N489WN
Service difficulty reports · 401
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 = 'N489WN' 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 = 'N489WN' 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 SWAA2024070508699Light · detachedPHOTOLUMNICENT STRIP DETACHED ROW 1 AIRCRAFT RIGHT<[01] REINSTALLED PHOTOLUMINESCENT STRIP REF AMM 33-51-15SDR SWAA2024031864395Light · missingAFT ISLE PHOTO ILLUMINESCENCE STRIP MISSING (10 INCHES)<[01] R+R PHOTO ILLUMINESCENCE STRIP PER MM 33-51-15SDR SWAA2024031362130Lamp · inoperativeR/S EXTERIOR EMERGENCY LIGHT OUT.<[01] REPLACED OVER WING LAMP IAW AMM 33-51-04. ALL EMERGENCY LIGHTS WORKING.SDR SWAA2024012343328Cover · missingFO SIDE EMER EXIT LIGHT COVER MISSING LOWER LEFT SIDE<[01] INSTALLED EMERGENCYBOTTOM EXT SIGN PLASTIC COVER REF SIP; NO DEFECTS NOTED.SDR SWAA2024011741470Skin · damagedLEFT WING; AFT FLAP; INBOARD SIDE HONEYCOMB EXPOSED. REPLACED LT OUTBOARD AFT FLAP REF AMM 27-51-22-400-801.SDR SWAA2023053153288Megaphone · looseAFT MEGAPHONE HANDLE IS LOOSE<[01] R&R?D AFT MEGAPHONE PER AMM 25-64-00.SDR SWAA2022092715979None · inoperativeL/H EMERGENCY GROUND ILLUMINATION LIGHT INOP / [01] REPLACED LAMP AND PERFORMED GOOD FUNCTIONAL TEST OF L/H EMERGENCY LOWER SLIDE / GROUND ILLUMINATION LIGHT PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2022092756907Floor Panel · out of position2EA FLOOR PANEL INSERTS REQUIRE REPOSITIONING TO ACCOMMODATE FLOOR BEAM REPAIR FLOOR PANEL 221EF / [01] GENERAL NOTE: REFERENCE EA 22-153-02676-WIP5 STEP2 ON FAULT TTG8Q00E9MAJ FOR ALLOWANCE TO REPOSITION (MOVE) INSERT LOCATIONS AS REQUIRED.;[02] IDENTIFIED MASDR SWAA2022092765277Intercostal · crackedINTERCOSTAL AT BL 0; IS CRACKED BS 345 WL 208 / [01] HIDDEN DAMAGE INSPECTION ACCOMPLISHED. NO ADDITIONAL DAMAGE NOTED.;[02] HIDDEN DAMAGE RE-INSPECT REQUIRED UPON REMOVAL OF INTERCOSTAL.;[03] ADDITIONAL DAMAGE FOUND TO T-CHORD AND STRAP UPON REMOVAL OF INTERCSDR SWAA2022092252766Intercostal · crackedINTERCOSTAL AT BL 0; IS CRACKED BS 345 WL 208 / [01] HIDDEN DAMAGE INSPECTION ACCOMPLISHED. NO ADDITIONAL DAMAGE NOTED.;[02] HIDDEN DAMAGE RE-INSPECT REQUIRED UPON REMOVAL OF INTERCOSTAL.;[03] ADDITIONAL DAMAGE FOUND TO T-CHORD AND STRAP UPON REMOVAL OF INTERCSDR SWAA2022092765266None · crackedWHILE REMOVING CRACKED FSD LOWER STUB FRAME AT BS294 RBL55 WL209 FOUND LOWER INBOARD ATTACH CLIP CRACKED / [01] ENTERED MEASUREMENTS;[02] B737-700 SRM 53-10-15-2R-7 IS APPLICABLE FOR THIS REPAIR.<BR><BR>ITEM {1} CLIP WAS REMOVED AND DISCARDED IAW SRM 53-10-15-SDR SWAA2022092250406None · crackedWHILE REMOVING CRACKED FSD LOWER STUB FRAME AT BS294 RBL55 WL209 FOUND LOWER INBOARD ATTACH CLIP CRACKED / [01] ENTERED MEASUREMENTS;[02] B737-700 SRM 53-10-15-2R-7 IS APPLICABLE FOR THIS REPAIR.<BR><BR>ITEM {1} CLIP WAS REMOVED AND DISCARDED IAW SRM 53-10-15-SDR SWAA2022092765252None · corrodedCORROSION ON R/W #2 FUEL TANK AFT BOOST PUMP UPPER ATTACH CLIP COMMON TO BONDING JUMPER ATTACH POINT / [01] REMOVED AND REPLACED CORRODED CLIP ON R/W #2 FUEL TANK AFT BOOST PUMP UPPER ATTACH CLIP COMMON TO BONDING JUMPER ATTACH POINT IAW AMM 20-50-11-910-801 TSDR SWAA2022092246101None · corrodedCORROSION ON R/W #2 FUEL TANK AFT BOOST PUMP UPPER ATTACH CLIP COMMON TO BONDING JUMPER ATTACH POINT / [01] REMOVED AND REPLACED CORRODED CLIP ON R/W #2 FUEL TANK AFT BOOST PUMP UPPER ATTACH CLIP COMMON TO BONDING JUMPER ATTACH POINT IAW AMM 20-50-11-910-801 TSDR SWAA2022092765237None · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM UPPER SURFACE AT STA 727A+18; LBL 23; WL 208. / [01] REMOVED CORRODED FILLER FOR LONGITUDINAL BEAM BS 727A+18; LBL 23; WL 208 PER SRM 51-40-02; FABRICATED REPLACEMENT FROM 7075T6-C#.090' LOT# 1482311 AS SHOWN ON EA 1-757SDR SWAA2022092765238Floor Panel · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM UPPER SURFACE AT STA 727A+17 TO 727A+19; RBL 44.5; WL 208. / [01] REMOVED CORRODED FILLER FOR LONGITUDINAL BEAM BS 727A+17 TO BS 727A+19; RBL 44.5; WL 208 PER SRM 51-40-02; FABRICATED REPLACEMENT FROM 7075T6-C#.090' LOT#SDR SWAA2022092244533None · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM UPPER SURFACE AT STA 727A+18; LBL 23; WL 208. / [01] REMOVED CORRODED FILLER FOR LONGITUDINAL BEAM BS 727A+18; LBL 23; WL 208 PER SRM 51-40-02; FABRICATED REPLACEMENT FROM 7075T6-C#.090' LOT# 1482311 AS SHOWN ON EA 1-757SDR SWAA2022092244534None · corrodedCORROSION ON PASSENGER CABIN FLOOR BEAM UPPER SURFACE AT STA 727A+17 TO 727A+19; RBL 44.5; WL 208. / [01] REMOVED CORRODED FILLER FOR LONGITUDINAL BEAM BS 727A+17 TO BS 727A+19; RBL 44.5; WL 208 PER SRM 51-40-02; FABRICATED REPLACEMENT FROM 7075T6-C#.090' LOT#SDR SWAA2022092765235None · delaminatedRIGHT WING O/B AFT FLAP HAS A DELAM ON I/B LOWER CORNER / [01] REMOVED RIGHT WING O/B AFT FLAP PER AMM 27-51-22-000-801[08] FABRICATED THE REPAIR DOUBLER AND FILLER FROM PRE-PRIMED 0.16' 7075 T6 ALUMINUM (LOT# 1351319-2) ACCORDING TO SRM 51-70-10-2R-0; PARA'S SDR SWAA2022092765234Stub Frame · crackedFSD UPPER STUB FRAME IS CRACKED 3' BELOW STR 8 R/H / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW <BR> 53-10-15-1A-2 ALLOWABLE DAMAGE 2 AND EVALUATED UPPER STUB FRAME WITH CRACK ; DIMENSIONS L: 2' FOUND OUT ALLOWABLE DAMAGE LIMITS IAW 53-10-15-1SDR SWAA2022092244530Stub Frame · crackedFSD UPPER STUB FRAME IS CRACKED 3' BELOW STR 8 R/H / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW <BR> 53-10-15-1A-2 ALLOWABLE DAMAGE 2 AND EVALUATED UPPER STUB FRAME WITH CRACK ; DIMENSIONS L: 2' FOUND OUT ALLOWABLE DAMAGE LIMITS IAW 53-10-15-1SDR SWAA2022092244531None · delaminatedRIGHT WING O/B AFT FLAP HAS A DELAM ON I/B LOWER CORNER / DELAMINATION I/B LOWER CORNER UPPER SKIN . 8'X2' EXCEEDS ALLOWABLE LIMITS AS GIVEN IN SRM 57-53-01-1A-1 PARA 4 . A. (5) APPLY A PERMANENT REPAIR IAW SRM 57-53-01-2R-4 PARA 1. A. PARA 3. A. & B . PER SRMSDR SWAA2022092765230Floor Panel · delaminatedFLOOR PANEL 242UF HAS A DELAMINATED PREVIOUS REPAIR ON THE UPPER SURFACE FWD O/B CORNER / [01] IDENTIFIED PANEL 242UF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6<BR><BR>DAMAGE AREA EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 F<BR><BR>DAMAGE IS REPSDR SWAA2022092344305Floor Panel · delaminatedFLOOR PANEL 242UF HAS A DELAMINATED PREVIOUS REPAIR ON THE UPPER SURFACE FWD O/B CORNER / [01] IDENTIFIED PANEL 242UF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6<BR><BR>DAMAGE AREA EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 F<BR><BR>DAMAGE IS REPSDR SWAA2022092765227Frame · crackedCRACKED FRAME AT PASSENGER CABIN BS747 S-8R. / [01] REQUEST NDI TO HFEC TO VERIFY CRACK LOCATION;[02] ACCOMPLISHED HFEC INSPECTION OF BS 747 FRAME AT STR 8R MARKED END OF CRACK IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 TOOL# ATS729 CAL. DUE 07/2023.;[03] REPASDR SWAA2022092244042Frame · crackedCRACKED FRAME AT PASSENGER CABIN BS747 S-8R. / [01] REQUEST NDI TO HFEC TO VERIFY CRACK LOCATION;[02] ACCOMPLISHED HFEC INSPECTION OF BS 747 FRAME AT STR 8R MARKED END OF CRACK IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 TOOL# ATS729 CAL. DUE 07/2023.;[03] REPASDR SWAA2022092243761Stringer Clip · crackedCRACKED STRINGER CLIP AT STA 927; STRINGER S-4L. CORRECTION: ON STRINGER S-5L / [01] HFEC INSPECTED STRINGER CLIP AT BS 927 STR 5L PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.<BR><BR>TOOL N500 IS000681 DUE 02/2023;[02] CARD COMPLETE NO FURTHER ACTSDR SWAA2022092765197None · damagedR/H OVERWING EXIT PANEL 232YJW LIGHT LENS IS DISCOLORED / [01] REMOVED AND INSTALLED R/H OVERWING EXIT PANEL 232YJW LIGHT LENS IAW AMM 33-21-00-960-805. 10. (4) (A)(B); (5) (F)(G).;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CORRECTIVE ACTIONS STEP 1.SDR SWAA2022092765193None · damagedR/H OVERWING EXIT PANEL 232YJW LIGHT LENS IS DISCOLORED CORRECTION TO DISCREPANCY DESCRIPTION SHOULD READ L/H PANEL 231YJW / [01] CORRECTION TO DISCREPANCY DESCRIPTION; SHOULD READ L/H PANEL 231YJW;[02] REMOVED AND INSTALLED L/H 231YJW OVERWING EXIT PANEL LIGHSDR SWAA2022092765187Intercostal · crackedCRACKED INTERCOSTAL AT STA 344+10; WL 208; LBL 1. / [01] REQUEST NDI TO VERIFY CRACK;[02] HFEC INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED AT AFT FASTENER HOLE. ENDS OF CRACK MARKED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PASDR SWAA2022092765189None · corrodedSTA 344 FLOOR BEAM UPPER FLANGE HAS CORROSION COMMON TO FASTENER HOLES AT LBL 11 AND BL 0; WL 208.1. / [01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1<BR>REMOVED CORROSION FROM STA 344 FLOOR BEAM UPPER FLANGE; BEING OUT OF LIMITS; WITH ORIGINAL THICKNESS 0.1SDR SWAA2022092765186Angle · corrodedCORROSION ON FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE FROM STA 303.9+13 TO STA 328+12; WL 209; LBL 60 TO LBL 65. / [01] REMOVED CORROSION IAW SRM 53-10-15-1A-1. 2'X.65X.015 BS 341.5-343.5. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1.;[02] TOOL ID: ATS401<BR>SDR SWAA2022092765188None · corrodedCORROSION ON FWD ENTRY DOOR MOP SILL FROM STA 294.5+7 TO STA 348.2+6; WL 208 TO WL 209; LBL 54 TO LBL 62. / [01] VERIFIED APPLICABILITY FOR SRM<BR>REMOVED CORROSION FROM FWD ENTRY DOOR MOP SILL AT STA 335 LBL 59 WL 208 WITH ORIGINAL THICKNESS 0.090' AND WITH MSDR SWAA2022092765182Intercostal · crackedCRACKED INTERCOSTAL AT STA 277+7; WL 208; RBL 1. / [01] REMOVED INTERCOSTAL AT STA 277+7' WL 208 RBL 1 IAW SRM 51-40-02.;[02] INTERCOSTAL IT IS OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM BY REPAIRED BY REPLACEMENT OF PART IAW SRM 51-10-02 PAR 9.;[03] LOCASDR SWAA2022092765181None · corrodedSTA 328 FLOOR BEAM UPPER FLANGE HAS CORROSION COMMON TO FASTENER HOLES AT BL 0; RBL 37.5; RBL 47.5; AND RBL 54.5; WL 208. / [01] REMOVED CORROSION ON FLOOR TO BEAM UPPER CHORD BS 328 BL 0 WL 208 IN L=1.500' X W=2' X D=0.045' FROM ORIGINAL TICKNESS OF .125' FOUSDR SWAA2022092765185Intercostal · crackedCRACKED INTERCOSTAL AT STA 328+8; WL 208; LBL 45. / [01] LOCATED AND DRILLED NEW INTERCOSTAL BS 328 TO 344 WL 208 LBL 45 IAW SRM 51-40-05-0G-0; AND OK TO INTALL;[02] REMOVED INTERCOSTAL BS 328 TO 344 WL 208 LBL 45 IAW SRM 51-40-02-0G-0;[03] UPDATED MEASUREMENTSDR SWAA2022092765184Intercostal · corrodedCORROSION ON INTERCOSTAL AT STA 312+8; LBL 45; WL 208. / [01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1<BR>REMOVED CORROSION FROM THE INTERCOSTAL OF THE FLOOR STRUCTURE AT STA 312+8 LBL 45 WL 208; WITH ORIGINAL THICKNESS 0.040' AND MEASUREMENTS OF THE REWORSDR SWAA2022092765183Intercostal · corrodedCORROSION ON INTERCOSTAL FROM STA 312 TO 328; WL 208; LBL 12. / [01] REMOVED PANEL BREAK AT STA 312 TO 328 WL 208 LBL 12 IAW SRM 51-40-02<BR><BR>REMOVED CORROSION ON PANEL BREAK BS 314 IN L=2' X W=2' X D=0.40' FROM ORIGINAL TICKNESS OF 0.80' FOUND TO BE OUT OFSDR SWAA2022092765180Intercostal · corrodedCORROSION ON INTERCOSTAL AT STA 294 TO STA 312; WL 208; LBL 10 TO LBL 12. / [01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1<BR>NO DAMAGE IS PERMITTED AT FLOOR BEAM UPPER CHORD UNDER INTERCOSTAL FOR GALLEY HARD MOUNT/ATTACHMENT IAW SRM 53-10-51-1A-1 PARAGRAPHSDR SWAA2022092765200Web · crackedPASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. MARKED. / [01] REMOVED FED FWD LWR STOP PAD FITTING AND STRAP FOR ACCESS IAW SRM 51-40-02-0G-0;[02] STOP PAD FITTING WEB IS CRACKED AND IS OUT OF LIMITS IAW SRM 53-10-15-1A-1. TO BE REPLACED SDR SWAA2022092765205Stub Frame · crackedFWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME CRACKED BS294 RBL55 WL209. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-15- 1A-2 ALLOWABLE DAMAGE 2 AND IDENTIFICATION IAW SRM 53-10-15-0I-2;[02] EVALUATED DAMAGE; DIMENSION OF CRACK LSDR SWAA2022092765178None · corrodedCORROSION ON FWD SERVICE DOOR MOP SILL FROM STA 291.5 TO STA 344; WL 208.1 RBL 52 TO 59. / [01] REMOVED CORROSION IAW SRM 53-10-15-1A-2. 2'X1'X.020. FOUND TO BE OUT LIMITS IAW IAW SRM 53-10-15-1A-2.;[02] TOOL ID: ATS2739<BR>S/N: A22004232<BR>DUE DATE: 04/2023;SDR SWAA2022092765179Intercostal · crackedCRACKED INTERCOSTAL AT STA 312+5 & STA 312+11; WL 208; RBL 31. / [01] NO ALLOWABLE LIMITS FOUND ON SRM REPLACEMENT OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR.9.C;[02] REMOVED INTERCOSTAL LOCATED BS312-BS328 RBL31 WL208 I.A.W SRM 51-40-02-0G-0;[03] LSDR SWAA2022092765190Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS562; BS683 - BS691. MARKED. / [01] REMOVED CORROSION IN THE BOTTOM OF SEAT TRACK RBL 45 BS 561 TO BS 563 IN L'=2 X W=1' X D= 0.011' IAW SRM 51-10-02-0G-0 AND EVALUATED BLEN AREA AND FOUND TO BE IN LIMITS IAW SRM SDR SWAA2022092343756Web · crackedPASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. MARKED. / [01] REMOVED FED FWD LWR STOP PAD FITTING AND STRAP FOR ACCESS IAW SRM 51-40-02-0G-0;[02] STOP PAD FITTING WEB IS CRACKED AND IS OUT OF LIMITS IAW SRM 53-10-15-1A-1. TO BE REPLACED SDR SWAA2022092243760Stub Frame · crackedFWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME CRACKED BS294 RBL55 WL209. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-15- 1A-2 ALLOWABLE DAMAGE 2 AND IDENTIFICATION IAW SRM 53-10-15-0I-2;[02] EVALUATED DAMAGE; DIMENSION OF CRACK LSDR SWAA2022092243352None · corrodedCORROSION ON FWD SERVICE DOOR MOP SILL FROM STA 291.5 TO STA 344; WL 208.1 RBL 52 TO 59. / [01] REMOVED CORROSION IAW SRM 53-10-15-1A-2. 2'X1'X.020. FOUND TO BE OUT LIMITS IAW IAW SRM 53-10-15-1A-2.;[02] TOOL ID: ATS2739<BR>S/N: A22004232<BR>DUE DATE: 04/2023;SDR SWAA2022092243356Intercostal · crackedCRACKED INTERCOSTAL AT STA 277+7; WL 208; RBL 1. / [01] REMOVED INTERCOSTAL AT STA 277+7' WL 208 RBL 1 IAW SRM 51-40-02.;[02] INTERCOSTAL IT IS OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM BY REPAIRED BY REPLACEMENT OF PART IAW SRM 51-10-02 PAR 9.;[03] LOCASDR SWAA2022092243361Intercostal · crackedCRACKED INTERCOSTAL AT STA 344+10; WL 208; LBL 1. / [01] REQUEST NDI TO VERIFY CRACK;[02] HFEC INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED AT AFT FASTENER HOLE. ENDS OF CRACK MARKED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PASDR SWAA2022092243355None · corrodedSTA 328 FLOOR BEAM UPPER FLANGE HAS CORROSION COMMON TO FASTENER HOLES AT BL 0; RBL 37.5; RBL 47.5; AND RBL 54.5; WL 208. / REMOVED CORROSION ON FLOOR TO BEAM UPPER CHORD BS 328 RBL 54.5 WL 208 IN L=1.500' X W=2' X D=0.035' FROM ORIGINAL TICKNESS OF .125' FOUN
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