N922WN
Service difficulty reports · 296
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 = 'N922WN' 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 = 'N922WN' 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 SWAA2026080368997Battery Pack · no testLEFT EMERGENCY EXIT EMERGENCY LIGHT BATTERY PACK M1668 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026080310598Battery Pack · no testFWD LEFT ENTRY EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 C/W INSPECTION.SDR SWAA2026080319518Battery Pack · no testROW 20 ABC EMERGENCY BATTERY PACK M1670 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06 INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.SDR SWAA2026061611648Girt Bar · out of adjustAFT SERVICE DOOR HAS A DAMAGED EVAC RELEASE STOP ON THE GIRT BAR. REMOVED AND REPLACED RELEASE STOP IAW AMM 25-66-00.SDR SWAA2026022372380Lamp · inoperativeLEFT OVERWING EXIT LIGHT IS HAS A BULB OUT. REMOVED AND REPLACED BOTTOM MOST LAMP IN THE LT OVERWING EXIT SIGN JUST FORWARD OF LT OVERWING EXIT AND PERFORMED SATISFACTORY OPERATIONAL TEST IAW AMM 33-51-01-960-801.SDR SWAA2026022368081Scuff Plate · crackedAFT ENTRY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2 STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRM 5SDR SWAA2026022368082Scuff Plate · crackedFWD GALLEY DOOR LOWER CENTER SCUFF PLATE CRACKED. REMOVED ALL THE COATINGS AND OTHER UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STEP 4.B.(3). REFERRED TO SOPM 20-30-03. REPAIRED BY FUSION WELD PROCESS THE SCUFF PLATE IAW SRMSDR SWAA2026022466142Skin · debondedLEFT WING OTBD AFT FLAP INBD AFT CORNER DISBONDED. REMOVED AND REPLACED THE LT WING OTBD AFT FLAP INBD IAW AMM 27-51-22-401.SDR SWAA2026022465349Retainer · crackedRIGHT WING AFT BULB SEAL RETAINER IS CRACKED AT THE TRANSVERSE WEB. REMOVED AND REPLACED THE AFT BULB SEAL RETAINER IAW SRM 51-40-02-OG-O.SDR SWAA2026022465014Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727B, S9L. ACCOMPLISHED HFEC SURFACE SCAN OF THE STRINGER CLIP IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. VERIFIED THE CRACK. REMOVED BS 727B; S-9L STRINGER CLIP IAW SRM 51-40-02, LOCATED AND DRILLED NEW STRINGER CLIP PER SRSDR SWAA2026022465018Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727C, S7L. ACCOMPLISHED HFEC SURFACE SCAN OF STRINGER CLIP AREA IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. VERIFIED CRACKED. REMOVED BS 727C; S-7L STRINGER CLIP PER SRM 51-40-02. LOCATED AND DRILLED NEW STRINGER CLIP PER SSDR SWAA2026022465019Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727D, S7R. FABRICATED A NEW STRINGER CLIP IAW SRM 51-30-01 & DWG 143A1010-1 REV C. .APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW AMM 51-21-41-370-802, & AMM 51-21-72-370-804. REMOVED THE STRINGER CLIP IAW SRM 51-40-02. INSSDR SWAA2026022465011Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727C, S6L. ACCOMPLISH HFEC INSPECTION OF THE STRINGER CLIP AREA IAW NDTM, PART 6, CHAPTER 51-00-00, PROCEDURE 23. REMOVED THE BS 727C; STRINGER CLIP 6L IAW SRM 51-40-02, FABRICATED A NEW STRINGER CLIP IAW SRM 51-30-01, & DWG 143SDR SWAA2026022465020Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727E, S5R, HFEC INSPECTED AREA IAW NDTM, PART 6; 51-00-00, PROCEDURE 23. CRACK NOTED. REMOVED THE STRINGER CLIP IAW SRM 51-40-02, LOCATED & DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, & DWG 146A1112, REV-. FABRICATED A NEW STSDR SWAA2026022465021Stringer Clip · no discrepancyCRACKED STRINGER CLIP, BS 767, S7R. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.SDR SWAA2026022464680Former · crackedLEFT WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN STRINGER 19L & 20L. EVALUATED CRACK ON THE WING TO BODY FAIRING, FOUND TO BE OUT LIMITS AND WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9. REMOVED AND REPLACED THE WING TO BODY FAIRING FORMESDR SWAA2026022364652Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACEMENT AFT FLOOR PANEL 241UF WAS FABRICATED IAW SRM 53-00-50-2R-0.SDR SWAA2026022364683Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022364653Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022364687Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.SDR SWAA2026022364657Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022364658Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED UPPER SKIN PULLED STRANDS IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.SDR SWAA2026022364646Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE THE FLOOR PANEL 221BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026022364648Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022364650Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022364651Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022364656Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ACF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026022365017Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 727B, S5R. ACCOMPLISH HFEC INSPECTION ON THE STRINGER CLIP IAW NDTM, PART 6, CHAPTER 51-00-00 PROCEDURE 23. LOCATED AND DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05, AND DWG 146A1102 REV-. FABRICATED A NEW STRINGER CLIP IAW SRSDR SWAA2026022464636Floor Support · crackedCRACKED FLOOR SUPPORT, BS 380-400, LBL 1, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.SDR SWAA2026022464523Seat Track · corrodedFOUND CORROSION ON TOP & IN WELL OF PASSENGER CABIN SEAT TRACK LBL 45, BS 727C+13 - 787+6, BS 807+6, BS 847+7, BS 847+8, WL 208. REMOVED THE DAMAGED SEAT TRACK AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 146A5300, REV-.SDR SWAA2026022464628Skin · crackedPOSSIBLE CRACK ON NR 4 SLAT NOSE SKIN AT ACTUATOR ATTACH FITTING. REPAIRED THE NR 4 SLAT NOSE SKIN IAW SRM 57-42-01-2R-8.SDR SWAA2026022364644Floorbeam · corrodedCORROSION AROUND FASTENER HOLE AT BS 986, LBL 47, WL 208. REMOVED AND REPAIRED THE DAMAGE OF THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.SDR SWAA2026022364679Support · corrodedCORROSION AROUND FASTENER HOLE, BS 986, RBL 47, WL 208. OPEN HOLE EXIST C/T INTERCOSTAL AND FLOOR PANEL SUPPORT AT BS 986 - 1006, WL 208 - WL 202 RBL38. REMOVE DAMAGED REPLACEMENT TEE ANGLE AND INSTALLED NEW REPLACEMENT -1 REPAIR IAW SRM 51-40-02-0G-0, SRM SDR SWAA2026022364635Floor Support · crackedCRACKED FLOOR SUPPORT BS 380 - 400, RBL 39, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.SDR SWAA2026022364666Floor Support · crackedCRACKED FLOOR SUPPORT BS 380 - 400, RBL 8, WL 208. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV A.SDR SWAA2026022364677Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. REMOVED AND REPLACED AFT CARGO BAY FWD SHIELD BETWEEN BS 767 - 794, RBL 22, WL 156 IAW SRM 51-40-02, & DWG 146A0081, REV-.SDR SWAA2026022364642Support · corrodedCORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, LBL 22, WL156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727+4 - 847, LBL 22, WL 156 IAW SRM 51-40-02, & DWG 146A7500, REV-.SDR SWAA2026022364643Support · corrodedCORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS 727B - 767, RBL 22, WL 156. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4 - 767, RBL 22, WL156 IAW SRM 51-40-02, DWG 146A7500, REVSDR SWAA2026022364634Floor Support · crackedCRACKED FLOOR SUPPORT BS 277 - 294, BL 0, WL 208. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, REV -.SDR SWAA2026022364418Crossbeam · crackedCRACKED CROSSBEAM, PASSENGER CABIN, BS 540, LBL 2, WL 208. REMOVED AND REPLACED THE CROSSBEAM, BS 540, LBL 0.0 TO LBL 24.75 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B;SDR SWAA2026022364419Crossbeam · crackedCRACKED CROSSBEAM AT PASSENGER CABIN, BS 540; LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540 LBL 24.75 - LBL 45.5 IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A0060, REV B.SDR SWAA2026022364092Floor Panel · pulledCABIN FLOOR PANEL 231YF HAS PULLED STRANDS. FABRICATED A NEW 231YF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.SDR SWAA2026022364090Floor Panel · pulledCABIN FLOOR PANEL 231ZF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, DUE TO THE EXTENT OF ALL OF THE DAMAGE.SDR SWAA2026022364094Floor Panel · pulledCABIN FLOOR PANEL 241AF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2026022364095Floor Panel · pulledCABIN FLOOR PANEL 241BF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG:144A5810 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026022364096Floor Panel · pulledCABIN FLOOR PANEL 242AF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026022364098Floor Panel · pulledCABIN FLOOR PANEL 241DF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2026022364099Floor Panel · pulledCABIN FLOOR PANEL 241EF HAS PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND BDWG:144A5810, DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026022364097Floor Panel · pulledCABIN FLOOR PANEL 242CF HAS PULLED STRANDS. THE FLOOR PANEL 242CF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0125.SDR SWAA2026022364100Floor Panel · pulledCABIN FLOOR PANEL 242DF HAS PULLED STRANDS. THE FLOOR SUPPORT REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810 ID:0123.
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