N8508W
Service difficulty reports · 111
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 = 'N8508W' 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 = 'N8508W' 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 SWAA2023072481117Fseu · faultyON CLIMBOUT AND AFTER THE FLAP HANDLE WAS IN THE UP POSITION; THE FLAP INDICATOR SHOWED FLAPS STILL AT 5. AND WE COULD SEE OUT THE WINDOW THAT THE LEADING EDGE DEVICES WERE EXTENDED<[01] T/S REF FIM 27-51 TASK 801;NO EXISTING FAULTS OR FAULT HISTORY @ FSEU NOTSDR SWAA2023072481547Indicator · faultyON CLIMBOUT AND AFTER THE FLAP HANDLE WAS IN THE UP POSITION; THE FLAP INDICATOR SHOWED FLAPS STILL AT 5. AND WE COULD SEE OUT THE WINDOW THAT THE LEADING EDGE DEVICES WERE EXTENDED<[01] T/S REF FIM 27-51 TASK 801;NO EXISTING FAULTS OR FAULT HISTORY @ FSEU NOTSDR SWAA2022100555821Girt Bar · out of positionL1 GIRT BAR DOES NOT ARM PROPERLY / [01] ACCOMPLISHED AN OPS CHECK OF THE L1 GIRT BAR PER 25-66-01; OPS CHECKED NORMAL; OK TO CONTINUE.SDR SWAA2022092922760Battery Pack · inoperativeAFT GALLEY EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED 2 AFT EMER BATTERY PACKS LEFT AND RIGHT IAW AMM 33-51-06;[02] VERIFIED THE REMOVAL AND REPLACEMENT OF AFT EMER BATTERY PACKS LEFT AND RIGHT AND OPS CHECK GOOD IAW AMM 33-51-06.SDR SWAA2022092982772Floor Panel · damagedAFT CARGO PANEL 140AF IS FOUND TO BE OUT OF LIMITS REQUIRES REPLACEMENT / [01] FABRICATED NEW FLOOR PANEL PER AMM. 25-52-01-201-801;[02] 1. DAVID YECK (TECHNICIAN); 20-SEP-2022 09:25 UTC<BR>FABRICATED NEW FLOOR PANEL PER AMM. 25-52-01-201-801SDR SWAA2022092982771Floor Panel · damagedAFT CARGO FLOOR PANEL 140DF FOUND OUT OF LIMITS REQUIRES REPLACEMENT / [01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140DF TO BE INSTALLED ON CLOSE CARD LINE 987 TTG8Q00385F PER AMM 25-52-10.SDR SWAA2022093052101None · corrodedAFT CARGO R/H TRANSITION ANGLE HAS EXFOLIATING CORROSION AT N/P HOLES AT STA. 770 AND 777 RBL 21 WL 155. MRKD / [01] AFT CARGO COMPARTMENT RT SIDEPLATE SHIELD ASSEMBLY DAMAGE BETWEEN STA 767 TO STA 792; RBL 21; WL 155 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IASDR SWAA2022093052115None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTNER HOLE AT STA. 787 LBL 21 WL 155. MRKD / [01] REMOVED DAMAGED SECTION OF L/H TRANSITION ANGLE FROM STA 727+11.5 TO 807+9 PER SRM 53-00-53-2R-5.;[02] PREVIOUS ACTION HAS INCORRECT STA LOCATION SHOULSDR SWAA2022093052118Strap · corrodedAFT CARGO FLOOR PANEL SPLICE STRAP STA. 772 HAS SURFACE CORROSION AT SCREW HOLES RBL 2.5 TO RBL 16 WL 156. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR OUT OF SDR SWAA2022093052114None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTNER HOLE AT STA. 767 LBL 21 WL 155. MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052099None · corrodedAFT CARGO R/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTENER HOLE AT STA. 747 RBL 21 WL 156. MRKD / [01] AFT CARGO COMPARTMENT RT SIDEPLATE CHANNEL CORROSION WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. SIDEPLATE ASSEMBLY BETWEEN STA 727SDR SWAA2022093052097None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTNER HOLE AT STA. 747 LBL 21 WL 156. MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052096None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTENER HOLE STA. 727J LBL 21 WL 156. MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052093None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTNER HOLE STA. 727I LBL 21 WL 156.MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052091None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLE STA. 727E+16 LBL 21 WL 156. MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052104None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 727F+8+13+16 LBL 21 WL 156. MRKD / [01] REMOVED DAMAGED PER SRM 51-10-02. FOUNED TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. FOR TRANSITION ANGLE REPLACEMENT REFER TO LINE # TTG8Q00EQ7E0SDR SWAA2022093052105None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTENER HOLE STA. 727G LBL 21 WL 156. MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052106None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 727G+2+6+13+16+20 LBL 21 WL 156.MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. FOR TRANSITION ANGLE REPLACEMENT REFER TO LINE# TTG8Q00EQ7ESDR SWAA2022093052107None · corrodedAFT CARGO R/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTENER HOLE STA. 727G RBL 21 WL 156. MRKD / [01] REMOVED AFT CARGO RT SIDEPLATE CHANNEL CORROSION AT STA 727G AND FOUND AREA TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED AFT CARGO SDR SWAA2022093052108None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT FASTENER HOLE STA. 727H LBL 21 WL 156. MRKD / [01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11.5 TO 807+9 LBL 21 ON NON ROUTINE CARD #TTG8Q00EQ7LC.SDR SWAA2022093052109None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 727H+2+6+9+13+16+20 LBL 21 WL 156. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. FOR TRANSITION ANGLE REPLACEMENT REFER TO LINE# TTG8Q00ESDR SWAA2022093052094None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 727I+3+5+6+10+14+18 LBL 21 WL 156. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. FOR TRANSITION ANGLE REPLACEMENT REFER TO LINE# TTG8Q00ESDR SWAA2022093052112None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 727J+5+10+14+18 LBL 21 WL 156. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 .;[02] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 727E+11SDR SWAA2022093052098None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 749-765 LBL 21 WL 156. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FOR REPLACEMENT REFER TO TT# TTG8Q00EQTE0SDR SWAA2022093052100None · corrodedAFT CARGO R/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 749-765 RBL 21 WL 156. MRKD / [01] REMOVED DAMAGE PER SRM 53-00-53-1A-2. FOUND TO BE IN LIMITS;[02] AFT CARGO COMPARTMENT RT SIDEPLATE CHANNEL ASSEMBLY BETWEEN STA 727E +10 TO STA 767; SDR SWAA2022093052102None · corrodedAFT CARGO R/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 768-792 RBL 21 WL 155. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SSDR SWAA2022093052119None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 769-786 LBL 21 WL 155. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FOR REPLACEMENT REFER TO TT# TTG8Q00EQTE0SDR SWAA2022093052120None · corrodedAFT CARGO L/H TRANSITION ANGLE HAS FILIFORM CORROSION AT N/P HOLES AT STA. 788-801 LBL 21 WL 154. MRKD / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FOR REPLACEMENT REFER TO TT# TTG8Q00EQTE0SDR SWAA2022093051848None · corrodedFWD CARGO COMPARTMENT R TRANSITION ANGLE BETWEEN STA. 500A TO 500I HAS CORROSION. / [01] REMOVED CORROSION FROM FWD CARGO COMPARTMENT RT ZEE SIDEPLATE CHANNEL ASSEMBLY BETWEEN STA 500A TO STA 500D+11; RBL 21. FOUND BLENDED AREAS TO BE WITHIN ALLOWABLE LIMITS WSDR SWAA2022093051850None · corrodedFWD CARGO COMPARTMENT AFT BULLHEAD L ANGLE AT STA 500I HAS CORROSION. / [01] NEEDED TO ADD MY REFERENCE FOR BEING OUT OF LIMITS;[02] FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR DAMAGE EXCEEDINGSDR SWAA2022092951288Post · corrodedFWD LAV DOOR POST IS CORRODED AT THE BOTTOM / [01] REMOVED DAMAGED 6.5? SECTION OF LAV POST IAW SRM 51-10-02.;[02] INSTALLED REPAIR PART PER EA# TTG8Q00ETZ11.;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR REPAIR PER EA 22-125-02765 ON TTG8Q00ETZ11.SDR SWAA2022071126301Flashlight Assy · failedFA REPORTS AFT GALLEY FLASH LIGHT INDICATOR FLASHING RED. / [01] REMOVED AND REPLACED FLASH LIGHT ASSEMBLY PER AMM 25-64-00SDR SWAA2021122255441Flashlight · inoperativeFWD FA FLASHLIGHT UNDER JUMPSEAT FLASHING RED ; FWD FA FLASHLIGHT NDER JMPSEAT FLASHING RED. REPLACED FORWARD FA JUMPSEAT INBOARD FLASHLIGHT BATTERY PER AMM 25-64-00 OPS GOODSDR SWAA2021092320146Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021092320148Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021092321045Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021092321047Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021091717126Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. ACCOMPLISH OPTION 1 OR 2. PREFORM 737-SDR SWAA2021091717127Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.ACCOMPLISDR SWAA2021091717302Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021091717303Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021090815116Handle · out of adjustFA REPORTS AFT ENTRY AND SERVICE DOORS SQUEELS AND AFT ENTRY DOOR HANDLE LOOSE AND POPS UP AN INCH IN FLIGHT / ADJUSTED AFT ENTRY DOOR HANDLE PER AMM 52-13-00 CHECKS GOOD LEAKED CHECKED BOTH AFT ENTRY AND SERVICE DOORS AND NO LEAKS NOTED CLEANED BOTH DOOR SEALSDR SWAA2021090815278Handle · looseFA REPORTS AFT ENTRY AND SERVICE DOORS SQUEELS AND AFT ENTRY DOOR HANDLE LOOSE AND POPS UP AN INCH IN FLIGHT / ADJUSTED AFT ENTRY DOOR HANDLE PER AMM 52-13-00 CHECKS GOOD LEAKED CHECKED BOTH AFT ENTRY AND SERVICE DOORS AND NO LEAKS NOTED CLEANED BOTH DOOR SEALSDR SWAA2021081204980Floor Panel · crackedFWD CARGO PANEL 121ZDC HAS 6 CRACKS. 1. 3' LONG 26' FROM AFT EDGE; 2. 2' LONG 43' FROM AFT EDGE 3. 2' LONG 55' FROM AFT EDGE 4. 4' LONG 29' FROM FRONT EDGE 5. 2' LONG 20' FROM FRONT EDGE 6. 1' LONG 11' FROM FRONT EDGEPEFORMED INTERIM REPAIR ON ALL CRACKS ON PASDR SWAA2021081104978Support Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021081104977Support Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021080903140Support Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23. /SDR SWAA2021080903141Support Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23 /SDR SWAA2021080503148Seal · crackedL/H UPPER FWD FRONT SPAR SLIDING SEAL CRACKED APPROXIMATELY 5 INCHES. REF IPC 53-31-31-03. / L/H STAB UPPER SLIDING SEAL REPLACED PER AMM 53-31-31. REF SA-M 326 A1102204SDR SWAA2021080901011Seal · crackedREF NRC D508024 RH UPPER FWD FRONT SPAR SLIDING SEAL CRACKED APPROXIMATELY 3 INCHES. REF IPC 53-31-31-03. / REPLACED SLIDING SEAL PER AMM 53-31-31
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