENTIRE FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED 1. WILSON WHITT (TECHNICIAN); 07-AUGAug 4, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085779Angle · corrodedFORWARD CARGO BIN; R/H TRANSITION ANGLE HAS CORR. FROM STA. 500H-500I.<[01] REMOVED ENTIRE FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED 1. WILSON WHITT (TECHNICIAN); 07-AUGAug 4, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085777Angle · corrodedFORWARD CARGO BIN; R/H TRANSITION ANGLE HAS CORR. FROM STA. 500D-500E.<[01] REMOVED ENTIRE FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED 1. WILSON WHITT (TECHNICIAN); 07-AUGAug 4, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085389Mount · corrodedAFT WET AREA STA. 947+2 INCHES; RBL51 ON MACHINED INTERCOSTAL; NEXT TO LAV MOUNT HAS CORROSION.<[01] REMOVED CORROSION; FOUND OUT OF LIMITS; REPLACED WITH NEW PART PER SRM 53-70-51-1A-1 AND SRM 51-40-02Aug 3, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085393Intercostal · corrodedAFT WET AREA STA. 947+2 INCHES; LBL51 ON MACHINED INTERCOSTAL; NEXT TO LAV MOUNT HAS CORROSION.<[01] INTERCOSTAL FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED WITH NEW PART PER SRM 53-70-51-1A-1 AND SRM 51-40-02Aug 3, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085195Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLE AT BS 727B-727C.<[01] FINAL SIGN OFF WILL BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085187Angle · corrodedAFT CARGO FLOOR RH TRANSITION ANGLE BETWEEN STA 767-787 HAS VARIOUS AREAS OF SURFACE CORROSION<[01] DUPLICATE WRITE UP. SIGNED OFF ON TTG8Q00ML1BJAug 2, 2023 · N8549Z · Boeing 7378H4 · Cargo CompartmentsSDR SWAA2023083085188Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727C TO 727D.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085190Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727D TO 727E.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085189Angle · corrodedAFT CARGO FLOOR LH TRANSITION ANGLE BETWEEN STA 747-767+3' HAS VARIOUS AREAS OF SURFACE CORROSION<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085196Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727F TO 727G.<[01] REMOVED R/H TRANSITION ANGLE;[02] R & R AFT CARGO R/H TRANSITION ANGLE BS 727-767 PER SRM 51-40-02;[03] REJECT: CORRECTIVE ACTION #2 HAS IMPROPER SRM REFERENCE NOTAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023083085192Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727G TO 727H.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085194Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727H TO 727J.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085197Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727J TO 747.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085220Web · corrodedAFT CARGO DOOR ENTRY WEB BELOW THRESHOLD HAS SIGNS OF MINOR SURFACE CORROSION<[01] REMOVED CORROSION WITH .003? MATERIAL LOSS OUT OF .050? ORIGINAL WHICH IS WITHIN ALLOWABLE LIMITS PER SRM 53-6015-1A-1. ALODINED AND PRIMED PER SRM 51-20-01;[02] REMOVED CORROSIAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085219Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 747 TO 767.<[01] FINAL SIGNOFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFAug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085198Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 767 TO 787.<[01] REJECT: IN THE MEASUREMENTS SECTION; ITEM #20 STATES 'YES' FOR THERE BEING A PICTURE ATTACHED WHEN THERE ARE NO PICTURES CURRENTLY ATTACHED. SEE STEP #1 FOR REJECT.;Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085199Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727C TO 727D.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085200Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727D TO 727E.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085201Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727F TO 727G.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .003. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085221Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727E TO 727F.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085222Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727G TO H<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;[02]Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085223Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727H TO 727J.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085202Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727J TO 747.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;[Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083085224Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 747 TO 767.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;[0Aug 2, 2023 · N8549Z · Boeing 7378H4 · Fuselage Structure (General)SDR SWAA2023083084151Panel · corrodedTHE REFUELING PANEL ON THE RIGHT WING HAS EVIDENCE OF CORROSION.<[01] REPLACED REFUEL PANEL ON RH WING. SEE TASK CARD TTG8R007B8YZ FOR REMOVAL AND INSTALLATION.;[02] INSPECTION C/W FOR REPLACEMENT OF R/H WING REFUEL PANEL. SEE TTG8R007B8YZ FOR REMOVAL AND INSTJul 31, 2023 · N8549Z · Boeing 7378H4 · Fuel StorageSDR SWAA2023083084439Bracket · corrodedCORROSION ON RIGHT WING FUEL GAUGE BRACKET<[01] DUPLICATE DISCREPANCY. SEE TASK TTG8Q00MJ5QR. REPLACED REFUEL PANEL ON RH WING. SEE TASK CARD TTG8R007B8YZ FOR REMOVAL AND INSTALLATION. AMM 28-41-61;[02] INSPECTION C/W FOR DUPLICATE DISCREPANCY FOR R/H FUEL PANJul 31, 2023 · N8549Z · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2022103166189Lamp · inoperativeAFT ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOP / [01] REPLACED AFT ENTRY DOOR EXTERIOR EMERGENCY LAMP REF AMM 33-51-04. OPS CHECK GOOD.Oct 30, 2022 · N8549Z · Boeing 7378H4 · Emergency LightingSDR SWAA2021081715338Frame · crackedFOUND CAMLOCK RECEPTACLE FLANGE CRACKED OFF FROM THE MOST FORWARD SECOND ONE DOWN FROM PANEL 192BL.ACCOMPLISHED INTERIM REPAIR PER EA 20-153-01484. THIS IS A TEMPORARY REPAIR; REPAIR OR PORT REPLACEMENT MUST BE ACCOMPLISHED WITHIN 30 DAYS. P/N 149A7177-3 ACCOSep 10, 2020 · N8549Z · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2021082010038Receptacle · crackedFOUND CAMLOCK RECEPTACLE FLANGE CRACKED OFF FROM THE MOST FORWARD SECOND ONE DOWN FROM PANEL 192BL. / ACCOMPLISHED INTERIM REPAIR PER EA 20-153-01484. THIS IS A TEMPORARY REPAIR; REPAIR OR PORT REPLACEMENT MUST BE ACCOMPLISHED WITHIN 30 DAYS. P/N 149A7177-3. RAug 20, 2020 · N8549Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2020081909065Slide · out of positionR-2 SLIDE DRAGS, TOO LOW. REPOSITIONED SERVICE AFT DOOR SLIDE IN ITS COMPARTMENT IAW MT 725-61-06.Aug 17, 2020 · N8549Z · Boeing 7378H4 · Escape Slide
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