N965WN
Service difficulty reports · 175
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 = 'N965WN' 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 = 'N965WN' 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 SWAA2023080975579Floor Panel · pulledFLOOR PANEL 231HF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231HF IAW SRM 53-00-50-2R-0.;[02] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION 1; 2; CURE SHEETS AND MEASUREMENTSSDR SWAA2023080975580Floor Panel · pulledFLOOR PANEL 231KF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 231KF MATERIALS IAW SRM 53-00-50-0I-1 FIG 3 TABLE 3.<BR><BR>DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231KF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1531001-1; INSTALLED INSERTS SDR SWAA2023080975572Floor Panel · pulledFLOOR PANEL 231LF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED COMPLETION OF PANEL 231LF FABRICATION IAW SRM 53-00-50-2R-0 AND BOEING DWG: 143A5810 ID: 0579.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023080975582Floor Panel · pulledFLOOR PANEL 231UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231UF IAW SRM 53-00-50-2R-0.;[02] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION 1; 2; CURE SHEETS AND MEASUREMENTSSDR SWAA2023080975574Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-0.;[02] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION 1; 2; CURE SHEETS AND MEASUREMENTSSDR SWAA2023080975575Floor Panel · pulledFLOOR PANEL 242NF UPPER SKIN HAS PULLED STRANDS.<[01] FLOOR PANEL 242NF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 PARA 1. A. NOTE. AND ATTACHED CURE SHEET TO THIS FAULT RECORD.;[02] JOB COMPLETE.SDR SWAA2023080975583Floor Panel · pulledFALOOR PANEL 241KF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241KF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 53-00-50-2R-0 PARA 1. A. NOTE AND DWG 146A5810 SHEET SDR SWAA2023080975584Floor Panel · pulledFLOOR PANEL 241NF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241NF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 53-00-50-2R-0 PARA 1. A. NOTE AND DWG 146A5810 SHEET 4SDR SWAA2023080975585Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241RF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 53-00-50-2R-0 PARA 1. A. NOTE AND DWG 146A5810 SHEET 4SDR SWAA2023080975586Floor Panel · pulledFLOOR PANEL 241TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241TF IAW SRM 53-00-50-2R-0 AND DWG 146A5810 SHEET 467;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023080975576Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241UF IAW SRM 53-00-50-2R-0 AND BOEING DWG:146A5810 ID:0470.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023080975587Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241VF IAW SRM 53-00-50-2R-0 PAR. 5. S. (1) (A) - (D) AND BOEING DWG: 146A5810 ID: 0469.;[02] FINAL INSPECTION. JOB COMPLETE.<BR><BR>VERIFIED MESDR SWAA2023080975588Floor Panel · pulledFLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241WF IAW SRM 53-00-50-2R-0 AND DWG 146A5810 SHEET 471;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023080976089Tension Tie · corrodedCORROSION ON TENSION STRAP AT AFT CABIN BS1016+12 RBL18 WL208.<[01] REMOVED TENSION STRAP AT AFT CABIN BS1016+12 RBL18 WL208 PER SRM 51-40-02-0G-0.;[02] UPDATED MEASUREMENTS TABLE.;[03] SRM DOES NOT HAVE ALLOWABLE DAMAGE FOR CORROSION ON TENSION STRAP. OUT OF SDR SWAA2023080976090Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT CABIN BS986 LBL43 WL208.<[01] VERIFIED SRM 53-70-51-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE TO SECT. 47 FLOOR STRUCTURE.;[02] CONCUR WITH APPLICABILITY OF SRM 53-70-51-1A-1.;[03] REMOVED CORROSION FROM UPPER FLANGE OF BS 986.5 FLSDR SWAA2023080976100Sill Drain · corrodedCORROSION ON FED MOP SILL BS294+9; BS317 - BS342 LBL56 WL208.<[01] VERIFIED APPLICABILITY FOR SRM 53-10-15-1A-1;[02] REMOVED CORROSION ALONG FED MOP SILL<BR>AT LBL56; WL208; BS294.5 + 10'; L: 2 X W:1'<BR>BS312 + 5'; L: 2.5' X W:1'<BR>BS312 + 9'; L: 1.5' X W:1'SDR SWAA2023080976098Sill Drain · corrodedCORROSION ON FSD MOP SILL BS294+7; BS326 - BS346 RBL56 WL208.<[01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-2;[02] REMOVED CORROSION ALONG FSD MOP SILL <BR>AT RBL56; WL208 BS 291.5 + 11' - BS312 + 10' L:20' X W:1'; REMOVED CORROSION ALONG FSD MOP SILL AT RBL5SDR SWAA2023080976099Support Angle · corrodedCORROSION ON FSD MOP SILL THRESHOLD SUPPORT ANGLE BS305 - BS323 RBL57 WL209.<REMOVED CORROSION ALONG FSD MOP SILL THRESHOLD SUPPORT ANGLE AT RBL57; WL209 BS 291.5 + 12' L:1.5' X W:1';<BR>BS312 L1:5' X W:1'; <BR>BS312 +5' L1:5' X W:1'; <BR>BS312 +8' L1:5' X W:1SDR SWAA2023080975569Floor Panel · damagedFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER (TANG) IS BROKEN<[01] FWD CABIN FLOOR PANEL 221BF WITH AFT O/B CORNER (TANG) BROKEN WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CORRECSDR SWAA2023080975570Floor Panel · damagedFWD CABIN FLOOR PANEL 221GF FORWARD O/B CORNER (TANG) BROKEN<[01] COMPLETED STEPS 11 AND 12.;[02] FWD CABIN FLOOR PANEL 221GF O/B CORNER (TANG) REPAIRED IAW SRM 53-00-50-2R-6;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED CORRECTIVE ACTION 2SDR SWAA2023081074776Support · corrodedFLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727A+5 - 727E+3 LBL 20 WL 156<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF ACB FLOOR TO SIDEWALL SUPPORT; BS727A+5 727E+3 LBL 20 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[05] FABRIACATED LOCATED SDR SWAA2023080974772Intercostal · crackedCRACKED INTERCOSTAL IN UPPER AFT RADIUS BS 947 RBL 17 WL 179<[01] VERIFIED APPLICABILITY OF SRM 53-70-53-01-2 IDENTIFICATION 2 - SECTION 47 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.;[03] MEASURED CRACK ON INTERCOSTAL ISSDR SWAA2023080974778Shield · corrodedFWD SHIELD IS CORRODED FROM BS 767-767+16 RBL 20 WL 157<[01] UPDATED MEASUREMENTS TABLE;[02] NOT FOUND ALLOWABLE ON SRM; PART WILL BE REPLACE PER SRM 51-10-02-0G-0; STEP 9;[03] REMOVED FWD SHIELD FROM AFT CARGO COMPARTMENT FROM BS 767 TO BS 794.25 IAW SRM 51-4SDR SWAA2023080974779Support · corrodedFLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727E+13 - 787+19 RBL 20 WL 156<[01] UPDATED MEASUREMENTS TABLE;[02] FOUND UNDER INVESTIGATION LOCATION IS BS 727E+13 TO BS 747+19; RBL 20; WL 156;[03] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[04] BLENDED CORROSION ONSDR SWAA2023080974773Stringer · corrodedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 23R BS 520-540 WL 156<[01] EVALUATED CRACK AT FCB STRINGER 23R/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A;[02] VERIFIED APPLICABILITY FOR STR 23R/H AT FSDR SWAA2023080974774Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 24R BS 520-540 WL 156<[01] EVALUATED CRACK AT FCB STRINGER 24R/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A.;[02] VERIFIED APPLICABILITY FOR STR 24R/H AT SDR SWAA2023080974775Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 26L BS 520-540 WL 156<[01] EVALUATED CRACK AT FCB STRINGER 26L;BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A.;CUTOUT AND REMOVED DAMAGE AT STRINGER SECTION 2SDR SWAA2023080974768Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 23L BS 520-540 WL 156<[01] EVALUATED CRACKAT FCB STRINGER 23L;BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A.;[02] EVALUATED CRACK AT FCB STRINGER 23L;BS 539 SDR SWAA2023080974771Strap · corrodedCORROSION ON THRESHOLD TIE STRAP AT FASTENER HOLES BS 787+8 - 807+13 RBL 20 WL 159<[01] VERIFIED APPLICABILITY IAW SRM 53-60-15-01-1 AND SRM 53-60-15-1A-1;[09] OK TO INSTALL NEW THRESHOLD TIE STRAP.;[10] OKAY TO INSTALL GIVEN.;[11] STARTED INSTALLATION OF THRESDR SWAA2023080974777Support · corrodedFLOOR TO SIDEWALL SUPPORT CORROSION BS 727A+9 - 767 RBL 20 WL 156<[01] UPDATE MEASUREMENTS TABLE;[02] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[03] BLENDED CORROSION ON FLOOR TO SIDEWALL SUPPORT CORROSION BS 727A+9 - 767 RBL 20 WL 156;<BR>WORK AREA <BR>BS 727ASDR SWAA2023080974520Shield · corrodedCORROSION ON AFT SHIELD AT BS 500-500A RBL 25 WL 156<[01] ENTERED MEASUREMENTS;[02] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS DAMAGE EVALUATION.<BR>NO ALLOWABLE DAMAGE FOUND IN 737-700 SRM FOR THIS PART.<BR>REPAIR BY REPLACEMENT SRM 51-10-02-0G-0 STEP 9;[03] VESDR SWAA2023080974522Support · chafedCHAFING DAMAGE ON FWD BULKHEAD SUPPORT BS400 LBL24 WL156<[01] REMOVED DAMAGE IAW SRM 51-10-02.<BR>DAMAGED AREA MEASURES 0.30' X 0.80';[02] VERIFIED CORRECTIVE ACTION #1;[03] NOT FOUND ALLOWABLE DAMAGE ON THE SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARASDR SWAA2023080974763Stringer · corrodedAREA AFT OF FWD CARGO BAY HAS A CORRODED STR. R25 BS500-540; WL 156<[01] EVALUATED CORROSION AT FCB STRINGER 25R/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL B;[02] VERIFIED APPLICABILITY FOR STR 25R/H AT FCB IAW SRM 53-00-03-2R-1 SDR SWAA2023080973920Scuff Plate · crackedFWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] WELDED CRACK ON FCB; AFT CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B.(2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUIPMESDR SWAA2023052450815Fuse · inoperativeEMERGENCY AISLE LIGHT AT ROW 7ABC INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY FUSE REF: AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023052450814Battery Pack · inoperativeEMERGENCY AISLE LIGHTS AT ROW 11CB AND 9ABC INOP.<[01] REMOVED AND REPLACED BATTERY PACK AT LH STATION 727C IAW AMM 33-51-06. OP CHECK GOOD.SDR SWAA2023042630408Light · inoperativeAFT R/H SERVICE DOOR EMER EXTERIOR LIGHT INOP<[01] REMOVED AND REPLACED AFT SERVICE DOOR EXTERIOR EMER LIGHT BULB PER AMM 33-51-04. OPS TEST GOOD.SDR SWAA2023011090191Slide · detachedFORWARD GALLEY SERVICE DOOR PARTIALLY OPENED WITH GIRT BAR ARMED<[01] INSPECTED DOOR SLIDE FOUND TO BE PULLED FROM COVER WAS NOT DEPLOYED REPACKED SLIDE REF AMM25-66-01 AC OK FOR SERVICESDR SWAA2022110968099Skin · crackedFOUND .5 CRACK AT LOCATION IDENTIFIED AS FIRST DENT LOCATED AT WS 271; AT APPROXIMATELY 21 FROM TRAILING EDGE. PERFORMED HFEC AS REQUIRED PER NDT MANUAL PART 6 51-00-00 PROC 23. AT BOTH DENTS IDENTIFIED IN DISCREPANCY. FOUND .5 CRACK AT LOCATION AT IDENTIFIED SDR SWAA2022092824668Light · inoperativeFWD LEFT STOWBIN BULLNOSE EMEERGENCY EXIT LIGHTS ARE INOP. FOUND FUSE BLOWN ON EMERGENCY BATTERY POWER SUPPLY FOR FWD BULLNOSE LIGHTS; ALSO FOUND FWD BULLNOSE LIGHT ASSEMBLY BAD. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-03-960-802 AND FUSE IAW AMM 33-51-06-960-8SDR SWAA2022080337728Sliding Sleeve · tornRT HORZ UPPER FWD SLIDING SEAL TORN / [01] R&R R/H UPPER SLIDER PER AMM 53-31-31SDR SWAA2022071527801Slide · out of adjustUNABLE TO READ GAUGE ON FWD SERVICE DOOR SLIDE / [01] READJUSTED FWD SERVICE DOOR SLIDE IN REFERENCE TO AMM 25-66-01. GAUGE IS NOW VISIBLESDR SWAA2022070124048Flashlight · brokenAFT INBOARD FLASHLIGHT BROKEN / [01] R&R AFT INBOARD FLASHLIGHT ASSY REF CMM 25-60-13SDR SWAA2022062721397Battery Pack · inoperativeEMERGENCY LIGHTS L733;L1223 AFT RIGHT SLIDE;AFT ENTRY INOP / [01] REPLACED M1672 POWER SUPPLY BATTERY PACK PER AMM 33-51-06SDR SWAA2021083112112Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 ARE INOP ; / [01] REMOVED; REPLACED; AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHT BATTERY PACK AT M1675 PER AMM 33-51-06-960-805.; [02] VERIFIED CORRECTIVE ACTION 1 PER AMM 33-51-06-960-805.SDR SWAA2021083109722Gusset · crackedFCB GUSSET CRACKED BS 500D STR 19L WL 188 ; / [01] REMOVED GUSSET BS 500D STR-19L WL 188. IAW. SRM 51-40-02.; [02] LOCATED AND DRILLED FCB GUSSET AT B.S 500D STR 19L PER SRM51-40-05-0G-0;DWG 143A7902. O.K TO INSTALL.; [03] OKAY TO INSTALL FCB GUSSET; [04] INSTSDR SWAA2021083109729Gusset · crackedFCB R/H GUSSET CRACKED BS 500D STR 19R WL 188 ; / [01] REMOVED GUSSET BS 500D; STR 19R; WL 188 IAW SRM 51-40-02.; [02] LOCATED; DRILLED AND DEBURRED NEW FCB R/H GUSSET BS 500D; STR 19R; WL 188 IAW SRM 51-40-05-0G-0 AND DWG 143A7902; [03] VERIFIED; [04] LOCATEDSDR SWAA2021083108453Bulkhead Web · crackedRIGHT HAND B.S. 663 VAPOR BARRIER HAS A CRACKED FASTENER HOLE AT O/B EDGE ; / IDENTIFIED B.S. 663 RIGHT HAND VAPOR BARRIER MATERIAL IAW SRM 57-10-10-0I-2 TABLE 2 FIGURE 2 ITEM 4. DAMAGED FASTENER HOLE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARAGSDR SWAA2021082308454Bulkhead Web · damagedRIGHT HAND B.S. 663 VAPOR BARRIER HAS MISALIGNED FASTENER HOLES AT I/B LOWER EDGE ; / [01] IDENTIFIED B.S. 663 RIGHT HAND VAPOR BARRIER MATERIAL IAW SRM 57-10-10-0I-2 TABLE 2 FIGURE 2 ITEM 4. DAMAGED FASTENER HOLES EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-SDR SWAA2021083107491Attach Angle · crackedR/H VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED; BS 663 RBL 8 W/L 164. ; / [01] VERIFIED APPLICABILITY IAW SRM 57-10-10-2R-5; [02] REMOVED 8 EA FASTENERS COMMON TO FUEL TANK AT BS 663 BETWEEN RBL 7 TO 20; WL 164 AND CUT OUT DAMAGE ANGLE IAW SRM 57-10-10-2R-5;
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